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{{#Wiki_filter:8210280060 ggg009 PDR'ADQCK 05000400 P PDR Carolina Power&Light Company PO Box 1551 Raleigh, North Carolina 27602 Shearon Harris Nuclear Power Plant Unit 1 Mechanical Analysis and Calculations for 1CS-746 Charging Pump A to Refueling Water Storage Tank Isolation Valve%II ISA MIIIIL"Il IJ.IlGeneric Letter 89-10 Applicable:~Yes No Valve Classification:
{{#Wiki_filter:8210280060 ggg009 PDR     'ADQCK 05000400 P                       PDR Carolina Power & Light Company PO Box 1551 Raleigh, North Carolina 27602 Shearon Harris Nuclear Power Plant Unit   1 Mechanical Analysis and Calculations for 1CS-746 Charging Pump             A to     Refueling Water Storage Tank Isolation Valve
Nuclear-Safety Related Calculation Number*CS-0021 Revision Reason Reason Prepared By/Date Verified By/Date Project Engineer/Date Signatures on file Signatures on file incorporation of Electrical Calculation E5-001, Revision 1 10/I/92 Incorporation of PC%.6562, Raviaion I Prin.or Res.Eng./Date Reason Prepared By: Checked By: Calc.ID!*CS-0021 Revision: 2 pacae 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 List of Effective Pa es prevision Attachment Attachment Attachment Attachment Attachment Attachment
                                %II   ISA         MIIIIL"IlIJ        .Il Generic Letter 89-10 Applicable:~Yes                                   No Valve Classification:                 Nuclear-Safety Related Calculation       Number *CS-0021 Revision Prepared By/Date   Verified By/Date   Project Engineer/Date    Prin. or Res. Eng./Date Signatures on file Signatures on file Reason  incorporation of Electrical Calculation E5-001, Revision 1 10/I/92 Reason  Incorporation of PC%.6562, Raviaion I Reason
 
Prepared By:                                   Calc. ID! *CS-0021 Checked By:                                    Revision: 2 List of Effective  Pa es pacae                                           prevision 1
2 3
4 5
6 7
8 9
10 11 12 13 14 15 16 17 18 19 Attachment A  Telecon w/Velan Inc.
Attachment B  Fax from            of Velan Attachment C  Flow Isolation/Seating Thrust Attachment D  Average Closing Packing Load Attachment E  Final Thrust Due to Inertia Attachment F  Thrust at Torque Switch Trip


==Attachment:==
==Attachment:==
G  Design Verification  Record 1CS-746                                                  Page No: 1
Prepared By:                                    Calc. ID! *CS-0021 Checked By:                                    Revision:  2 TABLE OF CONTENTS Section                Descri tion                              Pacae 1~0        Purpose 2.0        References 3.0        Bases and Assumptions 3.1        Analyzed Configuration 3 '        Valve Function and Control Configuration 3 '        Assumptions 4.0        Calculations 4.1        Generic Letter 89-10  Applicability 4.2        Design  Differential Pressure Evaluation        7 4.3        Valve Thrust 4~4        Recommended  Minimum Torque Switch  Setting    11 4.5        Motor Capacity Limits 4.6        Allowable Operating Ranges                      12 4.7    . Stall Evaluation                                14 4.8        Required Limit Switch Settings                  15 4.9        Nominal Operating Time                          17 5.0        Results, Conclusions and Recommendations            19 Attachment  A    Telecon w/Velan Inc.                1 page Attachment  B    Fax from            of Velan        3 pages Attachment  C    Flow Isolation/Seating Thrust        1 page Attachment  D    Average Closing Packing Load        1 page Attachment  E    Final Thrust Due to Inertia          1 page Attachment  F    Thrust at Torque Switch Trip        1 page Attachment  G    Design Verification  Record          2 pages 1CS-746                                                    Page No: 2
Prepared By:                                  Calc. ID: *CS-0021 Checked By:                                  Revision:  2 1~0  PURPOSE
: 1. 1  Pu  ose  of this Re ort The purpose of this report is to document various parameters pertaining to the subject motor-operated valve. This report:
reviews the design differential pressure against which the valve may have to operate calculates the MOV thrust/torque requirements evaluates the limitations of the actuator, motor, and valve (evaluation includes effects of a motor stall) evaluates the actuator limit switch settings 1.2 Reason for Revision PCR-6547, Revision 1, removed the Alternate Mini-flow Relief Valves and installed restricting orifices upstream of motor-operated valves 1CS-746 and 1CS-752. The control logic for these motor-operated valve will be modified such that they will automatically open upon high RCS pressure (2300 psig) coincident with an "S" signal and will automatically close at the reset pressure of 1750 psig. The reason for this revision, is to incorporate the changes made by PCR-6547, Revision 1.
2 '  RERERENCES 2.1        NED Design Guide DG-I.11, "Q-List Motor-Operated Valve Mechanical Evaluations", Revision 4.
2 '        NED Scope Document {}9-M0-002, Revision 2.
2.3        "Analysis of Overload Protection and Motor Torque Output  for AC Motor Operated Valves" E5-001, Sub-Calculation CPL-MOV-051, Revision 2.
2.4        Control Wiring Diagram CAR 2166-B-401 Sheet 317, Revision 5.
2.5        Corrective Maintenance Procedure CM-I0002, Revision 4.
2.6        Valve Vendor Print  1364-53850, Revision 1.
Technical Manual ISP, Volume 2, Revision 18.
1CS-746                                                  Page No: 3
Prepared By:                                  Calc. IDs *CS-0021 Checked By:                                  Revision:        2
==2.0    REFERENCES==
Continued 2.8        Chemical  & Volume Control Piping, Reactor Auxiliary Building, Plans, CAR-2165-G-140, Revision 23.
2.9        Chemical and Volume Control System Description, SD-107, Revision 2.
2.10        Crane Technical Paper No. 410, Nineteenth          Printing 1980.
2 ~ 11      Technical Memorandum "Performance and Properties of Limitorque Components", Number TM-G-XXXX-001, Rev. 0.
2.12        Piping Line List, CAR-1364-B-0070, Revision 44.
: 2. 13      Westinghouse E-Spec. No. G-678852, Revision 2.
2 ~ 14      Design Basis Document  DBD-104, Revision 0.
2.15        RAB Tank Area Sections, CAR-2165-G-251, Revision 18.
a.zs        Piping Isometric 1-CS-651, Revision 5.
2 ~ 17      Limitorque Order Sheet 3D0652-D 2.18        PCR-6547, Revision 1, "Alternate Mini-Flow Re-Design" 3 '    BASES AND ASSUMPTIONS
: 3. 1  Anal zed Confi  ration The configuration assumed  when performing  this analysis is as follows:
Actuator Dat Limitorque Order Number:            3D0652-D Actuator Size & Type:              SMB-00  1 Overall Unit Ratio:                82 ~ 0:1 Handwheel Ratio:                    4 ~ 3P:1 Handwheel Efficiency:                          '5%
Worm Set/Gear Ratio:                45:p Worm Set Efficiency:                36%
Applications Factor:                0.9 Installed Spring Pack:              60-600-0047-1 Pullout Efficiency:                40%
Run  Efficiency:                    50%
Stall Efficiency:                  50%
1CS-746                                                          Page No: 4
Prepared By:                                    Calc. ID: *C8-0021 Checked By:                                      Revision:  2 3.1  Anal sed Confi      ration Continued Motor Data Foot-Pounds:                        10 RPM:                                1700 Volts:                              460 AC Manufacturer:                        Velan Valve Size & Type:                  2-inch, globe Valve Pressure Class:                1500 psig Mean Contact Seat Diameter:          1.875 Stem  Configuration:                1.125D-1/3P-2/3L Stroke Length:                      1.5 inches 1    Walkdown Data "Motor-Operated-Valve Data Form" 2    NED Design Guide I.11 (Reference 2.1) 3    Limitorque Order Sheet (Reference 2.17) 4    Emdrac Print (Reference 2.7) 3.1.1
~  ~        Cross-reference Number s The Ebasco (construction identification) tag number for this valve is 2CS-V757SA-1.
        ~
The Westinghouse Identification Number and Location are 2TM78FNM and 8489A    respectively.
3.2  Valve Function and Control Confi    ration 3.2.1        Valve Function The alternate mini-flow line is for dead head protection of the CSIP's during safety injection (specifically the injection phase of the SIS operation). Valves 1CS-746 and 1CS-752 are designed to open automatically upon high RCS pressure (2300 psig) coincident with an "S" signal and will automatically close at the reset pressure of 1750 psig (Reference 2.18). These valves are located in parallel on the two alternate mini-flow lines which relieve to the RWST.                          I 1C8-746                                                    Page No: 5
Prepared By:                                    Calo. IDs *CS-0021 Checked By:                                    Revision:  2 3.2.2          Control Confi ration The following statements are derived from references 2.4, 2.5 and 2 ~ 18 ~
This    MOV  automatically opens upon high RCS pressure (2300 psig) coincident with an "S" signal and will close at the reset pressure of 1750 psig.
Under normal conditions this MOV can only open      if valves 1RH-25, 1RH-63 and either 1CS-165, 1CS-166 or 1CS-745 are closed.
This MOV trips out via the torque switch in the closing direction and is electrically de-energized by the open limit switch, in the opening      direction.
The open      torque switch and thermal overloads are automatically bypassed on loss      of offsite power or a safety injection actuation.
: 1)      The minimum torque delivered by the actuator motor    is assumed to be 5.9 ft-lbs per reference 2.3.
: 2)      The maximum torque  delivered by the actuator motor is assumed to be 11.3  ft-lbs per reference 2.3.
: 3)      The Stem Factor for a coefficient of friction of 0.15 is 0.0156 and a coefficient of friction of 0.2 is 0.0179 (reference 2.1).
: 4)      The flow limiting component in the alternate mini-flow line is the fixed orifice. The flow capacity of this orifice is 60 gpm nominally (reference 2.18).
: 5)      The maximum operating temperature and design temperature for line number 2CS2-785SN-1 is 130 F and 200 F respectively (reference 2.12).
: 6)      Piping frictional losses are ignored when calculating differential pressure at the valve.
: 7)      The 0.433 psig/ft conversion factor used in this calculation is based on water at 60 F (reference 2.10).
XCS-746                                                      Page No: 6
Prepared By:                                      Calc. ID: *CS>>0021 Checked By:                                        Revision: 2 4 '    CALCULATIONS 4.1    Generic Letter 89-10    A  licabilit Valve 1CS-746 is located in the CSIP alternate mini-flow line and is designed to open "S" automatically upon high RCS pressure coincident with an          signal and automatically close at the reset pressure    (Reference  2.18). The alternate mini-flow line is for dead head protection of the CSIP's during safety injection (specifically the injection        phase  of the SIS operation).
Based on  the preceding paragraph and the guidance provided in reference 2.2, the requirements of Generic Letter 89-10 are a  licable to this    MOV.
4.2    Desi n  Differential Pressure Evaluation 4~2~1        S stem Inlet Pressure Upstream .pressure    will be assumed to be equal to the shutoff head of the CSIPs plus the static head of the RWST at its maximum level.
CSIP shutoff head:
6200 feet (ref. 2.7)
* 0.433 psig/foot                      = 2,684 psig Static  Head:
RWST  Maximum  Level = 301    ft.  (ref. 2.15)
Valve Elevation = 249      ft.  (ref. 2.16)
(301  ft. 249    ft.)
* 0.433    psig/ft                      23 Pressure  is  equal  to:                            2,707 psig s'pstream 4.2.2      Differential Pressure The maximum differential pressure (dP) occurs when maximizing the upstream and minimizing the downstream pressure.          To maximize dP, it is assumed that the downstream pressure is psig. 0 Therefore, the maximum differential pressure is 2,707 psid.
1CS-746                                                        Page No: 7
Prepared By:                                      Calo. ID: *CS-0021 Checked By:                                      Revision:  2 4.2.2      Differential  Pressure    Continued I
Note: The subject  MOV  is  a pressure under the seat globe valve.
The most  conservative opening differential pressure assumption is to assume  0 psid since any line pressure would assist the valve in opening. For this reason opening upstream pressure and differential pressure are not calculated.
: 4. 3  Valve Thrust 4.3.1      Valve Thrust  Re  ired at  Maximum dP The maximum  thrust requirements for the operation of this pressure under the seat globe valve may be determined by the following equations, which are provided by reference 2.1.
CLOSING THRUST = (dp
* A
* FV) + SBL + [SA*(P-dP))
OPENING THRUST = SBL  (dP
* A)  [SA*(P-dP))
where:
THRUST =  The  required stem thrust, in pounds-force.
The differential pressure across the valve.
The seat area of the valve, which is 2.76 square inches based on contact seat diameter (Section 3  1)
An  empirical valve factor, which is 1.1 per reference 2.1.
SBL      The stuffing box load, or packing drag, expressed in pounds-force. This is 1500 pounds per reference 2.1.
SA        The area of the stem, in square inches.        For the stem diameter given in section 3.1, this area is 0.99 square inches.
The inlet system pressure.
1CS-746                                                      Page No: 8
Prepared By:                                            Calo. ZD! *CS-0021 Checked By:                                            Revision:    2 4.3.1        Valve Thrust    Re    ired at  Maximum dP    cont.
From  the information given above, the closing thrust may be calculated.
CLOSING THRUST        (2 i 707*2 76*1 1) + 1 i 500 + [0 99*(2 i 707 2 i 707]
                                ~      ~                  ~
8i218 + li500 +      0
                  = 9,718 pounds The value    of 9,718    pounds    includes a conservatism of approximately 10%      due to    the  assumed valve factor of 1.1, and an additional conservatism of approximately 500 to 1,000 pounds due to the assumed packing load of 1,500 pounds (see attachment D).
In addition, normal CP&L practice is to multiply the calculated closing thrust by 1.15 in order to account for possible VOTES measurement errors and torque switch repeatability.                Thus, the theoretical calculated closing thrust is 11,176 pounds.
NOTE:      Liberty Technologies issued a 10CFR21 notification on 10/2/92 which documents potential thrust measurement inaccuracies due to torsional effects on small stems.
A review of the design of 1CS-746 has confirmed that the anti-rotation device is located in the yoke flange, above that portion of the stem where the VOTES calibrator was installed.            Thus, the subject 10CFR21 notification does not apply to this valve.
The  calculated minimum allowable closing thrust of 11,176 pounds is within the thrust capabilities and ratings of              the valve and actuator, which are 14,432 and 14,000            pounds,  respectively.
However, there is a concern that inertial effects may cause the final thrust to exceed the continuous ratings              of the actuator and valve. A review of        differential    pressure  test  data for 1CS-752 (a sister valve),    which    was  tested  at  approximately    2,730 psid, indicates    that  thrust  at  torque    switch  trip  was  11,131 inertia pounds (attachment F).      Final    seating    thrust  due to            was  13,432 pounds    (attachment    E),  which    represents  a thrust  increase  of 21%.
Since the assumed VOTES measurement error is +10%, the actual final thrust may exceed the continuous            thrust ratings of the actuator and valve. Thus,            it  is desireable,  if  possible, to adjust the torque switch to trip at a lower value of thrust.
1CS-746                                                              Page No:  9
Prepared By!                                              Calo. ID: *CS-0021 Checked By!                                              Revision:  2 4.3.1      Valve Thrust    Re    ired at Maximum dP cont.
Test data for 1CS-752 indicates that flow isolation was achieved at 7,804 pounds (attachment C) of thrust at an indicated test dP of 2730 psid. This test was performed with a spool piece installed in lieu of the relief valve. The proposed configuration of multiple orifices installed upstream of the MOVs will reduce upstream pressure at          the valve, thereby making the The average closing results of this previous test          conservative.
packing load during the      RF03  test    of  1CS-752    was  456 pounds (attachment D). This packing          load  is  included    in  the 7,804 pounds of thrust at      flow  isolation;      therefore,    the  thrust required to    overcome  differential      pressure    is  equal  to 7,348 pounds. In  order  to  allow  for  variations    in  packing,  a packing load of  1500  pounds  will  be  assumed.
From the information given above, the expected closing thrust may be calculated.
CLOSING THRUST =    7,348 + 1,500 + [0.99*(2,707-2,707]
7i348 + li500 +      0
                  = 8,848 pounds A  differential pressure and line pressure of zero is                assumed  to provide for the most conservative opening thrust.
OPENING THRUST = 1,500  (0*2.76) - I'0.99*(0-0)]
1,500 - 0  0
                  = 1,500 pounds i.3.2      Minimum Allowed Dia          ostic  Th  st The minimum allowable closing/opening thrust at torque switch trip shall be 1.15      times the calculated required thrust when actuator torque is > 50 foot-pounds and 1.20 when actuator torque is ( 50 foot-pounds, in order to account for possible measurement errors and torque switch repeatability. Thus, MINIMUM CLOSING DIAGNOSTIC THRUST            =  REQUIRED THRUST
* 1.15 8,848
* 1.15 10,175 pounds 1CS-746                                                              Page No: 10
Prepared By:                                      Calc. ID: *CS-0021 Checked By:                                      Revisian:  2 4 ' '      Minimum Allowed Dia    astic Thrust Continued MINIMUM OPENING DIAGNOSTIC THRUST        =  REQUIRED THRUST
* 1.20 1,500
* 1.20 1,800 pounds 4.i    Recommended  Minimum Tor  e  Switch Settin s The  input torque (actuator torque) required to produce the thrust values calculated in section 4.3,        may be calculated using the following equation (reference 2.1).
ACTUATOR TORQUE    =  THRUST
* STEM FACTOR Based on  the stem factors given in section 3.3, Assumption 3, the actuator torque for the normal opening and closing conditions may be calculated as follows:
MINIMUM CLOSING TORQUE = 10,175
* 0.0179
                                = 182  ft-lbs MINIMUM OPENING TORQUE =  1,800
* 0.0179 32  ft-lbs i.5    Motor Ca  acit Limits The  available motor torque at degraded-voltage conditions limits the available actuator torque. If a torque switch is set above the minimum available torque, there is a possibility of stalling the motor before the torque switch can actuate. In order to prevent this situation, the maximum torque switch setting value shall not exceed the minimum available torque provided by the motor at degraded-voltage conditions.
1CS-746                                                      Page No: 11
Prepared By:                                    Calc. ZD: *CS-0021 Checked By:                                    Revision:  2 4.5.1      Closin Actuator Tor e as Limited b Motor Ca acit According to reference 2.1, the closing actuator torque that will be developed by the minimum available motor torque (reference 2.3) is calculated as follows.
ACTUATOR TORQUE = MOTOR TORQUE
* UNIT RATIO
* RUNNING EFF.
* 0.9 5.9
* 82.0
* 0.50
* 0.9 218 foot-pounds 4.5.2      0  enin  Actuator Tor e as Limited b Motor Ca ac t According to reference 2.1, the opening actuator torque that will be developed by the minimum available motor torque (reference 2.3) is calculated by:
ACTUATOR TORQUE = MOTOR TORQUE
* UNIT RATIO
* PULLOUT EFF.
* APPLICATION FACTOR 5.9
* 82.0
* 0.4
* 0.9 174 foot-pounds 4.6  Allowable  0 eratin  Ran es 4.6.1      Maximum  Thrust and Tor    e Limits Thrust Limits The allowable thrust limits of the actuator and valve are shown below. The limiting components in the opening and closing directions define the maximum allowable continuous thrust setting.
COMPONENT            LIMIT  POUNDS            SOURCE ACTUATOR                    *12 600              REF. 2.1 VALVE  CLOSING            **12 989            Attachment  B VALVE  OPENING            **12,989            Attachment  B This  limit is  904 of the Limitorque qualified continuous rating.
These limits represent 904 of the Velan continuous duty ratings as provided in attachment B.
1CS-746                                                    Page No: 12
Prepared By:                                        Calc. XD: *CS-0021 Checked By:                                        Revision:  2 4.6.1      Maximum  Thrust and Tar      e  Limits Cantinued Tar  e Limits The  allowable torque limits of the actuator and valve are shown below. The limiting component defines the maximum allowable continuous torque setting.
COMPONENT          LIMIT  FOOT-POUNDS            SOURCE MOTOR  CLOSING              218                    SECTION  4.4 MOTOR  OPENING              174                    SECTION  4.4 ACTUATOR                      *225                  REF. 2. 1 SPRINGSET PACK                250                    REF. 2.11
* This  limit is  904  of the Limitorque qualified continuous rating.
4.6.2      E  ivalent Varmshaft Tar      e From  reference 2.1, the wormshaft torque that must be applied to achieve a required output torque may be calculated by:
WORMSHAFT TORQUE    =    RE UIRED OU PUT TOR U WS  RATIO
* WS  EFFICIENCY 4.6.2.1    Clasin Warmshaft Tar e The equivalent wormshaft torque is provided for the purpose of verifying the closed torque switch setting with a torque wrench.
MINIMUM WORMSHAFT TORQUE                182            11.23  FOOT-POUNDS 45
* 0.36 135 INCH-POUNDS MAXIMUM WORMSHAFT TORQUE                  2 8          13.46  FOOT-POUNDS 45
* 0.36 162 INCH-POUNDS 1CS-746                                                        Page No> 13
Prepared By:                                        Calc. ZD: ~CS-0021 Checked By:                                          Revision:  2 4.6.2.2      0 enin  Wormshaft Tor    e For  this valve the  recommended    minimum opening  torque setting is 32 foot-pounds, and the maximum allowable open torque setting is 174 foot-pounds.      However,  it is not practical to set the opening torque switch with a torque wrench because this would cause the stem to be forced against the backseat.          Therefore, the open torque switch shall be adjusted to a setting of "1" (Reference 2 ~ 11) .
4.7    Stall Evaluation According to electrical analysis (reference 2.3) performed for this valve, the maximum available motor torque at the most favorable conditions is 11.3 foot-pounds.
According to reference 2.1, the stall torque of the operator may be  calculated by:
ACTUATOR STALL TORQUE MAXIMUM MOTOR TORQUE
* UNIT  RATIO
* STALL EFFICIENCY 11.3
* 82.0 * .50      =      463 FOOT-POUNDS The  corresponding stall thrust may be calculated as follows (reference 2.1):
Note: The stem factor for a coefficient of friction of 0.15 is used for conservatism (see section 3.3).
STEM FACTOR
                            ~63          '=    29,679  POUNDS 0  0156 The one-time    limits of the valve    and  actuator are as follows:
COMPONENT                      LIMIT                  SOURCE ACTUATOR  TORQUE          500 FOOT-POUNDS            REF. 2. 1 ACTUATOR  THRUST          35 000 POUNDS              REF. 2. 1 VALVE  CLOS ING            35 616 POUNDS            ATTACHMENT B VALVE  OPENING              35,616    POUNDS          ATTACHMENT B 1CS-746                                                          Page No: 14
Prepared By:                                  Calc. ZD: *CS<<0021 Checked By:                                    Revision:  2 4.7  Stall Bvaluation    Continued The  calculated stall forces for this Motor Operated Valve (MOV) indicate that the potential does not exist for damage to the actuator and valve power train and load-bearing components.
4.8  Re  ired Limit Switch Settin s As shown in reference 2.4, the actuator is equipped with a four train limit switch assembly, arranged in the following manner:
4.8.1        Bases of Limit Switch Set oint Re irements
      ~Rotor  1 Rotor gl acts as the open limit switch, in order to stop the motor after the valve has traveled to the full open position.      It provides position indication (it turns off the green indicator lamps when the valve is full open). In addition, rotor N1 provides a bypass around the closing torque switch as the valve starts closed.
The practice at    SHNPP has been  to set the open limit switches to actuate when the disc is at 96% of full open position unless otherwise specified on the control wiring diagram (reference 2.5). Operating experience has shown that this setting provides for proper flow rate, however, RF03 testing of a sister valve identified that the valve stem was coasting into the backseat.
Thus, a setpoint of 96% may not be adequate and therefore, a setpoint of 90% is recommended (see Attachment A for justification).
Rotor    2 When  the valve is given a signal to close, the motor runs in the closing direction until the torque switch is actuated, which stops the motor.
Rotor 42 is wired to provide a bypass around the open torque switch until the valve is unwedged. In addition, rotor g2 provides valve position indication (it turns off the red indicator lamps when the valve is fully closed).
1CS-746                                                    Page No: 15
Prepared By:                                Calc. ID: *CS-0021 Checked By:                                  Revision:  2 4.8.1      Bases of Limit 8witch Set oint Re irements Cont.
In order to assure proper position indication in the close direction, the close limit switch should be adjusted to indicate a closed condition only after the disc has covered the valve seat. The practice at SHNPP has been to set the close limit switches to actuate when the disc is at the 4% position unless otherwise specified on the control wiring diagram (reference 2.5). Operating experience indicates that 4% from fully closed is adequate to meet the setpoint requirements for rotor N2.
Thus, 4% is an acceptable setting, and can be retained.
Rotor  3 Rotor  43  is not used.
Rotor  4 Rotor  44  provides position indication to the main termination board.
to  open It also provides a permissive which allows valve 1RH-25 provided valve 1CS-746 is closed and other conditions are met.
order to assure proper position indication in the close direction, the close limit switch should be adjusted to indicate a closed condition only after the disc has covered the valve seat. The practice at SHNPP has been to set the close limit switches to actuate when the disc is at the 4% position unless otherwise specified on the control wiring diagram (reference 2.5). Operating experience indicates that 4% from fully closed is adequate to meet the setpoint requirements for rotor N4.
Thus, 4% is an acceptable setting, and can be retained.
4.8.2      Limit Switch Settin Re irements Limit Switch Rotor Settin s In this case, the various limit switch rotors are required to be set as follows:
ROTOR 01:    90% of full open ROTOR 42:    4% of full open ROTOR $ 3    NA ROTOR  44:    4%  of full open 1CS-746                                                  Page No: 16


A B C D E F G Telecon w/Velan Inc.Fax from of Velan Flow Isolation/Seating Thrust Average Closing Packing Load Final Thrust Due to Inertia Thrust at Torque Switch Trip Design Verification Record 1CS-746 Page No: 1 Prepared By: Checked By: Calc.ID!*CS-0021 Revision: 2 TABLE OF CONTENTS Section Descri tion Pacae 1~0 2.0 3.0 4.0 3.1 3'3'Purpose References Bases and Assumptions Analyzed Configuration Valve Function and Control Configuration Assumptions Calculations 4.1 4.2 4.3 Generic Letter 89-10 Applicability Design Differential Pressure Evaluation 7 Valve Thrust 4~4 Recommended Minimum Torque Switch Setting 11 4.5 4.6 Motor Capacity Limits Allowable Operating Ranges 12 4.7.Stall Evaluation 14 5.0 4.8 4.9 Required Limit Switch Settings Nominal Operating Time Results, Conclusions and Recommendations 15 17 19 Attachment A Attachment B Attachment C Attachment D Attachment E Attachment F Attachment G Telecon w/Velan Inc.Fax from of Velan Flow Isolation/Seating Thrust Average Closing Packing Load Final Thrust Due to Inertia Thrust at Torque Switch Trip Design Verification Record 1 page 3 pages 1 page 1 page 1 page 1 page 2 pages 1CS-746 Page No: 2 Prepared By: Checked By: Calc.ID:*CS-0021 Revision: 2 1~0 PURPOSE 1.1 Pu ose of this Re ort The purpose of this report is to document various parameters pertaining to the subject motor-operated valve.This report: reviews the design differential pressure against which the valve may have to operate calculates the MOV thrust/torque requirements evaluates the limitations of the actuator, motor, and valve (evaluation includes effects of a motor stall)evaluates the actuator limit switch settings 1.2 Reason for Revision PCR-6547, Revision 1, removed the Alternate Mini-flow Relief Valves and installed restricting orifices upstream of motor-operated valves 1CS-746 and 1CS-752.The control logic for these motor-operated valve will be modified such that they will automatically open upon high RCS pressure (2300 psig)coincident with an"S" signal and will automatically close at the reset pressure of 1750 psig.The reason for this revision, is to incorporate the changes made by PCR-6547, Revision 1.2'RERERENCES 2.1 NED Design Guide DG-I.11,"Q-List Motor-Operated Valve Mechanical Evaluations", Revision 4.2'NED Scope Document{}9-M0-002, Revision 2.2.3"Analysis of Overload Protection and Motor Torque Output for AC Motor Operated Valves" E5-001, Sub-Calculation CPL-MOV-051, Revision 2.2.4 Control Wiring Diagram CAR 2166-B-401 Sheet 317, Revision 5.2.5 2.6 Corrective Maintenance Procedure CM-I0002, Revision 4.Valve Vendor Print-1364-53850, Revision 1.Technical Manual ISP, Volume 2, Revision 18.1CS-746 Page No: 3 Prepared By: Checked By: Calc.IDs*CS-0021 Revision: 2
Prepared By:                                         Calc. ZD: *CS-0021 Checked By-                                          Revision:             2 4.8 ~ 2     Limit Switch Settin Re irements Continued The preferred method for setting limit switches is to determine the number of handwheel turns needed for a full stroke, and then to set the switches at the required percentages based upon that.
The total number of handwheel turns needed to stroke the valve may be handwheel determined ratio are ifall the stroke known.
length, thread lead, and The   total  handwheel(HW)   turns to  fully stroke    the valve is calculated    as follows:
TURNS~    =    VALVE STROKE  /  THREAD LEAD
* HANDWHEEL RATIO 1.5 inches  /  .667 inches
* 4.38 9.85 handwheel turns 44  of 9.85 handwheel turns is equal to 3/8 handwheel turn.
104 of 9.85 handwheel turns is equal to 1 handwheel turn.
4.9    Nominal 0  eratin Time o eratin time is rovided for i o atio o                            as actual motor RPMs can va        with a lied load. With the information provided in section 3.1, the stem nut revolutions per valve stroke and the stem nut revolutions per minute can be determined as follows:
STROKE'ominal
                              /        *      = EGZK-LEAD 1.5 0.667 2.25 STEM NUT REVOLUTIONS/MINUTE              MOTOR RP OVERALL UNIT RATIO 1700 82.0 20 '3 1CS-746                                                                     Page No: 17


==2.0 REFERENCES==
Prepared By:                                  Calc. ZD: *CS-0021 Checked Byt                                    Revision: 2 i.9  Nominal 0 eratin    Time  Continued With these calculated values the nominal expected operating time of this valve can be calculated using the following equation:
STROKE TIME = STEM NU        OLUTI S VALVE STRO STEM NUT REVOLUTIONS/MINUTE 2.25 20 '3 0 '1 MINUTES/VALVE STROKE 6.5  SECONDS/VALVE STROKE This valve has no specific stroke time requirements other than the generic 10 second maximum stroke time required by reference 2.13.
1CS-746                                                  Page No: 18


Continued 2.8 2.9 2.10 2~11 2.12 2.13 2~14 2.15a.zs 2~17 2.18 Chemical&Volume Control Piping, Reactor Auxiliary Building, Plans, CAR-2165-G-140, Revision 23.Chemical and Volume Control System Description, SD-107, Revision 2.Crane Technical Paper No.410, Nineteenth Printing-1980.Technical Memorandum"Performance and Properties of Limitorque Components", Number TM-G-XXXX-001, Rev.0.Piping Line List, CAR-1364-B-0070, Revision 44.Westinghouse E-Spec.No.G-678852, Revision 2.Design Basis Document DBD-104, Revision 0.RAB Tank Area Sections, CAR-2165-G-251, Revision 18.Piping Isometric 1-CS-651, Revision 5.Limitorque Order Sheet 3D0652-D PCR-6547, Revision 1,"Alternate Mini-Flow Re-Design" 3'BASES AND ASSUMPTIONS 3.1 Anal zed Confi ration The configuration assumed when performing this analysis is as follows: Actuator Dat Limitorque Order Number: Actuator Size&Type: Overall Unit Ratio: Handwheel Ratio: Handwheel Efficiency:
Prepared By:                                       Calc. ID! *CS-0021 Checked By:                                        Revision:   2 5'    RESULTS    CONCLUSIONS AND RECOMMENDATIONS 5.1   Results and Conclusions
Worm Set/Gear Ratio: Worm Set Efficiency:
: 1)     The actuator torque switch and limit switch ranges shall be established as shown in table 5.1.
Applications Factor: Installed Spring Pack: Pullout Efficiency:
TABLE 5 e 1         BASIC DATA AND SETO    RE UZREMENTS CLOSING THRUST RANGE (POUNDS)         OPENING THRUST RANGE (POUNDS)
Run Efficiency:
MINIMUM                  MAXIMUM    MINIMUM                    MAXIMUM 10 175                    12 600    1 800                    12 600 RECOMMENDED                        RECOMMENDED CLOSE TORQUE SWITCH SETTINGS          OPEN TORQUE SWITCH SETTINGS MINIMUM          ~
Stall Efficiency:
MAXIMUM    MINIMUM                    MAXIMUM 182 FT-LBS            218 FT-LBS    32 FT-LBS              174 FT-LBS EQUIVALENT                          EQUIVALENT CLOSE WORMSHAFT TORQUE          OPEN TORQUE SWITCH    DIAL SETTING MINIMUM                  MAXIMUM    MINIMUM                    MAXIMUM 135 IN-LBS            162 IN-LBS LIMIT SWITCH SETTINGS ROTOR  &#xb9;1           ROTOR  &#xb9;2       ROTOR &#xb9;3          ROTOR  &#xb9;4 90%                                N/A                   4%
3D0652-D SMB-00 1 82~0:1 4~3P:1'5%45:p 36%0.9 60-600-0047-1 40%50%50%1CS-746 Page No: 4 Prepared By: Checked By: Calc.ID:*C8-0021 Revision: 2 3.1 Anal sed Confi ration Continued Motor Data Foot-Pounds:
1 HW TURN          3/8 HW TURN                        3/8  HW TURN FROM  FULL          FROM  FULL                          FROM  FULL OPEN                CLOSED                              CLOSED 5.2   Recommendations It  is recommended that this valve be retested at maximum achievable differential pressure and flow upon completion of PCR-6547. The test results will be evaluated to confirm the setup ranges established in this calculation are acceptable.
RPM: Volts: 10 1700 460 AC Manufacturer:
1CS-746                                                         Page No: 19
Valve Size&Type: Valve Pressure Class: Mean Contact Seat Diameter: Stem Configuration:
Stroke Length: Velan 2-inch, globe 1500 psig 1.875 1.125D-1/3P-2/3L 1.5 inches 1-Walkdown Data"Motor-Operated-Valve Data Form" 2-NED Design Guide I.11 (Reference 2.1)3-Limitorque Order Sheet (Reference 2.17)4-Emdrac Print (Reference 2.7)~~~3.1.1 Cross-reference Number s The Ebasco (construction identification) tag number for this valve is 2CS-V757SA-1.
The Westinghouse Identification Number and Location are 2TM78FNM and 8489A respectively.
3.2 Valve Function and Control Confi ration 3.2.1 Valve Function The alternate mini-flow line is for dead head protection of the CSIP's during safety injection (specifically the injection phase of the SIS operation).
Valves 1CS-746 and 1CS-752 are designed to open automatically upon high RCS pressure (2300 psig)coincident with an"S" signal and will automatically close at the reset pressure of 1750 psig (Reference 2.18).These valves are located in parallel on the two alternate mini-flow lines which relieve to the RWST.I 1C8-746 Page No: 5 Prepared By: Checked By: Calo.IDs*CS-0021 Revision: 2 3.2.2 Control Confi ration The following statements are derived from references 2.4, 2.5 and 2~18~This MOV automatically opens upon high RCS pressure (2300 psig)coincident with an"S" signal and will close at the reset pressure of 1750 psig.Under normal conditions this MOV can only open if valves 1RH-25, 1RH-63 and either 1CS-165, 1CS-166 or 1CS-745 are closed.This MOV trips out via the torque switch in the closing direction and is electrically de-energized by the open limit switch, in the opening direction.
The open torque switch and thermal overloads are automatically bypassed on loss of offsite power or a safety injection actuation.
1)The minimum torque delivered by the actuator motor is assumed to be 5.9 ft-lbs per reference 2.3.2)The maximum torque delivered by the actuator motor is assumed to be 11.3 ft-lbs per reference 2.3.3)The Stem Factor for a coefficient of friction of 0.15 is 0.0156 and a coefficient of friction of 0.2 is 0.0179 (reference 2.1).4)The flow limiting component in the alternate mini-flow line is the fixed orifice.The flow capacity of this orifice is 60 gpm nominally (reference 2.18).5)The maximum operating temperature and design temperature for line number 2CS2-785SN-1 is 130 F and 200 F respectively (reference 2.12).6)Piping frictional losses are ignored when calculating differential pressure at the valve.7)The 0.433 psig/ft conversion factor used in this calculation is based on water at 60 F (reference 2.10).XCS-746 Page No: 6 Prepared By: Checked By: Calc.ID:*CS>>0021 Revision: 2 4'CALCULATIONS 4.1 Generic Letter 89-10 A licabilit Valve 1CS-746 is located in the CSIP alternate mini-flow line and is designed to open automatically upon high RCS pressure coincident with an"S" signal and automatically close at the reset pressure (Reference 2.18).The alternate mini-flow line is for dead head protection of the CSIP's during safety injection (specifically the injection phase of the SIS operation).
Based on the preceding paragraph and the guidance provided in reference 2.2, the requirements of Generic Letter 89-10 are a licable to this MOV.4.2 Desi n Differential Pressure Evaluation 4~2~1 S stem Inlet Pressure Upstream.pressure will be assumed to be equal to the shutoff head of the CSIPs plus the static head of the RWST at its maximum level.CSIP shutoff head: 6200 feet (ref.2.7)*0.433 psig/foot=2,684 psig Static Head: RWST Maximum Level=301 ft.(ref.2.15)Valve Elevation=249 ft.(ref.2.16)(301 ft.-249 ft.)*0.433 psig/ft 23 s'pstream Pressure is equal to: 2,707 psig 4.2.2 Differential Pressure The maximum differential pressure (dP)occurs when maximizing the upstream and minimizing the downstream pressure.To maximize dP, it is assumed that the downstream pressure is 0 psig.Therefore, the maximum differential pressure is 2,707 psid.1CS-746 Page No: 7 Prepared By: Checked By: Calo.ID:*CS-0021 Revision: 2 4.2.2 Differential Pressure Continued I Note: The subject MOV is a pressure under the seat globe valve.The most conservative opening differential pressure assumption is to assume 0 psid since any line pressure would assist the valve in opening.For this reason opening upstream pressure and differential pressure are not calculated.
4.3 Valve Thrust 4.3.1 Valve Thrust Re ired at Maximum dP The maximum thrust requirements for the operation of this pressure under the seat globe valve may be determined by the following equations, which are provided by reference 2.1.CLOSING THRUST=(dp*A*FV)+SBL+[SA*(P-dP))
OPENING THRUST=SBL-(dP*A)-[SA*(P-dP))
where: THRUST=The required stem thrust, in pounds-force.
The differential pressure across the valve.The seat area of the valve, which is 2.76 square inches based on contact seat diameter (Section 3 1)An empirical valve factor, which is 1.1 per reference 2.1.SBL The stuffing box load, or packing drag, expressed in pounds-force.
This is 1500 pounds per reference 2.1.SA The area of the stem, in square inches.For the stem diameter given in section 3.1, this area is 0.99 square inches.The inlet system pressure.1CS-746 Page No: 8 Prepared By: Checked By: Calo.ZD!*CS-0021 Revision: 2 4.3.1 Valve Thrust Re ired at Maximum dP cont.From the information given above, the closing thrust may be calculated.
CLOSING THRUST (2 i 707*2~76*1~1)+1 i 500+[0~99*(2 i 707 2 i 707]8i218+li500+0=9,718 pounds The value of 9,718 pounds includes a conservatism of approximately 10%due to the assumed valve factor of 1.1, and an additional conservatism of approximately 500 to 1,000 pounds due to the assumed packing load of 1,500 pounds (see attachment D).In addition, normal CP&L practice is to multiply the calculated closing thrust by 1.15 in order to account for possible VOTES measurement errors and torque switch repeatability.
Thus, the theoretical calculated closing thrust is 11,176 pounds.NOTE: Liberty Technologies issued a 10CFR21 notification on 10/2/92 which documents potential thrust measurement inaccuracies due to torsional effects on small stems.A review of the design of 1CS-746 has confirmed that the anti-rotation device is located in the yoke flange, above that portion of the stem where the VOTES calibrator was installed.
Thus, the subject 10CFR21 notification does not apply to this valve.The calculated minimum allowable closing thrust of 11,176 pounds is within the thrust capabilities and ratings of the valve and actuator, which are 14,432 and 14,000 pounds, respectively.
However, there is a concern that inertial effects may cause the final thrust to exceed the continuous ratings of the actuator and valve.A review of differential pressure test data for 1CS-752 (a sister valve), which was tested at approximately 2,730 psid, indicates that thrust at torque switch trip was 11,131 pounds (attachment F).Final seating thrust due to inertia was 13,432 pounds (attachment E), which represents a thrust increase of 21%.Since the assumed VOTES measurement error is+10%, the actual final thrust may exceed the continuous thrust ratings of the actuator and valve.Thus, it is desireable, if possible, to adjust the torque switch to trip at a lower value of thrust.1CS-746 Page No: 9 Prepared By!Checked By!Calo.ID:*CS-0021 Revision: 2 4.3.1 Valve Thrust Re ired at Maximum dP cont.Test data for 1CS-752 indicates that flow isolation was achieved at 7,804 pounds (attachment C)of thrust at an indicated test dP of 2730 psid.This test was performed with a spool piece installed in lieu of the relief valve.The proposed configuration of multiple orifices installed upstream of the MOVs will reduce upstream pressure at the valve, thereby making the results of this previous test conservative.
The average closing packing load during the RF03 test of 1CS-752 was 456 pounds (attachment D).This packing load is included in the 7,804 pounds of thrust at flow isolation; therefore, the thrust required to overcome differential pressure is equal to 7,348 pounds.In order to allow for variations in packing, a packing load of 1500 pounds will be assumed.From the information given above, the expected closing thrust may be calculated.
CLOSING THRUST=7,348+1,500+[0.99*(2,707-2,707]
7i348+li500+0=8,848 pounds A differential pressure and line pressure of zero is assumed to provide for the most conservative opening thrust.OPENING THRUST=1,500-(0*2.76)-I'0.99*(0-0)]
1,500-0-0=1,500 pounds i.3.2 Minimum Allowed Dia ostic Th st The minimum allowable closing/opening thrust at torque switch trip shall be 1.15 times the calculated required thrust when actuator torque is>50 foot-pounds and 1.20 when actuator torque is (50 foot-pounds, in order to account for possible measurement errors and torque switch repeatability.
Thus, MINIMUM CLOSING DIAGNOSTIC THRUST=REQUIRED THRUST*1.15 8,848*1.15 10,175 pounds 1CS-746 Page No: 10
* Prepared By: Checked By: Calc.ID:*CS-0021 Revisian: 2 4''Minimum Allowed Dia astic Thrust Continued MINIMUM OPENING DIAGNOSTIC THRUST=REQUIRED THRUST*1.20 1,500*1.20 1,800 pounds 4.i Recommended Minimum Tor e Switch Settin s The input torque (actuator torque)required to produce the thrust values calculated in section 4.3, may be calculated using the following equation (reference 2.1).ACTUATOR TORQUE=THRUST*STEM FACTOR Based on the stem factors given in section 3.3, Assumption 3, the actuator torque for the normal opening and closing conditions may be calculated as follows: MINIMUM CLOSING TORQUE=10,175*0.0179=182 ft-lbs MINIMUM OPENING TORQUE=1,800*0.0179 32 ft-lbs i.5 Motor Ca acit Limits The available motor torque at degraded-voltage conditions limits the available actuator torque.If a torque switch is set above the minimum available torque, there is a possibility of stalling the motor before the torque switch can actuate.In order to prevent this situation, the maximum torque switch setting value shall not exceed the minimum available torque provided by the motor at degraded-voltage conditions.
1CS-746 Page No: 11 Prepared By: Checked By: Calc.ZD:*CS-0021 Revision: 2 4.5.1 Closin Actuator Tor e as Limited b Motor Ca acit According to reference 2.1, the closing actuator torque that will be developed by the minimum available motor torque (reference 2.3)is calculated as follows.ACTUATOR TORQUE=MOTOR TORQUE*UNIT RATIO*RUNNING EFF.*0.9 5.9*82.0*0.50*0.9 218 foot-pounds 4.5.2 0 enin Actuator Tor e as Limited b Motor Ca ac t According to reference 2.1, the opening actuator torque that will be developed by the minimum available motor torque (reference 2.3)is calculated by: ACTUATOR TORQUE=MOTOR TORQUE*UNIT RATIO*PULLOUT EFF.*APPLICATION FACTOR 5.9*82.0*0.4*0.9 174 foot-pounds 4.6 Allowable 0 eratin Ran es 4.6.1 Maximum Thrust and Tor e Limits Thrust Limits The allowable thrust limits of the actuator and valve are shown below.The limiting components in the opening and closing directions define the maximum allowable continuous thrust setting.COMPONENT ACTUATOR VALVE CLOSING VALVE OPENING LIMIT POUNDS*12 600**12 989**12,989 SOURCE REF.2.1 Attachment B Attachment B This limit is 904 of the Limitorque qualified continuous rating.These limits represent 904 of the Velan continuous duty ratings as provided in attachment B.1CS-746 Page No: 12 Prepared By: Checked By: Calc.XD:*CS-0021 Revision: 2 4.6.1 Maximum Thrust and Tar e Limits Cantinued Tar e Limits The allowable torque limits of the actuator and valve are shown below.The limiting component defines the maximum allowable continuous torque setting.COMPONENT MOTOR CLOSING MOTOR OPENING ACTUATOR SPRINGSET PACK LIMIT FOOT-POUNDS 218 174*225 250 SOURCE SECTION 4.4 SECTION 4.4 REF.2.1 REF.2.11*This limit is 904 of the Limitorque qualified continuous rating.4.6.2 E ivalent Varmshaft Tar e From reference 2.1, the wormshaft torque that must be applied to achieve a required output torque may be calculated by: WORMSHAFT TORQUE=RE UIRED OU PUT TOR U WS RATIO*WS EFFICIENCY 4.6.2.1 Clasin Warmshaft Tar e The equivalent wormshaft torque is provided for the purpose of verifying the closed torque switch setting with a torque wrench.MINIMUM WORMSHAFT TORQUE MAXIMUM WORMSHAFT TORQUE 182 45*0.36 135 INCH-POUNDS 2 8 45*0.36 162 INCH-POUNDS 11.23 FOOT-POUNDS 13.46 FOOT-POUNDS 1CS-746 Page No>13


Prepared By: Checked By: Calc.ZD:~CS-0021 Revision: 2 4.6.2.2 0 enin Wormshaft Tor e For this valve the recommended minimum opening torque setting is 32 foot-pounds, and the maximum allowable open torque setting is 174 foot-pounds.
Attachment A Calc. No. CS~1 Revision 2 TELECON                    Valve No. 1CS-746 Page 1 of 1 BETWEEN:
However, it is not practical to set the opening torque switch with a torque wrench because this would cause the stem to be forced against the backseat.Therefore, the open torque switch shall be adjusted to a setting of"1" (Reference 2~11).4.7 Stall Evaluation According to electrical analysis (reference 2.3)performed for this valve, the maximum available motor torque at the most favorable conditions is 11.3 foot-pounds.
MECHANICAL ENGINEER CAROLINA POWER & LIGHT AND: MR.
According to reference 2.1, the stall torque of the operator may be calculated by: ACTUATOR STALL TORQUE MAXIMUM MOTOR TORQUE*UNIT RATIO*STALL EFFICIENCY 11.3*82.0*.50=463 FOOT-POUNDS The corresponding stall thrust may be calculated as follows (reference 2.1): Note: The stem factorfor a coefficient of friction of 0.15 is used for conservatism (see section 3.3).STEM FACTOR~63'=29,679 POUNDS 0 0156 The one-time limits of the valve and actuator are as follows: COMPONENT ACTUATOR TORQUE ACTUATOR THRUST VALVE CLOS ING VALVE OPENING LIMIT 500 FOOT-POUNDS 35 000 POUNDS 35 616 POUNDS 35,616 POUNDS SOURCE REF.2.1 REF.2.1 ATTACHMENT B ATTACHMENT B 1CS-746 Page No: 14 Prepared By: Checked By: Calc.ZD:*CS<<0021 Revision: 2 4.7 Stall Bvaluation Continued The calculated stall forces for this Motor Operated Valve (MOV)indicate that the potential does not exist for damage to the actuator and valve power train and load-bearing components.
MANAGER OF ENGINEERING VELAN INC.
4.8 Re ired Limit Switch Settin s As shown in reference 2.4, the actuator is equipped with a four train limit switch assembly, arranged in the following manner: 4.8.1 Bases of Limit Switch Set oint Re irements~Rotor 1 Rotor gl acts as the open limit switch, in order to stop the motor after the valve has traveled to the full open position.It provides position indication (it turns off the green indicator lamps when the valve is full open).In addition, rotor N1 provides a bypass around the closing torque switch as the valve starts closed.The practice at SHNPP has been to set the open limit switches to actuate when the disc is at 96%of full open position unless otherwise specified on the control wiring diagram (reference 2.5).Operating experience has shown that this setting provides for proper flow rate, however, RF03 testing of a sister valve identified that the valve stem was coasting into the backseat.Thus, a setpoint of 96%may not be adequate and therefore, a setpoint of 90%is recommended (see Attachment A for justification).
DATE:     JANUARY 6, 1992 TIME:     2:35PM
Rotor 2 When the valve is given a signal to close, the motor runs in the closing direction until the torque switch is actuated, which stops the motor.Rotor 42 is wired to provide a bypass around the open torque switch until the valve is unwedged.In addition, rotor g2 provides valve position indication (it turns off the red indicator lamps when the valve is fully closed).1CS-746 Page No: 15 Prepared By: Checked By: Calc.ID:*CS-0021 Revision: 2 4.8.1 Bases of Limit 8witch Set oint Re irements Cont.In order to assure proper position indication in the close direction, the close limit switch should be adjusted to indicate a closed condition only after the disc has covered the valve seat.The practice at SHNPP has been to set the close limit switches to actuate when the disc is at the 4%position unless otherwise specified on the control wiring diagram (reference 2.5).Operating experience indicates that 4%from fully closed is adequate to meet the setpoint requirements for rotor N2.Thus, 4%is an acceptable setting, and can be retained.Rotor 3 Rotor 43 is not used.Rotor 4 Rotor 44 provides position indication to the main termination board.It also provides a permissive which allows valve 1RH-25 to open provided valve 1CS-746 is closed and other conditions are met.order to assure proper position indication in the close direction, the close limit switch should be adjusted to indicate a closed condition only after the disc has covered the valve seat.The practice at SHNPP has been to set the close limit switches to actuate when the disc is at the 4%position unless otherwise specified on the control wiring diagram (reference 2.5).Operating experience indicates that 4%from fully closed is adequate to meet the setpoint requirements for rotor N4.Thus, 4%is an acceptable setting, and can be retained.4.8.2 Limit Switch Settin Re irements Limit Switch Rotor Settin s In this case, the various limit switch rotors are required to be set as follows: ROTOR 01: ROTOR 42: ROTOR$3 ROTOR 44: 90%of full open 4%of full open NA 4%of full open 1CS-746 Page No: 16 Prepared By: Checked By-Calc.ZD:*CS-0021 Revision: 2 4.8~2 Limit Switch Settin Re irements Continued The preferred method for setting limit switches is to determine the number of handwheel turns needed for a full stroke, and then to set the switches at the required percentages based upon that.The total number of handwheel turns needed to stroke the valve may be determined if the stroke length, thread lead, and handwheel ratio are all known.The total handwheel(HW) turns to fully stroke the valve is calculated as follows: TURNS~=VALVE STROKE/THREAD LEAD*HANDWHEEL RATIO 1.5 inches/.667 inches*4.38 9.85 handwheel turns 44 of 9.85 handwheel turns is equal to 3/8 handwheel turn.104 of 9.85 handwheel turns is equal to 1 handwheel turn.4.9 Nominal 0 eratin Time motor RPMs can va with a lied load.With the information provided in section 3.1, the stem nut revolutions per valve stroke and the stem nut revolutions per minute can be determined as follows:/*=EGZK-LEAD STROKE'ominal o eratin time is rovided for i o atio o as actual 1.5 0.667 2.25 STEM NUT REVOLUTIONS/MINUTE MOTOR RP OVERALL UNIT RATIO 1700 82.0 20'3 1CS-746 Page No: 17 Prepared By: Checked Byt Calc.ZD:*CS-0021 Revision: 2 i.9 Nominal 0 eratin Time Continued With these calculated values the nominal expected operating time of this valve can be calculated using the following equation: STROKE TIME=STEM NU OLUTI S VALVE STRO STEM NUT REVOLUTIONS/MINUTE 2.25 20'3 0'1 MINUTES/VALVE STROKE 6.5 SECONDS/VALVE STROKE This valve has no specific stroke time requirements other than the generic 10 second maximum stroke time required by reference 2.13.1CS-746 Page No: 18 Prepared By: Checked By: Calc.ID!*CS-0021 Revision: 2 5'RESULTS CONCLUSIONS AND RECOMMENDATIONS 5.1 Results and Conclusions 1)The actuator torque switch and limit switch ranges shall be established as shown in table 5.1.TABLE 5 e 1 BASIC DATA AND SETO RE UZREMENTS CLOSING THRUST RANGE (POUNDS)MINIMUM MAXIMUM OPENING THRUST RANGE (POUNDS)MINIMUM MAXIMUM 10 175 12 600 1 800 12 600 RECOMMENDED CLOSE TORQUE SWITCH SETTINGS MINIMUM~MAXIMUM RECOMMENDED OPEN TORQUE SWITCH SETTINGS MINIMUM MAXIMUM 182 FT-LBS 218 FT-LBS 32 FT-LBS 174 FT-LBS EQUIVALENT CLOSE WORMSHAFT TORQUE MINIMUM MAXIMUM EQUIVALENT OPEN TORQUE SWITCH DIAL SETTING MINIMUM MAXIMUM 135 IN-LBS ROTOR&#xb9;1 90%1 HW TURN FROM FULL OPEN 162 IN-LBS LIMIT SWITCH SETTINGS ROTOR&#xb9;2 ROTOR&#xb9;3 N/A 3/8 HW TURN FROM FULL CLOSED ROTOR&#xb9;4 4%3/8 HW TURN FROM FULL CLOSED 5.2 Recommendations It is recommended that this valve be retested at maximum achievable differential pressure and flow upon completion of PCR-6547.The test results will be evaluated to confirm the setup ranges established in this calculation are acceptable.
1CS-746 Page No: 19 TELE CON BETWEEN: MECHANICAL ENGINEER CAROLINA POWER&LIGHT AND: MR.MANAGER OF ENGINEERING VELAN INC.Attachment A Calc.No.CS~1 Revision 2 Valve No.1CS-746 Page 1 of 1 DATE: JANUARY 6, 1992 TIME: 2:35PM  


==SUBJECT:==
==SUBJECT:==
2n AND SMALLER VELAN GLOBE VALVES MR.STATED THAT 90\OF FULL OPEN STROKE WOULD ALLOW FULL DESIGN FLOW.
2n AND SMALLER VELAN GLOBE VALVES MR.           STATED THAT 90\ OF FULL OPEN STROKE WOULD ALLOW FULL DESIGN FLOW.
Attachment B Calc.No.'CS4)021 Revision 2 Valve No.1CS-746 Page I of 3 YIA FAX Number of pages including this page: Q Please reply by FAX to: Q Head Office and Plant No, 1 (514)748-8635 Q Marketing (514)748-7592 Q Plant No.2 (514)341-3032 Q Spare Parts (514)342-2311 Q Plant No.3 (802)862-4014 Q Plant No.4 (514)378-6865 Message No.:<'a~8 Oate;8 9Q From: To: Attention:
 
Copies to: Subject/
Attachment B Calc. No. 'CS4)021 Revision 2 Valve No. 1CS-746 Page   I of 3 Number of pages YIA FAX            including this page: Q Please reply by FAX to:           Message No.: <'a ~8 To:
Q Head Office and                 Oate;        8 9Q Plant No, 1 (514) 748-8635 Q Marketing   (514) 748-7592 Q Plant No. 2 (514) 341-3032   From:              Attention:
Q Spare Parts (514) 342-2311 Q Plant No. 3 (802) 862-4014                         Copies to:
Q Plant No. 4 (514) 378-6865 Subject/  


==Reference:==
==Reference:==


/~am nyk~W uaduaa.~+.
        /~am nyk         ~     W uaduaa.~+.
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                        ~. 45.0'F...,.......
~~yga~imrm GLOBE VALVE-2 in STEM ANALYSIS Attachment B Calc.No.*CS4021 Revision 2 Valve No.1CS-746 Page 2 of 3 UTILITY: CAROLZNA POWER AND LIGHT W.I~D.4: 2TM78FNM VALVE DWG: E73-62S STEM DWG.7913-22 Order no.P9-Design Temp.Pressure Class 125 deg F 1500 lb STEM THRD.1 1/8-3 ACME double lead STEM MAT.SS 630 A 564 sa=45950 Psi Code Case N-62-4 STEM DATA dl d2 0 917 in-0.425 in.0.396 in.0.792 in.root.dia of thread dim.at.sec.d2 dim.at sec.k rad.d/2 0.016 ft.lb./lb thread.fact:or a3 0.492 in."2 0.660 in.2 1.224 in."2 0.039 in 4 0 in.0 in.0.019 in."4 root area of thread area of sec.d2 area at d2 in shear polar moment of iner-t'.a ov: scam thread eff.length of stem torcpze arm radius Moment of Inertia Er2'd TT'E2 2>E t TS 2d SLHd 3HUdS NU'Hah 9t''ST 26r$8 lDO GLOBE VALVE-2 in STEM ANALYSZS Attachment B Calc.No.'CS-0021 Revision 2 Valve No.1CS-746 Page 3 of 3 UTZLZTY: CAROXZNA POWER AND LIGHT Order no.P9-W.I'D.2TM78FNM VALVE DWG: E73-62S STEM DWG 7913-22 Design Temp.Pressure Class 125 deg F 1500 lb STEM THRD.1 1/8-3 ACME double lead STEM MAT.SS 630 A 564 Sy~, 113396 Psi Code Case N-62-4 STEM CALCULATION At Section d1 Max Tr At Section d2 14432 lbs.f rom Eq.(19)Max Tr At Section k 30347 lbs.from Eq.(20)Max Tr 33756 lbs.from Eq.(21)MAX Thrust/Torque CLOSZNG OPENING Tr./lbs.Tor./lb-ft Tr./lbs.Tor./lb-xt CONTINUOUS DUTY ONE TIME 14432 35616 224 14432 554 35616 224 554 ErE'd 7 TK2 2IE ITS 2d SJ.Hd 3HUdS NU l3h Z1: ST 26 w 88 J.DO AITACHMENT C<<CS4021, Rev.2 Page 1 of 1 Test: 4 3/23/3i 22'49'i VOTES 8ENSOR 5000 Tag: iCS-752-ioooo oIce=-7SM (Ihs)-isooo.20000 52997 53997 5%997 55997 55897 57997 SWITCH A SWITCH B SWITCH C SWITCH D 52997 53997 Tin: im Seconds 55.397 5%997 55997 55997 57997 1CS-752: Flow Isolation/Seating Thrust2730 PSID ATI'ACHMENT D*CS4021, Rev.2 Page 1 of 1 Test: i 3(23/3i 22'25'45 VERS SENSOR.%50-%60 Tag: iCS-752 orce=-456 (1hS)-%~0-%80 25209 25309 25%09 25509 25609 25709 OLS 25209 25309 25%09 25509 25C09 25709 Tiae in Seconds 25.453 Y-EXPO ON 1CS-752: Average Closing Packing Load, Static Conditions ATl ACHMENT E'CS4021, Rev2 Page 1 of 1 Ted: 4 3(23/3i 22'49'i Tag: iCS-752 VOTES BEMOR orce=-i3432 (Ih)-i5000-20000 5530%55%0%5550%556 5570%5580%SMITCH A SMITCH B SMITCH C SMITCH D 5530%55%0%Tiae im Seconds 55.688 5550'}SS6 SP0%SSS0%Y-EKPND ON 1CS-752, Final Thrust Due to Inertia A1TACHMENT F CS-0021, Rev.2 Page 1 of 1 Test'3/23/3i 22'49'i V jTES SENSOR-F0000 Tag'C8-752 orce=-iii3i)15000.20000 5550%55%0%550'f 5560'I 5570%5580%SWITCH A SMITCH B SWITCH C SWITCH 9 5530'f 55%0%Time in Seconds 55.488 550't 5560%5570'f 5580%'Il'-m'll ox 1CS-752, Thrust At Torque Switch Trip E DES>~~ER3:mumm RzcoR]]I~~f~to Verification Pcrsc&#xc3;%%tl Attachment G Calc.No.'CS~1 Revision 2 Valve No.1CS-746 Page 1 of 2 Plant Project Fflc No.Oocuncnt No.C-0 I Rev 4 Level g 4 (Class A)(]Seismic (Class B)(]FP 4 (Class 0)(]Other Ocsign verification should be done in accordance ufth ANSI N45,p I), Scctfon 6, as amended by Regulatory Guide 1.64, Rev.2.Special instructions:
        ~~         yga~imrm
Oisciplinc Project Engineer II.Veri f Icatf cn Oo~tatf cn Appl f cabf l I ty Ofsci t inc Necnanf ca L HVAC ELectricaL fSC Other X]Ofsci fne Civil Structural Seismic Eaufp.Oual.Civil Stress F f re Protect Ion Envirormantai Oual if fcation Humn Factors Naterials (](](](](][](](][]Verification Nethods Used: Oesign Review (]Alternate Calculations
 
[]oualfffcation testing Ocsign Oocunent Acccetable:
Attachment B GLOBE VALVE       -   2 in                         Calc. No. *CS4021 Revision 2 STEM ANALYSIS                                    Valve No. 1CS-746 Page 2 of 3 UTILITY:     CAROLZNA POWER AND LIGHT               Order no. P9-W. I ~ D. 4:   2TM78FNM VALVE DWG:     E73-62S                           Design Temp.              125 deg F STEM DWG.       7913-22                           Pressure Class           1500   lb STEM THRD.     1 1/8 3 ACME   double lead STEM MAT.       SS 630 A 564 sa =     45950 Psi                                   Code Case N-62-4 STEM DATA dl                         0.792     in.         root. dia     of thread d2                        0 917 in-            dim. at. sec. d2 0.425 in.            dim. at sec. k 0.396 in.            rad. d/2 0.016   ft.lb./lb       thread. fact:or 0.492   in."2       root area of thread 0.660 in. 2           area of sec. d2 a3                        1.224 in."2           area at d2 in shear 0.039 in 4           polar moment of iner-t'.a ov: scam thread 0 in.          eff. length of stem 0 in.          torcpze arm radius 0.019    in."4        Moment     of Inertia Er2'd                           TT'E2 2>E t TS 2d SLHd 3HUdS NU'Hah 9t''ST 26r $ 8 lDO
~Y~No (].ccaaants attached.Ocsign verifier oats'~V4 Ackncwlcdgcment okgerfff~tfm+
 
~(OPE)oats III.Rcsolutfm at Ccmmnst Cazeants Resolved (See Attached): (RE)Action taken makes Ocsign Oocusents Acceptable:
Attachment B Calc. No. 'CS-0021 Revision 2 GLOBE VALVE      2    in                            Valve No. 1CS-746 Page 3 of 3 STEM ANALYSZS UTZLZTY:   CAROXZNA POWER AND LIGHT               Order no. P9-W.I'D.         2TM78FNM VALVE DWG:     E73-62S                         Design Temp.                125 deg F STEM DWG       7913-22                       Pressure Class             1500   lb STEM THRD.     1 1/8   3 ACME   double lead STEM MAT.     SS 630 A 564 Sy ~, 113396 Psi                                     Code Case N-62-4 STEM CALCULATION At Section d1 Max Tr                   14432   lbs.         from    Eq. (19)
Oesign veriffer Oate Oats (OPE)Oate Proc.3.3 Rev.38 OISCIPLIRE OESICS VERIFIClTIM RSXRO CA%EST SHEET Attachment G Calc.No.CS4021 Revision 2 Ualve No.1CS-746 Page 2 of 2 Plant Pr oieot File Qo.Oocmmn Mo.~S&oZl a Z This sheet is catv recaired Men coocaents are, bein%nba.Cccooant Mo Resolution Resolved lnitfatlOate
At Section    d2 Max Tr                   30347   lbs.         from Eq. (20)
~V 1~".;ev.>>'0 Eeet.osuRa 2  
At Section k Max Tr                   33756   lbs.         from Eq. (21)
MAX   Thrust/Torque                       CLOSZNG                   OPENING Tr./lbs. Tor./lb-ft Tr./lbs. Tor./lb-xt CONTINUOUS DUTY                       14432            224      14432                224 ONE TIME                             35616           554       35616                 554 ErE'd                           7 TK2 2IE ITS 2d SJ.Hd 3HUdS NU l3h Z1: ST 26 w 88 J.DO
 
AITACHMENTC
                                                          <<CS4021, Rev. 2 Page 1 of 1 Test: 4                                                           Tag: iCS-752 3/23/3i 22'49'i 5000 VOTES 8ENSOR
                -ioooo oIce = -7SM (Ihs)   -isooo
                .20000 52997     53997       5%997 55997       55897       57997 SWITCH A SWITCH B SWITCH C SWITCH D 52997     53997       5%997 55997        55997      57997 Tin:   im Seconds   55.397 1CS-752:     Flow Isolation/Seating Thrust            2730 PSID
 
ATI'ACHMENTD
                                                          *CS4021, Rev. 2 Page 1 of 1 Test:   i                                                         Tag: iCS-752 3(23/3i 22'25'45
                    .%50 VERS    SENSOR
                    -%60 orce =     -456
( 1hS)       -%~0
                    -%80 25209   25309       25%09 25509       25609       25709 OLS 25209   25309       25%09 25509       25C09       25709 Tiae in Seconds   25.453                           Y-EXPO     ON 1CS-752:     Average Closing Packing Load, Static Conditions
 
ATlACHMENT E
                                                          'CS4021, Rev2 Page 1 of 1 Ted: 4                                                             Tag: iCS-752 3(23/3i 22'49'i VOTES BEMOR orce = -i3432
                -i5000 (Ih )
                  -20000 5530%       55%0%       5550% 556       5570%       5580%
SMITCH A SMITCH B SMITCH C SMITCH D 5530%       55%0%       5550'} SS6       SP0%       SSS0%
Tiae    im Seconds    55.688                          Y-EKPND ON 1CS-752, Final Thrust Due to Inertia
 
A1TACHMENT F CS-0021, Rev.2 Page 1 of 1 Test'                                                             Tag'C8-752 3/23/3i 22'49'i
                -F0000 V jTES SENSOR orce = -iii3i15000
            )
                .20000 5550%   55%0%       550'f 5560'I       5570%         5580%
SWITCH A SMITCH B SWITCH C SWITCH 9 5530'f 55%0%       550't 5560%         5570'f       5580%
Time in Seconds    55.488                            'Il'-m'll ox 1CS-752, Thrust     At Torque     Switch Trip
 
Attachment G Calc. No. 'CS~1 Revision 2 E DES>~ ~ER3:mumm RzcoR))                          Valve No. 1CS-746 Page  1 of 2 I~~f~ to Verification         Pcrsc&#xc3;%%tl Plant Project                                                       4 g( ] Seismic 4 (Class A)
(Class B)
Fflc  No.                                                    Level                ( ] FP 4 (Class 0)
Oocuncnt No.          C      0  I    Rev                                        ( ] Other Ocsign verification should be done in accordance       ufth ANSI N45,p   I), Scctfon 6, as amended by Regulatory Guide 1.64, Rev. 2.
Special     instructions:
Oisciplinc Project Engineer II.             f Veri Icatf cn Oo~tatf cn Appl f cabf l I ty Ofsci t inc                                             Ofsci    fne Necnanf ca L                 X]                         Civil Structural                     (]
HVAC                                                    Seismic Eaufp. Oual.                 (]
ELectricaL                                                Civil Stress                         (]
fSC                                                      Ff re Protect Ion                     (]
Envirormantai Oual iffcation          (]
Humn Factors                         []
Naterials                            (]
(]
Other                                                                                          []
Verification Nethods       Used:
Oesign Review         ( ] Alternate Calculations           [ ] oualfffcation testing Ocsign Oocunent Acccetable: ~Y Ocsign verifier
                                        ~     No ( ] . ccaaants attached.
oats   '~       V4 Ackncwlcdgcment       okgerfff~tfm+ ~
(OPE)                                                                       oats III. Rcsolutfm     at Ccmmnst Cazeants Resolved (See Attached):
(RE)                                                                         Oate Action taken makes Ocsign Oocusents Acceptable:
Oesign     veriffer                                                           Oats (OPE)                                                                         Oate Proc. 3.3 Rev. 38
 
Attachment G Calc. No. CS4021 Revision 2 Ualve No. 1CS-746 OISCIPLIRE OESICS VERIFIClTIM RSXRO              Page 2 of 2 CA%EST SHEET Plant Pr oieot File   Qo.
Oocmmn     Mo.           ~S&oZl       a   Z This sheet is catv recaired Men coocaents are, bein% nba.
Cccooant                                                                             Resolved Mo                                                                     Resolution lnitfatlOate
                                                                                        ~   V1 ~
                                                                                        ".;ev. >>'0
 
Eeet.osuRa 2


==SUMMARY==
==SUMMARY==
OF EVALUATION FOR SUPPORTS AND PIPE SUPPORT CALCULATIONS FOR REDESIGNED ANCHORS PIPE SUPPORT EVALUATION The Civil Engineering pipe support effort for this modification consisted of the redesign of pipe hanger anchors CS-H-4400, CS-H-4403, and CS-H-4406, as well as the review of 29 other hangers for load changes.The anchors were redesigned due to new anchor locations.
OF EVALUATION FOR SUPPORTS AND PIPE SUPPORT CALCULATIONS FOR REDESIGNED ANCHORS
All support impact resulted from changing the piping model by removing the relief valves, adding flow orifices and adding strainers.
 
The three anchors referred to above were redesigned and new calculations were created.A copy of the calculations are attached.The 29 hanger calculations were reviewed for load changes and the new loads were compared to the loads used in the existing analysis.The load comparison evaluation showed that the minor load changes on all of the 29 hangers were within the design margin of the existing calculations.
PIPE SUPPORT EVALUATION The Civil Engineering pipe support effort for this modification consisted of the redesign of pipe hanger anchors CS-H-4400, CS-H-4403, and CS-H-4406, as well as the review of 29 other hangers for load changes. The anchors were redesigned due to new anchor locations. All support impact resulted from changing the piping model by removing the relief valves, adding flow orifices and adding strainers.
Therefore, these hangers were found to be acceptable without modification.
The three anchors referred to above were redesigned and new calculations were created. A copy of the calculations are attached.
324~cM OTY PART NO.0 STATUS DESCRIPTION 4".~~IV&X O-~"Ir.5A55.TP504~t TOhuII)0CI a: f)iz&vfQV5 Wl&7.ggPW~C%H-~C4j g&/$0-M3 CLc" LOCATION PLAN REFERENCE DOCUMENTS PROI'ESSIONAL ENCIIIEER FI.:fY l2ELhTEU&&ISHIC PIPE DWG'2I--~gE,V, M MECH.DWG.Cr STRESS CALC.-I~SuPPORT CANC.r CAROLINA POWER 8c LIGHT COM ANY NUCLEAR ENGINEERING DEPARTMENT l PLANT: HARRIS NUCLEAR PROJECT-UIIIT I SCALE l l I"'"E: C'4&Iv(ICOSI k~dM&CO~MI lZQ~Og.AUXILI~54~.&..2 2&-~IlaZ.MF PeP<Io g.fg g&lISQIr I%6M I Ie~P8L Rg.&541.I DESCRIPTION wNIDSN~CHK~
The 29 hanger calculations were reviewed for load changes and the new loads were compared   to the loads used in the existing analysis.       The load comparison evaluation showed that the minor load changes on all of the 29 hangers were within the design margin of the existing calculations. Therefore, these hangers were found to be acceptable without modification.
DV DPE DPPE REV DAT A,-8-28&-l-c5.H-REVVED s~T I or 8 SKETCH NO.~W&W f-C l&#x17d;8 I 32i043 g"0 PIPGp 2:Aptp5 rl/G4AQ&lr4Cr PLIM&'OHl PLY!RagaC.~IN&K, o.P.cog",(Ra-,)
 
L I TJF.'4'0 vhHf'am (~)(N2+<~)PROFESSIONAL ENGINEER~h~l2E.~~~IQQIC, CAROLINA POWER 8c LIGHT COMPANY NUCLEAR ENGINEERING DEPARTMENT PIANT: MRIS NUCL842 KbHT'CALE'M IO.2-ff 5fS QADI S~SAT I DATE OESCRIPTION WN OSN CH OV OPE OPPE yg NO/.Q-'gg(jt I.6+-405 RgIA SHT: g Qr'2 qynrp ga 5<&94 I-C-tGe75 S+T.g."r 8 Mod Number~cg-g~yp FR Number Calculation Affected Drawing Affected Reason for Change:@i~~~w<a~esrez~~~zz~g roan+i mo~ra VZ<Z<~<~2 Z rZ STOCK/A'YEjV)cr/'/.
324~
Justification for Change Approval: Minor Change (i.e., editorial, reference dimension, etc.), Calculations are not attached.Supplementary Other (provide basis, attach supplementary calculations) su/<7/7 U7/~/8 ACCT~E'C, EE~V$6 pIdP SEC7/OAJ OFBP7/DS 7+9~7X O'X4 X~cP.DPE*r CI*Signatures indicate design verification has been performed in accordance with NED Procedure 3.3.This form serves as the design verification record.
cM OTY         PART           0                                  DESCRIPTION NO.       STATUS 4".   ~~         IV&X O-~"Ir. 5A55. TP504               ~t TOhuII )
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~"PAR MES.Io-g.tZIIFE4<ggm
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!f6,%I c~.g jl&~~~.&541 CESCRiPTION i i I I QwNlosNICHKI ov jopE loppE PLANT HARRIS NUCLEAR PRO'ECT-UNIT I SCA" E O'0&tv(ICAl k~dM&CDhtTML ga~~Au/IL.I~M~.~.2%C-0~isa@.MF'P'oa<gp A 8'8&.l-CS.H.~RE!r
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                          - ~     gE,V,   M                                   FI.:fY l2ELhTEU &&ISHIC STRESS CALC.       -   I ~                                   CAROLINA POWER 8c LIGHT COM ANY SuPPORT CANC.                r                                NUCLEAR ENGINEERING DEPARTMENT           l PLANT: HARRIS NUCLEAR PROJECT - UIIIT I   SCALE l         l I             "'"E: C'4&Iv(ICOSI     k~dM& CO~MI Io g.fg g&lISQIr I%6M      I lZQ~Og.       AUXILI~54~. &..2 2&-
32444j PROFESSIONAL ENGINEER;GhF~Qa,&Ted 5EtsMic, CAROLINA POWER dc LIGHT COMPANY NUCLEAR ENGINEERING DEPARTMENT PlPNT: kRR6 AU~~KbnlT SCALE: Q~$IIO.2-1Z 259k--yI~AT-565 PtkW I Seemr I DESCRIPTION WN DSNIC" DV DPEIDPPE"'"': CHavi~I$VDL.UH&~rlZOI ca~a-hdXII t~~B.m.&.284-O 9%~4%R,+u~a.T os'Nop).gR-I.A-)-4405 REvgw SI T;2 or'2 SKETCH gp 5'-(at&A 1-C-I~5 S~T.2 or 8 i DE Mod Number~R-4~+7 FR Number Calculation Affected C-CS-8-~D Drawing Affected Reason for Change: SUPP&RE'-ld'r~Zg R PHrrsuu N&J" SZ chz<CWK PU~P Wrml FLouJ PzczRc.57RHxnJE'ustification for Change Approval: Minor Change (i.e., editorial, reference d'mension, etc.).Calculations are not attached.~Other (provide basis, attach supplementary calculations)
Ie~ P8L Rg.&541       .
CdC.c~drzach'C2-Supplementary Pr r DPE**Signatures indicate design verification has been performed in accordance with NED Procedure 3.3.This form serves as the design verification record.
I
CALCULATION NO PAGE t REV/LIST OF EFFECTIVE PAGES PAGE REV PAGE REV PAGE REV ATTACHMENTS NED Guideline E-4 ATTACHMENT D CALCULATION NO~+"~'H-+SO PAGE REV/TABLE OF CONTENTS List of Effective Pages Table of Contents Purpose List of References Body of Calculation Conclusions Page No.Attachments HEo><gwwg8~Q7: 7-Zz-<2 WEo=~pacer Rn 2r.p-Zz-Z-c~@4 Hc-/dp Page(s)gage.g:0 ZW./g/8 Z4.
                                                                        ~IlaZ.          MF PeP<
FORT.1 NO.18055 REV.10I85 Commuted by: Date: CAROLINA POWER&LIGHT COMPANY Calculation ID: c-cz-H-0+oz Checked by: Date: Tar/PID No.: Project Title: CALCULATION SHEET Pg.of Rev.File: Calculation Title: Status: Prelim.Q Final~Void Q PuRpo<E 7o Prov'/kE''4'ArcffoR s ppdg7-784/~Z~~i~-.//~~A oA Pe~~r~us<.)34'+-og<8+Z.wo2:.k'.A5.Sg-g cw7-N.Poop.7-+/~rpwcpo~28/dw 4~4-$88>8=/FZ g p'RR+hC-4')~IScu=/onj///2 PpZ'r/ouc-up//r?8-3-ZZ4-/-C=-h'o=
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                            ~IN&K,       o.P. cog",(Ra-,)
CAROLIHA POWER fi LIGHT COHPANY PLANT HARRIS NUCLEAR PLANT CALCULATION NUMB EII 141-1A PCH/HD NUMBER PCR-6547 PAOE REVISION SUBJECf SI CHARGING PUMP ALTERNATE MINI-FLOW LINE, RELIEF VALVES REMOVED, FLOW ORIFICES AND STRAINERS ADDED WITH LEAD'BLANKETS.
TJF.'
Q~emeu'Leou Vev ('ave.f.eL-N LQL-2 0~a 14'..nornmivnu>s wrrlALs/DATE CHECKER'S INIITALS/DATE
L I 4'0 vhHf'am
~y HANGER NO.CS--4 03 NODE PT.ISO NO>-36-CS-59 SUPPORT SYSTEM CONDITION Fx (LBS)Fy (LBS)Bf.-1 LR L-Z,~Q Fg (LBS)Xx (FT-LBS)&#xc3;y (FT-LBS)Rz (FT-LBS)t4o<L 2 DEADWEIGHT THERMAL I THERMAL II (E)E.Nc.a cue~<I.~5 THERMAL III PAD&TAD Lola 104.(l.ml-~MS Nn-406.-35'ob,~0.-Sn 8 2~Qalh.,uS I=Z,(Dto n1 (Lhasa)-51 I.-7 l.5 l-Z.Z 5h 26.I'I3 PP I-43~(>i:'>Iso DBE SAM OBE(Inertia DBE(Inertia)
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UPSET (+)UPSET (-)EMERGENCY+EMERGENCY(-)
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86.'L3 Q1 138.$05 l 1 ZZ 162.286.ISR 159.H Z'I'I 258.sb 30 Lo IZ.101.92."I I 161.'I4 141.2.2.D Lo 341 45.THERMAL I (NakMAL)THERMAL IZ THERMAL III II>tNT ACCUK&#xc3;l)0.00 DI SPLACEMENTS Y (in)0.00 0.00 LCM<44.0 Pil4l Mc LoaQS'>('u.: 1 SL-l.Q 2u 8-23-%Z,8 W'O'.OK (QV'AL-L Ou Q:31-M 0 Lan.l l&X Ou I LE>K 8 LZ:31o,v.NOTES: l.+X~NORTH,+Y~UP,+2~EAST.2.Sate.5mms C av.XQi,-2 Voc Geo Qz~*v~~, 3~
PROFESSIONAL ENGINEER
FORI>I No, 7d 055 REV, 10/b5 Computed by: Date: CAROLINA POWER 6 LIGHT COMPANY Calculation ID: c-cs-h'-4+0=Checked by: Tar/PID No,: Pro)ect Title: Date: CALCULATION SHEET Pg.of Rev.File: Calculation Title: Status: Prelim.Q Final$f Void~odE U I i+<~PA/A'7 Conz-Q/+'cS WCh'Q~+)+(ia)=//o=++>y(jo).=
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CAROLINA POWER 8c LIGHT COMPANY
FOR'8 NO.78055 REV.10/85 Comnuted bv: Date: CAROLINA POWER 6 LIGHT CO~~Calculation ID: C-CS-h'-++o2 Checked bv: Tar/PID No.: Pro)ect Title: Date: CALCULATION SHEET Pg.of Rev.File: Calculation Title: Status: Prelim.Q Final Q Void TYPE'-z~a.W 8"x/"-n F-6 Zm8.4 8 x/TS4'>cdX 4 P/PC CFEVER o.@1'-2.'(RCi=.Fiwiiiii, o y Y (v/)Z h/ORE ufo<<<cA56 4/(~8'77wc~~')HP.g AC!O<AEK CO~b~z3.3-/8.og (4ooo Psi comas>>)7puu AEooh/ET'o'47+/oo'pEF.
                                                                                            ~IQQIC, NUCLEAR ENGINEERING DEPARTMENT PIANT: MRIS NUCL842     KbHT'CALE'M IO.2-ff 5fS QADI S~   SAT   I DATE       OESCRIPTION     WN OSN CH OV OPE OPPE     yg   NO/.Q-'gg(jt I.6+-405 RgIA SHT: g Qr'2 qynrp ga 5< &94 I-C - tGe75     S+T. g ."r 8
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Mod Number       ~cg- g~yp FR Number Calculation Affected                               Drawing Affected Reason for Change:
)<AC,CO~<gyp F2 Checked by: Date: Tar/PID No.: Project Title: Calculation Title: FOFE II No.78055 REV.10/$5 Commuted.by: Date: CAROLINA POWER 6 LIGHT CP~~CALCULATION SHEET Calculation ID: C'-cs-+~g Pg.of Rev.File: Status: Prelim.Q Final Void Q>~/Pc~T~E-~=ZWZc Ps]c'.r5 (Zd,doc j z)HE'r..rP 77a<g.g Zca5 C~~+Z~7M';f/r7C/ryCrZorv'
    @i~~~     w<a~esrez         ~~~zz ~g           roan   +i   mo~
.78$(/o OR~77A~CH.'A'ZHP.Cg g>2~dL d>b'Eg, 3 E'<V CHECK 4/8 dg, Zp'dwrrtR/-
ra   VZ <Z<~<~       2 Z rZ   STOCK /A'YEjV)cr/'/.
<4 V)Ca<Ca'ag~g~gpp~g-P-234-I-C~-h'-4QY<.ger'g j'd CA'ZC (-C5-+-4+>~PP Q7, CAC.C~FOg.C.-+-<Wd HZE Cdnr~ER y.F~R C c-i:--+~~=CALCU)dr./SJrgdF 7/5 HCC+$739$+
Justification for   Change Approval:
NE035/11 DATE 92.09.25 PAGE 1 1~1 1~1~1 1~1 1 1 1~1~1~1 1~~~~~1*~1 1 1~1 1 t 1 PROJECT JOB NO.CALC NO.4-CS'-ff-4+0~SNT NO.CALC ID'TtACHMENT" F-OF PREPARED BY*DATE CHECKED BY DATE 1**1111****
Minor Change (i.e., editorial, reference dimension, etc.), Supplementary Calculations are not attached.
~1~11~1111~1**~11~~~~1 1 t~1111~~c~se>f F~E 4 3c"W.EEEEEEEEE EE E EE EEEE EE EE E EEEEEEEEE 0000000 00 00 00 00 00 00 00 00 00 00 0000000 33333333 33 33 3333333 33 33 33333333 55555555 55.55 55555555 55 55 55555555 VERS ION LEASED AUGUST 1989 SER NANUAL VERSION 8 THEORETICAL NAKUAL VERSION: 8 VER I F I CAT ION NANUAL VERS I ON: 10 1~~~1~1 1 1~1~1*1~1 1~1 1 1 1 1 1~1 1 1~1~*IN CASE OF PROBLEHS MITH NE035, CONTACT THE~BASEPLATE USER REPRESENTATIVES
Other (provide basis, attach supplementary calculations) su/ <7 /7 U7/ ~       /8 ACCT ~E'C,           EE~V$ 6 pIdP         SEC7/OAJ         OFBP7/DS       7+9~ 7X O'X4 X ~cP.
*LOCATION EXTENSION 1~11~~~~11~1~11~~*~1~~1~1*1~~~1111 1 1 1~1 1~1 1~1~~~1~1~~1 1 1 1 1 1~1 1 1~~1~COPYRIGHT 1984,1987 BECHTEL POMER CORP.ALL RIGHTS RESERVED.~~1 1 1 1~1 1~1~1 1 1~1*1 1 1~1 1 1 1 1 1 1~~1 1 1 1~1~1 1 1 HE035/11 DATE 92 09 25 PAaE 2 tIOPt404tt 0~0~%1tlltO+yyyygy~OtlttOtOOOtlt1ttlt001P PREPROCESSOR lNPUT DATA CARDS 111I110ltltOttt1tlltttttt11WtfO~lt011fttttlttlt1111*liteeeltttt1ttfll0001tototll CARD 1 2--3 4 5 6 7 8 NO 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 23 24 25 26 27 28 29 30 31 1)CASE 1 CS.H.4403 3 FlLEKAHE>HHPBP24 TYPE F-2 EHBED PLATE (BX SIT g~g 1/COH~g g@4000/PLA 6,11~gd,30/1/29/
DPE*
BPR~, 1,d,dE5,1.25E6,5987,3473/
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BOL 3,2,1,1.5,3/
  *Signatures indicate design verification has been performed in accordance with NED Procedure 3.3. This form serves as the design verification record.
BOL 3y6g 1~1~5~15/BOt.3,10,1,1.5,27/
 
BOL 5,2,1,6.5,3/
334943 4I   ~ v   ~
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  = -"- ."w"                 -  po    QE.v. 2k
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PLANT      HARRIS NUCLEAR PRO'ECT - UNIT I   SCA" E i    i I
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32444j PROFESSIONAL ENGINEER; GhF~       Qa,&Ted 5EtsMic, CAROLINA POWER dc LIGHT COMPANY NUCLEAR ENGINEERING DEPARTMENT PlPNT: kRR6 AU~~ KbnlT           SCALE: Q~
                                                    "'"': CHavi~I        $ VDL.UH& ~rlZOI
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--yI ~AT-        DESCRIPTION WN DSNIC" DV DPEIDPPE os'Nop ).gR -I.A-)-4405     REvgw SI T; 2 or'2 SKETCH gp 5'-(at&A 1-C   -I~5     S~T. 2 or 8
 
i                                   DE Mod Number     ~R-4~+7 FR Number Calculation Affected         C-CS-8   - ~D                       Drawing Affected Reason for Change:
SUPP&       RE '   - ld'r~Zg   R PHrrsuu N&J " SZ                       chz<CWK PU~P Wrml FLouJ PzczRc.
57RHxnJE'ustification for Change   Approval:
Minor Change   (i.e., editorial,   reference d'mension, etc.).             Supplementary
  ~      Calculations are not attached.
Other (provide basis, attach supplementary calculations)
CdC.c ~   drzach'C2-DPE*
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  *Signatures indicate design verification has been performed in accordance with NED Procedure 3.3. This form serves as the design verification record.
 
CALCULATION NO PAGE   t REV   /
LIST OF EFFECTIVE PAGES PAGE REV     PAGE     REV     PAGE     REV ATTACHMENTS
 
NED Guideline E-4 ATTACHMENT D CALCULATION NO ~ +" ~ 'H- +SO PAGE REV     /
TABLE OF CONTENTS Page No.
List of Effective   Pages Table of Contents Purpose List of References Body of Calculation Conclusions Attachments                                                    Page(s)
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FORT.1 NO. 18055   REV. 10I85 Commuted     by:         Date:                                         Calculation ID:
CAROLINA POWER & LIGHT COMPANY       c-cz-H- 0+oz Checked by:             Date:
Pg. of                Rev.
CALCULATION SHEET Tar /PID No.:                                                         File:
Project
 
==Title:==
Calculation
 
==Title:==
Status:       Prelim. Q     Final ~     Void Q PuRpo <E 7o Prov'/kE''4'ArcffoR s ppdg7
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CAROLIHA POWER fi LIGHT COHPANY PLANT                                                                                                   CALCULATIONNUMBEII HARRIS NUCLEAR PLANT                                                                                           141-1A PCH/HD NUMBER                                                                                           PAOE            REVISION PCR-6547 SUBJECf                                                                                               nornmivnu>s wrrlALs/DATE SI     CHARGING PUMP ALTERNATE MINI-FLOW                                   LINE, RELIEF CHECKER'S INIITALS/DATE VALVES REMOVED, FLOW ORIFICES AND STRAINERS ADDED WITH LEAD 'BLANKETS.                                                                                                   ~
y Q~emeu         'Leou Vev             ('ave. f.eL-N LQL-2 0~a                       14'..
HANGER     NO.CS- -4 03                       NODE     PT.                       ISO   NO>     - 36-CS-59 SUPPORT Bf.- 1         LR L-Z,
                                            ~   Q SYSTEM CONDITION                  Fx                Fy                Fg                 Xx                 &#xc3;y                   Rz (LBS)            (LBS)              (LBS)              (FT-LBS)         (FT-LBS)               (FT-LBS)
Nn                  8 51 DEADWEIGHT                                -406.                   2~                -7                    l. I.
26.
THERMAL     I      Lola 104.             -35                                  5l          -Z.Z 5h                  I'I3            PP I
                                                                                                                                      -43  ~
t4o<L 2 THERMAL      II (E)
                      <I. ~5 THERMAL III E.Nc.a cue~
l.ml-~MS          0.- Sn
                                                          'ob,~
(                                Qalh.,uS  I =Z,(Dto n1 (Lhasa)-                                 ( > i:'>Iso PAD & TAD DBE SAM OBE(Inertia                 86.
l1            ZZ              ISR sb              30  Lo            IZ. Lo            341 162.                159.                101.                  92.                  45.
DBE(Inertia)
                              'L3 138.
Q1                        H            Z'I'I "I I         'I4 286.              258.                161.               141.
UPSET    (+)            $ 05 UPSET    (-)                                                                                            2.2. D EMERGENCY +
EMERGENCY(-)
DISPLACEMENTS                            LCM<44.0 Pil4l Mc LoaQS'>
Y
('u.: 1 SL- l.Q 2u 8-23-%Z,8 W'O'.OK
( QV'AL-L Ou Q:31-M 0 (in)                              Lan.l   l&X Ou       I LE> K8      LZ:31o,v.
THERMAL (NakMAL)
I          0.00              0.00                0.00 THERMAL      IZ THERMAL      III II>tNT ACCUK&#xc3;l)
NOTES:     l. +X ~ NORTH, +Y ~ UP, +2 ~ EAST.
: 2. Sate. 5mms         C av. XQi,-2 Voc Geo Qz~*v~~,
3~
 
FORI>I No, 7d 055   REV, 10/b5 Computed by:             Date:                                               Calculation ID:
CAROLINA POWER   6 LIGHT COMPANY           c-cs-   h'- 4+0 =
Checked by:               Date:                                                      of          Rev.
Pg.
CALCULATION SHEET Tar /PID No,:                                                               File:
Pro)ect
 
==Title:==
Calculation
 
==Title:==
Status:         Prelim. Q       Final $ f   Void
      ~odE U                                                                             i I
                                                              +<~PA/A'7 Conz - Q /
                                    +'cS WCh'Q
                                                                            ~   +)+(ia) //o=
                                                                                            =
                                                                            ++>y(jo).= z< z
                                                                            + 3os(/a) i- Z2+(/o)
Pr. A'x=                 ay=
                                                            +x=
4y=
                  >HTfo         r Z4. Z. Fu>   SPICA'7 C,o/hd Fz:                                           3/oso/> >>
                                                                              - /.gc c o<<8'+//s   dzcaosE w/ o Reredos             'o~. 2     ) I. '3 gyCZ~7 /)         +'Hi(g M-c'//v'oR EF'FZC7;               Ai +     +E'     /,
                      ~AC/ EB. 4         ~Egg ~ ro 9E <PZ<KEQ.
 
FOR'8 NO. 78055   REV. 10/85 Comnuted bv:           Date:                                             Calculation ID:
CAROLINA POWER 6 LIGHT CO~~           C-CS- h'- ++o2 Checked bv:             Date:                                            Pg.      of      Rev.
CALCULATION SHEET Tar /PID No.:                                                             File:
Pro)ect
 
==Title:==
Calculation
 
==Title:==
Status:       Prelim. Q       Final Q   Void TYPE'-z                                     F-6
                                    ~a. W 8"x/"
n Zm8. 4 8 x/
TS4'>cdX 4 CFEVER P/PC o.@1'-   2.'(RCi=. Fiwiiiii, o y Y             h/ORE (v/)     Z ufo <<<
cA56 4 /   (~     8'77wc~   ~')
HP. g                                     (4ooo Psi comas>> )
AC!O<AEK CO~b~                   7puu AEooh/     ET'o'47+/oo'pEF.         3 )
                                                        / Z.S" 5 " p~c/n/4 RE'gc/c7/0%
n pe~sr. erne RCZI<7>>4>
z3.3- /8.og                  (Z.5" 7o PEVO7: WOE'okuOVIO<i       )
            <AC,CO~
            <gyp F2
 
FOFE II No. 78055   REV. 10/$ 5 Date:                                              Calculation ID:
Commuted.
Checked by:
by:
Date:
CAROLINA POWER   6 LIGHT CP~~         C'-cs-+ ~g Pg. of       Rev.
CALCULATION SHEET Tar/PID No.:                                                                File:
Project
 
==Title:==
Calculation
 
==Title:==
Status:        Prelim. Q      Final         Void Q
                                >~/Pc   ~T~E -~ = ZWZc Ps] c'. r5 HE'r.. rP 77a<g.       g     Zca5 C~
(Zd,doc
                                                                        ~ +Z j z)
                                ~7M'; f/r7C/ryCrZorv'         . 78$ ( /o   OR
                                          ~77A~CH.     'A'ZHP.       Cg g > 2
              ~dL d>b'Eg, 3 E'< V CHECK                   4/8 dg, Zp'dwrrtR/- <4 V) Ca<Ca'ag ~g~gpp ~ g- P-234-I - C ~-h'- 4QY<.
ger'g j'd       CA'ZC       (- C5- +- 4+> ~PP Q7, CAC.C~ FOg. C. -+- <Wd HZE Cdnr~ER y. F~R C c-i:-- +~~=
CALCU )dr./             SJrgdF   7   /5 HCC+$ 739$ +
 
JOB  NO.
CALC NO.
PREPARED BY 4-CS'-      ff-4+0~
NE035/11 1 ~ 1 1 ~ 1 ~ 1 1 ~ 1 1 1 1 ~ 1 ~ 1 ~ 1 1 ~ ~ ~ ~ ~ 1 PROJECT DATE SNT NO.
CHECKED BY DATE 92.09.25
                                                                            ~ 1 1 1 ~ 1 1 DATE PAGE t1 1
1 CALC FID'TtACHMENT" OF
**1111**** 1          ~   ~ 11 ~ 1111     ~ 1** ~ 11     ~ ~ ~ ~ 1 1   t ~ 1111   ~ ~
c~se > f F~E 4 3c "W.
EEEEEEEEE         0000000        33333333          55555555 EE     E       00     00               33        55 .
EE              00     00               33        55 EEEE            00     00       3333333          55555555 EE              00     00               33              55 EE      E        00     00               33              55 EEEEEEEEE          0000000         33333333         55555555 VERS ION LEASED                                                     AUGUST   1989 SER NANUAL               VERSION                             8 THEORETICAL NAKUAL VERSION:                                     8 VER     I F I CAT     ION NANUAL VERS                 I ON:     10 1 ~ ~ ~ 1 ~ 1 1 1 ~ 1 ~ 1     *1   ~ 1 1 ~ 1 1 1 1 1 1 ~ 1 1 1 ~ 1 ~
* IN CASE OF PROBLEHS MITH NE035, CONTACT THE
  ~ BASEPLATE USER REPRESENTATIVES LOCATION EXTENSION 1
  ~ 11   ~ ~ ~ ~ 11   ~ 1 ~ 11   ~ ~ *~   1 ~ ~ 1 ~ 1*1 ~   ~ ~   1111 1 1 1 ~ 1 1 ~ 1 1 ~ 1 ~ ~ ~ 1 ~ 1 ~ ~ 1 1 1 1 1 1 ~ 1 1 1 ~ ~ 1 ~
COPYRIGHT 1984,1987   BECHTEL POMER CORP. ALL RIGHTS RESERVED.
~ ~ 1 1 1 1 ~ 1 1 ~ 1 ~ 1     1 1 ~ 1   *1 1 1 ~ 1 1 1 1 1 1 1 ~ ~ 1 1 1 1 ~ 1 ~ 1 1 1
 
HE035/11                       DATE 92 09 25 PAaE   2 tIOPt404tt                           ~0~%1tlltO+yyyygy~OtlttOtOOOtlt1ttlt001P 0                                      PREPROCESSOR   lNPUT DATA CARDS 111I110ltltOttt1tlltttttt11WtfO~lt011fttttlttlt1111*liteeeltttt1ttfll0001tototll CARD NO 1             2       -3         4         5         6 12345678901234567890123456789012345678901234567890123456789012345678901234567890 7     8 1 3 FlLEKAHE>HHPBP24 TYPE F-2 EHBED PLATE (BX1) CASE           1 CS.H.4403 2 SIT   g ~ g 1/
3  COH ~ g g @4000/
4  PLA 6,11 ~ gd,30/1/29/
5  BPR   ~, 1,d,dE5,1.25E6,5987,3473/
6  BOL 3,2,1,1.5,3/
7  BOL 3y6g     1 ~ 1 ~ 5 ~ 15/
8  BOt. 3,10,1,1.5,27/
9  BOL 5,2,1,6.5,3/
10  BOL 5/6/1,6.5,15/
11  BOL 5,10,1,6.5,27/
12  END/
13  ATT 4,63.5,15/
14  JST 4,6,3,2,180/
15  JST 3,6,2,1 ~ 180/
16  1ST 2,6,7,3/90/
17  JST 2,7,3     '/0/
18  JST 3/7/4/2,0/
19  JST 4,7,5,3,0/
T 5,7,5,6,270/
T 5,7,5,6,270/
T 5,5,4,3,180/
T 5,5,4,3,180/
ST 4,5,3,2, 180/JST 3,5,2,1~180/1ST 2,5,6,3,90/
ST 4,5,3,2, 180/
END/END/POl 4,6/LOA1,550,-794,990,19120,-31056, 12512/LOA2,-550,794,990,-19120,31056,-12512/EKD/EHD OF JOB*~END OF lNPUT DATA~
23  JST 3,5,2,1 180/ ~
I%035/11 DATE 92-09-25 PAGE 3>>>>tt>>~>>>>t>>t>>t>>>>>>>>ttt>>tttt>>>>t>>>>ttttttttt>>
24  1ST 2,5,6,3,90/
PREPROCESSOR INPUT DATA CARDS~>>tttttttttt>>tttt>>>>t>>ttt>>>>>>>>>>>>>>>>1>>>>tt>>>>>>ttt>>ttltttttttttttttttt>>ttttttttttttttttttttt CARD 1 2-4 5 6 7 8 NO 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 3 F ILENANE>>HKPBP24 2 OJT 0>>0 3 CON 0 0 4 PLA 6>>11 5 BPR 0>>0 6 BOL 3>>2 7 BOL 3>>6 8 BOL 3>>10 9 BOL 5>>2 10 BOL 5>>6 11 BOL 5>>10 12 END 13 ATT 4>>6 14 JST 4>>6 15 JST 3>>6 16 1ST 2 6 17 JST 2>>7 18 JST 3>>7 JST 4>>7 T 5>>7 5>>JST 4>>5 23 JST 3>>5 24 IST 2 5 25 END 26 END 27 POI 4>>6 28 LOA 0 0 29 LOA 0 0 30 END 31 END OF JOB TTPE F-2 EHBED PLATE (8X1)CASE 1 0>>1 0 0 0.000 4000.000 0.000 0 8.000 30.000 1.MO 1>>.880E+06>>.125E+07.599E+04>>1>>1.500 3.000 0.000>>1>>1.500 15.000 0.000>>1>>1.500 27.000 0.000>>1>>6.500 3.000 0.000>>1*6.500>>15.000>>0.000>>1>>6.500 27.000 0.000 CS.H.4403 0.000 29.000.347E+04>>0.000 0.000>>0.000 0.000>>p pppt 0.000>>0.000 0+000 0.0 0.000>>O.OM>>0.000 0.0M>>0.000 0.000 0.000 0.000 0.0 0.000 0.000 0.0M 0.000 0.000 0.000 3>>2 r 3>>4>>5>>5>>4>>3>>2 6>>3.500 2.000 1.MD>>3.0M>>1.000 2.MP>>3.MO 6.000>>3.000>>2.000 1.000>>3.000*15.000 180.M0>>180.000 90.000 0.000 0.000 0.000 270.000 180.000>>180.000 180.000 90.000 0.000 0.000 0.000 0.000 0.0M 0.000 0 000>>0 000>>0.000>>0.000>>0.000.0.000>>0.000 0 0.000 0.000 1>>550.0-794.0 2>>.550.0>>794.0>>~END Of INPUT DATA DECK~0.000 0.000 0.000 990.0 19120.0.31056.0 12512.0 990.0-19120.0 31056.0-12512.0  
25  END/
26  END/
27  POl 4,6/
28  LOA  1,550, -794,990,19120, -31056,         12512/
29  LOA  2, -550,794,990,         -19120,31056, -12512/
30  EKD/
31  EHD OF JOB
                                  *~ END OF lNPUT DATA   ~
 
I%035/11                           DATE 92-09-25   PAGE     3
        >>>>tt>>                                             ~ >>>>t>>t>>t>>>>>>>>ttt>>tttt>>>>t>>>>ttttttttt>>
PREPROCESSOR   INPUT DATA CARDS
~ >>tttttttttt>>tttt>>>>t>>ttt>>>>>>>>>>>>>>>>1>>>>tt>>>>>>ttt>>ttltttttttttttttttt>>ttttttttttttttttttttt CARD NO 1         2                     4           5         6 12345678901234567890123456789012345678901234567890123456789012345678901234567890 7         8 1 3 F ILENANE>>HKPBP24 TTPE F-2   EHBED PLATE   (8X1)   CASE 1 CS.H.4403 2  OJT        0>>  0    0>>   1     0 3  CON        0   0   0      0.000   4000.000       0.000      0.000      0.000    0.000 4  PLA        6>>  11    0       8.000     30.000       1.MO       29.000      0+000    0.000 5  BPR        0>>  0    1>> .880E+06>>   .125E+07   .599E+04>> .347E+04>>          0.0        0.0 6  BOL        3>>  2    1>>     1.500       3.000       0.000>>      0.000      0.000>>    0.000 7  BOL        3>>   6    1>>     1.500     15.000       0.000>>      0.000>>    O.OM>>    0.000 8  BOL        3>> 10    1>>     1.500     27.000       0.000>>      0.000      0.000     0.0M 9  BOL        5>>   2    1>>     6.500       3.000       0.000>>      0.000>>    0.0M>>    0.000 10  BOL        5>>   6    1*     6.500>>     15.000>>     0.000>>     p pppt    0.000    0.000 11  BOL        5>>  10    1>>     6.500     27.000       0.000       0.000>>     0.000     0.000 12  END 13  ATT        4>>   6            3.500      15.000      0.000       0.000 14  JST        4>>   6    3>>     2.000   180.M0>>        0.000 3>>
15 16 17 JST 1ST JST 2
2>>
6 6
7 r
2 3>>
1.MD>>
3.0M>>
1.000 180.000 90.000 0.000 0.000 0.000 0.0M 18  JST        3>>  7    4>>      2.MP>>      0.000       0.000 JST        4>>  7    5>>     3.MO        0.000      0 000>>
T        5>>   7    5>>     6.000>>   270.000        0 000>>
5>>       4>>     3.000>>   180.000>>       0.000>>
JST        4>>   5    3>>     2.000   180.000        0.000>>
23  JST        3>>  5    2      1.000>>   180.000       0.000.
24  IST        2    5    6>>     3.000*    90.000       0.000>>
25  END 26  END 27  POI        4>>  6    0      0.000       0.000       0.000       0.000      0.000 28  LOA        0   0   1>>     550.0     -794.0       990.0     19120.0   .31056.0   12512.0 29  LOA        0   0   2>>   .550.0>>       794.0>>     990.0   -19120.0   31056.0 -12512.0 30  END 31  END OF JOB
                                    ~    END  Of INPUT DATA    DECK  ~


NE 035/11 DATE 92-09-25 PAGE 4 ttttttttttttttttttttttttttttttttttttttlttttttttttttttttttttttttttttttttttttttt FlLENANEtHNPBP24 TTPE F-2 ENBED PLATE (8X1)CASE 1 CS H.4403 ttttttttttttttttttttttttt1tttttttt1tttttttttt11tttttt1*ttt11tttttttttttt11ttttttttttt 1NPUT PARANETERS PLATE THlCKNESS......~..PLATE X DlllENSlON
NE 035/11                            DATE  92-09-25 PAGE 4 ttttttttttttttttttttttttttttttttttttttlttttttttttttttttttttttttttttttttttttttt FlLENANEtHNPBP24 TTPE      F-2    ENBED PLATE  (8X1)  CASE 1 CS  H.4403 ttttttttttttttttttttttttt1tttttttt1tttttttttt11tttttt1*ttt11tttttttttttt11ttttttttttt 1NPUT PARANETERS PLATE THlCKNESS    ...... .. ~        1.000 PLATE X DlllENSlON    ~~ ~ ~ ~~ ~    8.000 Y-DlNENSlON      ..            30.000 NODULUS OF    ELASTlClTY            .290E+08
~~~~~~~Y-DlNENSlON
                                        ~ ~
..NODULUS OF ELASTlClTY
CONCRETE NODULUS    ..            .360E+07 CONC. C(WP. STRENGTH        ~ ~ ~ ~  4000.0 BOLT LOCATlONS BOLT  l    J  NODE      X.COORD.        Y.COORD.
~~CONCRETE NODULUS.." CONC.C(WP.STRENGTH~~~~1.000 8.000 30.000.290E+08.360E+07 4000.0 BOLT LOCATlONS BOLT l J NODE X.COORD.Y.COORD.1 3 2 2 3 6 3 310 4 5 2 5 5 6 6 510 24 1.500 3.000 28 1.SOO 1S.OOO 32 1.500 27.000 46 6.500 3.000 50 6.500 15.000 54 6.500 27.000 BOLT PROPERTIES BOLT STIFFNESS (
1  3    2    24          1.500        3.000 2  3    6    28          1.SOO        1S.OOO 3  310        32          1.500        27.000 4  5    2    46          6.500          3.000 5  5    6    50          6.500        15.000 6  510        54          6.500        27.000 BOLT PROPERTIES BOLT      STIFFNESS  (LB/lN.)              ALLOMABLE FORCE    (LB)
TENS lON        SHEAR              TEN SlON      SHEAR
                  .MOE+06      .125E+07                    5987.        3473.
                  .BME+06      .125E+07                    5987.        3473.
                  .8ME+06      .125E+07                    5987.        3473.
                  .880E+06      .125E+07                    5987.        3473.
                  .880E+06      .125&07                    5987.        3473.
                  .880E+06      .125 E+07                  5987.        3473.
 
NE 035/11              DATE 92 09 25 PAGE  5
  ) ttttttttttttttttttttt'tt*tt''t'ttttttttttttttttttttttttttttttttttttttttttttfttftf    t t      FILENANEtHNPBP24 TYPE F-2 ENBED PLATE (8X1) CASE          1 CS H 4403 ttttttt1ttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttt1ttttttttttttttt NON STANDARD ATTACHHENT DATA ATTACHNENT NLNBER                  1 SEGHENT NIWBER            ...                    1 TYPE  ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~                JST HE I 0HT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~              0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~                  2.000 ORIENTATION ANGLE                            180.0 THICKNESS        ~ ~ .~.~~~                  0.000 SEGNENT NWBER              ...                    2 TYPE  ~~~~ ~ ~ ~ ~ ~ ~ ~ ~~                  . JST HEIGHT    ~~~ ~ ~ ~ ~ ~ ~ ~~                0.000 D I STANCE    ~ ~ ~ ~ ~ ~ ~ ~ ~            1.000 ORIENTATION ANGLE                            180.0 THICKNESS        ~ ~ ~ ~ ~ ~ ~ ~            0.000 SEGHENT NIWBER            ...                    3 TYPE  ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~                    IST HEIGHI'      ~~ ~ ~ ~ ~ ~ ~ ~~              0.000 DISTANCE      ~ ~ ~ ~ ~ ~ ~ ~ ~            3.000 ORIENTATION ANGLE                              90.0 THICKNESS        ~ ~ ~ ~ ~ ~ ~ ~            0.000 SEGHENT NUHBER            ...                    4 TYPE  ~ ~ ~ ~ ~ ~
4,2,2,6,180/
4,2,2,6,180/
2 ST 2,3,4,2.5,90/
2    ST 2,3,4,2.5,90/
23 EHD/24 END/25 POI 3,4/26 LOA1,383,-721,1062,25436,-34867,18309/
23  EHD/
27 LOA2,-383,721,1062,-25436
24  END/
25  POI 3,4/
26  LOA    1,383,-721,1062,25436,-34867,18309/
27  LOA  2,-383,721,1062,-25436,34867,.18309/
28  EHD/
29  EHD OF JOB
                            ~~* END OF  INPUT DATA ~~*
 
HE 035/11                        DATE 92-09-25  PAGE    3
          ~ )))))))t)>>>>t)))>>>>t>>))>>>>>>>>)))>>)))>>)))>>))t)>>>>)))>>))))1))))))))))t))>>>>))))))))))
                                                                                                  )
PREPROCESSOR      INPUT DATA CARDS I))))))*>>)))))))))))))1))*)1*)))>>)))1))))))))))))I)))))>>))))))
3~
3~
FORM t40.7$0SS REV.10/4$ComPuted by: Date: 9 is.5>Check@~b~-'ate: P-zw-yz.IPID No'ro)ect Title: Calculation Title: CAROLINA POWER&LIGHT CO~ANY CALCULATION SHEET Calculation ID: Pg.of Pile: Rev.Status1 PrelimFinal Q Void Q To8Z Z.rcpt C CRc/k F~=25.$4s/&a~/3/=///5 JZ g/4, 5'y 3 Ps./O4C C C/f 7//ff g~TO FAC//-/7/q 7 E Cafe~/h/g CO<</~~)Hu>COwM<i~ZN.2 Al864JAZdc T5 CO/0L>S TQ SWq4'4'c57 5'/pg/.5, P4//4X'~rg)
+E//arE/-OPF 44}$pp~cyg AuaO/08dc5 tc'/0)PRf 5r.8855=ll Oft/ssf (RCRtBO//O/
rroW Ig 4t4X4)f/=44>5f/1 d<ks/c's Zws/fc~-,$(std).-Zj g/o=W z)"-5 Ssks ((Acr 4).Kf.-,4/44)'l8,4
/772+/5/g 25/on Z t.'z vr)i PC Z./C//)/I'0 0+/, fur.-oRcrfofJ
=-o (~>=,53</0/8.4+(~f 4)J 5.5.fosrm rfz G4'.zo4l(rrs~~fj)red C0 n484'Z S 44-y=~Q PS/~/Ob r r~--F4'.2/S/e/ZSr-"'(WhX.FA///.kg 7"c fof)<(z,/C/g3-co s.r~=/7 8 CfloCK@.p Sc/I.gQ fC/Pg NR//SMcss=1 Pks/<I4.5 ks/2,zo I~pc/4=2'VS Ps/(9 7/:s/dl~Zo.7F=/7.Z P5'/Fg=.g pp.2)=/4.5'y~,4(zg.2).-5''Z 9~/Zie 2 oO ck.IforroRorfoof fo,5" g.44)7d Frf////7AT4-" CP/C CK/4 (g LdWb/Ncj/4plQ 84.2 4<l.owwa//5 fy o4'o Ks l (cof s&'f.F'o R S441 ofofo@PC)
ChectR~by: Tar/PID No.: Date: f 27~Pro)ect Title: Calculation Title: FORM No.100SS REV.10/SS Computed by: Date: C1"-i 9 25 9g CAROLINA POWER&LIGHT CO~ANT CALCULATION SHEET Calculation ID: c-cs-4-e~Pg.of Rev.File: Status: Prel3sa Q Final Q Void Q EC 8 O'Mz/F/CA T/o Q 4" P]0/PZ To/'Ac'pi>4T>
~CCK/A C ZdAbS<~~/4 Zf./5'c'~p/)Wx=SOO+Fy=&SCAN/~i~/I-+Mg=//240/F)y.ZZ700 P1g=/8arC)CcZE~A.4 Lor44$E'Q,P Aggytgisqggz I Au-I4.l h'g lg.Z~q" JQ tl kin>l~/'~'~~0')<WXt Z.Z>)7/.C (0'bo<q]4'fg~g~~//zclo (g.gg-)g-~//f)V/9,/Fx (w~zi We,z)~g 78-/AV~5/J>ca+(Zzyoo y I$'d3o)4.t~/5,=(4z t 4 2)~=(op v/7og~)~/'gc 6<i~/968~in<~-Pd/sss~70'7 P/8oo o)+da 4 IQ~~c.~~~6,>tE/n Iu T~II FORM No.70055 REV.10/05 Computed by: Date: Checked lgr:.r/PID No.: Pro]ect Title: Calculation Title: CAROLINA POWER&LIGHT C~ANT CALCULATION SHEET Calculation ID: PS.of Pile: Rev.Status: PrelifII.~Final Q Void Q QEI 0 AEc.K Ll&B Lc>mDs c 5UPM+<['wR 7T<r1 g C Jr,>2, denim iz)4 WI-Ie,<I Ig g P~e re.A xg I 748 HiLL.dPU4I-IF-/
~LL QgE,g~JQ~~Jg W/dc~rMeo 4 I><=I&+5+I7$O x g'g'<Lo P ac mr q,r~P.m.g Az=IS n FORM NO.74055 REV.10/$5 Computed by: Che~'-<bw:.Tar f PID No.: Prospect Title: Date: W 5SR1.Date:-Z~P CAROLINA POWER 6 LIGBZ COMPANY CALCULATION SHEET Calculation ID: Pg.of File: Rev.Calculation Title: Status: Prelim~Final Q Void Q I get c'I~w~l 4 k,gI.cTkcW UBQ5 AQS bk c'o~f~s~d A,L40W a gg I/I br=9"'4y"~e)'(>57+leel+~os)Roe7'in e~c.woe.*tuuJ>>e>J=~~~'0 l ((8 ee(g)6 IN It&, Zf.4, (fYlI pj.I)0%XTE~LGd P5 Z~F.MTcool F h.~4LLow Abbe&Sx=IISo Wy=I211 Pg=Iu%b thy.)2>co gy r I=4+go Z2.bg,~zs tL-t 4g vp+()~~&2l ZS-5(-7 4)Tate(c)'o e4l I 5/PF O~~iTK gVQ eaO~S/II 9+<<~Z~e Z>5-5 5 f-II'C l)+TED~2-~-24 (gee,~'C)&Ac<(6)=ZS S-0 lf Il 9 jM RGP~(LOA'05 Q<Ttl E Q,2 ALL~P SU&j,g pL'-r<~nseee A<<ok.+~E~~e~404+I e"A&a JPJTct<CTIy A CQ,=~954 o~4k-T/PK,~+TeIF'~~
FORM NO.7$055 REV.10/$5 Computed by'T Checked I~-'r/PID No.: Prospect Title: Date: lt Date: 9-2.7 P CAROLINA POWER ItT LIGHT COMPANY CALCULATTON SHEET Calculation ID: Pg,(of File.'ev.Calculation Title: Status: PreliIIr,+Final Q Void Q~T.B NIZ 3T.lZ~<ZTZ~f Ft~e S,Z.Z fx-i&&5 Fy=l185 pp y fAx"-lo7<a fYlz-%oh')M~>o Err.~runt, RE.'I As-P vice LocAq lo<RcF.Al'T.A;YXLT.='.O5 (Z)25 T5~'%l Xz.FZWI.55IXX~ox)X gx)iS SXW,~Z5~'Z.S.z.t (')WB,F'.W~ga K a~A O~.O>S/II z zx Tzzx vz.~o s.zg (IRF g ATY.Tx)~Sou.'+>>TZ~'(41 ('1 I'5 EQ.N I.oyzT0's Q)T<p'Q.Q AI.t ovyz RTL<S SVkiSS AuF'C (dO457 CD5i IQT~~C fi0<=,759<I.0 0 e FL vpj, sz z~K (XTXTXI (IXuAT TTE5O<'[IXM5 g<Qb pc%5HcWc.50i 70 KD6E, T)IST,'O P~PPPy0a-gCP RTf.F 0g.RC-'QAI-I y5'(OUT.
FORM No.70055 REV.10/$5 ComPuted by: Date:~"-ala Checked bg:.Date:-~Y'-',~-s~r/PlD No.: Project Title: Calculation Title: CAROLINA POWER 6 LIGHT COMPANY CAL'CULATION SHEET Calculation ID: Pg.of File: Reve Status: Prelim~Final Q Void Q sw XpMe 7 lo 7 R+~'7 X&-l LA.lo-8.~&" x'3z so-d'z L~~.W TF~7 I 5 cog a caTc 0 To w4.4X4 o~o~c.s>oc, a I kcF.6k, F0R.5obl+b~~I-
>+-<X lr O~THa OTgce.Fo NO gl4u iCIC~T~cMDI&g U>t I.~RE P ACE~T~1 IO)5 Mwwc,c7cD To 7'5, 4X4 (mi~.)0~yuE S I Dc Q 4 f C4'4>>)dw THc.6THiR., SA5 Q OQ THc~AH H KR.tM 4d I+ICH: THc PLA fC IS 5'7I P'Fg~cD I P>f AT'Te CH C7, Mi=.Mt3cR.S gglt.RQIDmO IJCLDS vsEO)HO SIAM>G>C>
NT BWMCg Q)t g'TA k5.K>Cc ITEM+7 (co c IC',~~we<(~J 4f>x~oJ F C l2P 5TRUDL 5x~o c'lg~P.OZZ 4 FORM NQ.$0071 REV.I/00 R/PW/PHP NO.OWNG.NO.CPhL-HPES CALCULATION SHEET 0 REV.BY:, DATE:~+5 CHK:DATE:~/~i~~SUBJECT'4HL'V>>ATTACHMENT
" 0 0 0 GT1CES 3.38 92/N/24.N.36.35.PAGE 1~t;ALC lf)'TrACHMENT" PNIE OF tttttttttttttt1tttttttt1tttt1tt1tttttttttttttttttttttttt1ttttttttttttttt1111ttltttltt GEORGlA lNSTlTUTE OF TECQOLOGY lNTEGRATED COMPUTER ENGlKEERlNG STSTEN GTl CES 3.38 GEORGlA TECN PRQ%lETARY PRUCT GENERATED 88/02/16.15.25.46 DATE~92/N/24.
GTICES 3o3$'2J09/24.09.36.3$.PAGE 2 NPUT~L~PUT>>PL~>>~>>SF 4 PD 8>>LT$8,S1SDATA,OA,NC,~P.
~~~~~~~~~~'CALC NO NNP PCR 6547>>S>>PROJOPCR6$
47>>>>PILSAR~.N.4400>>
~ttlltttttOIOIOIOOOIIOOOtl~tttt
**Ill tll Ill OOIOO t 11 11 GTSTRUOL~1*tltttllttl
~litt tO tt It Ill I I tttttttt OIIIIO OIOIOI 1111 tt 11 11 OIOIIO It I~11 Otlllllttt 11 11 Ot tt 11 11 11 11 IIIIOIIOII I ttt1 tt I OIOOII 11 tt 11 11 11 11 11111**11 11 11 11 I tt tt tl lt 11 tttllt IOOOIO OOIOIO~11111 11 11 tt ttlt 11111 IttltO~QNED SY AND PROPRIETARY TO TNE GEORGIA TECN RESEARCN CNIPORAT I ON RELEASE DATE HARCK 1988 VERSlON 8701 CDC NM LEVEL 0 CCNPLET I ON NO.2180 jbs~ttttttttttttttttttttttttttttttttttttttt 1111 ACTiVE UNITS-LENGTN tttl ASS%ED TO SE INCH lKIGNT ANGLE TENPERATURE Tile PtRJle RAD I AN FAHRENHEIT SECOND TYP SPA UNIT IN JOI COO 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15'6 NEN INC 1127 778;FRA LSS DEG'i 00.00 00.00 00.00-6.00.6.00 00.00 9.375 9.375 9.375 00.00 00.00 00.00 00.00 00.00 2.875 10.00 00.00'00.00 00.00 00.00 00.00 14.375 14.375 17.375 20.37$20.375 27.00 27.N S 26.375 26.375 26.375 26.375 00.00 12.00 20.80 20.M 24.00 12.00 12.00 12.00 12.00 12.00 12.00 00.00 12.00 18.00 18.00 18.00 223;334;445;$
26;667 8 8 9;9 9 10 7 10 6 10;11 10 13 g 12 11 12 CALC NO HNP-PCR-6547 11 I 14 13 14 I 15'l4'15 I 16 1$'l6 GT I CES 3.3B 92/09/24.09.36.36.PAGE 3 1'TUSESO<<TS6X6X4' 14 T<TlaaaO>>TS4X4X4>
5 10 11 12 13 T'TISE80<<TS5X5X4'6 T iAISCPIPEi
>P4.00XS<NEN PRa PRIS 4 6 TO 9 15 AX 10 AY 10 AZ-10-IX 100 1Y 100 IZ 100 SY'100 SZ 100 CONSTANTS E 29+OOE6 ALL G 11.15E6 ALL OEN 0.203 ALL QVT 0.0 NEH 4 6 TO 9 15 BETA 0 ALL POI 0.300 ALL S STEEL ccccccccccccccccccccccccccccccccccccc>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>
ACT 1VE LNITS ikIGNT LS LENGTH INCll c TOTAL LENGTH, lklGHT Ale VOLQK FOR SPECIFED HEHBERS c LENGTN>1.0975E+02 RIGHT>1.0462E+02 VOL SE~6.7795E+02 cccccccccccccccccccccccccccccccccc>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>
PLOT DEVICE PRINTER LEN 6 PLOT PLANE XY THRV 1


CAI.C N NP-PCE-4547 TCE PRLIITEE LQI 4 YZ TIRU 1 CT I CE$3.3$%/N/24.09.36.38.PACE 5 CALC NO NNP.PCR 6547 GT I CES 3+38 92/09/24.09.36.39.PAGE 6 T I(NI;Y T t N(aIZONTAL
FORM t40. 7$ 0SS          REV. 10/4$
ComPuted by:                    Date:                                                          Calculation ID:
9  is.5>          CAROLINA POWER & LIGHT CO~ANY Check@~      b~-'ate:      P-zw-yz.                                                          Pg.      of            Rev.
CALCULATION SHEET IPID No                                                                                    Pile:
 
==Title:==
'ro)ect Calculation
 
==Title:==
Status1              Prelim            Final Q        Void    Q To8Z    Z.rcpt C      CRc /    k TO FAC//-/7/q 7 E        Cafe~/h/g CO<</~~) Hu> COwM<i              ~      ZN. 2 Al864JAZdc T5 CO/0L>S TQ SWq4'4'c57 5'/pg /. 5, P4//4X'~rg)
                                            +  E//arE/-OPF 44}$ pp~cyg                                    AuaO/08dc5 tc'/0)
PRf      5r.8855 =    ll  Oft /ssf (RCRtBO//O/ rroW            Ig  4t4X4)            f/    = 44 >5f
                                  /772
                                      /1 d<ks/
                                          + /5/g c's 25/onZws/                                            fc~ -,$ (std).-    Zj g
                                                                            "-  5 Ssks
                        /o  =                      W                                    ( (Acr  4)        .Kf .-,4/44)'l8,4 fur.-oRcrfofJ        =    /I'0 Z t.'z o
vr)iz    )
( /8.4 ~ +> =,53      < /0
(~f 4) 0+
PC F~      =
Z.
                                                                                                                          /,
                                                                                                                            /C//)
25.$ 4s/
                            &a~/3/=///5 JZ g /4,            5'y 3 Ps. /O4C C C/f 7//ff g
T 2,3,4,2.5,90/
T 2,3,4,2.5,90/
/END/23 POl 3,4/24 LOA1,913,-1355,1788,30537,9486,10763/
        /
25 END/26 END OF J08 t END OF 1NPUT DATA~  
END/
%035/11 DATE 92 09.24 PACE 3 ttttt>>>>tttttttt>>tttt>>tttttt>>ttt>>>>
23 POl 3,4/
PREPROCESQS INPVT DATA CARDS ttt>>t1*ttttttt t>>tttt>>1111*11111>>ttttttttttttttt>>
24 LOA  1,913,-1355,1788,30537,9486,10763/
CARO 1 2=---3 4 5 6 7 8 No 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 3 FILE 2 OJT 3 CQI 4 PLA 5 BPR 6 BOL 7 BOL 8 BOL 9 BOL 10 ENO 11 ATT 12 JST 13 IST 14 IST 15 JST 16 I ST 17 IST 18 1ST 1 T NAKE>>KNPBP28 0 0 0 0 6>>7 0 0 2 2 2 5 5>>2 5'>>5 31 4 3>>4 4 2 5 6 4 6 4 5 4>>4 4 2 3 1 0 0.000 10.000 1>>.880E+06>>1>>2.000 1>>2.000 1>>8.000 11 8,000 4.500 2.500 5 1+750>>6>>.75O 41 5.000 5>>.7501 4*1.750>>3>>2.500 5.000>>4>>2,500 3000.000 10.000.125 E+071 2.000 8.000 2+000 8.000 6.250 180.000 90.000 90.000 0.000 270.000 270.000 270.000 180.000 90.000 0.000 1~000>>.602E+04>>0.000 0.000 0.000 0.000 0.000>>0.000 0.0001 0,000 0.000 0.000 O.OOO>>0.000 0.000 0.000>>0,000 29.000.521 E+04'.000 0.000 0.000 0.000 0.000 0.000 0.000 0.0 0.000 0,000 0.000 0.000 0.000 0.000 0.0 0.000 0.000 0.000 0.000 3*4 0 0 22 END 23 Pol 24 LOA 25 END 26 END OF JOB 0 0.000 0.000 0.000 0.000 0.000 1>>913.0.1355.0 1788.0 30537.01 9486.0 10763.0~ENO OF INPUT DATA DECK~
25 END/
NE 035/11 DATE 92-09-24 PAGE 4~ttttttttttttttttttttttttttttttttttt F ILENA%tHHPQP28 t tttttttet tttttttttttttttttttttttttttttttttt INPUT PARAHETERS PLATE THICKNESS~~~~~~~~PLATE X-DIHENSION
26 END OF     J08 t   END OF 1NPUT DATA ~
.......Y OIHENSION......NCOULUS OF ELASTICITY
 
...CONCRETE INmULUS~~~~~~~~CONC.CSP.STRENGTH o." 1.000 10.000 10.MO~290E+08.312E+07 3000.0 BOLT LOCATIONS BOLT I J NME X-COORD., Y-COORD.1 2 2 9 2.000 2.000 2 2 5 12 2.000 8.000 3 5 2 30 8.000 2.000 4 5 5 33 8.000 8.000 BOLT PROPERTIES BOLT STIFFNESS<LB/IN.)ALLOIABLE FORCE (LB)TENSION SHEAR TENSION SHEAR 1 2 3.880E+06.880E+06.880E+06.880E+06.125E+07.125E+07.125E+07.125E+07 6020.6020.6020.6020.5210.5210.5210.5210.
                                  %035/11                           DATE 92 09.24 PACE     3 ttttt>>>>tttttttt>>tttt>>tttttt>>ttt>>>>
I%035/11 DATE 92 09-24 PAQK 5 tttttttttttttttttttttttttttttttttttt F ILENA%iHNPSP28 t*ttt tt tttt ttttttlttttttttttttttttttttttttttttt ISN.STANDARD ATTACHHENT DATA ATTACHHENT IRNSER 1 SEGHENT NOBER~~~~~~~~~TYPE~~~~~~~~~~~~~~~~~~~HEIGHT~~~~~~~o~~~~~~~~~D I STANCE~~~~~~~~~~~~~~~ORIENTATION ANGLE."".THICOESS~o~~o~~~~~~~~~1 JST 0.000 2.500 180e0 0.000 SKQNKNT NQIER~~~~~~~~~TYPE~~~~~~~~~~~~~~~~~~~HEIGHT~~~~~~~~~~~~~~~~~D I STANCE~~~~~~~~~~~~~~~ORIENTATION ANGLE..o" THINESS~~~~~~~~~~~~~~2 IST 0.000 1.750 90.0 0.000 SEGNENT NSER~~~~~~~~~TYPE~~~~~~~~~~~~~~~~~~~HEIGHT~~~e~~~~~~~~~~~~~DISTANCE~~~~~~~~~~~~~~~ORIENTATION ANGLE~~~~~~THICOESS~~~~~~~o~~~~~~3 IST 0.000.750 90.0 0,000 SEQNENT NNSER~~~~~~~~~TYPE~~~~~~~~~~~~~~~~~~~HEIGHT~~~~~~~~~~~~~~~~~DISTANCE~~~~~~~~~~~~~~~OR!ENTATION ANGLE.".~THICOESS~~~~~~~~~~~~~~4 JST 0.000 5.000 0.0 0,000 SEGHENT IRNSER~~~~oooo~TYPE~~~~~~~o~ooo~~~~~~~HEIGHT~~~~~oooooee~oooo DISTANCE~~eeo~~ooo~~~~~ORIENTATION ANGLE THICOESS~~~~~ooo~~~o~e 5 IST 0.000.750 270.0 0.000 I%035/11 DATE 92 09-24 PACK 6~ttttt 1 1 1 1 1 1 1 11 1 1 1 1 t tt 1 t t t 1 ttt tt t ttt t 1 1 t t 1~P ILENA%tHNPSP25 1 1 ttt1ttttttktt1111 ttttttttttttttttttttttttttttttttttttttttttttt NON STANDARD ATTACHNENT DATA SKGNKNT NQSER"....." TYPE~~~~~~~~~~~~~~~~o~~HEIGHT~~~~~~~~~~~~~~~~~DISTANCE~~~~~~~~~~~~~~~ORIENTATION ANGLE..TNINESS~~~~~~~~~~oo~~6 IST 0.000 1.750 270.0 0 000 SKINT NSER~~~~~~~~~TYPE~~~~~~~~~~~~~~~~~~~HEIGHT~~~~~~~~~~~~~~~~~DISTANCE~~~~~~~~~~~~~~~ORIENTATION ANGLE."...THINESS~~~~~~~~~~~~~~7 IST 0.000 2.500 270.0 0.000 SKGHKNT NQSER~~~~~~~~~TYPE~~~~~~~o~~~~~~~~~~~NKIGHT~~~~~~~~~~~~~o~~~DISTANCE~~~~~~~~~~~~~~~ORIENTATION ANGLE....THINESS~~~~~~~~~~~~~~8 JST 0.000 5.000 1SO.O 0.000 SECANT NLSOER~~~~~~~~~TYPE~~~~~~~~~~~~~~~~~~~HEIGHT~~~~~~~~~~o~~~~~~DISTANCE~~~~~~~~~~~~~~~ORIENTATION ANGLE."...THICQIESS~~~~~~~~~~~~~~9 IST 0.000 2.500 90.0 0.000 NE 035/11 DATE 92 09 24 PAGEF lLENANE<NNPBP28 y*~y~~yyyyiiilOPOPteltll11*OIOOtOtlOtttlOO
PREPROCESQS     INPVT DATA CARDS ttt>>t1*ttttttt                                           t>>tttt>>1111*11111>>ttttttttttttttt>>
~PIIIIOIOIIPIOI
CARO           1         2 =--     -3         4           5             6       7         8 No 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 3 FILENAKE>>KNPBP28 2 OJT       0    0          1      0 3 CQI       0    0            0.000  3000.000      0.000      0,000      0.000    0.000 4 PLA     6>>    7         10.000      10.000    1 ~ 000>>   29.000      0.000    0.000 5 BPR      0     0   1>> .880E+06>> .125 E+071 .602E+04>> .521 E+04'.000 0.0       0.0 6 BOL      2     2   1>>     2.000      2.000    0.000                  0.000   0.000 7 BOL      2    5    1>>     2.000       8.000    0.000       0.000       0,000   0.000 8 BOL      5>>   2    1>>     8.000      2+000    0.000       0.000      0.000    0.000 9 BOL      5'>>   5    11      8,000      8.000     0.000      0.000      0.000   0.000 10  ENO 11  ATT      31    4            4.500      6.250     0.000>>      0.000 12  JST      3>>    4            2.500    180.000     0.000 13  IST            4    5      1+750>>    90.000     0.0001 14  IST      2    5    6>>       .75O    90.000     0,000 15  JST            6    41      5.000       0.000     0.000 16  I ST    4    6    5>>      .7501  270.000     0.000 17  IST      4    5    4*      1.750>>  270.000     O.OOO>>
~&Ottt101111&OIPP14100111111110fii101t LOADlNG CONDlTlONS LQADlNG CASE NO.~1 LOADlNGS APPLIED AT NODE~43 FORCE FX>913.00 FORCE FY~-1355.00 FORCE F2~1788.00 NOIENT NX~30537.00 NINENT NY~9486.00 lKNENT NZ~10763.00 NE035/1'1 DATE 92-09-24 PACE 8 11I I ttttttlttt ttttlttltllttttltl*lltltlllttttttt F l LENA%I HNPQP28 I Itltllltttltttt
18  1ST      4>>    4    3>>      2.500    270.000     0.000 1      T    4                  5.000>>   180.000      0.000 2    3    4>>      2,500    90.000     0.000>>
~tttttttttttttttttlttttttttttttttttttttttttt BASEPLATE CONNECT lVl TY ELENENT NO.CIE JA JS JC JD ELEKENT SSE NO.JA JB JC JD 1 1 8 9 2 3 3 10 11 4 5 5 12 13 6 2 2 9 10 3 4 4 11 12 5 6 6 13 14 7 7 8 15 16 9 9 10 17 18 11 11 12 19 20 13 8 9 16 17 10 10 11 18 19 12 12 13 20 21 14 13 15 22 23 16 15 17 24 25 1d 17 19 26 27 20 14 16 23 24 17 16 1d 25 26 19 18 20 27 28 21 19 22~a 27 31 29 33 29 30 23 31.32 25 33 34 27 36 37 30 38 39 32 40 41 34 20 23 30 31 24 22 25 32 33 26 24 27 34 35 28 26 30 37 38 31 28 32 39 40 33 30 34 41 42 35 NE 035/11 DATE 92-09-24 PAGE 9 ititiieiii t F ILENANEtHNPSP28 t~titttttttttt*tttttttt
22  END 23  Pol      3*    4    0      0.000       0.000     0.000       0.000       0.000 24  LOA      0     0   1>>      913.0   .1355.0     1788.0     30537.01    9486.0 10763.0 25 END 26 END OF JOB
~tttttttttttttttttttttttttttttttttttttttttttttt ttttt*ttttttttttttt*ttttttititttit*tttt**tt*ttt lNSAL COOS I NATES I J FRANK LINE LINE INSE IKSE X Y 2 COORDINATE COORD I NATE COORDINATE 1 1 1 1 1 1 1 2 2 2 2 2 2 2 3 3 3 3 3 3 3 4 4 4 4 4 5 5 5 5 5 5 5 6 6 6 6 1 2 3 4 5 6 7 1 2 3 4 5 6 7 1 2 3 5 6 7 1 2 3 5 6 7 1 2 3 4 5 6 7 1 2 3 4 1 2 3 4 5 6 7 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 26 27 28 29 30 31 32 33 34 35 36 37 38 39 0.000 0.000 0.000 0.000 0.000 0.000 0.000 2.000 2.000 2.000 2.000 2.000 2.000 2.000 4.500 4.500 4.500 4.500 4.500 4.500 4.500 7.000 7.000 7.000 7 000 7.000 7.000 7.000 d.000 d.000 d.000 8.000 8.000 8.000 8.000 10.000 10.000 10.000 10.000 D.DDD 2.000 3.750 6.250 8.000 8.750 10.000 0.000 2.000 3.750 6.250 8.000 8.750 10.000 0.000 2.000 3.750 6.250 8.000 8.750 10.000 0.000 2.000 3.750 6.250 d.000 8.750 10.000 0.000 2.000 3.750 6.250 8.000 8.750 10.000 0.000 2.000 3.750 6.250 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 I%035/11 OATE 92-09-24 PACE 10 t tttt t ttttttt tt t t t t t t t t t t 1 t ttt 1 t t t t t F TLEXA%tNNPSP28
                                  ~   ENO OF INPUT DATA DECK   ~
*ttttttttttttttttttttttttttttttttttttttttttt11ttttttttttttt1tttttttttttttt11tttttttttt INSAL CXRD I NATES l J FRAIS INBE X Y 2 L 1NE L lKE NME COOS l NATE COORD l NATE COOROl NATE 6 5 40 6 6 41 6 7 42 INSES AT APPLlCATlON OF LOADS 3 4(OFFSET)43 4.500 6.250.500 10.000 8.000 0.000 10.000 8.750 0.000 10.000 10.000 0.000 m 035/11 DATE 92-09-24 PACK 11 MOO*~yrtOOot4tOt1t11000t10tttOW1 f ILENA%<NNPSP28
 
~t0110lttlttltOtt~tt&
NE 035/11                         DATE 92-09-24 PAGE   4
&ttOI1**1111t1tiltt1111114ttt11tOOtttttt1tt CONCRETE STIFFNESS DATA INSE EF FECT IVE CONCRETE AREA STIFFNESS INSE KFFECT I VE CONCRETE AREA STIFFNESS 1 3 5 7 9 11 13 15 17 19 21 23 31 33 35 37 39 41 1.000 2.125 1.250.625 4.219.4.78'I 2.250 2.500 5.312 3.125 1.562 3.281 3.719 1.750 1.500 3.187 1.875.937 1.875 2.125 1.000.336E+06.714E+06.420E+06.21 DE+06.142E+07.161E+07.756E+06.840E+06.179K+07.105E+07.525E+06.110K+07.125K+07.588K+06.504E+06.107E+07.630E+06.315K+06.630K+06.714E+06.336E+06 2 1.875 4 2.125 6 1.000 8 2.250 10 4.781 12 2.812 14 1.406 16 4.687 1d 5.312 20 2.500 22 1.750 24 3.719 26 2.1d7 28 1.094 30 2.812 32 3.187 34 1.500 36 1.000 38 2.125 40 1.250 42.625.630E+06.714E+06.336E+06.756E+06.161E+07.946E+06.473K+06.158E+07.179E+07.840E+06.5ME+06.125E+07.735E+06.368E+06.946Ei06.107E+07.504E+06.336E+06.714E+06.420E+06.210E+06 SLNIATION Of EFFECTIVE AREAS~100.000 PLATE AREA~100.000 TOTAL CONCRETE STIFFNESS~.336E+08~INPIIT DATA PROCESSINQ CCHPLETE.~
                                                            ~ ttttttttttttttttttttttttttttttttttt F ILENA%tHHPQP28 t
I%035/11 P PLOT PLAN VIEN Of TME BASEPLATE'WE DATE 92 N.24 PACE THE X AXIS (CONSTANT J LINES)ARE IKNI?OITAL, AMD THE Y AXIS (CONSTANT I LINES)ARE VERTICAL.NJJJJJJJJJJJJJNJJJJJJJJJJJJ 4444JJKJJJJJJJJJJJJJJJJJJNJJJJJJJMJJJJJJJJJJJJJJN I I I I I I I I I I I I I I I I I I I I I I NJJJJJJJJJJJJJ JJJJJJJNJJJJJJJJJJJJJJM I A I A I I I A I A I I I A I A 8 I NJJJJJJJJJJJJJAJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJAJJJJJJSBBJJJJJJJJJJJJJM I A I A 8 I I A I A I I I A I A I I I A I A I I I A I A I I I A A I I A I A I I I A I A I I NJJJJJJJJJJJJ JJJJJJJJJJJJJJJJJAJJJJJJJNJJJJJJJJJJJJJJN I A I A I I I A I A I I I A A I I I A I A I I I A A I I I A I A I I I A I A I I I A I A I I I A I A I I I A I A I I I A I A I I NJJJJJJJJJJJJJ JJJJJJJMJJJJJJJJJJJJJJN I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I 8 I I 8 I NJJJJJJJJJJJJSSSJJJJJJJJJJJJJJJJJJMJJJJJJJJJJJJJJJJJJMJJJJJJBSSJJJJJJJJJJJJJM I 8 I I 8 I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I NJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJNJJJJJJJNJJJJJJJJJJJJJJM PROGRAN: NE035 SASEPLATE SNQI: S9601 0110 AAII 7081 RELEASE 11 NOS/VE 1.5.3 L765 DATE: 92.09-24 TINE: 12:34)25 PAGE: 13 1111111111111111
tttttttet                                                     tttttttttttttttttttttttttttttttttt INPUT PARAHETERS PLATE THICKNESS ~ ~ ~ ~   ~ ~~~       1.000 PLATE X-DIHENSION   .......         10.000 Y OIHENSION   ......           10.MO NCOULUS OF ELASTICITY       ...   ~ 290E+08 CONCRETE INmULUS   ~ ~ ~ ~ ~ ~ ~ ~ .312E+07 CONC. CSP. STRENGTH     o."       3000.0 BOLT LOCATIONS BOLT I J NME           X-COORD., Y-COORD.
~E 0 I N S 0 L U T I 0 N P N A S E L 0 A 0 C A S E N 0:~~~ttttttttttttttttttttttttttttt1111tt TITLE: FILENANEtHMPSP28 LOAD CASE NO.(TOP TEN VALUES)0 I S P L A C E N E N T S NME 7 14 6 21 13 5 28 35 12 20 0ISPL..60'l470E.02
1   2   2     9           2.000         2.000 2   2   5   12           2.000         8.000 3   5   2   30           8.000         2.000 4   5   5   33           8.000         8.000 BOLT PROPERTIES BOLT     STIFFNESS   <LB/IN.)             ALLOIABLE FORCE (LB)
.557485E.02
TENSION           SHEAR             TENSION       SHEAR 1     .880E+06     .125E+07                    6020.      5210.
.509943E.02
2    .880E+06     .125E+07                   6020.       5210.
.501649E.02
3    .880E+06    .125E+07                   6020.       5210.
.466271Ee02
                  .880E+06    .125E+07                    6020.       5210.
.454994Eo02
 
~445364E-02
I%035/11                     DATE 92 09-24   PAQK   5 tttttttttttttttttttttttttttttttttttt F ILENA%iHNPSP28 t*ttttttttt                                                        ttttttlttttttttttttttttttttttttttttt ISN. STANDARD           ATTACHHENT DATA ATTACHHENT IRNSER                   1 SEGHENT NOBER             ~ ~~ ~~ ~ ~ ~ ~         1 TYPE   ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~   JST HEIGHT     ~ ~ ~ ~ ~ ~ ~ o~~~   ~ ~ ~ ~ ~~ 0.000 D I STANCE     ~~~~~~~ ~ ~ ~ ~~ ~~ ~         2.500 ORIENTATION ANGLE               ."".       180e0 THICOESS         ~o~~o~~ ~~ ~~ ~~ ~         0.000 SKQNKNT     NQIER         ~~~~~~~~ ~             2 TYPE   ~~ ~~~~~~~~~~~~ ~~~~~                   IST HEIGHT     ~~~~~~~ ~ ~~~~~ ~ ~ ~~           0.000 D I STANCE     ~~~~~~ ~~~ ~ ~ ~~~~           1.750 ORIENTATION ANGLE               ..o"         90.0 THINESS         ~~~~~~ ~ ~ ~ ~ ~~ ~ ~       0.000 SEGNENT     NSER         ~~ ~ ~ ~ ~~ ~ ~       3 TYPE   ~ ~ ~ ~ ~ ~~~~~~~~~~~~~~                 IST HEIGHT ~ ~ ~ e ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~     0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~         .750 ORIENTATION ANGLE ~ ~ ~ ~ ~ ~                 90.0 THICOESS         ~~~~~~~o~ ~~~~~             0,000 SEQNENT NNSER             ~~ ~ ~ ~ ~ ~~~         4 TYPE   ~~ ~~~ ~ ~ ~~~~~ ~~ ~~ ~~~               JST HEIGHT     ~~ ~~~ ~ ~~~~~~~ ~~ ~ ~           0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~       5.000 OR!ENTATION ANGLE               .".       ~   0.0 THICOESS         ~ ~ ~ ~ ~ ~ ~~~~~~~~       0,000 SEGHENT IRNSER             ~~~~   oooo   ~     5 TYPE   ~~~~~~~o~         ooo   ~~~~~~~         IST HEIGHT ~ ~ ~ ~ ~ oooooee ~ oooo             0.000 DISTANCE ~ ~ eeo ~ ~ ooo ~ ~ ~ ~ ~           .750 ORIENTATION ANGLE                           270.0 THICOESS ~ ~ ~ ~ ~ ooo ~ ~ ~ o ~ e           0.000
.416473E-02
 
.411625E.02
I%035/11                                     DATE 92 09-24   PACK     6
.410428E.02 NtIE 22 15 23 30 29 37 36 8 16 1 0 ISPL~-.643703E 03 e.637019E.03 e.621235E 03-.617772E.03
                                                              ~ ttttt1 11 1 1 1 1 11 1 1 1 1 ttt1 ttt1 tttttttttt1 1 tt1
-.587693E.03
~        P ILENA%tHNPSP25 11 ttt1ttttttktt1111                                     ttttttttttttttttttttttttttttttttttttttttttttt NON STANDARD ATTACHNENT DATA SKGNKNT NQSER           "....."               6 TYPE ~ ~ ~ ~ ~~~~~~~~~~~~o~~                 IST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~   0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~     1.750 ORIENTATION ANGLE               ..         270.0 TNINESS         ~~~ ~~ ~~~~ ~     oo   ~~ 0 000 SKINT NSER               ~ ~ ~~~ ~ ~ ~ ~         7 TYPE ~ ~~~~~~~~ ~~~~~~~~~~                   IST HEIGHT   ~ ~ ~ ~ ~ ~~ ~~ ~ ~ ~~~~ ~ ~     0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~     2.500 ORIENTATION ANGLE             ."...       270.0 THINESS         ~~~~~~~ ~~ ~~ ~ ~ ~       0.000 SKGHKNT NQSER           ~~ ~~~ ~~ ~~           8 TYPE ~~~ ~ ~~~o~~~~~~ ~~~ ~~                 JST NKIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ o ~ ~ ~   0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~     5.000 ORIENTATION ANGLE             ....       1SO.O THINESS         ~~~~ ~~ ~~~ ~ ~ ~ ~~       0.000 SECANT NLSOER           ~~ ~~ ~~ ~~ ~           9 TYPE ~~~~~~ ~ ~~ ~ ~~ ~~~ ~ ~ ~ ~           IST HEIGHT   ~~~~~ ~~~ ~ ~o~~ ~~ ~ ~           0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~     2.500 ORIENTATION ANGLE             ."...       90.0 THICQIESS     ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000
-.526119E-03
 
-.474248E.03 e.441528E 03 e.320971E.03 e.218181E 03 QUADR I LATERAL PLATE PRINCIPAL STRESSES ELENENTS+Z FACE ELEN SIGNA ELEN SIGNA ELEN SIGNA ELEN SIGNA 20.5840.2 e 2977.24 1687.14 5409.23 1986.22 1555.8.4144.13 e 1973.26 e 3632.27 e 1963 ELENENTS 2 FACE ELEN SIGNA ELEN SIGNA ELEN SIGNA ELEN SIGNA ee oooo ooo 20 5998.14 S369.26 3725.8 3655.2 2464.27 2092.13 1858.23 o 1694.24 e 1548.7 1533.CONCRETE LOADS NtOE ZoPRESS SSE 2 PRESS NRE ZePRESS INOE Z.PRESS 22 e 216.1S-214.23 e 208.29 e197.37 e177.36 e 159.16.108.38 e73.30 e208.8 e 148.
NE 035/11                   DATE 92 09 24 PAGE y*~y~~yyyyiiilOPOPteltll11*OIOOtOtlOtttlOO F lLENANE<NNPBP28
PROGRAN!NESS SASEPLATE SIRRII S9601 0110 AAN 7081 DATE: 92-09 24 RELEASE 11 NOS/VE 1.5.3 L765 T INE: 12:34 46 PAGE: 14 a 0 L T LOADS N(HIE X SHEAR T SHEAR SRSS TENSlON 9 12 30 33 654.-199.652.-194.-761.1004.-792, 817.91.658.102.219.96.3622.0.2372.80LT INTERACT lON EOUAT lON EGUATlONt((TENSlON/TALL(N)tt 1.000+(SHEAR/SALLOI)tt 1.000))tt 1.000 IKCE TENS lON SHEAR TENS lON ALL(HI AL LCM RATIO SHEAR RATIO INTERACT RAT10 SAFETY FACTOR 9 6020.5210..016 12 6020.5210..602 30 6020.5210..001 33 6020.5210..394.193.157.126.042.209.759.127.436 4.795 1.318 7.853 2.293~ttttttttkttttttttttttttttttttttttttttttttttt END LOAD CASE ttttttttttttttttttttttttttttttttttttttttttttt
~ PIIIIOIOIIPIOI                           ~&Ottt101111&OIPP14100111111110fii101t LOADlNG CONDlTlONS LQADlNG CASE NO. ~     1 LOADlNGS APPLIED AT NODE ~   43 FORCE FX >     913.00 FORCE FY ~   -1355.00 FORCE F2 ~     1788.00 NOIENT NX ~   30537.00 NINENT NY ~     9486.00 lKNENT NZ ~   10763.00
~tttttttttttttttttttt*tttt**tt**tt*tttttttttt
 
*END POSTPROCESS l NG 11***tttttttttt*t*t*tt*tttt*tttt*t*tttttttttt Pile f CP!tL uNn f G93 CALC ID TTACHMENT NED ZNTERDZSCZPLZNE REVIEW REQUEST (ZRR)Tos Froms j ZRR fs~>/RET/ggggPCN Ps'nit/Subunit.t/Subunit, Plant~~Details of Review Requests REFERENCE-PCR-6547, DELETION OP RELIEF VALVES AND ADDITION OP ORIPZCES AND STRAINERS~ATTACHED ARE THE SIGNED OFF SUPPORT LOAD SHEETS POR PCR-6547 AS WE KNOW IT AS OP 12s00 P.M.ON SEPTEMBER 25, 1992~PLEASE USE THESE LOADS IN YOUR SUPPORT DESIGNS AND EVALUATIONS FOR THE ABOVE MENTIONED PCR.THESE, LOADS ARE AS GOOD AS THE INFORMATION USED TO DEVELOP THEM SINCE NO APPROVED DRAWINGS HAVE BEEN RECEIVED AS OP THIS WRITING+IP THERE ARE ANY QUESTIONS PLEASE CONTACT JOHN HOPKINS AT X-6734~sponse Required Bys Authorised Man-hours MAPS Project No.s-7 Responsible Supervisor/Data Charge Number Phases Activity: Response/Justifications Attachments (liat)s Responsible Supervisor/Date Actual Man-hours expended Distributions NED Guideline No.E-24 Revision 4 (EO6d/rlj}}
NE035/1'1                       DATE 92-09-24 PACE 8 11I I ttttttlttt                               ttttlttltllttttltl*lltltlllttttttt F l LENA%IHNPQP28 I
Itltllltttltttt                           ~ tttttttttttttttttlttttttttttttttttttttttttt BASEPLATE CONNECT lVlTY ELENENT             CIE                      ELEKENT          SSE NO.         JA   JS   JC     JD           NO.     JA     JB   JC JD 1       1     8     9     2               2    2      9    10    3 3       3    10   11     4               4    4    11    12    5 5       5    12   13     6               6     6     13   14   7 7       8   15   16     9              8    9     16    17  10 9     10   17   18     11             10    11     18    19  12 11      12    19   20     13             12     13     20   21   14 13     15   22   23     16             14    16    23    24  17 15      17   24   25     1d             16    1d    25    26  19 17     19   26   27     20             18     20     27   28 21 19     22   29   30     23             20    23    30    31  24 31 . 32     25             22    25    32    33  26
            ~a 33   34     27             24    27    34   35 28 36    37    30            26     30     37   38 31 27    31     38    39    32            28     32     39   40 33 29    33    40    41    34            30     34     41   42 35
 
NE 035/11                       DATE 92-09-24 PAGE 9 ititiieiii                     ~ tttttttttttttttttttttttttttttttttttttttttttttt t
F ILENANEtHNPSP28 t
~ titttttttttt*tttttttt                 ttttt*ttttttttttttt*ttttttititttit*tttt**tt*ttt lNSAL COOS I NATES I   J   FRANK   IKSE       X           Y           2 LINE  LINE    INSE        COORDINATE   COORD I NATE COORDINATE 1     1             1       0.000      D.DDD        0.000 1     2           2         0.000      2.000        0.000 1    3           3         0.000      3.750        0.000 1    4           4         0.000      6.250        0.000 1    5           5         0.000      8.000        0.000 1    6           6         0.000      8.750        0.000 1     7            7         0.000      10.000        0.000 2    1                     2.000      0.000        0.000 2     2           9        2.000      2.000        0.000 2     3           10        2.000      3.750        0.000 2    4           11        2.000      6.250        0.000 2    5           12         2.000       8.000       0.000 2    6          13        2.000       8.750        0.000 2    7          14        2.000     10.000       0.000 3    1          15        4.500      0.000       0.000 3    2           16        4.500      2.000       0.000 3    3          17        4.500       3.750        0.000 3                18        4.500       6.250        0.000 3    5          19        4.500       8.000       0.000 3    6          20        4.500      8.750        0.000 3    7           21        4.500      10.000        0.000 4    1          22        7.000       0.000       0.000 4    2          23        7.000       2.000       0.000 4    3          24        7.000       3.750        0.000 7 000      6.250        0.000 4    5          26        7.000       d.000       0.000 4    6          27        7.000       8.750        0.000 7          28        7.000     10.000       0.000 5    1          29        d.000       0.000        0.000 5    2          30        d.000       2.000       0.000 5    3          31        d.000       3.750       0.000 5    4          32        8.000      6.250       0.000 5    5          33        8.000       8.000       0.000 5    6          34        8.000       8.750       0.000 5    7          35        8.000      10.000       0.000 6    1          36        10.000       0.000       0.000 6    2           37        10.000       2.000       0.000 6    3          38        10.000       3.750        0.000 6    4          39        10.000       6.250        0.000
 
I%035/11                        OATE  92-09-24    PACE  10 ttttttttttttttttttttt t ttt1 tttt1 ttttt F TLEXA%tNNPSP28 ttttttttttttttttttttttttttttttttttttttttttt11ttttttttttttt1tttttttttttttt11tttttttttt INSAL  CXRD  I NATES l    J  FRAIS  INBE      X            Y          2 L 1NE L lKE  NME          COOS l NATE        l COORD NATE  COOROl NATE 6    5          40      10.000         8.000       0.000 6    6          41      10.000         8.750      0.000 6    7          42      10.000       10.000       0.000 INSES AT APPLlCATlON OF LOADS 3    4(OFFSET)  43        4.500        6.250        .500
 
m 035/11                        DATE  92-09-24 PACK 11 MOO*~yrtOOot4tOt1t11000t10tttOW1 fILENA%<NNPSP28
~ t0110lttlttltOtt~tt&                        &ttOI1**1111t1tiltt1111114ttt11tOOtttttt1tt CONCRETE STIFFNESS DATA INSE  EF FECT IVE    CONCRETE          INSE  KFFECT I VE  CONCRETE AREA      STIFFNESS                    AREA    STIFFNESS 1      1.000    .336E+06              2     1.875    .630E+06 3       2.125    .714E+06              4     2.125    .714E+06 5      1.250    .420E+06              6      1.000   .336E+06 7        .625    .21 DE+06              8      2.250    .756E+06 9      4.219    .142E+07              10      4.781    .161E+07 11     .4.78'I    .161E+07              12      2.812    .946E+06 13      2.250    .756E+06              14      1.406    .473K+06 15       2.500    .840E+06              16      4.687    .158E+07 17      5.312    .179K+07              1d      5.312   .179E+07 19      3.125     .105E+07              20      2.500    .840E+06 21        1.562    .525E+06              22      1.750    .5ME+06 23        3.281    .110K+07              24      3.719    .125E+07 3.719    .125K+07              26      2.1d7    .735E+06 1.750    .588K+06             28      1.094    .368E+06 1.500    .504E+06             30      2.812    .946Ei06 31        3.187    .107E+07             32      3.187    .107E+07 33        1.875    .630E+06             34      1.500    .504E+06 35        .937    .315K+06             36      1.000    .336E+06 37        1.875    .630K+06             38      2.125    .714E+06 39        2.125    .714E+06             40      1.250    .420E+06 41        1.000     .336E+06            42        .625    .210E+06 SLNIATION Of EFFECTIVE AREAS ~          100.000 PLATE AREA                        ~    100.000 TOTAL CONCRETE STIFFNESS          ~    .336E+08
                  ~    INPIIT DATA PROCESSINQ CCHPLETE.   ~
 
I%035/11                            DATE 92  N.24   PACE P        PLOT PLAN VIEN    Of TME BASEPLATE'WE THE X  AXIS (CONSTANT J LINES) ARE IKNI?OITAL, AMD THE Y  AXIS (CONSTANT I LINES) ARE VERTICAL.
NJJJJJJJJJJJJJNJJJJJJJJJJJJ      4444JJKJJJJJJJJJJJJJJJJJJNJJJJJJJMJJJJJJJJJJJJJJN I                                        I                      I          I              I I                I                      I                      I          I              I I                I                      I                      I          I I                I                      I                      I          I              I NJJJJJJJJJJJJJ                                                      JJJJJJJNJJJJJJJJJJJJJJM I                A                        I                      A            I              I I                A                        I                      A            I              I I                A                        I                      A          8                I NJJJJJJJJJJJJJAJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJAJJJJJJSBBJJJJJJJJJJJJJM I                A                        I                      A          8                I I                A                        I                      A            I              I I                A                        I                      A            I              I I                A                        I                      A          I                I I                A                        I                      A          I                I I                A                                                A                            I I                A                        I                      A          I                I I                A                        I                      A          I                I NJJJJJJJJJJJJ                                JJJJJJJJJJJJJJJJJAJJJJJJJNJJJJJJJJJJJJJJN I                A                        I                      A          I              I I               A                        I                      A          I              I I                 A                                                A          I               I I                 A                        I                       A          I               I I                 A                                                A          I               I I                 A                        I                       A          I               I I                 A                        I                       A          I               I I                 A                        I                      A            I               I I                 A                       I                     A           I               I I               A                         I                     A           I               I I               A                       I                       A           I               I NJJJJJJJJJJJJJ                                                        JJJJJJJMJJJJJJJJJJJJJJN I                 I                       I                       I         I               I I                 I                       I                       I         I               I I                 I                                               I         I               I I                 I                                               I         I               I I                 I                       I                       I         I               I I               I                       I                       I         I               I I                 I                       I                       I           I               I I                 8                        I                       I           8                I NJJJJJJJJJJJJSSSJJJJJJJJJJJJJJJJJJMJJJJJJJJJJJJJJJJJJMJJJJJJBSSJJJJJJJJJJJJJM I                 8                        I                       I           8              I I                 I                       I                       I           I               I I                 I                       I                       I           I               I I                 I                       I                       I           I               I I                 I                       I                       I           I               I I                 I                       I                       I           I               I I                 I                       I                       I                           I I                 I                       I                       I           I               I I                 I                       I                                   I               I NJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJNJJJJJJJNJJJJJJJJJJJJJJM
 
PROGRAN:  NE035 SASEPLATE          SNQI: S9601 0110 AAII 7081                DATE:  92.09-24 RELEASE 11        NOS/VE    1.5.3 L765                      TINE: 12:34)25 PAGE:    13 1111111111111111
                ~ E 0  I N    S  0 L U T  I 0    N    P N A S E L 0 A 0      C A S E    N  0:
            ~ ~~ttttttttttttttttttttttttttttt1111tt TITLE: FILENANEtHMPSP28 LOAD CASE NO.
(TOP        TEN VALUES) 0 I S  P L A C E N E N T S NME              0ISPL.          NtIE              0 ISPL ~
7      .60'l470E.02            22        -.643703E 03 14      .557485E.02            15        e.637019E.03 6      .509943E.02            23        e.621235E 03 21      .501649E.02            30        -.617772E.03 13       .466271Ee02            29        -.587693E.03 5      .454994Eo02            37        -.526119E-03 28       ~ 445364E-02            36        -.474248E.03 35      .416473E-02               8        e.441528E 03 12      .411625E.02             16        e.320971E.03 20      .410428E.02               1        e.218181E 03 QUADR I LATERAL PLATE PRINCIPAL STRESSES ELENENTS              +    Z      FACE ELEN  SIGNA        ELEN      SIGNA      ELEN        SIGNA        ELEN      SIGNA 20    .5840.        14      5409.          8      .4144.           26    e 3632.
2  e 2977.         23      1986.         13      e 1973.         27    e 1963 24    1687.         22      1555.
ELENENTS                    2      FACE ELEN  SIGNA       ELEN     SIGNA       ELEN         SIGNA       ELEN       SIGNA ee  oooo      ooo 20     5998.         14      S369.        26          3725.          8      3655.
2     2464.         27      2092.         13        1858.         23     o 1694.
24  e 1548.           7    1533.
CONCRETE                LOADS NtOE  ZoPRESS      SSE      2 PRESS    NRE      ZePRESS        INOE    Z.PRESS 22  e 216.       1S      -214.       23      e 208.         30      e208.
29  e197.         37      e177.       36      e 159.           8      e 148.
16  .108.         38      e73.
 
PROGRAN!     NESS SASEPLATE       SIRRII S9601 0110 AAN 7081     DATE: 92-09 24 RELEASE 11     NOS/VE 1.5.3 L765             T INE: 12:34 46 PAGE:     14 a 0 L T     LOADS N(HIE     X SHEAR       T SHEAR         SRSS       TENSlON 9         654.         -761.         1004.       96.
12        -199.         -792,         817.     3622.
30          652.          91.         658.         0.
33          -194.          102.         219.     2372.
80LT INTERACT lON                     EOUAT lON EGUATlONt((TENSlON/TALL(N)tt 1.000+(SHEAR/SALLOI)tt       1.000))tt 1.000 IKCE     TENS lON       SHEAR   TENS lON     SHEAR  INTERACT    SAFETY ALL(HI       ALLCM      RATIO       RATIO   RAT10     FACTOR 9       6020.       5210.       .016       .193    .209      4.795 12       6020.       5210..602               .157    .759      1.318 30       6020.       5210..001               .126    .127      7.853 33       6020.       5210..394               .042     .436     2.293
              ~ ttttttttkttttttttttttttttttttttttttttttttttt END LOAD CASE ttttttttttttttttttttttttttttttttttttttttttttt
              ~ tttttttttttttttttttt*tttt**tt**tt*tttttttttt
* END       POSTPROCESS l           NG 11***tttttttttt*t*t*tt*tttt*tttt*t*tttttttttt
 
Pile f                                                             CALC ID TTACHMENT CP!tL uNn f                                 NED G93 ZNTERDZSCZPLZNE REVIEW REQUEST (ZRR)
ZRR fs Tos
                                            ~>/RET/ggggPCN
                                          'nit/Subunit Ps                  Plant ~~
Froms j                                  .t/Subunit, Details of Review Requests   REFERENCE - PCR-6547, DELETION OP RELIEF VALVES AND ADDITION OP ORIPZCES AND STRAINERS ~
ATTACHED ARE THE SIGNED OFF SUPPORT LOAD SHEETS POR PCR-6547 AS WE KNOW IT AS OP 12s00 P.M.
ON SEPTEMBER 25, 1992 ~ PLEASE USE THESE LOADS IN YOUR SUPPORT DESIGNS AND EVALUATIONS FOR THE ABOVE MENTIONED PCR. THESE, LOADS ARE AS GOOD AS THE INFORMATION USED TO DEVELOP THEM SINCE NO APPROVED DRAWINGS HAVE BEEN RECEIVED AS OP THIS WRITING+
IP   THERE ARE ANY QUESTIONS PLEASE CONTACT JOHN HOPKINS AT     X-6734 ~
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Latest revision as of 02:47, 18 March 2020

Rev 2 to Calculation CS-0021, Mechanical Analysis & Calculations for 1CS-746 Charging Pump a to Refueling Water Storage Tank Isolation Valve. Info Applicable to GL 89-10
ML18010A833
Person / Time
Site: Harris Duke Energy icon.png
Issue date: 10/09/1992
From:
CAROLINA POWER & LIGHT CO.
To:
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ML18010A832 List:
References
CS-0021, CS-0021-R02, CS-21, CS-21-R2, GL-89-10, NUDOCS 9210280060
Download: ML18010A833 (194)
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8210280060 ggg009 PDR 'ADQCK 05000400 P PDR Carolina Power & Light Company PO Box 1551 Raleigh, North Carolina 27602 Shearon Harris Nuclear Power Plant Unit 1 Mechanical Analysis and Calculations for 1CS-746 Charging Pump A to Refueling Water Storage Tank Isolation Valve

%II ISA MIIIIL"IlIJ .Il Generic Letter 89-10 Applicable:~Yes No Valve Classification: Nuclear-Safety Related Calculation Number *CS-0021 Revision Prepared By/Date Verified By/Date Project Engineer/Date Prin. or Res. Eng./Date Signatures on file Signatures on file Reason incorporation of Electrical Calculation E5-001, Revision 1 10/I/92 Reason Incorporation of PC%.6562, Raviaion I Reason

Prepared By: Calc. ID! *CS-0021 Checked By: Revision: 2 List of Effective Pa es pacae prevision 1

2 3

4 5

6 7

8 9

10 11 12 13 14 15 16 17 18 19 Attachment A Telecon w/Velan Inc.

Attachment B Fax from of Velan Attachment C Flow Isolation/Seating Thrust Attachment D Average Closing Packing Load Attachment E Final Thrust Due to Inertia Attachment F Thrust at Torque Switch Trip

Attachment:

G Design Verification Record 1CS-746 Page No: 1

Prepared By: Calc. ID! *CS-0021 Checked By: Revision: 2 TABLE OF CONTENTS Section Descri tion Pacae 1~0 Purpose 2.0 References 3.0 Bases and Assumptions 3.1 Analyzed Configuration 3 ' Valve Function and Control Configuration 3 ' Assumptions 4.0 Calculations 4.1 Generic Letter 89-10 Applicability 4.2 Design Differential Pressure Evaluation 7 4.3 Valve Thrust 4~4 Recommended Minimum Torque Switch Setting 11 4.5 Motor Capacity Limits 4.6 Allowable Operating Ranges 12 4.7 . Stall Evaluation 14 4.8 Required Limit Switch Settings 15 4.9 Nominal Operating Time 17 5.0 Results, Conclusions and Recommendations 19 Attachment A Telecon w/Velan Inc. 1 page Attachment B Fax from of Velan 3 pages Attachment C Flow Isolation/Seating Thrust 1 page Attachment D Average Closing Packing Load 1 page Attachment E Final Thrust Due to Inertia 1 page Attachment F Thrust at Torque Switch Trip 1 page Attachment G Design Verification Record 2 pages 1CS-746 Page No: 2

Prepared By: Calc. ID: *CS-0021 Checked By: Revision: 2 1~0 PURPOSE

1. 1 Pu ose of this Re ort The purpose of this report is to document various parameters pertaining to the subject motor-operated valve. This report:

reviews the design differential pressure against which the valve may have to operate calculates the MOV thrust/torque requirements evaluates the limitations of the actuator, motor, and valve (evaluation includes effects of a motor stall) evaluates the actuator limit switch settings 1.2 Reason for Revision PCR-6547, Revision 1, removed the Alternate Mini-flow Relief Valves and installed restricting orifices upstream of motor-operated valves 1CS-746 and 1CS-752. The control logic for these motor-operated valve will be modified such that they will automatically open upon high RCS pressure (2300 psig) coincident with an "S" signal and will automatically close at the reset pressure of 1750 psig. The reason for this revision, is to incorporate the changes made by PCR-6547, Revision 1.

2 ' RERERENCES 2.1 NED Design Guide DG-I.11, "Q-List Motor-Operated Valve Mechanical Evaluations", Revision 4.

2 ' NED Scope Document {}9-M0-002, Revision 2.

2.3 "Analysis of Overload Protection and Motor Torque Output for AC Motor Operated Valves" E5-001, Sub-Calculation CPL-MOV-051, Revision 2.

2.4 Control Wiring Diagram CAR 2166-B-401 Sheet 317, Revision 5.

2.5 Corrective Maintenance Procedure CM-I0002, Revision 4.

2.6 Valve Vendor Print 1364-53850, Revision 1.

Technical Manual ISP, Volume 2, Revision 18.

1CS-746 Page No: 3

Prepared By: Calc. IDs *CS-0021 Checked By: Revision: 2

2.0 REFERENCES

Continued 2.8 Chemical & Volume Control Piping, Reactor Auxiliary Building, Plans, CAR-2165-G-140, Revision 23.

2.9 Chemical and Volume Control System Description, SD-107, Revision 2.

2.10 Crane Technical Paper No. 410, Nineteenth Printing 1980.

2 ~ 11 Technical Memorandum "Performance and Properties of Limitorque Components", Number TM-G-XXXX-001, Rev. 0.

2.12 Piping Line List, CAR-1364-B-0070, Revision 44.

2. 13 Westinghouse E-Spec. No. G-678852, Revision 2.

2 ~ 14 Design Basis Document DBD-104, Revision 0.

2.15 RAB Tank Area Sections, CAR-2165-G-251, Revision 18.

a.zs Piping Isometric 1-CS-651, Revision 5.

2 ~ 17 Limitorque Order Sheet 3D0652-D 2.18 PCR-6547, Revision 1, "Alternate Mini-Flow Re-Design" 3 ' BASES AND ASSUMPTIONS

3. 1 Anal zed Confi ration The configuration assumed when performing this analysis is as follows:

Actuator Dat Limitorque Order Number: 3D0652-D Actuator Size & Type: SMB-00 1 Overall Unit Ratio: 82 ~ 0:1 Handwheel Ratio: 4 ~ 3P:1 Handwheel Efficiency: '5%

Worm Set/Gear Ratio: 45:p Worm Set Efficiency: 36%

Applications Factor: 0.9 Installed Spring Pack: 60-600-0047-1 Pullout Efficiency: 40%

Run Efficiency: 50%

Stall Efficiency: 50%

1CS-746 Page No: 4

Prepared By: Calc. ID: *C8-0021 Checked By: Revision: 2 3.1 Anal sed Confi ration Continued Motor Data Foot-Pounds: 10 RPM: 1700 Volts: 460 AC Manufacturer: Velan Valve Size & Type: 2-inch, globe Valve Pressure Class: 1500 psig Mean Contact Seat Diameter: 1.875 Stem Configuration: 1.125D-1/3P-2/3L Stroke Length: 1.5 inches 1 Walkdown Data "Motor-Operated-Valve Data Form" 2 NED Design Guide I.11 (Reference 2.1) 3 Limitorque Order Sheet (Reference 2.17) 4 Emdrac Print (Reference 2.7) 3.1.1

~ ~ Cross-reference Number s The Ebasco (construction identification) tag number for this valve is 2CS-V757SA-1.

~

The Westinghouse Identification Number and Location are 2TM78FNM and 8489A respectively.

3.2 Valve Function and Control Confi ration 3.2.1 Valve Function The alternate mini-flow line is for dead head protection of the CSIP's during safety injection (specifically the injection phase of the SIS operation). Valves 1CS-746 and 1CS-752 are designed to open automatically upon high RCS pressure (2300 psig) coincident with an "S" signal and will automatically close at the reset pressure of 1750 psig (Reference 2.18). These valves are located in parallel on the two alternate mini-flow lines which relieve to the RWST. I 1C8-746 Page No: 5

Prepared By: Calo. IDs *CS-0021 Checked By: Revision: 2 3.2.2 Control Confi ration The following statements are derived from references 2.4, 2.5 and 2 ~ 18 ~

This MOV automatically opens upon high RCS pressure (2300 psig) coincident with an "S" signal and will close at the reset pressure of 1750 psig.

Under normal conditions this MOV can only open if valves 1RH-25, 1RH-63 and either 1CS-165, 1CS-166 or 1CS-745 are closed.

This MOV trips out via the torque switch in the closing direction and is electrically de-energized by the open limit switch, in the opening direction.

The open torque switch and thermal overloads are automatically bypassed on loss of offsite power or a safety injection actuation.

1) The minimum torque delivered by the actuator motor is assumed to be 5.9 ft-lbs per reference 2.3.
2) The maximum torque delivered by the actuator motor is assumed to be 11.3 ft-lbs per reference 2.3.
3) The Stem Factor for a coefficient of friction of 0.15 is 0.0156 and a coefficient of friction of 0.2 is 0.0179 (reference 2.1).
4) The flow limiting component in the alternate mini-flow line is the fixed orifice. The flow capacity of this orifice is 60 gpm nominally (reference 2.18).
5) The maximum operating temperature and design temperature for line number 2CS2-785SN-1 is 130 F and 200 F respectively (reference 2.12).
6) Piping frictional losses are ignored when calculating differential pressure at the valve.
7) The 0.433 psig/ft conversion factor used in this calculation is based on water at 60 F (reference 2.10).

XCS-746 Page No: 6

Prepared By: Calc. ID: *CS>>0021 Checked By: Revision: 2 4 ' CALCULATIONS 4.1 Generic Letter 89-10 A licabilit Valve 1CS-746 is located in the CSIP alternate mini-flow line and is designed to open "S" automatically upon high RCS pressure coincident with an signal and automatically close at the reset pressure (Reference 2.18). The alternate mini-flow line is for dead head protection of the CSIP's during safety injection (specifically the injection phase of the SIS operation).

Based on the preceding paragraph and the guidance provided in reference 2.2, the requirements of Generic Letter 89-10 are a licable to this MOV.

4.2 Desi n Differential Pressure Evaluation 4~2~1 S stem Inlet Pressure Upstream .pressure will be assumed to be equal to the shutoff head of the CSIPs plus the static head of the RWST at its maximum level.

CSIP shutoff head:

6200 feet (ref. 2.7)

  • 0.433 psig/foot = 2,684 psig Static Head:

RWST Maximum Level = 301 ft. (ref. 2.15)

Valve Elevation = 249 ft. (ref. 2.16)

(301 ft. 249 ft.)

  • 0.433 psig/ft 23 Pressure is equal to: 2,707 psig s'pstream 4.2.2 Differential Pressure The maximum differential pressure (dP) occurs when maximizing the upstream and minimizing the downstream pressure. To maximize dP, it is assumed that the downstream pressure is psig. 0 Therefore, the maximum differential pressure is 2,707 psid.

1CS-746 Page No: 7

Prepared By: Calo. ID: *CS-0021 Checked By: Revision: 2 4.2.2 Differential Pressure Continued I

Note: The subject MOV is a pressure under the seat globe valve.

The most conservative opening differential pressure assumption is to assume 0 psid since any line pressure would assist the valve in opening. For this reason opening upstream pressure and differential pressure are not calculated.

4. 3 Valve Thrust 4.3.1 Valve Thrust Re ired at Maximum dP The maximum thrust requirements for the operation of this pressure under the seat globe valve may be determined by the following equations, which are provided by reference 2.1.

CLOSING THRUST = (dp

  • A
  • FV) + SBL + [SA*(P-dP))

OPENING THRUST = SBL (dP

  • A) [SA*(P-dP))

where:

THRUST = The required stem thrust, in pounds-force.

The differential pressure across the valve.

The seat area of the valve, which is 2.76 square inches based on contact seat diameter (Section 3 1)

An empirical valve factor, which is 1.1 per reference 2.1.

SBL The stuffing box load, or packing drag, expressed in pounds-force. This is 1500 pounds per reference 2.1.

SA The area of the stem, in square inches. For the stem diameter given in section 3.1, this area is 0.99 square inches.

The inlet system pressure.

1CS-746 Page No: 8

Prepared By: Calo. ZD! *CS-0021 Checked By: Revision: 2 4.3.1 Valve Thrust Re ired at Maximum dP cont.

From the information given above, the closing thrust may be calculated.

CLOSING THRUST (2 i 707*2 76*1 1) + 1 i 500 + [0 99*(2 i 707 2 i 707]

~ ~ ~

8i218 + li500 + 0

= 9,718 pounds The value of 9,718 pounds includes a conservatism of approximately 10% due to the assumed valve factor of 1.1, and an additional conservatism of approximately 500 to 1,000 pounds due to the assumed packing load of 1,500 pounds (see attachment D).

In addition, normal CP&L practice is to multiply the calculated closing thrust by 1.15 in order to account for possible VOTES measurement errors and torque switch repeatability. Thus, the theoretical calculated closing thrust is 11,176 pounds.

NOTE: Liberty Technologies issued a 10CFR21 notification on 10/2/92 which documents potential thrust measurement inaccuracies due to torsional effects on small stems.

A review of the design of 1CS-746 has confirmed that the anti-rotation device is located in the yoke flange, above that portion of the stem where the VOTES calibrator was installed. Thus, the subject 10CFR21 notification does not apply to this valve.

The calculated minimum allowable closing thrust of 11,176 pounds is within the thrust capabilities and ratings of the valve and actuator, which are 14,432 and 14,000 pounds, respectively.

However, there is a concern that inertial effects may cause the final thrust to exceed the continuous ratings of the actuator and valve. A review of differential pressure test data for 1CS-752 (a sister valve), which was tested at approximately 2,730 psid, indicates that thrust at torque switch trip was 11,131 inertia pounds (attachment F). Final seating thrust due to was 13,432 pounds (attachment E), which represents a thrust increase of 21%.

Since the assumed VOTES measurement error is +10%, the actual final thrust may exceed the continuous thrust ratings of the actuator and valve. Thus, it is desireable, if possible, to adjust the torque switch to trip at a lower value of thrust.

1CS-746 Page No: 9

Prepared By! Calo. ID: *CS-0021 Checked By! Revision: 2 4.3.1 Valve Thrust Re ired at Maximum dP cont.

Test data for 1CS-752 indicates that flow isolation was achieved at 7,804 pounds (attachment C) of thrust at an indicated test dP of 2730 psid. This test was performed with a spool piece installed in lieu of the relief valve. The proposed configuration of multiple orifices installed upstream of the MOVs will reduce upstream pressure at the valve, thereby making the The average closing results of this previous test conservative.

packing load during the RF03 test of 1CS-752 was 456 pounds (attachment D). This packing load is included in the 7,804 pounds of thrust at flow isolation; therefore, the thrust required to overcome differential pressure is equal to 7,348 pounds. In order to allow for variations in packing, a packing load of 1500 pounds will be assumed.

From the information given above, the expected closing thrust may be calculated.

CLOSING THRUST = 7,348 + 1,500 + [0.99*(2,707-2,707]

7i348 + li500 + 0

= 8,848 pounds A differential pressure and line pressure of zero is assumed to provide for the most conservative opening thrust.

OPENING THRUST = 1,500 (0*2.76) - I'0.99*(0-0)]

1,500 - 0 0

= 1,500 pounds i.3.2 Minimum Allowed Dia ostic Th st The minimum allowable closing/opening thrust at torque switch trip shall be 1.15 times the calculated required thrust when actuator torque is > 50 foot-pounds and 1.20 when actuator torque is ( 50 foot-pounds, in order to account for possible measurement errors and torque switch repeatability. Thus, MINIMUM CLOSING DIAGNOSTIC THRUST = REQUIRED THRUST

  • 1.15 8,848
  • 1.15 10,175 pounds 1CS-746 Page No: 10

Prepared By: Calc. ID: *CS-0021 Checked By: Revisian: 2 4 ' ' Minimum Allowed Dia astic Thrust Continued MINIMUM OPENING DIAGNOSTIC THRUST = REQUIRED THRUST

  • 1.20 1,500
  • 1.20 1,800 pounds 4.i Recommended Minimum Tor e Switch Settin s The input torque (actuator torque) required to produce the thrust values calculated in section 4.3, may be calculated using the following equation (reference 2.1).

ACTUATOR TORQUE = THRUST

  • STEM FACTOR Based on the stem factors given in section 3.3, Assumption 3, the actuator torque for the normal opening and closing conditions may be calculated as follows:

MINIMUM CLOSING TORQUE = 10,175

  • 0.0179

= 182 ft-lbs MINIMUM OPENING TORQUE = 1,800

  • 0.0179 32 ft-lbs i.5 Motor Ca acit Limits The available motor torque at degraded-voltage conditions limits the available actuator torque. If a torque switch is set above the minimum available torque, there is a possibility of stalling the motor before the torque switch can actuate. In order to prevent this situation, the maximum torque switch setting value shall not exceed the minimum available torque provided by the motor at degraded-voltage conditions.

1CS-746 Page No: 11

Prepared By: Calc. ZD: *CS-0021 Checked By: Revision: 2 4.5.1 Closin Actuator Tor e as Limited b Motor Ca acit According to reference 2.1, the closing actuator torque that will be developed by the minimum available motor torque (reference 2.3) is calculated as follows.

ACTUATOR TORQUE = MOTOR TORQUE

  • UNIT RATIO
  • RUNNING EFF.
  • 0.9 5.9
  • 82.0
  • 0.50
  • 0.9 218 foot-pounds 4.5.2 0 enin Actuator Tor e as Limited b Motor Ca ac t According to reference 2.1, the opening actuator torque that will be developed by the minimum available motor torque (reference 2.3) is calculated by:

ACTUATOR TORQUE = MOTOR TORQUE

  • UNIT RATIO
  • PULLOUT EFF.
  • APPLICATION FACTOR 5.9
  • 82.0
  • 0.4
  • 0.9 174 foot-pounds 4.6 Allowable 0 eratin Ran es 4.6.1 Maximum Thrust and Tor e Limits Thrust Limits The allowable thrust limits of the actuator and valve are shown below. The limiting components in the opening and closing directions define the maximum allowable continuous thrust setting.

COMPONENT LIMIT POUNDS SOURCE ACTUATOR *12 600 REF. 2.1 VALVE CLOSING **12 989 Attachment B VALVE OPENING **12,989 Attachment B This limit is 904 of the Limitorque qualified continuous rating.

These limits represent 904 of the Velan continuous duty ratings as provided in attachment B.

1CS-746 Page No: 12

Prepared By: Calc. XD: *CS-0021 Checked By: Revision: 2 4.6.1 Maximum Thrust and Tar e Limits Cantinued Tar e Limits The allowable torque limits of the actuator and valve are shown below. The limiting component defines the maximum allowable continuous torque setting.

COMPONENT LIMIT FOOT-POUNDS SOURCE MOTOR CLOSING 218 SECTION 4.4 MOTOR OPENING 174 SECTION 4.4 ACTUATOR *225 REF. 2. 1 SPRINGSET PACK 250 REF. 2.11

  • This limit is 904 of the Limitorque qualified continuous rating.

4.6.2 E ivalent Varmshaft Tar e From reference 2.1, the wormshaft torque that must be applied to achieve a required output torque may be calculated by:

WORMSHAFT TORQUE = RE UIRED OU PUT TOR U WS RATIO

  • WS EFFICIENCY 4.6.2.1 Clasin Warmshaft Tar e The equivalent wormshaft torque is provided for the purpose of verifying the closed torque switch setting with a torque wrench.

MINIMUM WORMSHAFT TORQUE 182 11.23 FOOT-POUNDS 45

  • 0.36 135 INCH-POUNDS MAXIMUM WORMSHAFT TORQUE 2 8 13.46 FOOT-POUNDS 45
  • 0.36 162 INCH-POUNDS 1CS-746 Page No> 13

Prepared By: Calc. ZD: ~CS-0021 Checked By: Revision: 2 4.6.2.2 0 enin Wormshaft Tor e For this valve the recommended minimum opening torque setting is 32 foot-pounds, and the maximum allowable open torque setting is 174 foot-pounds. However, it is not practical to set the opening torque switch with a torque wrench because this would cause the stem to be forced against the backseat. Therefore, the open torque switch shall be adjusted to a setting of "1" (Reference 2 ~ 11) .

4.7 Stall Evaluation According to electrical analysis (reference 2.3) performed for this valve, the maximum available motor torque at the most favorable conditions is 11.3 foot-pounds.

According to reference 2.1, the stall torque of the operator may be calculated by:

ACTUATOR STALL TORQUE MAXIMUM MOTOR TORQUE

  • UNIT RATIO
  • STALL EFFICIENCY 11.3
  • 82.0 * .50 = 463 FOOT-POUNDS The corresponding stall thrust may be calculated as follows (reference 2.1):

Note: The stem factor for a coefficient of friction of 0.15 is used for conservatism (see section 3.3).

STEM FACTOR

~63 '= 29,679 POUNDS 0 0156 The one-time limits of the valve and actuator are as follows:

COMPONENT LIMIT SOURCE ACTUATOR TORQUE 500 FOOT-POUNDS REF. 2. 1 ACTUATOR THRUST 35 000 POUNDS REF. 2. 1 VALVE CLOS ING 35 616 POUNDS ATTACHMENT B VALVE OPENING 35,616 POUNDS ATTACHMENT B 1CS-746 Page No: 14

Prepared By: Calc. ZD: *CS<<0021 Checked By: Revision: 2 4.7 Stall Bvaluation Continued The calculated stall forces for this Motor Operated Valve (MOV) indicate that the potential does not exist for damage to the actuator and valve power train and load-bearing components.

4.8 Re ired Limit Switch Settin s As shown in reference 2.4, the actuator is equipped with a four train limit switch assembly, arranged in the following manner:

4.8.1 Bases of Limit Switch Set oint Re irements

~Rotor 1 Rotor gl acts as the open limit switch, in order to stop the motor after the valve has traveled to the full open position. It provides position indication (it turns off the green indicator lamps when the valve is full open). In addition, rotor N1 provides a bypass around the closing torque switch as the valve starts closed.

The practice at SHNPP has been to set the open limit switches to actuate when the disc is at 96% of full open position unless otherwise specified on the control wiring diagram (reference 2.5). Operating experience has shown that this setting provides for proper flow rate, however, RF03 testing of a sister valve identified that the valve stem was coasting into the backseat.

Thus, a setpoint of 96% may not be adequate and therefore, a setpoint of 90% is recommended (see Attachment A for justification).

Rotor 2 When the valve is given a signal to close, the motor runs in the closing direction until the torque switch is actuated, which stops the motor.

Rotor 42 is wired to provide a bypass around the open torque switch until the valve is unwedged. In addition, rotor g2 provides valve position indication (it turns off the red indicator lamps when the valve is fully closed).

1CS-746 Page No: 15

Prepared By: Calc. ID: *CS-0021 Checked By: Revision: 2 4.8.1 Bases of Limit 8witch Set oint Re irements Cont.

In order to assure proper position indication in the close direction, the close limit switch should be adjusted to indicate a closed condition only after the disc has covered the valve seat. The practice at SHNPP has been to set the close limit switches to actuate when the disc is at the 4% position unless otherwise specified on the control wiring diagram (reference 2.5). Operating experience indicates that 4% from fully closed is adequate to meet the setpoint requirements for rotor N2.

Thus, 4% is an acceptable setting, and can be retained.

Rotor 3 Rotor 43 is not used.

Rotor 4 Rotor 44 provides position indication to the main termination board.

to open It also provides a permissive which allows valve 1RH-25 provided valve 1CS-746 is closed and other conditions are met.

order to assure proper position indication in the close direction, the close limit switch should be adjusted to indicate a closed condition only after the disc has covered the valve seat. The practice at SHNPP has been to set the close limit switches to actuate when the disc is at the 4% position unless otherwise specified on the control wiring diagram (reference 2.5). Operating experience indicates that 4% from fully closed is adequate to meet the setpoint requirements for rotor N4.

Thus, 4% is an acceptable setting, and can be retained.

4.8.2 Limit Switch Settin Re irements Limit Switch Rotor Settin s In this case, the various limit switch rotors are required to be set as follows:

ROTOR 01: 90% of full open ROTOR 42: 4% of full open ROTOR $ 3 NA ROTOR 44: 4% of full open 1CS-746 Page No: 16

Prepared By: Calc. ZD: *CS-0021 Checked By- Revision: 2 4.8 ~ 2 Limit Switch Settin Re irements Continued The preferred method for setting limit switches is to determine the number of handwheel turns needed for a full stroke, and then to set the switches at the required percentages based upon that.

The total number of handwheel turns needed to stroke the valve may be handwheel determined ratio are ifall the stroke known.

length, thread lead, and The total handwheel(HW) turns to fully stroke the valve is calculated as follows:

TURNS~ = VALVE STROKE / THREAD LEAD

  • HANDWHEEL RATIO 1.5 inches / .667 inches
  • 4.38 9.85 handwheel turns 44 of 9.85 handwheel turns is equal to 3/8 handwheel turn.

104 of 9.85 handwheel turns is equal to 1 handwheel turn.

4.9 Nominal 0 eratin Time o eratin time is rovided for i o atio o as actual motor RPMs can va with a lied load. With the information provided in section 3.1, the stem nut revolutions per valve stroke and the stem nut revolutions per minute can be determined as follows:

STROKE'ominal

/ * = EGZK-LEAD 1.5 0.667 2.25 STEM NUT REVOLUTIONS/MINUTE MOTOR RP OVERALL UNIT RATIO 1700 82.0 20 '3 1CS-746 Page No: 17

Prepared By: Calc. ZD: *CS-0021 Checked Byt Revision: 2 i.9 Nominal 0 eratin Time Continued With these calculated values the nominal expected operating time of this valve can be calculated using the following equation:

STROKE TIME = STEM NU OLUTI S VALVE STRO STEM NUT REVOLUTIONS/MINUTE 2.25 20 '3 0 '1 MINUTES/VALVE STROKE 6.5 SECONDS/VALVE STROKE This valve has no specific stroke time requirements other than the generic 10 second maximum stroke time required by reference 2.13.

1CS-746 Page No: 18

Prepared By: Calc. ID! *CS-0021 Checked By: Revision: 2 5' RESULTS CONCLUSIONS AND RECOMMENDATIONS 5.1 Results and Conclusions

1) The actuator torque switch and limit switch ranges shall be established as shown in table 5.1.

TABLE 5 e 1 BASIC DATA AND SETO RE UZREMENTS CLOSING THRUST RANGE (POUNDS) OPENING THRUST RANGE (POUNDS)

MINIMUM MAXIMUM MINIMUM MAXIMUM 10 175 12 600 1 800 12 600 RECOMMENDED RECOMMENDED CLOSE TORQUE SWITCH SETTINGS OPEN TORQUE SWITCH SETTINGS MINIMUM ~

MAXIMUM MINIMUM MAXIMUM 182 FT-LBS 218 FT-LBS 32 FT-LBS 174 FT-LBS EQUIVALENT EQUIVALENT CLOSE WORMSHAFT TORQUE OPEN TORQUE SWITCH DIAL SETTING MINIMUM MAXIMUM MINIMUM MAXIMUM 135 IN-LBS 162 IN-LBS LIMIT SWITCH SETTINGS ROTOR ¹1 ROTOR ¹2 ROTOR ¹3 ROTOR ¹4 90% N/A 4%

1 HW TURN 3/8 HW TURN 3/8 HW TURN FROM FULL FROM FULL FROM FULL OPEN CLOSED CLOSED 5.2 Recommendations It is recommended that this valve be retested at maximum achievable differential pressure and flow upon completion of PCR-6547. The test results will be evaluated to confirm the setup ranges established in this calculation are acceptable.

1CS-746 Page No: 19

Attachment A Calc. No. CS~1 Revision 2 TELECON Valve No. 1CS-746 Page 1 of 1 BETWEEN:

MECHANICAL ENGINEER CAROLINA POWER & LIGHT AND: MR.

MANAGER OF ENGINEERING VELAN INC.

DATE: JANUARY 6, 1992 TIME: 2:35PM

SUBJECT:

2n AND SMALLER VELAN GLOBE VALVES MR. STATED THAT 90\ OF FULL OPEN STROKE WOULD ALLOW FULL DESIGN FLOW.

Attachment B Calc. No. 'CS4)021 Revision 2 Valve No. 1CS-746 Page I of 3 Number of pages YIA FAX including this page: Q Please reply by FAX to: Message No.: <'a ~8 To:

Q Head Office and Oate; 8 9Q Plant No, 1 (514) 748-8635 Q Marketing (514) 748-7592 Q Plant No. 2 (514) 341-3032 From: Attention:

Q Spare Parts (514) 342-2311 Q Plant No. 3 (802) 862-4014 Copies to:

Q Plant No. 4 (514) 378-6865 Subject/

Reference:

/~am nyk ~ W uaduaa.~+.

~. 45.0'F...,.......

~~ yga~imrm

Attachment B GLOBE VALVE - 2 in Calc. No. *CS4021 Revision 2 STEM ANALYSIS Valve No. 1CS-746 Page 2 of 3 UTILITY: CAROLZNA POWER AND LIGHT Order no. P9-W. I ~ D. 4: 2TM78FNM VALVE DWG: E73-62S Design Temp. 125 deg F STEM DWG. 7913-22 Pressure Class 1500 lb STEM THRD. 1 1/8 3 ACME double lead STEM MAT. SS 630 A 564 sa = 45950 Psi Code Case N-62-4 STEM DATA dl 0.792 in. root. dia of thread d2 0 917 in- dim. at. sec. d2 0.425 in. dim. at sec. k 0.396 in. rad. d/2 0.016 ft.lb./lb thread. fact:or 0.492 in."2 root area of thread 0.660 in. 2 area of sec. d2 a3 1.224 in."2 area at d2 in shear 0.039 in 4 polar moment of iner-t'.a ov: scam thread 0 in. eff. length of stem 0 in. torcpze arm radius 0.019 in."4 Moment of Inertia Er2'd TT'E2 2>E t TS 2d SLHd 3HUdS NU'Hah 9tST 26r $ 8 lDO

Attachment B Calc. No. 'CS-0021 Revision 2 GLOBE VALVE 2 in Valve No. 1CS-746 Page 3 of 3 STEM ANALYSZS UTZLZTY: CAROXZNA POWER AND LIGHT Order no. P9-W.I'D. 2TM78FNM VALVE DWG: E73-62S Design Temp. 125 deg F STEM DWG 7913-22 Pressure Class 1500 lb STEM THRD. 1 1/8 3 ACME double lead STEM MAT. SS 630 A 564 Sy ~, 113396 Psi Code Case N-62-4 STEM CALCULATION At Section d1 Max Tr 14432 lbs. from Eq. (19)

At Section d2 Max Tr 30347 lbs. from Eq. (20)

At Section k Max Tr 33756 lbs. from Eq. (21)

MAX Thrust/Torque CLOSZNG OPENING Tr./lbs. Tor./lb-ft Tr./lbs. Tor./lb-xt CONTINUOUS DUTY 14432 224 14432 224 ONE TIME 35616 554 35616 554 ErE'd 7 TK2 2IE ITS 2d SJ.Hd 3HUdS NU l3h Z1: ST 26 w 88 J.DO

AITACHMENTC

<<CS4021, Rev. 2 Page 1 of 1 Test: 4 Tag: iCS-752 3/23/3i 22'49'i 5000 VOTES 8ENSOR

-ioooo oIce = -7SM (Ihs) -isooo

.20000 52997 53997 5%997 55997 55897 57997 SWITCH A SWITCH B SWITCH C SWITCH D 52997 53997 5%997 55997 55997 57997 Tin: im Seconds 55.397 1CS-752: Flow Isolation/Seating Thrust 2730 PSID

ATI'ACHMENTD

  • CS4021, Rev. 2 Page 1 of 1 Test: i Tag: iCS-752 3(23/3i 22'25'45

.%50 VERS SENSOR

-%60 orce = -456

( 1hS) -%~0

-%80 25209 25309 25%09 25509 25609 25709 OLS 25209 25309 25%09 25509 25C09 25709 Tiae in Seconds 25.453 Y-EXPO ON 1CS-752: Average Closing Packing Load, Static Conditions

ATlACHMENT E

'CS4021, Rev2 Page 1 of 1 Ted: 4 Tag: iCS-752 3(23/3i 22'49'i VOTES BEMOR orce = -i3432

-i5000 (Ih )

-20000 5530% 55%0% 5550% 556 5570% 5580%

SMITCH A SMITCH B SMITCH C SMITCH D 5530% 55%0% 5550'} SS6 SP0% SSS0%

Tiae im Seconds 55.688 Y-EKPND ON 1CS-752, Final Thrust Due to Inertia

A1TACHMENT F CS-0021, Rev.2 Page 1 of 1 Test' Tag'C8-752 3/23/3i 22'49'i

-F0000 V jTES SENSOR orce = -iii3i15000

)

.20000 5550% 55%0% 550'f 5560'I 5570% 5580%

SWITCH A SMITCH B SWITCH C SWITCH 9 5530'f 55%0% 550't 5560% 5570'f 5580%

Time in Seconds 55.488 'Il'-m'll ox 1CS-752, Thrust At Torque Switch Trip

Attachment G Calc. No. 'CS~1 Revision 2 E DES>~ ~ER3:mumm RzcoR)) Valve No. 1CS-746 Page 1 of 2 I~~f~ to Verification PcrscÃ%%tl Plant Project 4 g( ] Seismic 4 (Class A)

(Class B)

Fflc No. Level ( ] FP 4 (Class 0)

Oocuncnt No. C 0 I Rev ( ] Other Ocsign verification should be done in accordance ufth ANSI N45,p I), Scctfon 6, as amended by Regulatory Guide 1.64, Rev. 2.

Special instructions:

Oisciplinc Project Engineer II. f Veri Icatf cn Oo~tatf cn Appl f cabf l I ty Ofsci t inc Ofsci fne Necnanf ca L X] Civil Structural (]

HVAC Seismic Eaufp. Oual. (]

ELectricaL Civil Stress (]

fSC Ff re Protect Ion (]

Envirormantai Oual iffcation (]

Humn Factors []

Naterials (]

(]

Other []

Verification Nethods Used:

Oesign Review ( ] Alternate Calculations [ ] oualfffcation testing Ocsign Oocunent Acccetable: ~Y Ocsign verifier

~ No ( ] . ccaaants attached.

oats '~ V4 Ackncwlcdgcment okgerfff~tfm+ ~

(OPE) oats III. Rcsolutfm at Ccmmnst Cazeants Resolved (See Attached):

(RE) Oate Action taken makes Ocsign Oocusents Acceptable:

Oesign veriffer Oats (OPE) Oate Proc. 3.3 Rev. 38

Attachment G Calc. No. CS4021 Revision 2 Ualve No. 1CS-746 OISCIPLIRE OESICS VERIFIClTIM RSXRO Page 2 of 2 CA%EST SHEET Plant Pr oieot File Qo.

Oocmmn Mo. ~S&oZl a Z This sheet is catv recaired Men coocaents are, bein% nba.

Cccooant Resolved Mo Resolution lnitfatlOate

~ V1 ~

".;ev. >>'0

Eeet.osuRa 2

SUMMARY

OF EVALUATION FOR SUPPORTS AND PIPE SUPPORT CALCULATIONS FOR REDESIGNED ANCHORS

PIPE SUPPORT EVALUATION The Civil Engineering pipe support effort for this modification consisted of the redesign of pipe hanger anchors CS-H-4400, CS-H-4403, and CS-H-4406, as well as the review of 29 other hangers for load changes. The anchors were redesigned due to new anchor locations. All support impact resulted from changing the piping model by removing the relief valves, adding flow orifices and adding strainers.

The three anchors referred to above were redesigned and new calculations were created. A copy of the calculations are attached.

The 29 hanger calculations were reviewed for load changes and the new loads were compared to the loads used in the existing analysis. The load comparison evaluation showed that the minor load changes on all of the 29 hangers were within the design margin of the existing calculations. Therefore, these hangers were found to be acceptable without modification.

324~

cM OTY PART 0 DESCRIPTION NO. STATUS 4". ~~ IV&X O-~"Ir. 5A55. TP504 ~t TOhuII )

0CI a:

f) iz&vfQV5 Wl&7. ggPW~ C% H-~C4j g&/ $ 0-M3 CLc" LOCATION PLAN REFERENCE DOCUMENTS PROI'ESSIONAL ENCIIIEER PIPE DWG '2I MECH. DWG.

Cr

- ~ gE,V, M FI.:fY l2ELhTEU &&ISHIC STRESS CALC. - I ~ CAROLINA POWER 8c LIGHT COM ANY SuPPORT CANC. r NUCLEAR ENGINEERING DEPARTMENT l PLANT: HARRIS NUCLEAR PROJECT - UIIIT I SCALE l l I "'"E: C'4&Iv(ICOSI k~dM& CO~MI Io g.fg g&lISQIr I%6M I lZQ~Og. AUXILI~54~. &..2 2&-

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PROFESSIONAL ENGINEER

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CAROLINA POWER 8c LIGHT COMPANY

~IQQIC, NUCLEAR ENGINEERING DEPARTMENT PIANT: MRIS NUCL842 KbHT'CALE'M IO.2-ff 5fS QADI S~ SAT I DATE OESCRIPTION WN OSN CH OV OPE OPPE yg NO/.Q-'gg(jt I.6+-405 RgIA SHT: g Qr'2 qynrp ga 5< &94 I-C - tGe75 S+T. g ."r 8

Mod Number ~cg- g~yp FR Number Calculation Affected Drawing Affected Reason for Change:

@i~~~ w<a~esrez ~~~zz ~g roan +i mo~

ra VZ <Z<~<~ 2 Z rZ STOCK /A'YEjV)cr/'/.

Justification for Change Approval:

Minor Change (i.e., editorial, reference dimension, etc.), Supplementary Calculations are not attached.

Other (provide basis, attach supplementary calculations) su/ <7 /7 U7/ ~ /8 ACCT ~E'C, EE~V$ 6 pIdP SEC7/OAJ OFBP7/DS 7+9~ 7X O'X4 X ~cP.

DPE*

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  • Signatures indicate design verification has been performed in accordance with NED Procedure 3.3. This form serves as the design verification record.

334943 4I ~ v ~

PAR I Q NO STATS DE SCRIP TION I I i A, T5 C

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PLANT HARRIS NUCLEAR PRO'ECT - UNIT I SCA" E i i I

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CESCRiPTION QwNlosNICHKI ov jopE loppE gp A 8'8&.l-CS.H.~RE!r %I!I s~T I or 2 S~:-TCH e) 54-9Q'T-C- ICt7$

32444j PROFESSIONAL ENGINEER; GhF~ Qa,&Ted 5EtsMic, CAROLINA POWER dc LIGHT COMPANY NUCLEAR ENGINEERING DEPARTMENT PlPNT: kRR6 AU~~ KbnlT SCALE: Q~

"'"': CHavi~I $ VDL.UH& ~rlZOI

$ IIO.2-1Z 565 PtkW I ca~a- hdXII t~~ B.m. & .284-O 259k Seemr I 9%~4% R, +u~a.T

--yI ~AT- DESCRIPTION WN DSNIC" DV DPEIDPPE os'Nop ).gR -I.A-)-4405 REvgw SI T; 2 or'2 SKETCH gp 5'-(at&A 1-C -I~5 S~T. 2 or 8

i DE Mod Number ~R-4~+7 FR Number Calculation Affected C-CS-8 - ~D Drawing Affected Reason for Change:

SUPP& RE ' - ld'r~Zg R PHrrsuu N&J " SZ chz<CWK PU~P Wrml FLouJ PzczRc.

57RHxnJE'ustification for Change Approval:

Minor Change (i.e., editorial, reference d'mension, etc.). Supplementary

~ Calculations are not attached.

Other (provide basis, attach supplementary calculations)

CdC.c ~ drzach'C2-DPE*

Pr r

  • Signatures indicate design verification has been performed in accordance with NED Procedure 3.3. This form serves as the design verification record.

CALCULATION NO PAGE t REV /

LIST OF EFFECTIVE PAGES PAGE REV PAGE REV PAGE REV ATTACHMENTS

NED Guideline E-4 ATTACHMENT D CALCULATION NO ~ +" ~ 'H- +SO PAGE REV /

TABLE OF CONTENTS Page No.

List of Effective Pages Table of Contents Purpose List of References Body of Calculation Conclusions Attachments Page(s)

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CAROLINA POWER & LIGHT COMPANY c-cz-H- 0+oz Checked by: Date:

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CAROLIHA POWER fi LIGHT COHPANY PLANT CALCULATIONNUMBEII HARRIS NUCLEAR PLANT 141-1A PCH/HD NUMBER PAOE REVISION PCR-6547 SUBJECf nornmivnu>s wrrlALs/DATE SI CHARGING PUMP ALTERNATE MINI-FLOW LINE, RELIEF CHECKER'S INIITALS/DATE VALVES REMOVED, FLOW ORIFICES AND STRAINERS ADDED WITH LEAD 'BLANKETS. ~

y Q~emeu 'Leou Vev ('ave. f.eL-N LQL-2 0~a 14'..

HANGER NO.CS- -4 03 NODE PT. ISO NO> - 36-CS-59 SUPPORT Bf.- 1 LR L-Z,

~ Q SYSTEM CONDITION Fx Fy Fg Xx Ãy Rz (LBS) (LBS) (LBS) (FT-LBS) (FT-LBS) (FT-LBS)

Nn 8 51 DEADWEIGHT -406. 2~ -7 l. I.

26.

THERMAL I Lola 104. -35 5l -Z.Z 5h I'I3 PP I

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NOTES: l. +X ~ NORTH, +Y ~ UP, +2 ~ EAST.

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JOB NO.

CALC NO.

PREPARED BY 4-CS'- ff-4+0~

NE035/11 1 ~ 1 1 ~ 1 ~ 1 1 ~ 1 1 1 1 ~ 1 ~ 1 ~ 1 1 ~ ~ ~ ~ ~ 1 PROJECT DATE SNT NO.

CHECKED BY DATE 92.09.25

~ 1 1 1 ~ 1 1 DATE PAGE t1 1

1 CALC FID'TtACHMENT" OF

    • 1111**** 1 ~ ~ 11 ~ 1111 ~ 1** ~ 11 ~ ~ ~ ~ 1 1 t ~ 1111 ~ ~

c~se > f F~E 4 3c "W.

EEEEEEEEE 0000000 33333333 55555555 EE E 00 00 33 55 .

EE 00 00 33 55 EEEE 00 00 3333333 55555555 EE 00 00 33 55 EE E 00 00 33 55 EEEEEEEEE 0000000 33333333 55555555 VERS ION LEASED AUGUST 1989 SER NANUAL VERSION 8 THEORETICAL NAKUAL VERSION: 8 VER I F I CAT ION NANUAL VERS I ON: 10 1 ~ ~ ~ 1 ~ 1 1 1 ~ 1 ~ 1 *1 ~ 1 1 ~ 1 1 1 1 1 1 ~ 1 1 1 ~ 1 ~

  • IN CASE OF PROBLEHS MITH NE035, CONTACT THE

~ BASEPLATE USER REPRESENTATIVES LOCATION EXTENSION 1

~ 11 ~ ~ ~ ~ 11 ~ 1 ~ 11 ~ ~ *~ 1 ~ ~ 1 ~ 1*1 ~ ~ ~ 1111 1 1 1 ~ 1 1 ~ 1 1 ~ 1 ~ ~ ~ 1 ~ 1 ~ ~ 1 1 1 1 1 1 ~ 1 1 1 ~ ~ 1 ~

COPYRIGHT 1984,1987 BECHTEL POMER CORP. ALL RIGHTS RESERVED.

~ ~ 1 1 1 1 ~ 1 1 ~ 1 ~ 1 1 1 ~ 1 *1 1 1 ~ 1 1 1 1 1 1 1 ~ ~ 1 1 1 1 ~ 1 ~ 1 1 1

HE035/11 DATE 92 09 25 PAaE 2 tIOPt404tt ~0~%1tlltO+yyyygy~OtlttOtOOOtlt1ttlt001P 0 PREPROCESSOR lNPUT DATA CARDS 111I110ltltOttt1tlltttttt11WtfO~lt011fttttlttlt1111*liteeeltttt1ttfll0001tototll CARD NO 1 2 -3 4 5 6 12345678901234567890123456789012345678901234567890123456789012345678901234567890 7 8 1 3 FlLEKAHE>HHPBP24 TYPE F-2 EHBED PLATE (BX1) CASE 1 CS.H.4403 2 SIT g ~ g 1/

3 COH ~ g g @4000/

4 PLA 6,11 ~ gd,30/1/29/

5 BPR ~, 1,d,dE5,1.25E6,5987,3473/

6 BOL 3,2,1,1.5,3/

7 BOL 3y6g 1 ~ 1 ~ 5 ~ 15/

8 BOt. 3,10,1,1.5,27/

9 BOL 5,2,1,6.5,3/

10 BOL 5/6/1,6.5,15/

11 BOL 5,10,1,6.5,27/

12 END/

13 ATT 4,63.5,15/

14 JST 4,6,3,2,180/

15 JST 3,6,2,1 ~ 180/

16 1ST 2,6,7,3/90/

17 JST 2,7,3 '/0/

18 JST 3/7/4/2,0/

19 JST 4,7,5,3,0/

T 5,7,5,6,270/

T 5,5,4,3,180/

ST 4,5,3,2, 180/

23 JST 3,5,2,1 180/ ~

24 1ST 2,5,6,3,90/

25 END/

26 END/

27 POl 4,6/

28 LOA 1,550, -794,990,19120, -31056, 12512/

29 LOA 2, -550,794,990, -19120,31056, -12512/

30 EKD/

31 EHD OF JOB

  • ~ END OF lNPUT DATA ~

I%035/11 DATE 92-09-25 PAGE 3

>>>>tt>> ~ >>>>t>>t>>t>>>>>>>>ttt>>tttt>>>>t>>>>ttttttttt>>

PREPROCESSOR INPUT DATA CARDS

~ >>tttttttttt>>tttt>>>>t>>ttt>>>>>>>>>>>>>>>>1>>>>tt>>>>>>ttt>>ttltttttttttttttttt>>ttttttttttttttttttttt CARD NO 1 2 4 5 6 12345678901234567890123456789012345678901234567890123456789012345678901234567890 7 8 1 3 F ILENANE>>HKPBP24 TTPE F-2 EHBED PLATE (8X1) CASE 1 CS.H.4403 2 OJT 0>> 0 0>> 1 0 3 CON 0 0 0 0.000 4000.000 0.000 0.000 0.000 0.000 4 PLA 6>> 11 0 8.000 30.000 1.MO 29.000 0+000 0.000 5 BPR 0>> 0 1>> .880E+06>> .125E+07 .599E+04>> .347E+04>> 0.0 0.0 6 BOL 3>> 2 1>> 1.500 3.000 0.000>> 0.000 0.000>> 0.000 7 BOL 3>> 6 1>> 1.500 15.000 0.000>> 0.000>> O.OM>> 0.000 8 BOL 3>> 10 1>> 1.500 27.000 0.000>> 0.000 0.000 0.0M 9 BOL 5>> 2 1>> 6.500 3.000 0.000>> 0.000>> 0.0M>> 0.000 10 BOL 5>> 6 1* 6.500>> 15.000>> 0.000>> p pppt 0.000 0.000 11 BOL 5>> 10 1>> 6.500 27.000 0.000 0.000>> 0.000 0.000 12 END 13 ATT 4>> 6 3.500 15.000 0.000 0.000 14 JST 4>> 6 3>> 2.000 180.M0>> 0.000 3>>

15 16 17 JST 1ST JST 2

2>>

6 6

7 r

2 3>>

1.MD>>

3.0M>>

1.000 180.000 90.000 0.000 0.000 0.000 0.0M 18 JST 3>> 7 4>> 2.MP>> 0.000 0.000 JST 4>> 7 5>> 3.MO 0.000 0 000>>

T 5>> 7 5>> 6.000>> 270.000 0 000>>

5>> 4>> 3.000>> 180.000>> 0.000>>

JST 4>> 5 3>> 2.000 180.000 0.000>>

23 JST 3>> 5 2 1.000>> 180.000 0.000.

24 IST 2 5 6>> 3.000* 90.000 0.000>>

25 END 26 END 27 POI 4>> 6 0 0.000 0.000 0.000 0.000 0.000 28 LOA 0 0 1>> 550.0 -794.0 990.0 19120.0 .31056.0 12512.0 29 LOA 0 0 2>> .550.0>> 794.0>> 990.0 -19120.0 31056.0 -12512.0 30 END 31 END OF JOB

~ END Of INPUT DATA DECK ~

NE 035/11 DATE 92-09-25 PAGE 4 ttttttttttttttttttttttttttttttttttttttlttttttttttttttttttttttttttttttttttttttt FlLENANEtHNPBP24 TTPE F-2 ENBED PLATE (8X1) CASE 1 CS H.4403 ttttttttttttttttttttttttt1tttttttt1tttttttttt11tttttt1*ttt11tttttttttttt11ttttttttttt 1NPUT PARANETERS PLATE THlCKNESS ...... .. ~ 1.000 PLATE X DlllENSlON ~~ ~ ~ ~~ ~ 8.000 Y-DlNENSlON .. 30.000 NODULUS OF ELASTlClTY .290E+08

~ ~

CONCRETE NODULUS .. .360E+07 CONC. C(WP. STRENGTH ~ ~ ~ ~ 4000.0 BOLT LOCATlONS BOLT l J NODE X.COORD. Y.COORD.

1 3 2 24 1.500 3.000 2 3 6 28 1.SOO 1S.OOO 3 310 32 1.500 27.000 4 5 2 46 6.500 3.000 5 5 6 50 6.500 15.000 6 510 54 6.500 27.000 BOLT PROPERTIES BOLT STIFFNESS (LB/lN.) ALLOMABLE FORCE (LB)

TENS lON SHEAR TEN SlON SHEAR

.MOE+06 .125E+07 5987. 3473.

.BME+06 .125E+07 5987. 3473.

.8ME+06 .125E+07 5987. 3473.

.880E+06 .125E+07 5987. 3473.

.880E+06 .125&07 5987. 3473.

.880E+06 .125 E+07 5987. 3473.

NE 035/11 DATE 92 09 25 PAGE 5

) ttttttttttttttttttttt'tt*ttt'ttttttttttttttttttttttttttttttttttttttttttttfttftf t t FILENANEtHNPBP24 TYPE F-2 ENBED PLATE (8X1) CASE 1 CS H 4403 ttttttt1ttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttt1ttttttttttttttt NON STANDARD ATTACHHENT DATA ATTACHNENT NLNBER 1 SEGHENT NIWBER ... 1 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ JST HE I 0HT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ 2.000 ORIENTATION ANGLE 180.0 THICKNESS ~ ~ .~.~~~ 0.000 SEGNENT NWBER ... 2 TYPE ~~~~ ~ ~ ~ ~ ~ ~ ~ ~~ . JST HEIGHT ~~~ ~ ~ ~ ~ ~ ~ ~~ 0.000 D I STANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ 1.000 ORIENTATION ANGLE 180.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGHENT NIWBER ... 3 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ IST HEIGHI' ~~ ~ ~ ~ ~ ~ ~ ~~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ 3.000 ORIENTATION ANGLE 90.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGHENT NUHBER ... 4 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ JST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ 1.000 ORIENTATION ANGLE 0.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGNENT HISSER ". 5 TYPE ~~~~ ~~~ ~~ ~~~e JST HEIGHT ~~ ~~ ~~~ ~~~~ 0.000 0 I STANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ 2.000 OR I ENTAT ION ANGLE 0.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ 0.000

NE 035/11 DATE 92 09.25 PAGE 6 tttttttttttttttttttttttttttt~ttttttttttttttttttttttttttttt'ttttttt1*tttttt FILEMANEtHNPBP24 TYPE P-2 EMBED PLATE (8X1) CASE 1 CS H 4403 ttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttt NON.STNNARD ATTACHMENT DATA SEGMENT NWBER ~ ... 6 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ JST HEIGHT ~~~~ ~ ~ ~ ~ ~ ~ ~~ ~ ~ ~ ~ ~ 0.000 0 I STANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 3.000 ORIENTATION ANGLE ...... 0.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGMENT ROBER ~ ~ ... ~ ~ ~ 7 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ IST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 6.000 ORIENTATION ANGLE ...... 270.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGMENT NBER ~ ~ ~ ~ ~ ~ ~ ~ ~ 8 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ JST HEIGHT ....""......". 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ o~ ~ ~ 3.000 ORIENTATION ANGLE ~~ ~ ~ ~ ~ 180.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGMENT NNBER ....."" 9 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~~ ~ ~ ~ ~ ~ ~ ~ ~ ~ JST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~~ ~ ~ ~ ~ ~ ~~ ~ 2.000 ORIENTATION ANGLE .. 180.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGMENT MQIBER ~ ~ ~ ~ ~ ~ ~ ~ ~ 10 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ JST HEIGHT ~~~ ~ ~ ~~ ~ ~ ~ ~o~~~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 1.000 ORIENTATION ANGLE ~ ~ ~ ~ ~ ~ 180.0 THICKNESS ~ ~ ~ ~ ~ ~~~~~~ ~ ~ ~ 0'000 SEGMENT IQSER o....o.o. 11 TYPE ~~~ ~ ~ ~ ~ ~ ~~~~ ~~ ~~ ~~ ~ IST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ o~~~~~~~~ 0.000 DISTANCE ~~~ ~~ ~ ~ ~~~ ~ ~ ~ ~~ 3.000 ORIEMTATIQI ANGLE .. 90.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000

NE 035/11 DATE 92-09.25 PAGE 7 tttttttttttttttt~~t~ ~~ttttttttttttttttttttttttt't't'ttttttttttttt FLLENANEtHNPSP24 TYPE F-2 9$ ED PLATE (8X1) CASE 1 CS H 4403 ttt1ttt1tttttttttttt1tttttttttttttttttttttttttttttttt*ttttt1tttt*tttttttttttt1ttttttt LOADlKQ COND I T IONS LOADlNQ CASE NO. t 1 LOADINGS APPLlED AT NODE t 67 FMCE FX t 550.00 FORCE FY ~ -794.00 FORCE FZ < 990.00 IDENT NX t 19120.00 NCKENT NY < -31056.00 IDENT NZ ~ 12512.00 LOADlkG CASE kO. ~ 2 LOADlkGS APPLIED AT NIXIE t 67 FMCE FX ~ -550.00 FMCE FY ~ . 794.00 FMCE FZ t 990.00 NCIIENT HX ~ -19120.00 NCKENT NY ~ 31056.00 NOHENT NZ ~ -12512.00

NE 035/11 DATE 92-09 25 PAGE 8

~ tltttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttttfttt FILENANEtHNPBP24 TYPE F 2 EKBED PLATE (8X1) CASE 1 CS-H-4403

~ ttt1tttt11ttttttttttttttt1t11ttttt1ttttttttttttt1tttttttt1ttttttttt1t1ttt1tttttttttt BASEPLATE CONNECTlVITY ELEKENT KQ) E ELEKENT KCDE KO. JA JB JC JD KO JA JB JC JD 1 1 12 13 2 2 2 13 14 3 3 3 14 15 4 4 4 15 16 5 5 5 16 17 6 6 6 17 18 7 7 7 18 19 8 8 8 19 20 9 9

11 9

12 20 23 21 24 10 13 10 12 10 13 21 24 22 25 '411 13 14 25 26 15 14 15 26 27 16 15 16 27 28 17 16 17 28 29 18 17 18 29 30 19 18 19 30 31 20 19 20 31 ., 32 21 20 21 32 33 22 21 23 34 35 24 22 24 35 36 25 23 25 36 37 26 24 26 37 38 27 25 27 38 39 28 26 28 39 40 29 27 29 40 41 30 28 30 41 42 31 29 31 42 43 32 30 32 43 44 33 31 34 45 46 35 32 35 46 47 36 33 36 47 48 37 34 37 48 49 38 35 38 49 50 39 36 39 50 51 40 37 40 51 52 41 38 41 52 53 42 39 42 53 54 43 40 43 54 55 44 41 45 56 57 46 42 46 57 58 47 43 47 58 59 48 44 48 59 60 49 45 49 60 61 50 46 50 61 62 51 47 51 62 63 52 48 52 63 64 53 49 53 64 65 54 50 54 65 66 55

HE035/11 DATE 92.09.25 PAGE 9

~ tttttl*tltttttttttttllt'1ll' ll'1'll'1~ tlttlttttttl*lltttltllttlltttltlltlttttlll1 FILENANE1HNPSP24 TYPE F-2 EHSED PLATE (SXT) CASE 1 CS-H 4403 1 1*tttttt111111111***1*tltlttttttttlttlllltlltttttttttltttlttt**tttttt'ttttttltlttttttt NODAL COORD I NATES I J F RAKE NODE X Y 2 LINE LINE NCOE COORDINATE COORDINATE COORDINATE 1 1 1 0.000 0.000 0.000 1 2 2 0.000 3.000 0.000 1 3 3 0.000 6.000 0.000 1 4 4 0.000 9.000 0.000 5 5 0.000 12.000 0.000 1 6 6 0.000 15.000 0.000 1 7 7 0.000 18.000 0.000 1 8 8 0.000 21.000 0.000 9 9 0.000 24.000 0.000 1 10 10 0.000 27.000 0.000 1 11 11 0.000 30.000 0.000 2 1 12 .500 0.000 0.000 2 2 13 .500 3.000 0.000 2 3 14 .500 6.000 0.000 2 4 15 .500 9.000 0.000 2 5 16 .500 12.000 0.000 2 6 17 .500 15.000 0.000 2 7 18 .500 18.000 0.000 2 8 19 .500 21.000 0.000 2 9 20 .500 24.000 0.000 2 10 21 .500 27.000 0.000 2 11 22 .500 30.000 0.000 3 1 23 1.500 0.000 0.000 3 2 24 1.500 3.000 0.000 3 3 25 1.500 6.00D 0.000 3 26 1.500 9.000 0.000 3 5 27 1.500 12.000 0.000 3 6 28 1.500 15.000 0.000 3 7 29 1.500 1S.OOO 0.000 3 8 30 1.500 21.000 O.OOD 3 9 31 1.500 24.000 0.000 3 10 32 1.500 27.000 0.000 3 11 33 1.500 30.000 0.000 4 1 34 3.500 0.000 0.000 4 2 35 3.500 3.000 0.000 3 36 3.500 6.000 0.000 4 4 37 3.500 9.000 0.000 4 5 38 3.500 12.000 0.000 4 6 39 3.500 15.000 0.000

KE 035/11 DATE 92.09.25 pACE 10

~ tttt*ttttttttttttt*lttttttttttttttlttttttttttttttttttttttttttttttttttttttttttt FILENANEaNNPBP24 TYPE F 2 ENSED PLATE (8X1) CASE 1 CS-H.4403 *

~ ttttttttttttkttttt1t1tttttttt1tttttttttttttttttttttttttttttttttttttt1ttttttttt1tttt NODAL COORDINATES I J FRANE NQ)E X Y 2 LIKE LINE KCOE COORD I NATE COORD I NATE COORD I KATE 7 40 3.500 18.000 0.000 8 41 3.500 21.000 0.000 9 42 3.500 24.000 0.000 3.500 27.000 0.000 2'6 10 43 11 44 3.500 30.000 0.000 1 45 6.500 0.000 0.000 6.500 3.000 0.000 3 47 6.500 6.000 0.000 4 48 6.500 9.000 0.000 5 49 6.500 12.000 0.000 6 50 6.500 15.000 0.000 7 51 6.500 18.000 0.000 8 . 52 6.500 21.000 0.000 9 53 6.500 24.000 0.000 10 54 6.500 27.000 0.000 11 55 6.500 30.000 0.000 6 1 56 8.000 0.000 0.000 6 2 57 8.000 3.000 0.000 6 3 58 8.000 6.000 0.000 6 59 8.000 9.000 0.000 6 5 60 8.000 12.000 0.000 6 6 61 8.000 15.000 0.000 6 7 62 8.000 18.000 0.000 6 8 63 8.000 21.000 0.000 6 9 64 8.000 24.000 0.000 6 10 65 8.000 27.000 0.000 6 11 66 8.000 30.000 0.000 NODES AT APPLICATION OF LOADS 4 6(OFFSET) 67 3.500 15.000 .500

NE035/11 DATE 92 09 25 PAGE 11

~ ~~~~yyyyygyygggg~)))~~gyp(gyp'~tHOIIIOlttt11tlttOOOllt FlLENANEsNNPBP24 TYPE F 2 ENBED PLATE (8XT) CASE 1 CS.H 4403 1

~ Ot10111111l110&l1f t11t1ttt~tt'W1114lltlt00011tttt1*11t1OPttttl1ttlttt11t1 CONCRETE STlFFNESS DATA NODE EFFECTlVE CONCRETE NODE EFFECT lVE CONCRETE AREA l ST F FNESS AREA STlFFNESS 1 ~ 375 .104E+06 2 .750 .208E+06 3 .750 .208E+06 4 .750 .208E+06 5 .750 .208E+06 6 .750 .208E+06 7 .750 .2ME+06 8 .750 .208E+06 9 .750 .208E+06 10 .750 .208E+06 11 .375 .104E+06 12 1.125 .312E+06 13 2.250 .625E+06 14 2.250 .625E+06 15 2.250 .625E+06 16 2.250 .625E+06 17 2.250 .625E+06 18 2.250 .625E+06 19 2.250 .625E+06 20 2.250 .625E+06 21 2.250 .625E+06 22 1.125 .312E+06 23 2.250 .625E+06 24 4.500 .125E+07 25 4.500 ~

.125E+07 26 4.500 .125E+07 27 4.500 .125E+07 28 4.500 .125E+07 29 4.500 .125E+07 30 4.500 .125E+07 31 4.500 .125E+07 32 4.500 .125E+07 33 2.250 .625E+06 34 3.750 .104E+07 35 7.500 .208E+07 36 7.500 .208E+07 37 7.500 .208E+07 38 7.500 .208E+07 39 7.500 .208E+07 40 7.500 .208E+07 41 7.500 .208E+07 42 7.500 .208Ei07 43 7.500 .2m+07 44 3.750 .104Et07 45 3.375 .937K+06 46 6.750 .187E+07 47 6.750 .187E+07 48 6.750 .187E+07 49 6.750 .187E+07 50 6.750 .187K+07 51 6.750 .187E+07 52 6.750 .187E+07 53 6.750 .187E+07 54 6.750 .187E+07

55. 3.375 .937K+06 56 1.125 .312E+06 57 2.250 .625E+06 58 2.250 .625E+06 59 2.250 .625E+06 60 2.250 .625E+06 61 2.250 .625E+06 62 2.250 .625E+06 63 2.250 .625E+06 64 2.250 .625E+06 65 2.250 .625E+06 66 1.125 .312E+06 QltlATION OF EFFECTlVE AREAS > 240.000 PLATE AREA 240.000 TOTAL CONCRETE STTFFNESS a .666Et08

%03j/11 BATE 92 O9-25 PAGE 12 PLOT PLAN VIEM OF THE BASEPLATE MHERE THE X AXIS (CONSTANT J LINES) ARE NORIZONTAL~ AHO THE Y AXIS (CONSTANT I LINES) ARE VERTICAL.

NJJJKJJJJJJJJNJJJJJJJJJJJJ44hfAIJNJJJJJJJJJJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJN I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I B I 8 I NJJJNJJJJJJJBBBJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJBBBJJJJJJJJJJJJN I I B I B I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I~ I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I NJJJNJJJJJJJJNJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJN I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I' I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I KJJJNJJJJJJJJNJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJN

I I

I I

I I

I I

I I

I I

I I

I I

I JJ JJJJJJJJJJJN I A I A I A I A I A I A I A I A I A I A I A I A I A I A I A I A I A I A J JJJJJJJJJJJJJJJJJJJJJJJJJJJAJJJJJJJJJJJJJN I A I A I A I A I A A

I A I A I A I A I A I A A

I A I A I A I A JJ JJJJJJJJJJJN I I I I I I I I I I I I I I I I I I I I

I I I I I I I '. I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I NJJJNJJJJJJJJNJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJN I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I ' I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I ~

I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I NJJJNJJJJJJJJNJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJN I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I S I B I NJJJNJJJJJJJSBBJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJBSBJJJJJJJJJJJJN I I S I 8 I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I "I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I NJJJNJJJJJJJJNJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJN

PROaRAN: NE035 RASEPLATE SIR+- S9601 0110 AAN 8014 DATE- 92.09-25 REI.EASE 11 KOS/VE TINE: 10:53:07 PAGE t 13 ttttttttttttttttttttttttttttttttttttttttttttt

~ SEQ IN SOLUT ION P RASE LOAD CASE NO:

ttttttttttttttttttttttttttttttttttttttttttttt TITLE: FILEKAHEtKKPSP24 TYPE F-2 EHSED PLATE (8XI) CASE 1 CS.N.4403 LOAD CASE KO.

(T 0 P I' N V A L U E S)

D I SPLACEHE NTS KODE 0 I SPL. KCOE DISPL.

62 .685353E-02 5 -.191326E-02 63 .620190E-02 16 -. 147032E.02 61 .609194E.02 4 -.129075E.02 51 .550537E-02 6 -.114674E-02 60 .526031E-02 15 .978655E-03 52 .506041E-02 17 ..691929E-03 50 .C72195E-02 27 -.566160E-03 64 .397056E.02 3 -.477061E-03 49 .395085 E-02 11 -.394188E-03 59 .394491E-02 7 -.361038E 03 QUADR I LATERAL PLATE PRINCIPAL STRESSES ELENENTS + 2 FACE ELEN SI QW ELEH Sl QW ELEH SI QIA ELBI SIQW 4 -3846. 14 -3801. C7 3647. 37 3359.

24 -2917. 27 2489. 17 2097. 48 1944.

38 1933. 28 1837.

E L E N E N T S - 2 FACE EL EN S I QW ELEN S I QW ELEN Sl QW ELEN Sl QW 47 -3954. 37 -3379. 14 3351. 4 3057.

24 2841. 27 -2190. 48 2049. 3 -2022.

13 -1952. 38 -1834.

CON CR ET E LOAD S K(OE 2-PRESS NODE 2-PRESS IKSE 2-PRESS NCOE 2-PRESS 5 -531. 16 -408. 4 -358. 6 -318.

15 -272 17 -192. 27 -157. 11 -109.

26 -99. 22 -94.

PROGRANs NE035 BASEPLATE SNN: $ 9601 0110 AAH 8014 DATE: 92-09-25 RELEASE 11 NOS/VE 1.5.3 L765 TINE! 10:54:32 PAGE 14 BOLT LOADS NODE X SHEAR Y-SHEAR SRSS TENSION 24 323. -156. 359. 21.

28 129. -234. 268. 194.

32 '177. -181. 253. 184.

46 324. -102. 340. 628.

50 128. -46. 136. 4155.

54 -178. -75. 193. 1111.

BOLT INTERACTION EOUAT ION EQUATION>((TENSION/TALLN)~ 1.000+(SHEAR/SALL%)~~ 1.000))~ 1.000 NODE TENSION SHEAR TENSION SHEAR INTERACT SAFETY ALLOM ALLOJ RATIO RATIO RATIO FACTOR 24 5990. 3470. .003 .103 .107 9.360 5990. 3470. .032 .077 .109 9.138 32 5990. 3470. .031 .073 .104 9.642 46 5990. 3470. .105 .098 .203 4.930 5990. 3470. .694 .039 .733 1.364 si 5990. 3470. .185 .056 .24'I 4.148 tH01111ilt1101411110001I011111000I000110IIII 0 E N D LOAD CASE

PROGRAN: NE035 QASEPLATE SINAI: S9601 0110 AAN 8014 DATE: 92 09-25 RELEASE 11 NOS/VE 1.5.3 L765 TlNE: 10:54:32 PAGE: 15 tttttttttttlttttttttttttttttttttttttttttttttt SEGlN SOLUT lON PHASE

~ LOAD CASE NO ttttttttttttttttttttttttttttttttttttttttt*tt' TlTLE: FlLENANEtHNPBP24 TYPE F 2 ENSED PLATE (F1) CASE 1 CS N.4403 LOAD CASE NO.

(T 0 P T E N V A L U E S)

D l S P L A C E N E N T S NODE DISPL. HQ)E D lSPL ~

5 .702977E 02 62 -.173157E-02 16 .656655E-02 63 -.109723E 02

.643646E.02 61 .106081E.02 6 .621388E-02 51 -.568531E.03 15 .602761E.02 56 -.379196E-03 17 .574981E.02 64 -.365284E.03 27 .564397E-02 52 -.319490E.03 7 .539708E.02 60 -.259792E.03 26 .522830E.02 45 -.254871 E.03 18 +494210E.02 34 -.149459E.03 QUADR l LATERAL PLATE PR 1NCI PAL STRESSES ELENENTS + Z FACE ELEN Sl QIA ELEN Sl QIA ELEN SlGHA ELEN SlGNA 4 4606. 14 4472. 24 3760. 47 -3124.

37 .2M8. 34 2430. 3 2330. 13 2204.

23 1902. 12 -1691.

E L E N E N T S - 2 FACE ELBI SlQIA ELHI SlQIA ELBI SlQIA ELEN SlGNA 14 -3800. 4 -3682. 24 -3512. 47 3356.

37 2755. 34 -2742. 12 1975. 13 -1964.

3 -1941. 23 -1906 CONCRETE LOADS NCOE 2 PRESS NODE Z PRESS N(mE Z PRESS IIODE Z-PRESS 62 .481 ~ 63 .305. 61 -295. 51 -158.

56 -105. 64 -101. 52 -89. 60 -72.

45 .71. 34 .41.

PROGRAN: NE035 SASEPLATE SM: S9601 0110 AAH 8014 DATE: 92-09.25 RELEASE 11 NOS~ 1.5.3 L765 TIKE: 10:55:09 PAGE:

SOLT LOADS 0 \ 0 Ng)E )( SHEAR T SHEAR SRSS TENSION 24 -323. 156. 359. 1153+

28 -129. 234. 268. 4241.

32 177 181. 253. &23.

46 -324. 102. 340. 208.

50 -128. 46. 136. 206.

54 178. 75. 193. 8.

eOL T I N T ERIC T ION EauA T ION E(NIATION ((TENSION/TALLOJ)tt 1.000+(SHEAR/SALLOM) 1.000))*t 1.000 K(mE TENS IOI SHEAR TENSION SHEAR INTERACT SAFETT ALLOM ALLOM RATIO RAT10 RAT10 FACTOR 24 5990. 3470. .193 .103 3.379 28 5990. 3470. .708 .077 1.274 32 5990. 3470. .104 ~ 073 77 5.654 46 5990. 3470. .035 .098 .133 7.534 5990. 3470. .034 .039 .074 13.584 si 5990. 3470. .001 .056 .057 17.567 ttttttltttttttttttttttttttttttttttttttttttttt

  • E N D LOAD CASE 2

~ tttttttttttttttttttttttttttttttttttttttttttt

~ tttttttttttttttttttttttttt*ttttttttttttttttt END POSTPROCESS I NG ttttttttttttttttttttttttttttttttttttttttttttt

NE035/11 PATE 9P 09 P5 CALC ID PAGE 1 ATTACHMENT PROJECT t IIIII~ IIIII~ IIIt ~ IIIIt IIIIIIII AAE gF

/S' JOB NO.

CALC NO. C-C H- ++DZ SHT NO.

PREPARED BY DATE CHECKED BY DATE

~ II~ ~ t t I*I*IIIIIIIIIIII~ III~ IIII~ ~

EEEEEEEEE 0000000 33333333 55555555 EE E 00 00 33 55 EE 00 00 33 55 EEEE 00 00 3333333 55555555 EE 00 00 33 55 EE E 00 00 33 55 EEEEEEEEE 0000000 33333333 55555555 VERS I ON LEASED AUGUST 1989 USER NANUAL VERS ION 8 THEORET ICAL NANUAL VERSION: 8 VER IF ICATION NANUAL VERSION: 10 IIII~ I*I*~ IIIII*IIIIIII I IN CASE OF PROBLENS NITH NE035, COHTACT THE

  • BASEPLATE USER REPRESENTATIVES:

NANE LOCATIOH EXTENSION I I

I>> ~ IIIIIt I*I~ II~ IIt IIIII*III IIIIIIII~ IIII~ *II**IIIIIIII~ IIII COPYRIGHT 1984,1987 BECHTEL POMER CORP. ALL RIGHTS RESERVED.

111111*1 *I ~ 111 ~ ~ 111 ~ I I t**1*111111111 ~ 11

HE035/11 DATE 92 09 25 PAGE 2

~~gff+ffg~gg*ggfftttltt111lt**01101ttlteyyygg~fQ*ffyttt0t1t0t0f 00 Ifttt0t00 0l1t PREPROCESSOR lHPUT DATA CARDS

~ ii*1014111111*1fO~~iiiii~yiiitiOiOititOOt040i*iiitkti11ii01t *****

CARD 1 6 7 8 HO 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 3 F1LENANEQHNPBP25 TYPE F-2 EHBED PLATE (8X1) CASE 2 CS-H-4403 2 OUT ~ gg1/

3 CON g ~ g ~ 4000/

4 PLA 5,78,18,1,29/

5 APR 1,6,6,.25,.25/

6 BPR gt1g8.8E5,1.25E6,5987,8100/

7 BOL 2,2, 1, 1.5,3/

8 BOL 2,6,1,1.5,15/

9 BOL 4,2, 1,6.5,3/

10 BOL 4,6,1,6.5,15/

11 EHD/

12 TUB 3,4,1,3.5,9/

13 EHD/

14 POl 3,4/

15 LOA ~ ~ 1 ~ 550'94e990 ~ 19120r 31056e12512/

16 LOA 2,.550,794,990,.19120,31056, -12512/

17 END/

18 END OF JOB

~~* END OF INPUT DATA *~~

HE035/11 PATE 92.09-25 PAGE 3

    • >>**i>>i>>i>>>>>>>>>>>>>>ti*>>1>>>>>>i>>>>>>>>>>>>i>>11>>>>1>>i>>iii>>11>>ii>>*>>it>>1>>ii>>>>>>t>>>>i*i>>>>i>>i>>it

>> PREPROCESSOR INPUT DATA CARDS >>

1*11>>>>>>>>>>it>>11*>>1>>111>>i>>*i>>i*ii**1111>>>>1>>>>1>>>>>>>>>>i>>i>>>>>>1>>i>>i>>i>>i>>i>>i>>i>>i>>i>>>>i>>i>>i>>i>>i>>

CARD 1 2 3 4 5 6 7 8 NO 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 3 FlLEHAHE>>HNPBP25 TYPE F-2 EHBED PLATE (BX1) CASE 2 CS-H-4403 2 OUT 0* 0 p>>

3 CON 0>> 0 0* 0.000>> 4000.000>> 0.000>> 0.000>> 0.000>> 0.000 4 PLA 5* 7 0>> 8.000* 18.000>> 1.000>> 29.000* 0.000>> 0.000 5 APR 0>> 0 1* 6 000>> 6 000>> 250>> 250 0.000* 0.000 6 BPR 0>> 0 1>> .880E+06>> .125E+07 .599E+04* .810E+04>> 0.0>> 0.0 7 BOL 2. 2 1* 1.500>> 3.000* 0.000>> 0.000* 0.000* 0.000 8 BOL 2>> 6 1>> 1 500>> 15 000>> 0.000>> 0 000* 0.000>> 0.000 9 BOL 4* 2 6.500. 3.000>> 0.000>> 0.000. 0.000>> 0.000 10 BOL 4>> 6 1>> 6 500>> 15 000>> 0 000>> 0 000>> 0.000>> 0.000 11 END 12 TUB 3* 4 1>> 3.500>> 9.000>> 0.000>> 0.000>>

13 END 14 Ppl 3>> 4 p>> p ppp>> p ppp>> p ppp>> p ppp>> p ppp>>

15 LOA 0>> 0 1>> 550.0>> .794.0>> 990.0>> 19120.0>> .31056.0>> 12512.0 16 LOA 0>> 0 2>> -550.0* 794.0>> 990.0>> -19120.0>> 31056.0>> -12512.0 17 END 18 EHD OF JOB

    • >> EHD OF 1HPUT DATA DECK **i

HE035/11 DATE 92-09-25 PAGE 4 tttttttttttttttttttt'ttttttttttttttttttttt*ttttttttt*ttttttttttttttttttttt*ttttt FILENAHE HNPBP25 TYPE F-2 EHBED PLATE (BX1) CASE 2 CS-H 4403 t tttttttttttttttttttttttttttttttttt'tt'tttttttttttttttt*tttt*ttttttttttttttttttttttttltt INPUT PARAHETERS PLATE THICKNESS ......... 1.000 PLATE X-DIHEHSION ....... 8.000 Y-DIHENSION 18.000 NODULUS OF ELASTICITY ... .290E+08 CONCRETE NODULUS . " .... ~ .360E+07 CONC. COND STRENGTH 4000.0 BOLT LOCATIONS BOLT I J NODE X-COORD. Y.COORD.

1 2 2 9 1.500 3.000 2 2 6 13 1.500 15.000 3 4 2 23 6.500 3.000 4 4 6 27 6.500 15.000 BOLT PROPERTIES BOLT STIFFNESS (LB/IK.) ALLOMABLE FORCE (LB)

TENSION SHEAR TENSION SHEAR

.880Ei06 .125E+07 5987. 8100.

.880E+06 .125E+07 5987. 8100.

.880E+06 .125E+07 5987. 8100.

.880E+06 .125E+07 5987. 8100.

ME035/11 BATE 92-09.25 PAGE 5 Itttttti**tttttt*ttttttttttttttttittti*tttiiiittt*ttit**tttttttttttttttttitttit FILENAMEtHHPBP25 TYPE F-2 EMBED PLATE (BX1) CASE 2 CS H-4403

~ tttttttttttttttttttttittttiitttttttttttttttltttttttt*tttttt*t*tttttttt'tttttttttttttt ATTACHMENT DATA ATTACHMENT NUMBER 1 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ TUB PROPERTY NUMBER .... 1 0 DIMENSION . ~ .. ~ 6.000 I LINE NUMBER ~ ..... 3 8 OIMENSIOH ..... 6.000 J LINE NUMBER ...... 4 HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 X.COOROINATE ....... 3.500 THICKNESS (71) " .250 Y COORDIHATE ....... 9.000 THICKNESS (72) " .250 ORIENTATIOH ANGLE .. 0.0

HE035/11 DATE 92-09-25 PAGE 6 1111t**ttttttttttttt'tt't'tt' 't'tt'

'tttttttt*ttttttttttttt*tttt'ttttttt*ttttttttttt 1

FILENAME=NMPBP25 TYPE F-2 EMBED PLATE (BXI) CASE 2 CS H-4403 *

~ tttttt*tttttttttttttttttttttttt***tttttttttttttttttttttttttttttttttttttttt*ttttttttt LOADING CONDITIONS LOADIMG CASE MO. ~ 1 LOADINGS APPLIED AT NODE ~ 36 FORCE FX  % 550.00 FORCE FY i -794.00 FORCE FZ ~ 990.00 HOHEMT HX ~ 19120.00 HOHEMT HY ~ -31056.00 HOHEMT HZ > 12512 F 00 LOADING CASE NO. ~ 2 LOADINGS APPLIED AT MODE i 36 FORCE FX > -550.00 FORCE FY t 794.00 FORCE FZ i 990.00 HCHENT HX ~ .19120.00 HOHENT HY > 31056.00 HOHENT HZ > -12512.00

HE035/11 DATE 92-09.25 PAGE 7 itllti1I11ilttttt1tt1PiltlOiiOililiOOllg*yyy*g*ytt11POOOlii1tttt10iitti1111111t FlLENAHEsNNPBP25 TYPE F-2 EHBED PLATE (BX1) CASE 2 CS-N 4403 *

~ ttt00114ittS*1*ttitttt1tt1t*it1iit' '+' '++Otltlt110*ti10t00100t10$ *tti11*4111*tP1%14111 BASEPLATE CONNECTlVlTY ELEHENT KOOE ELEHEN'T NODE NO. JA JB JC JD KO. JA JB JC JD 1 1 8 9 2 2 2 9 10 3 3 3 10 11 4 4 4 11 12 5 5 5 12 13 6 6 6 13 14 7 7 8 15 16 9 8 9 16 17 10 9 10 17 18 11 10 11 18 19 12 11 12 19 20 13 12 13 20 21 14 13 15 22 23 16 14 16 23 24 17 15 17 24 25 18" 16 18 25 26 19 17 19 26 27 20 18 20 27 28 21 19 22 29 30 23 20 23 30 31 24 21 24 31 32 25 22 '5 32 33 26 23 26 33 34 27 24 27 34 35 28

HE035/11 OATE 92-09 25 PAQE 8

~ ttttttttttt*tttttttttttttttttttt*tttttttttttt**t*ttttttttttttt*tttttttttttttt t

FILEHAHEtHNPBP25 TYPE F-2 EMBED PLATE (8X1) CASE 2 CS.H-4403

~ tttttttttttttttlttt1*ttltl1tttttt1t1ttttttt1ttttttttt1ttttttttt1ttttttttttttttttt1**

NCOAL COORDINATES I J FRAME X Y 2 LIME LINE NOOE COORDINATE COORDINATE COORDINATE 1 0.000 0.000 0.000 2 0 ~ 000 3.000 0.000 3 0.000 6.000 0.000 4 0.000 9.000 0.000 5 0.000 12.000 0.000 6 0.000 15.000 0.000 7 0.000 18.000 0.000 8 1.500 0.000 0.000 9 1.500 3.000 0.000 10 .500 6.000 0.000 11 .500 9.000 0.000 12 .500 12 F 000 0 F 000 13 1.500 15.000 0.000 14 1.500 18.000 0.000 15 3.500 0.000 0.000 16 3.500 3.000 0.000 3 17 3.500 6.000 0.000 3 18 3.500 9.000 0.000 3 19 3.500 12.000 0.000 3 20 3.500 15.000 0.000 3 21 3 ~ 500 18.000 0.000 4 22 6.500 0.000 0.000 4' 23 6.500 3.000 0.000 24 6.500 6.000 0.000 25 6.500 9.000 0.000 4 26 6.500 12.000 0.000 27 6.500 15.000 0.000 4 28 6.500 18.000 0.000 5 29 8.000 0.000 0.000 5 30 8.000 3.000 0.000 5 31 8.000 6.000 0.000 5 32 8.000 9.000 0.000 5 33 8.000 12.000 0.000 5 34 8.000 15.000 0.000 5 35 8.000 18.000 0.000 NODES AT APPL I CAT IOH OF LOAOS 3 4(OFFSE T) 36 3.500 9.000 F 500

HE035/11 DATE 92-09-25 PAGE

~ 1t*tttlttkttlt1tltll41IPIII1111110010layyyyygyygyPtt01lt0011tttt100110ty+)jggf FILEHAKEsKHPBP25 TYPE F 2 EHBEO PLATE (BX1) CASE 2 CS-K-4403

+'+I**000tl1tk*tt000**tttt*OP10tttlttt+ ~ '+1ltf1100tktttOOtttk*1ftt001tllf'tlatttttltttel CONCRETE STIFFNESS DATA NODE EFFECTIVE CONCRETE NODE EFFECTIVE COHCRETE AREA STIFFNESS AREA STIFFNESS 1 1.125 .380E+06 2 1.875 .633E+06 3 1.125 .380E+06 .750 .253E+06 5 1.125 .380E+06 6 1.875 ~ 633E+06 7 1.125 .380E+06 8 2.625 .887E+06 9 5.250 ~ 177E+07 10 5.250 .177E+07 11 5.250 .177E+07 12 5.250 .177E+07 13 .5.250 .177E+07 14 2.625 .887E+06 15 3.750 .127E+07 16 7.875 .266E+07 17 8.625 .291E+07 18 9.000 .304E+07

'19 8.625 .291E+07 20 7.875 .266E+07 21 3.750 . 127E+07 . 22 3.375 .114E+07 23 6.750 .228E+07 24 6.750 .228E+07 25 6.750 .228E+07 26 6.750 .228E+07 6.750 '.228E+07 28 3.375 .114E+07 1.125 .380E+06 30 2.250 .760E+06 2.250 .760E+06 32 2.250 .760E+06 33 2.250 .760E+06 34 2.250 .760E+06 35 1.125 .380E+06 1

SUHMATIOH OF EFFECTIVE AREAS m 144.000 PLATE AREA ~ 144.000 TOTAL CONCRETE STIFFNESS > .486E+08

~** INPUT DATA PROCESSING CONPLETE. ~~~

NE035/11 DATE 92-09 25 PAGE 10 R PLOT PI.AH VIEM OF THE BASEPLATE, MHERE ANIS (CONSTANT J LINES) ARE HORIZONTAL~ AND THE T ANIS (CONSTANT I LINES) ARE VERTICAL~

NJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJH I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I 8 I B I NJJJJJJJJJJJBBBJJJJJJJJJJJJJJJJJJHJJJJJJJJJJJJJJJJJJJJJJJJJJJBBBJJJJJJJJJJJJH I 8 I I I I I I I I I- I I I I I I I I I I

HJJJ JJJJJJJJJJJJJH I A I A I A I A I A I A I A I A A

I A I A I A I A I

I I A HJJJ JJJJJJJJJJJJJJJJJJJJJJJJJJJJAJJJJJJJJJJJJJH

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

PROGRAH: KE035 BASEPLATE SNUH: S9601 0110 AAN 8015 DATE: 92.09-25 RELEASE 11 NOS/VE 1 ',3 L765 TIKE: 10:55:44 PAGE: 11 01 11 1PP1011000tt10*f tt+*yyygyyyyyyy*jtPlii1tl

~ BEGIN SOLUT ION PHASE

  • LOAD CASE NO: 1

~ yygP1*iiikii11t1*00t01111t010i1i11i00i++++*+

FILENAKE~NNPBP25 TYPE F-2 EHBED PLATE (BX1) CASE 2 CS N 4403 LOAD CASE NO, 1 (T 0 P T E N V A L U E S)

D I S P L A C E H E N T S NCOE DISPL. NODE D ISPL.

33 .620874E-02 3 -.135401E.02 32 .582501E 02 2 -.959458E-03 31 .527734E-02 10 .941597E.03 26 .500365E.02 4 .897977E-03 25 .454502E-02 7 ..590503E.03 34 .454058E 02 1 -.530048E-03 24 .408283E.02 11 .477146E-03 27 .357956E 02 5 .429463E.03 30 .349911E.02 6 ..243172E-03 23 .258474E-02 9 -.137765E-03 1 U A 0 R I L A T E R A L PLATE PRINCIPAL STRESSES ELEHENTS + Z FACE ELEH SIGNA ELEH S I GHA ELEH SIGNA ELEH SIGHA 17 4741. 23 4312. 11 3014. 2 -2867.

14 2366. 20 2342. 5 2062. 19 .1918.

24 .1889. 8 -1546.

ELEHENTS - 2 FACE ELEH Sl GHA ELEH Sl GHA ELEH S IGHA ELEH SIGMA 17 -4605. 23 .4443. 14 .2683. 11 -2675.

2 2661. 20 -2198. 24 1899. 19 1890.

8 1701. 5 -1602.

CONCRETE LOADS NODE 2 PRESS NODE Z PRESS NODE 2-PRESS NODE Z-PRESS 3 -457. 2 .324. 10 -317. 4 -303.

7 -199. 11 -161. 9 .46. 8 -44.

14 -11. 12 .6.

PROGRAN: NE035 BASEPLATE SNUN: $9601 0110 AAH 8015 DATE: 92 09-25 RELEASE 11 NOS/VE 1.5,3 L765 TINE: 10:56:02 PAGE: 12 BOL*-T LOADS NODE X.SHEAR Y-SHEAR SRSS TENSION 9

13 594.

-319,

-391

.396.

'11. 508.

0.

588.

23 593. .7. 593. 2275.

27 -319. 0. 319. 3150.

BOLT INTERACT ION EOUAT ION EQUATIONt((TENSION/TALLOM)tt 1.000+(SHEAR/SALLOM)tt 1.000))tt F 000 NCOE TENSION SHEAR TENSION SHEAR INTERACT SAFETY ALLOM ALLOll RATIO RATIO RATIO FACTOR 9 5990. 8100. .001 .088 .089 11.263 13 5990. 8100 ~ .098 .063 .161 6.211 23 5990. 8100..380 .0?3 .453 2.208 27 5990. 8100..526 .039 .565 1.769 ttitttitttt**ttttttttttttttittt*tttitttttittt t E N D L 0 A 0 CASE

~ ttttttttittttttttttitttttttttt*iittttttttttt 1

PROGRAH: HE035 BASEPLATE SMUH: $ 9601 0110 AAH 8015 DATE: 92-09-25 RELEASE 11 MOS/VE 1.5.3 L765 TIHE: 10:56:02 PAGE: 13 111000110111111100100000000011111*00011100010 BEGIN SOLUT ION PHASE LOAD CASE MO:

  • 10000*10101001001*00000*0*0001100000000000000 TITLE~ FII.EHAHE0HHPBP25 TYPE F.2 EHBED PLATE (SX1) CASE 2 CS-H-4403 LOAD CASE HO. 2 (T 0 P T E M V A L U E S) 0 I SPLACEHE HTS NODE DISPL. NODE DISPL.

3 .645676E-02 33 .1C7581E-02 10 .600036E 02 32 .109617E-02 4 ~ 594732E-02 34 .905492E-03 11 .549689E-02 29 -.588216E-03 5 .543703E.02 31 -.579969E-03 12 .498749E.02 35 ..430385E.03 2 .492961E-02 26 -.368S69E-03 9 .377422E.02 30 -.305957E-03 6 .371726E-02 27 -.203192E-03 17 .330949E 02 28 ..117708E-03 Q U A 0 R I L A T E R A L PLATE PRINCIPAL STRESSES ELEHENTS + 2 FACE ELEH SIGMA ELEH S I GHA ELEH S IGHA ELEH SIGMA 2 SC25. 8 4462. 1C 3132. 5 2731.

23 -2643. 17 -2201. 1 -2196. 11 2178.

6 .2101 ~ 22 -1850.

ELEHENTS - 2 FACE ELEH S IGHA ELEH SIGHA ELEH SIGNA ELEH SIGHA 2 .4903. S .4399. 14 .343C. 5 .3038.

23 2621. 11 -2226. 1 2196. 6 2088.

17 2006. 20 .1828.

C 0 N C R E T E LOAD S NODE Z-PRESS NODE 2-PRESS NCOE Z.PRESS NXE Z.PRESS 33 -498. 32 -370. 34 .306. 29 -199.

31 -196. 35 -145. 26 -125. 30 -103.

27 -69. 28 .40.

PROGRAN: NE035 BASEPLATE SlQI: S9601 0110 AAH 8015 DATE: 92-09-25 RELEASE 11 NOS/VE 1.5.3 I.765 TIKE: 10:56:12 PAGE: 14 BOLT LOADS NODE X-SHEAR Y-SHEAR SRSS TENSION 9 -594, -

391. 711. 3321.

13 319. 396. 508. 2327.

23 -593. 7. 593. 524.

27 319. 0. 319. 0.

BOLT INTERACT ION EOUAT ION EOUATIONq((TENSION/TALLOllee 1 000~(SHEAR/SALLN)*e 1 000lloo 1 ~ 000 NODE TENSION SHEAR TENSION SHEAR INTERACT SAFETY ALLOI ALLON RATIO RATIO RAT!0 FACTOR 9 5990. 8100. .554 .088 .642 1.557 13 5990. 8100. .388 .063 .451 2.216 23 5990. 8100..087 .073 .161 6.224 27 5990. 8100..001 .039 .040 24.790 411141PIOOPIPOOIIIP11100000i0100000100I100111

  • E N D LOAD CASE

~ IOIOIP11011011t1111111111111**1111*11111**11 11144I110110*000**100001110100*ttOP1010110110 E N D P 0 S T P R 0 C E S S I N 0 10100itPOOOI j0104PO jPP010000000001010410140it

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INTERDISCIPLZNE REVIEW REQUEST (ZRR)

IRR g' e leal/ Plant ~H Too Unit/Subunit V U Fromm Unit/Subunit u d ov d c v M d Details of Review Request: REFERENCE - PCR-6547, DELETION OF RELIEF VALVES AND ADDITION OF ORIFICES AND STRAZNERS ~

ATTACHED ARE THE SIGNED OFF SUPPORT LOAD SHEETS FOR PCR-6547 AS WE KNOW IT AS OF 12:00 P.M.

ON SEPTEMBER 25,1992. PLEASE USE THESE LOADS IN YOUR SUPPORT DESIGNS AND EVALUATIONS FOR THE ABOVE MENTIONED PCR. THESE LOADS ARE AS GOOD AS THE INFORMATION USED TO DEVELOP THEM SINCE NO APPROVED DRAWINGS HAVE BEEN RECEIVED AS OF THIS WRZTZNG.

IF THERE ARE ANY QUESTIONS PLEASE CONTACT JOHN HOPKINS AT X-6734 ~

sponse Required By:tt e Responsible Supervisor/Dat~n thorized Man<<hours e

Charge Number MAPS Project No.: C -6 47 Phase: Act ivity a Response/Justifications Attachments (list):

Responsible Supervisor/Date Actual Man-hours expended Distribution:

NED Guideline No. E-24 Revision 4 (EG66f re

I TEM QTY PART 0 NO. NO. STATUS DE SCRIP TION TS ~ C

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STRESS CA'. - z ~ I- 4 CAROLINA POWER 4 LIGHT COMPANY SI PPQRT CALC. C NUCLEAR ENGINEERING DEPARTMENT PLANT: HARRIS NUCLEAR PROJECT - UNIT I ISCALE.'i

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Reason for Change:

A'EcPuE$ 7ED cFfWd'2 o8 /72m / Ewe 7s dxgx >a ro 7S dad~'z. Bury n WcK r'Arlr&/7d~-

Justification for Change Approval:

Minor Change (i.e., editorial, .reference dimension, etc.). Supplementary Calculations are not attached. ~

Other (provide basis, attach supplementary calculations) su/5 T~7u7/o~ ~~ HccEP78/~ 8E<rku'SE 7 S 4 X4 8 <i k4$

Pr< m SZCrr~nJ PA'oP&'re recur 75 4XNX ->8 DPE*

lg Signatures indicate design verification has been performed in accordance with NED Procedure 3.3. This form serves as the design verification record.

OTY PART 0 DE SCRIP TION 40 NO. STATUS

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STRESS Ca C. - >- ~ I-A CAROLINA POWER & LIGHT COMPANY S '>PORT CALC. < NUCLEAR ENGINEERING DEPARTMENT

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QUALITY LEVEL:

ShF&rY ~~~T59 SE'ISgIC CAROLINA POWER 4 LIGHT COMPANY NUCLEAR ENGINEERING DEPARTMENT PuNT:446?I2IQ NLIGL&62 ~51 SCALE: N~

'CHB1VII~L3 V&I JET &'TI2Ol ME, +Wl Z~ma WuxILg,aV @i~. m.2~'-o eT~IN&a. +ueeaaT RPyI OA r OESCRrPTION WN(OSN(CH OV jOPE[OPPE ~~'NOA-3-85&-I- C5 0-WOCn REVWNII S':, '2 o 2

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Mod Number CR 454 7 FR Number JA Calculation Affected <-~S- h'- ~OCn Drawing Affected ~> +-~>d Reason for Change:

>U+Pd+7 ~FX4~E8 7-~ SrW+Zn/ PEur " S< CZamruZ Un78 Wfn// Fdd~ PM/RC ~ 4'~HA'IA'EA Justification for Change Approval:

Minor Change (i.e., editor:al, reference dimension, etc.). Supplementary Calculations are not attached.

Other (provide basis, attach supplementary calculations)

CASES 8-Tach'Eh DPE*

+Signatures indicate design verification has been performed in accordance with NED Procedure 3.3. This form serves as the design verification record.

CALC~TION NO.

PAGE /

REV /

LIST OF EFFECTIVE PAGES PAGE REV PAGE REV PAGE REV ATTACHMENTS

ATTACHMEÃT D CALCULATION NO. 4-CS'-/Y-~Oh PAGE II REV /

TABLE OF CONTENTS Page No.

List of Effective Pages Table of Contents Pu rp o s e ~ ~ ~ ~ ~

List of References Body of Calculation Conclusions Attachments Page(s)

A %7 S'7Rubc F/oem~

8 WzoSS- PZ~~~~ 2r /4 c kg + +c-ldll /

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'f FORM No. 74055 REV 10/$ 5 Ccgyute4 bv: Date: Calculation ID:

-Z5-gZ- CAROLINA POSER 6 LIGHT COMPANY C-cs-8 -Wo4 Date: Rev.

9-z S .9z. Pg. I CALCULATION SHEET Ter /PID No.: File:

Pro)ect

Title:

Calculation

Title:

Status: Prelim. Q Final ~ Void PuRPoSE'0 PRD V/c?)E'A'n/CHOR 5" U/ j'OR 7 2)8S/4/U A 7 7rPCP'2'D 7o H 5'7+9/AE4 85'8ocuN W'&N 7 3W4'. /3 4 + - o P4 8++

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PRE I//os' uFPo<T 9-2-Z34,- 1-CS'-8'- +506 EE'lr. $ 0- Pl t

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CAROZ,ZgA PO%ER 6 Z,Z~ CQXPMPL CALCULATIONNUMBERS HARRIS NUCLEAR PLANT 14 1-1A paVPQ) NUMIER PAGE PCR-6547 SUBJECT ORIGINATOR'S INIIIALS/DATE SI CHARGING PUMP ALTERNATE MINI-FLOW LINE/ RELIEF -23 l~

a;marco e!IIALS/DATE VALV~KEMOVEDt FLOW I ORIF CES AND STRAINERS ADDED IJTgi) ~

WITH LEAD BLANKETS.

Lnshsoc 0 Los% Wacs. C ~. ill-lA 19'- l 4o NODE PT ISO NO.

HANGER NO.

(bed SUPPORT SYSTEM CONDITION Fg r FS ling My u (FT-LBS)

(LBS) (LBS) (LBS) (FT LBS) (FT-LBS)

SI S SL EO -24.

DEADWE ZGHT -406.

50 M - Zlo S(o THERMAL I 7 ~ -45.

Z.Cs

83. 17. -25. -48.

THERMAL II E.

aTHERMAL Ih f PAD Cc TAD DBE SAM 3 Qg I lgR Bl OBE Inertia 84. 161. 100 ~ 54. 27 43

'51 300 EK Enh IO

'3

\ IQ DBE(Inertia) 136. 285. 173. 93. 47. 70 UPSET (+)

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'MERGENCY(+)

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FORM NO. 14055 I'~niited bv: Date: Calculation ID:

9-Zs'-PL CAROLINA POWER & LIGHT COMPANY C- cs-H-Dat,e:

9-2s -9~ Pg. of Rev.

CALCULATION SHEET Tar I PID No.: File:

Px'o)ect

Title:

Calculation

Title:

Status: Prelim. Q Final Uoid Q s'7Ru3g ~ogpu 2Z.4

'ogg.

3F//o JO/N7 Cuogg .

/ D e o o zo o 2 Z. ZO7 ZO j.W3

/2 14$ Zo 5 /0 Ze 4 R/<i4 C//VMS 7S 444X

+p

+8'Em.

Q3 5'Ck. 8Q

/S (0/ o~ o)

Hnr~~~ = 2~-~'~~ O/

c.o4pg ca py- ~

~.  ?

4L Z/3

/y = 8'3P /ooZ Fz= >Zg w=?+? (/?.3 = zygo/" ~ /h- ZZg (/Z 3 =

Wfz 3M'=

//y= >>~ 6~) = zest. 39/ Ca}=

4= sp+ (]~) = p/Zp ~ = >xi C'i?.>/= //oso

FORM NO. 15055 REV. 10/45 P.runner ~ hv: Date: Calculation ID:

9-zs'-)2 CAROLINA POWER & LIGHT CO~ANY Date: of Rev.

9 X5 0a.

~ Pg.

CALCULATION SHEET Tar/PID No.: File:

Pro)ect

Title:

Calculation

Title:

Status: Prel3m. Q Final ~ Void Q m~~e-~7r.< Cw~.

J7. 5 oo8" If Qy =, 0/+"

. 8// ( Y/@

75 4xp X ~8 C+zoo Sy = ~ CeO /SI

~. j(ao) F~ = 2C, 2/o js ~

z. z)

~ ro (<,ooo) PSf Co&SFRV.

/+5/ D/

'k'4 wA'y- hoR~Rc. 57/G5 = Ea. 4 w z4,2/o Ps/

04 t +0 + 8/+ /83/0 v q z z (sszs)'(~>s')

bVZrg. = +

m,WO

'~i /~c r -..g/ C//0

'1 W,ooo)

+4 so/I. Bo PfFE ($83/2. TP3o+)

/y= ~d<~ A/ W /oo F F>

= 2/Zoo Ps/ H 23s'F ar srvfovvv~ (sr~~oc Jr. +)

= oc g R>> = zo,zoo( ~Q= 4,zsg ps~

(3o,ooo) = /BiOOf3 PS)

(2+Zoo) = A,526) ps) & JT.

JVo TQ: ~U' 7EinP. b1/ rRu/1/~/O/J RZ8U4ZS F'gal /A/CH ZP'dO 8/5'74/f/4'8 H~A P' RI/~

>r

FORM NO. 7IOSS REV. 10/SS P~euetoR hVS Date:

5-Zs-9 Date:

CAROL~ PO~ & LXGBT COMPANY c-cs-z- ~c Calculation Q):

pg. of Rev.

CALCULATION SHEET Tat /PI& nO.: File:

Pro)ect

Title:

Calculation

Title:

Status: Prelim. Q Final Void Q CoAsERg w/qg. Ao/m~c, spazzy~ B J7; p = 7g~y Ps/' AS'2Q gs/

(/lo//'+ +A") '

/st (/'+$

- Bo+> Z.zz) Fs/

v z.>> <()ti) =

(.+ 2o) = ~oQ 7') p I la3s

( /.c) CJK

///Tz//Ao7/a// =

r~SZo (

(. Stoa gQ oK

< ~~ ~&~~xC~> rs oK 8'P'amW~Zon/ dF ~gg

+C/ OWNS FS Dud 7n Pldj'g//py

~<cd~ M os X/3~

+ g Pl~ oN e7-~

808'Lp 7o

~EJn. /, J7: / C~wgs;

/

F~ = rocz ~ &, - laaio Wy~ = 3/Zro

<~= ei+ n,= q~~a~

s =M J=ZZB

/s+ ass A)i <as+ izt c') gl

~ 4 z+ z88 j]'8

- >o/ (/oooo)

. /3" ~ lgy

FOAM No. 74055 AEV. 10/4S Comouted bv: Date: Calculation ID:

9-ZS-9 Date:

CAROLINA POWER & LIGHT COMPANY C-c's'- p-~b

'3 P-f 0>

~ Pg. of Rev.

CALCULATION SHEET Tar /PID No.: File:

Project

Title:

Calculation

Title:

Status: Prelim. Q Final Void Q wELh + PIPE ro Pw~

Jr. 3 zoW2s:

/

zan o

+z = Z5780 s = rag J

// /g

/g~ (/S~g bc?3/BQ

//5, 9

) ) + / (/Olg +8/+ ) 80+)(Z.ZS)

'7/. g )

.~o> P/s,oooo o TIIER cuELM eke oK dg cowWR/sD// i'// azoVE M/ C

FORM NO. 70055 REV. LO/05 Camnutad hv: Date: Calculation ID:

$ '-Z.5-5'2- CAROLINA POWER & LIGHT COMPANY C-c'z- A'-Mo(

Date:

e. ~s'9z. Pg. of Rev.

CALCULATION SHEET Tar /PID No.: File:

Pro)ect

Title:

Calculation

Title:

Status: Preliin. Q Final ~ Void Q

~Ur~QQ Km$ . 4 cbecK,

~d'8Q oo Q 3oO X' iVECSonl STub 7x'4'x /8 7'//PE'3+ C<c..= 44 )

CTVa)

Tree P-2

~E.A 8'~i i%4 83' I

'/oRT/l PdrFN V/ZMJ

&OOO /T/ Co O/CC+TC )

/lccoouaoTcoo Cou9ds'oR Tt;u/ //&co// cru/os c/rr//coo, (/E'F: S 2 Z. 8to 7.+P 2-O9. Z/ BOO. Z (ZS" Sauk Clo/OCulo Rb/OCT/OO/)

7+/f0~ I.z (Zg" grus z/olcuoc /aucr/o//)

23.30 J/ CZ Z3 9D EB. 4

/r///y. /c/lre sz~esz = 9z9o ps/ ~ .>s. (2c,oooo Psl)

Con/SE+Y.

sT un r~rzggcT/ok = . c /'+ ~ l. o ok . (. 4r, z, scow/8c~ )

R~F. HTrgCZ. 'B Zg. C Ma &Se

GTICES 3.3Q WHO'D/25. 1OA1.08. PAGE 1 CALC ID'TTACHMENT" P OF PAGE ttttttttttttttttttttttt100ttt ttttttttttttttttt tttt1111*111ttttttt*111 GEORGIA INSTITUTE Of TECINOLOGY INTEGRATED CCNPUTER ENGINEERING SYSTEH GTICES 3.3$ - GEORGIA TECN PRIÃERIETARY PRQNICT GENERATEO 88/02/16. 15.25.46.

DATE ~ 92/09/25.

GTI CES 3.3B'2/09/25. 10.41.08. PAGE 2.

NPUT>> L~>>PLo99999>>~e Bf

>>CALC NO NNP-PCR-6547>>

o4>> PDA>> LT~>> S1 oSDATA>> QA>>NC, P~-

>>PN~7>> FILQA%CS-N-4406>>

ttttt1 1 tttOOt111 t

'1 tt OOOO GTSTRUDL 1

1 11111 11 11 OOOOO OO 1

~ 11 OOOttttttl OOOOOO OOOOOO OOOOOO tt 11 AttN 1 tO OOOOOOOOOO 11 1

  • 11 **11 ~1 OOOOOO tt tt 11 1O t OOOOOOOOOO
  • tttttt tt 11 11 11 11 11 11 11 11 11 11*111 t ttttt 1 11 11 1111 1*111 111111 ~

SHIED BY AND PROPRIETARY TO THE GEORGIA TECH RESEARCH CORPORATIOI 1

RELEASE DATE VERSIOI Ne LEVEL CQtPLET ION NO.

KARCH 1988 8701CDC 0 2180/85 1

~ ttttttt11t11111111111 ttttttttttttttttttttttttttt 1111 ACTIVE UNITS - LENGTH INSIGHT ANGLE TEKPERATURE TIKE 1111 ASSWED TO BE INCH PING RADIAN FAHRENHEIT SECOND TYP SPA FRA UNIT IN LBS DEG JOI COO 1 00.00 00.00 00.00 S 2 00.00 20.00 00.00 3 3.207 20.00 1.403 4 12.965 20.00. 5.672 5 16.00 20.00 7.00 KEK INC 11 2 I 223 I 334 F445 KEK PROP 1 T 'TUBE80'TS6X6X6' T 'AISCPIPE'P4.00XS'EK PROP PRIS 2 4 AX 10 AY 10 AZ 10 IX 100 IY 100 IZ 100 SY 100 SZ 100 CONSTANTS E 29.00Eb ALL G 11.15E6 ALL DEN 0.283 ALL BUT 0.0 %N 2 4 BETA 0. ALL BUT 23.6 %N 1 POI 0.300 ALL S

CALC NO NNP-PCR-6547 GTICES 3.3Q 92/09/25. 10.41.14. PAGE 3.

cc<cccccccccccccccccccccc<<ccccccccco>>i>>>jj>M>>>i>>>>>>>>>>j>>>jj>j>>>>>

c ACTIVE UNITS MEME:LS LENGTN INCH c

TOTAL LENGTH, MEIGHT ANO VOLTE FOR SPECIFED HEHSERS LENGTH ~ 3.7464E+01 iKIGHT ~ 5.8992E+01 VOL Mf s 2.765SE+02 c

c ccc<ccccccccccccccccccccc<<cc<ccccc<~M ip>ijpixppphhpppp0phpM ipi jiiiiiiii PLOT DEVICE PRINTER LEN 6 PLOT PLANE XY PROJ JOI 1 2 5

ClLC NO NNP-PCR.6547 GT I CES 3.3$ 92/N/25. 10.41.16. PAGE 4 TIW: WWIZONTAL SCALE ~ 2 50OQ IN WITS PER IKCN VERTICAL SCALE ~ 2.6667 IN UNITS PER INCH a

T 5

X t

Ntttt+t )tttttttlttttttttttttttttttS PLOT I NTERPRETATIOI t SIDE SELOIGING TO INIE ELBKNT SIDE SELLING TO TlO OR NORE ELEMENTS REE JOINT LOCATIONS T JOINT LOCATIOIS R

CALC NO HNP.PCR.6547 GTICES 3.38 92/09/25. 10.41.16. PAGE 5 2 LOADS FOR JOINT 5 LOAD 1 JOI 5 LQA FOR X 213 LOAD 2 JOI 5 LOA FOR Y 839 LOAD 3 JOI 5 LOA FOR Z 540 LOAD 4 JOI 5 LOA NCN X 2964 LOAD 5 JOI 5 LOA NQI Y 2352 LOAD 6 JOI 5 LOA NN Z 7128 S

S EQ. 6 LOADS FOR JOINT 5 S

LOAD 7 JOI 5 LOA FOR X 383 LOAD 8 JOI 5 LOA FOR Y 1003 LOAD 9 JOI 5 LOA FOR Z 721 LOAD 10 JOI 5 LOA NOI X 3948 LOAD 11 JOI 5 LOA NCN Y 4092 L 12 LOA NCN 2 11052 D OA 13 DIR -Y ALL NEN STIFFNESS ANALYSIS TINE FOR CONSISTENCY CHECKS FOR 4 NENSERS .3l SECONDS TINE FOR BANDMIDTH REDUCTION ~ 00 SECONDS TINE TO GENERATE 4 ELENENT STIF. NATRICES .18 SECONDS TINE TO PROCESS 4 KENBER LOADS .12 SECONDS TINE TO ASSEKBLE THE STIFFNESS NATRIX .17 SECONDS TIKE TO PROCESS 5 JOINTS .04 SECONDS TINE TO SOLVE lllTH 2 PARTITIONS ,26 SECONDS TINE TO PROCESS 5 JOINT DISPLACEKENTS .12 SECONDS TIKE TO PROCESS 4 ELENENT DISTORTIOIS .36 SECONDS TIKE FOR STATICS CHECK .29 SECONDS S

CREATE PEAK LOAD 'EG. 2'RCN 1 2 3 4 5 6 13 CREATE PEAK LOAD 'EO. 6'RON 7 8 9 10 11 12 13 LOAD LIST 'EG. 2'EO.

DEC 1 6'UTPUT IXJTPUT SY NEN LIST FOR, REA ALL

CALC NO HNP-PCR-6547 Gl'ICES 3.38 92/09/25. 10.41.25. PAGE 6 ttIOOtt*01l RESULTS OF LATEST ANAL'YSEB

~ s et te te tsaa~atmot~ot PROBLEH PROJ>PCR TITI.E F ILENAHE<CS H 4406 ACTIVE WITS INCH LB DEG DEGF SEC HEHBER FORCES HEHBER LOADING JOINT /- FORCE---~~--~---~-~------//------ -------------HNENT- /

AXIAL SHEAR T SHEAR 2 TORSIONAL BENDING Y BENDING 2 1 EO. 2 1 898.0 411.4 580.1 12483.0 2S014.1 25975.6 2 852.3 411.4 580.1 12483.0 16411.9 17748.1 EO. 6 1 1062.0 639.6 814.0 15309.0 36475.2 37267.7'0987.1 2 1016.3 639.6 814.0 18309.0 23682.8 2 EQ. 2 2 411.6 852.3 580.1 5572.7 12483.0 22488.2 3 411.6 852.3 580.1 5572.7 10452.4 19504.8 EO. 6 2 639.9 1016.3 814.1 8047.0 18309.0 29341.7 3 639.9 1016.3 814.1 8047.0 15459.4 25784.2 EO. 2 3 411.6 852.3 580.1 5572.6 10452.4 19504.8 4 411.6 839.0 580.1 5572.6 4273.8 10497.9 EQ. 6 3 639.9 1016.3 514+1 8047.0 15459.4 25784.2 4 639.9 1003.0 814.1 8047.0 6788.9 15030.6 EQ. 2 4 411.6 839.0 580.1 5572.5 4273.5 10497.8 5 411.6 839.0 580.1 5572.8 2352.0 7718.4 EQ. 6 4 639.9 1003.0 814.1 8047.3 678S.9 15030.5 5 639.9 1003.0 814.1 8047.3 4092.0 11707.8 RESULTANT JOINT LOADS QPPOtTS JOINT LOADING /- - FORCE- -//--------------------HOHENT----------- ----" /

X FORCE Y FORCE 2 FORCE X IKNENT Y IDENT 2 HOHENT 0LISAL EQ. 2 213.0 898.0 540.0 19684.0 12483.0 24919.4 EQ, 6 3S3.0 1062.0 721.0 25436.0 18309.0 34867.4

CALC NO HO PCS 654l GTlCES 3.38 M09/25. 10.41.26. PAGE 7.

DEC 3 L lSP ALL

CALC NO HHP.PCR 6547 GTICES 3.38 92/09/25. 10.41.26. PAGE d 1111111 RESULTS OF LATEST ANALYSES1 tttttttttttttttttltttttttttt PROBLEK - PROJ1PCR TITLE - FILENAKECS H 4406 ACTIVE UNITS INCH LB DEG DEGF SEC RESUI.TANT JOINT DISPLACEKENTS SUPPORTS JOINT LOADING /------------- -- DISPLACEKENT--- -------------//--------------- ROTATION- --"-----------"/

X DISP, Y DISP. Z DISP. X ROT Y ROT ~ Z ROT.

GLOBAL EQo 2 .000 .000 .000 .000 .000 .000 EQ. 6 .000 .000 .000 .000 .000 .OOO LTANT JOINT DISPLACEKENTS FREE JOINTS JOINT LOADING / ---------------- DISPLACEKENT- ---------------//---------------- -ROTATION------------ --""/

X DISP Y DISP. Z DISP X ROT ~ Y ROT. Z ROT.

GLOBAL EQ. 2 .004 .000 .003 .014 .019 .022 EQ, 6 .006 .000 .004 .017 .027 .029 GLOBAL EQ. 2 .004 .002 .004 .015 .019 .023 EQ. 6 .006 .002 .005 .019 .028 .032 GLOBAL EQ. 2 .007 .010 .009 .031 .036 .055 EQ+ 6 .010 .014 .013 .040 .053 .075 GLOBAL EQ. 2 .005 .014 .011 .032 .036 .056 EQo 6 .011 .019 .016 .041 .053 .077

CALC NO HKP PCR 6547 GT lCES 3.3S %/09/25. 10.41.26. PACE 9.

DEC 1 1ST 'EQ. 2i LlST MAX STR ALL KEN SEC FRA KS 3 0.0 0.5 1.0

CALC HO HHP.PCR-6547 GTI CES 3.38 92/09/25. 10.41.26, PAGE 10

  • RESVLTS Of LATEST ANALYSES ttNfHOOAO~OOt~~

PROBLEN - PROJWPCR TITLE - FILEHANECS.H.4406 ACTIVE VHITS INCH LB DEG DEGF SEC INTERNAL IKÃBER RESVLTS NENSER NAXIIRSI STRESS

/ o STRESS eeoc@/

NOSER NAX HORNAL AT SECTION LOAD Nlk HORNAL AT SECTION LOAD 1 4005.7 .000 FR EQ. 2 -3783.3 000 FR EQ 2 390.9 .000 FR EQ. 2 -308.6 .000 FR EQ. 2 7106.9 .000 FR EQ. 2 -6920.2 .000 FR EQ. 2 188.9 .000 FR EQ. 2 -106.6 .000 FR EQ. 2

CALC NO INP PCS 6547 GT! CES 3.3S 92/00/25. 10.41.27. PAGE 11.

Sf 'EO. 4~

L STR ALL ION SEC Rtj IS 3 Oe0 0 5 1,0

I CALC NO NNP-PCR-6547 GT I CES 3,38 92/09/25. 10.41.28. PAGE 12 tttttt*ttttttttttttttttttttt RESULTS OF LATEST ANALYSES tttttttttttttttttttttttttttt PROBLEN - PROJtPCR TITLE - F1LENANEtCS H 4406 ACTIVE UNlTS lNCH LS DEG DEGF SEC INTERNAL NENSER RESULTS NENSER NAXIIRNI STRESS

/ oooo STRESS o/

MENSE R KAX NORNAL AT SECTTQI LOAD MIN KOOQL AT SECTlON LOAD 1 5450.9 ~ 000 FR EGo 6 o 5187.9 .000 FR EGo 6 540.5 ~ 000 FR EG 6 412.5 ~ 000 FR EO. 6 9801.1 .000 FR Eoo 6 o9510.7 .000 FR EQ. 6 282.2 000 FR EG. 6 o154.2 .000 FR EO. 6

CANC N HNP KR 647 GT1ggg g,38 92/09/2S 10A1.20. PAGE 1X

. CALC NO NNP.PCR.&547 QT ICES 3.3B 92/09/25. 10.41.28. PAGE 14 DYNANIC AREA 5QOQRY STATISTICS, INITIAL POX. SI2E 4091 POOL SIZE INCRENENT 4091 kWBER Of DATA POOL NOVES 207 DATA CON'ACTIONS 2 LOI RELEASED 0 HIGH RELEASED 0 L(M UNRELEASED 0 LOI NmULES 1 HI GN lkmULES 0 BLOtXS READ FROI DISK 87 BLOCKS READ FROI ECS 10 SEQUENTIAL READ-AHEADS INITIATED 0 BLOCKS READ AHEAD DISCARDED 0 ONE-PRU READ CNNT 0 ONE-PRLI lWITE CtXHIT 4 BLOCKS IBIITTEN TO DISK 0 ONE.IRWD KOATES IN ECS 0 BLOtXS REIBIITTEN TO ECS 0 NAXWBI IRBWER OF ALLOCATED 1JDRDS 271250 NAXIIRBI F IELD LENGTH ATTAINEO 366400 IRWBER OF CRASHES 49 IRWBER Of FIELD LENGTH !kCREASES 48 NOSER OF FIELD LENQTN DECREASES 5 R OF OVERFLON.ACTION CALLS 3

KE035/11 DATE 92-09-25 PAGE 1 1 ~ ~ t 0 ~ ~ ~ 0 ~ ~ 1 0 t0~ 0 ~ 0 0 ~ 1 ** 1 0 ~ ~ ~ 1 ~ 1 ~ 0 1 ~

PROJECT JOB NO. ATTACHMENT

  • CALC NO. + +4 8 ++~+ SHT NO. @lif I OF PREPARED BY DATE CHECKED BY DATE

~ ~ *01 ~ ~ **00 ~ 0*101101 ~ tt ~ ~ ~ 00 ~ 000 ~ 1000 ~ 0 ~

EEEEEEEEE 0000000 33333333 55555555 EE E 00 00 33 55 EE 00 00 33 55 EEEE 00 00 3333333 55555555 EE 00 00 33 55 EE E 00 00 33 55 EEEEEEEEE 0000000 33333333 55555555 VERSION LEASED AUGUST 1989 SER HANUAL VERSION 8 THEORET ICAL HANUAL VERSION: 8 VER IF I CAT ION HANUAL VERSION: 10 0 ~ 0 1 0 1 t0 ~ 1**111*10**11*0001*1**1 1 IH CASE OF PROBLEHS IIITH KE035, CONTACT THE 1 BASEPLATE USER REPRESENTATIVES:

HAKE LOCATIOH EXTENSION 0 AHN ARBOR EPD(AAAO)

  • GAITHERSBURG EPD 8-4084 HOUSTON HO 5-4215 t NORIIALK IIPO SAN FRANCISCO NPD(SFAO) 8 4362 0

~ 0001100 ~ 10 ~ 0000 ~ ~ ~ 010000110 0 PROGRAH SPONSOR SF 45/4 8.7706 0 TECHNICAL SPECIALIST- SF 45/4 8-2265 1 1 0 0 ~ 0

  • 0 t 0 ~ *** 0 ~ 0 0 t~01 *0 1 **1 1 1 1 1 COPYRIGHT 1984,1987 BECHTEL POIIER CORP. ALL RIGHTS RESERVED.

0 ~ 1 ~ 0 ~ ~ ~ 1 ~ 0 0 ~ 0 0 0 0 ~ ~ 0 ~ 0 ~ 0 0 1 0 ~ 0 ~ 0 0 1 ~ 0 0 ~ 0 1 1

  • HE035/11 DATE 92 09 25 PAGE 2 yyyyyiIiytPP01ttlt114111111101014t0111tOt1ttOPII10tt1t41141lllt11*t100l001tPPO PREPROCESSOR INPUT DATA CARDS 0*1****411~i0100000tlt*tl*1t*1110I1101t0011011***010000*tie*1t1POfltt00111000tl101t01 CARD 1 2 3 4 5 6 7 8 NO 123456789012345678901234Y&89012345678901234567890123456789012345678901234567890 1 3 FILEHAHEsHNPBP26 TYPE F-2 EHBED PLATE (8XI) CS.H.4406 2 KIT ~ gg1/

3 COH ~ ~ g g 4000/

4 PLA 7$ 7g ~ 18,8,1@29/

5 BPR 1,8.8E5,1.25E6,8210,11650/

6 BOL 2,3,1,3,1.5/

7 BOL 2,5,1,3,6.5/

8 BOL 6/3,1/15/1.5/

9 BOL 6,5, 1 g 15 /6.5/

10 END/

11 ATT 3,'46,4/

12 JST 3,4,2,3,180/

13 I ST 2,4,5,2.5,90/

14 IST 2,5$ 6t 5/90/

15 JST 2,6,4,6,0/

16 IST 4,6,5,.5,270/

17 IST 4,5,4,2.5,270/

18 IST 4,4,3,2.5,270/

19 IST 4,3,2,.5,270/

4,2,2,6,180/

2 ST 2,3,4,2.5,90/

23 EHD/

24 END/

25 POI 3,4/

26 LOA 1,383,-721,1062,25436,-34867,18309/

27 LOA 2,-383,721,1062,-25436,34867,.18309/

28 EHD/

29 EHD OF JOB

~~* END OF INPUT DATA ~~*

HE 035/11 DATE 92-09-25 PAGE 3

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)

PREPROCESSOR INPUT DATA CARDS I))))))*>>)))))))))))))1))*)1*)))>>)))1))))))))))))I)))))>>))))))))*)))))))))))1)>>))))))

CARD 1 2 3 4 5 6 7 8 NO 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 3 FILENAHE>>HHPBP26 TYPE F-2 EHBED PLATE (BX1) CS-H-4406 2 OUT 0>> 0 0* 1 0 3 CON 0>> 0 0* 0.000>> 4000.000>> 0.000* 0.000>> 0.000* 0.000 4 PLA 7>> 7 0* 18 000>> 8 000) 1.000>> 29 000>> 0.000* 0.000 5 BPR 0* 0 1* .880E+06>> .125E+07 .821E+04>> .117E+05>> 0.0* 0.0 6 BOL 2>> 3 1>> 3.000>> 1.500>> 0.000>> 0.000>> 0 000* 0.000 7 BOL 2>> 5 1>> 3.000 6.500 0.000* 0.000>> 0.000>> 0.000 8 BOL 6* 3 1>> 15.000 1.500 0.000>> 0.000>> 0.000>> 0.000 9 BOL 6>> 5 1

~ 15 000>> 6 500* 0 000) 0 000) 0.000* 0.000 10 ENO

'l1 ATT 3) 4 o. 6 ooo>> 4.000>> 0 000>> 0 000 12 JST 3) 4 2>> 3.000>> 180.000>> 0 000*

13 I ST 2>> 4 5>> 2.500>> 90 000) o.ooo.

14 1ST 2) 5 6>> .500 90.000 0 000>>

15 JST 2) 6 4>> F 000>> 0.000>> 0 000>>

16 IST 4) 6 5 o 500 270.000 0.000*

17 1ST 4>> 5 4>> 2.500>> 270.000>> 0.000>>

18 I ST 4) 4 3>> 2.500* 270.000 0.000 19 1ST

" 4) 3 2 .500 270.000* 0.000>>

T 4>> 2 2 6.000 180.000 0.000*

2 3>> .500 90 000>> 0.000>>

2 IST 2 3 4>> 2.500>> 90 000) 0 000>>

23 END 24 END 25 POI 3) 4 0* 0.000>> 0.000>> 0 000* 0 000* 0 000>>

26 LOA 0* 0 1>> 383.0>> -721.0>> 1062.0* 25436.0* -34867.0) 18309.0 27 LOA 0) 0 2* -383.0* 721 0* 1062.0>> -25436.0>> 34867.0* .18309.0 28 EHD 29 END OF JOB

      • END OF INPUT DATA DECK >>*>>

NE035/11 DATE 92.09-25 PACE 4 tttttttttttttttttttttttt**tt*tttttttt*tttt*ttttttttt*ttt***ttt*t*tttt*ftttf*ft FlLEHAHEtHNPBP26 TYPE F-2 ENBED PLATE (BX1) CS.H.4406 1 F 11*11*11ttttttttt1tttttt1t1tt*tttttt1tttttttt1ttttt1tttttttttttttttttttttttttttttttt lNPUT PARANETERS PLATE THlCKNESS PLATE X DlHEHSION

~

1.000 18.000 Y DlNENSlOH ~ .~~~~~ 8.000 NODULUS OF ELASTlClTY ... .290E+08 CONCRETE NODULUS .~ ...... .360E+07 CONC. COKP. STRENGTH . 4000.0 BOLT LOCAT lONS BOLT l J NODE X-COORD. Y.COORD.

1 2 3 10 3.000 1.500 2 2 5 12 3.000 6.500 3 6 3 38 15.000 1.500 4 6 5 40 15.000 6.500 BOLT PROPERTlES BOLT STlFFHESS (LB/1N.) ALLONABLE FORCE (LB)

TEHSlOH SHEAR TENS lON SHEAR

.880E+06 ~ 125 E+07 8210. 11650.

.880E+06 .125E+07 8210. 11650.

.880E+06 .125E+07 8210. 11650.

.MOE+06 .125E+07 8210. 11650.

ME035/11 DATE 92-09.25 PAGE 5 ttttttttttttttttttttttttttttttt**ttttttttttttttttttttttttttttttttttttttffttttt t

  • t FILEHAMEtHNPBP26 TYPE F 2 EMBED PLATE (SX1) CS.H-4406

~ ttttt1ttt1tttttttttttttttttttttttttttttttttttttt1t1ttttttttttttttttttttt1ttttttttttt NON STANDARD ATTACHMENT DATA ATTACKHENT NINBER 1 SEGMENT HlllBER .. ~ ~ ~ ~ ~ ~ ~

TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ JST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 3.000 ORIENTATION ANGLE . " o" 180.0 THICKHESS e ~ ~ ~ ~ ~ ~ ~ o ~ o ~ ~ ~ 0.000 SEGMENT NUMBER TYPE

~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~

2 IST HEIGHT . ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ... 0.000 DISTAHCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 2.500 ORIENTATION ANGLE ~ " ... 90.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGMENT HISSER " .o 3 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ IST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 0 I STANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ .500 ORIENTATION ANGLE ~ ~ 90.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGMENT NUMBER TYPE

~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ JST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 6.000 ORIENTATIOH ANGLE ... ~ 0.0 THICKNESS ~~ ~ ~~ ~ ~ ~ ~ ~~ ~ ~ ~ 0.000 SEGMENT NUMBER ~ ~ ~ ~ ~ ~ ~ ~ ~ 5 T YPE ~ ~ ~ ~ ~ ~ ~ ~~ ~ ~ ~ ~ ~ ~~ ~ ~ ~ IST HEIGHT ~ ~ ~ ~ ~ ~~ ~ ~ ~ ~ ~ ~~ ~~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ .500 ORIENTATIOH ANGLE ~ ~ ~ ~ ~ ~ 2?0.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000

NE035/11 DATE 92 09-25 PAGF. 6 ttttttttttttttttttttttttttttttttltttt\tttttttttttttttttttttttttttttttttttttttt FILEHANEtHHPBP26 TYPE F-2 ENBED PLATE (8X1) CS-H-4406

~ ttttttttttt**1*tttttttttttttttttttttttttttttttt*tttttttttttttttttttttttttttttttttttt NON STANDARD ATTACHHENT DATA SEGNEHT HUNBER ~ ... ~ ~ ~ .~ 6 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ IST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE o.oooo.oooo.oo 2.500 ORIENTATIOH ANGLE . ~ ~ ~ .~ 270.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGNENT NUNBER ~ ~ ~ ~ . ~ .. ~ 7 TYPE ~~ ~ ~ ~ ~~ ~ ~~ ~ ~ ~ ~ ~ ~ ~ ~ ~ IST HEIGHT ~ ~ ~ ~ o ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 2.500 ORIENTATION ANGLE ...... 270.0 THICKHESS oo.ooooooo. "o 0.000 SEGNEHT NUHBER . ~ ... 8 T'YPE ~ ~ ~ ~ ~ ~ ~ ~ ~ o. ~ ~ ~ ~ ~ IST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ .500 ORIENTATIOH ANGLE .. 270.0 THICKNESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGNENT NUNBER ......... 9 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ JST HEIGHT ~ ~ ~ ~ ~ ~~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 6.000 ORIENTATIOH ANGLE ...... 180.0 THICKNESS ,oooo, ~ ~ ~ ~ ~ ~ ~ ~ 0.000 SEGNENT NWBER T YPE

~~ ~ ~ ~~~~ ~ ~ ~~ ~ ~ ~ ~ ~ ~ ~

10 IST HEIGHT ................. 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ .500 ORIENTATION ANGLE .."" 90.0 THICKNESS o. ~ .~~~~~~~~~~ 0.000 SEGNEHT NUNBER ......... 11 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 1ST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 2.500 ORIENTATION ANGLE ... .. ~ 90.0 THICKNESS ~ ~ o ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000

KE035/11 DATE 92-09 25 PAGE 7

~ tttttt**tttttttttttttttttttttt'tttt*tttttttttttttttttt*ttttt'tt'ttttttt*tttttttt FILENAHEtHNPBP26 TYPE F.2 EHBED PLATE (8X1) CS-H.4406 ttttttttttt*tttttttttttttttttttttttttt*ttttttttttttttttttttttttt*ttttttttttttttt*t*)t LOADING CONDITIONS LOADING CASE NO. t 1 LOADINGS APPLIED AT NODE ~ 50 FORCE FX t 383.00 FORCE FY ~ -721.00 FORCE FZ ~ 1062.00 IKWENT HX > 25436.00 HOHENT HY ~ -34867.00 HOHENT HZ ~ 18309.00 LOADING CASE NO ~ 2 LOADIKGS APPLIED AT NCOE > 50 FORCE FX t -383.00 FORCE FY ~ 721.00 FORCE FZ t '062.00 HOHENT HX t -25436.00 INNOCENT HY t 34867.00 HCHENT HZ ~ .18309.00

HE035/11 DATE 92 09 25 PACE 8

  • tt00011ltl00*t*04t111*N*014t*10tietiaOit400t*tillt4114telgyygtit0011lt111ttf1 FlLENAHEsHNPBP26 TYPE F 2 EHBED PLATE (BX1) CS H 4406

~ OoioliStiOiPOOi1IO*1101IPOO'I'lI'I'P*i4010ioiioiOP000110i04iioiioi*4100000itf*ii11011001 BASEPLATE CONNECTlVlTY ELENEHT NDDE ELEHEHT KDDE NO. JA JB JC JD ND. JA JB JC JD 1 1 8 9 2 2 2 9 10 3 3 3 10 11 4 4 4 11 12 5 5 5 12 13 6 6 6 13 14 7 7 8 15 16 9 8 9 16 17 10 9 10 17 18 11 10 11 18 19 12 11 12 19 20 13 12 13 20 21 14 13 15 22 23 16 14 16 23 24 17 15 17 24 25 18 16 18 25 26 19 17 19 26 27 20 18 20 27 28 21 19 22 29 30 23 20 23 30 31 24 24 31 32 25 22 25 32 33 26 a 26 33 34 27 24 27 34 35 28 29 36 37 30 26 30 37 38 31 27 31 38 39 32 28 32 39 40 33 29 33 40 4'1 34 30 34 41 42 35 31 36 43 44 37 32 37 44 45 38 33 38 45 46 39 34 39 46 47 40 35 40 47 48 41 36 41 48 49 42

HE035/11 DATE 92.09-25 PABE 9 tttttttttjttjjttttttttttttttttttttjttjtjj*ttjttjtttttjttttjjjjjttjtjfjjjtjfjt FILENANE*HNPBP26 TYPE F-2 EHBED PLATE (BX1) CS.H-4406 t

~ jjttjj*ttttjtttjjjjtjtj*tttttttttttttttttttttttltjjttttt*tjt*tttjjtjjttjjtt**tjt*jtt NODAL COORDINATES J 'RANE NODE X Y 2 L 1NE L1KE NODE COORD !NATE COORD1NATE COORD I NATE 1 1 1 0.000 0.000 0.000 1 2 2 0.000 1.000 0.000 1 3 3 0.000 1.500 0.000 1 4 0.000 4.000 0.000 1 5 5 0.000 6.500 0.000 1 6 6 0.000 7.000 0.000 1 7 7 0.000 8.000 0.000 2 1 8 3.000 0.000 0.000 2 2 9 3.000 '1.000 0.000 2 3 10 3.000 1.500 0.000 2 4 11 3.000 4.000 0.000 2 5 12 3.000 6.500 0.000 2 6 13 3.000 7.000 0.000 2 7 14 3.000 8.000 0.000 3 1 15 6.000 0.000 0.000 3 2 16 6.000 1.000 0.000 3 3 17 6.000 1.500 0.000 3 4 18 6.000 4.000 0.000 3 5 19 6.000 6.500 0.000 3 6 20 6.000 7.000 0.000 3 7 21 6.000 8.000 0.000 1 22 9.000 0.000 0.000 4 2 23 9.000 1.000 0.000 4 3 24 9.000 1.500 0.000 4 4 25 9.000 4.000 0.000 4 5 26 9.000 6.500 0.000 4 6 27 9.000 7.000 0.000 4 7 28 9.000 8.000 0.000 5 1 29 12.000 0.000 0.000 5 2 30 12.000 1.000 0.000 5 3 31 12.000 1.500 0.000 5 32 12.000 4.000 0.000 5 5 33 12.000 6.500 0.000 5 6 34 12.000 7.000 0.000 5 7 35 12.000 8.000 0.000 6 1 36 15.000 0.000 0.000 6 2 37 15.000 1.000 0.000 6 3 38 15.000 1.500 0.000 6 39 15.000 4.000 0.000

NE035/11 DATE 92-09-25 PAGE 10 QQQQ f$ Q Q ~ Q Q Q Q 'g yy 0 lt ll0 0 Il1 ***i1 Itt l0 0 t 0 t t l1 t 0 1 0 ltI t t I1 lt t 0 tt 0 tIt l l 1 I0 P 0 4 0 1 0 0 1 11

~ FILENAHE~HNPSP26 TYPE F 2 EHBED PLATE (8X1) CS.H-4406

      • 001140001*01*1000t010101*0110001tt11IPtttOI0101*000001001*I010100001101*0011111001 NODAL COORDINATES I J FRANE NODE X Y 2 L I HE L I HE KCOE COORDINATE COORDINATE COORD IHATE 6 5 40 15 F 000 6.500 0.000 6 6 41 15.000 7.000 0.000 6 7 42 15.000 8.000 0.000 7 1 43 18.000 0.000 0.000 7 2 44 18.000 1.000 0.000 7 3 45 18.000 1.500 0.000 7 4 46 1e.ooo 4.000 0.000 7 5 47 1e.ooo 6.500 0.000 7 6 48 18.000 7.000 0.000 7 7 49 18.000 8.000 0.000 NODES AT APPLICATION OF LOADS 3 4(OFFSET) 50 6.000 4.000 .500

NE035/11 DATE 92-09-25 PACE

  • ~~~y11itl1011t111111101llfllt11llttittiffg~f4f*f*+1ttt44410ttt000tttt1tttf*gg FILENANE*HNPBP26 TTPE F-2 ENBED PLATE (8X1) CS-H-4406

~ eeaattiagyq*qaet1titttttI11t11f1itt1fIaIt11HiiiIitItpitatti4itteeaaaleaetfttt1tePai CONCRETE STIFFNESS DATA NODE EFFECTIVE CONCRETE KOOE EFFECTIVE CONCRETE AREA STIFFNESS AREA STIFFNESS 1 .750 .253E+06 2 1.125 .380E+06 2.250 .760E+06 4 3.750 .127E+07 5 2.250 .760E+06 6 1.125 .380E+06 7 .750 .253E+06 8 1.500 .507E+06 9 2.250 .760E+06 10 4.500 .152E+07 11 7.500 .253E+07 12 4.500 .152E+07

'13 2.250 .760E+06 14 1.500 .507E+06 15 1.500 .507E+06 16 2.250 .760E+06 17 4.500 .152E+07 18 7.500 .253Eior 19 4.500 .152E+07 20 2.250 .760E+06 21 1.500 .507E+06 22 1.500 .507E+06 2.250 .760E+06 24 4.500 .152E+07 7.500 .253E+07 26 4.500 .152E+07

", 33 2.250 1.500 4.500 4.500

.760E+06

.507E+06

.152E+07

.152E+07 28 30 32 34 1.500 2.250 7.500 2 '50

.507E+06

.760E+06

.253E+07

.760E+06 35 1.500 .507E+06 36 1.500 .507E+06 37 2.250 .760E+06 38 4.500 .152E+07 39 r.soo .253E+07 40 4.500 .152E+07 41 2.250 .760E+06 42 , 1.500 .507E+06 43 .750 .253E+06 44 1.125 .380E+06 45 2.250 .760E+06 46 3.750 .127E+07 47 2.250 .760E+06 48 1.125 .380E+06 49 .750 .253E+06 SUNNAT ION OF EFFECTIVE AREAS ~ 144.000 PLATE AREA ~ 144.000 TOTAL CONCRETE STIFFNESS ~ .486E+08

~** INPUT DATA PROCESSING COHPLETE ~ **~

HE035/11 DATE 92-09.23 PAGE 12 PLOT PLAN VIEN OP T"E BASEPLATE'HERE THE X AXIS (CONSTANT J LINES) ARE HORIZONTAL, AHD THE Y AXIS (COHSTANT I LINES) ARE VERTICAL.

HJJJJJJJJJJJNJJJJJJJJJJJJNJJJJJJJJJJJJNJJJJJJJJJJJHJJJJJJJJJJJJNJJJJJJJJJJJJN I I I I I I I HJJJJJJJJJJJ JJJJJJJJJJJHJJJJJJJJJJJJBJJJJJJJJJJJJN NJJJJJJJJJJJAJJJJJJJJJJJJKJJJJJJJJJJJJAJJJJJJJJJJJNJJJJJJJJJJJBBBJJJJJJJJJJJN I A I A I B I I A I A I I I I A I A I I I I A I A I I I I A I A I I I I A I A I ~ I I HJJJJJJJJJJJAAAAAAAAAAAAAAJJJJJJJJJJJJAJJJJJJJJJJJHJJJJJJJJJJJJHJJJJJJJJJJJJH I A I A I I I I A I A I I I I A I A I I I I A I A I I I I A I A I I I I A I A I B I NJJJJJJJJJJJAJJJJJJJJJJJJNJJJJJJJJJJJJAJJJJJJJJJJJHJJJJJJJJJJJBBBJJJJJJJJJJJN NJJJJJJJJJJJ JJJJJJJJJJJNJJJJJJJJJJJJBJJJJJJJJJJJJH I I I I I I I I I I I I I I HJJ JJJJJJJJKJJJJJJJJJJJJHJJJJJJJJJJJJNJJJJJJJJJJJHJJJJJJJJJJJJKJJJJJJJJJJJJH

PROGRAH: HE035 BASEPLATE SNOI: $9601 0110 AAN 8025 DATE: 92.09.25 RELEASE 11 NOS/VE 1.5.3 L765 TIKE: 11:42:03 PAGE: 13

~ t*t**tttttttttttttttttttttttttttttttt BEGIN SOLUT ION PHASE LOAD CASE NO: t

~ tttt**tttttttttttt*ttttttttttttttttttttttttt TITLE: FILENAMEtNNPBP26 LOAD CASE NO. (T 0 TYPE P

F-2 T E N EMBED PLATE V A L U E (BX1) CS.N-4406 S) 0 I S P L A C E H E N T S NODE DISPL ~ N(OE 0ISPL.

28 .845128E.02 1 -.207719E 02 27 .766563E-02 8 -.171645E 02 35 .746633E.02 2 -.148922E 02 26 .728577E 02 3 -.120377E.02 34 .680186E 02 9 -.991198E.03 33 ~ 649039E 02 10 -.612182E-03 21 .639193E.02 43 ..588561E.03 20 .562270E 02 44 ..428321E.03 25 .537901E.02 45 -.366745E-03 19 .524436E.02 46 ..211471E.03 QUADRILATERAL PLATE PRINCIPAL STRESSES ELEHENTS + 2 FACE ELEH SIGHA ELEH SIGMA ELEH SIGMA ELEH Sl GHA 23 9290. 24 9258. 22 8450. 21 6883.

20 5860. 19 5361. 1 4164. 2 -4156.

3 .3933. 35 .2405.

E L E H E N T S - 2 FACE ELEM SIGMA ELEH SIGHA ELEH SIGMA ELEH SIGHA 23 .8602. 24 -8373. 22 .8255. 21 -7379.

20 .6786. 19 -6331. 1 4163. 2 4157.

3 3933. 35 2450.

CONCRETE LOADS NODE Z.PRESS K(eE Z.PRESS KIX)E Z.PRESS N(X)E Z.PRESS 1 -701. 8 -580. 3 -407. 9 -335.

10 -207. 43 -199. 44 -145. 45 -124.

46 -72. 47 -42.

PROGRAN: NE035 BASEPLATE SKI: S9601 0110 AAH 8025 DATE: 92 09-25 RELEASE 11 NOS/YE 1,5,3 L765 TINE: 11:42,31 PACE: 14 BOLT LOADS NODE H-SHEAR Y SHEAR SRSS TENSION 10 446. -904. 1008. 0.

12 -247. -904. 937. 2810.

38 366. 543. 655. 1308.

40 -182. 543. 573. 2563.

BOLT INTERACTION EQUATION EQUATIONt((TENSION/TALLSI)tt 1.000+(SHEAR/SALLOM)tt 1.000))*t 1.000 HME TENSION SHEAR TENSION SHEAR INTERACT SAFETY ALLOI ALLOJ RATIO RATIO RATIO FACTOR 10 8210. 11700. .001 .086 .087 11.478 12 8210. 11700. .342 .080 .422 2.368 38 8210. 11700.,159 .056 .215 4.645 40 8210. 11700..312 .049 .361 2.769 tttttttttt*1*ttttt*tttttttttttttttttttttttttt E N 0 LOAD CASE tttttttttttt*t*tttt*t*ttt*ttt*tttt*tttttttttt

PROGRAH! HE035 BASEPLATE SNNI: $ 9601 0110 AAH 8025 DATE: 92-09-25 RELEASE 11 NOS/VE 1.5.3 L765 TINE: 11!42:31 PAGE: 15 00010010101110000010*110100010100000010010*11 BEGIN SOLUT ION PHASE *

  • LOAD CASE NO:

~ 0000111101110000*010011*11110111000001000000 TITLE: FILENAHEIHNPBP26 TYPE F-2 EHBED PLATE (SXI) CS H.4406 LOAD CASE NO. 2 (T 0 P T E M V A L U E S) 0 I S P L A C E H E N T S NME DISPL. NME DISPL.

1 .706320E-02 28 -.163211E-02 2 .637827E-02 35 -.110677E.02 3 .603626E.02 27 -. 100326E.02 8 .595421E 02 34 .708989E 03 9 .526936E-02 26 ..666366E.03 10 .492677E 02 21 ..589303E-03 15 .485091E-02 33 -.505115E.03 4 .432928E-02 42 -.313510E-03 16 .416782E 02 41 -.171125E-03 17 .382673E.02 40 -.977272E.04 0 U A D R I L A T E R A L PLATE PRINCIPAL STRESSES ELEHEKTS + Z FACE ELEH SIGNA ELEH SIGNA ELEH Sl GHA ELEH S IQIA 24 .4210. 23 -4102. 22 -3311. 21 .1496.

30 1446. 29 1445. 27 -1348. 26 .1329.

19 1120. 32 -1100.

ELEHENTS Z FACE ELEH SI QIA ELEH SI QIA ELEH Sl GHA ELEII SIGNA 23 3701. 24 3452. 22 3394. 21 2108.

29 -1934. 26 1868. 30 -1832. 27 1706.

25 1498. 20 1321.

COKCRETE LOADS NME Z-PRESS NME Z PRESS KME Z PRESS NODE Z PRESS 28 -552. 35 -374. 27 -339. 34 -239.

26 -225. 21 -199. 33 .171. 42 -106.

41 -58. 40 -33.

PROGRAN: NE035 BASEPLATE SNLI: $ 9601 0110 AAH 8025 DATE: 92-09-25 RELEASE 11 NOS/VE 1.5.3 L765 TINE: 11:42:49 PAGE: 16 8 0 L T LOAD S NCOE X SHEAR Y-SHEAR SRSS TENSION 10 ~ .446. 904. 1008. 4336.

12 247. 904. 937. 1333.

38 .366. 543. 655. 645.

40 182. -543. 573. 0.

BOLT INTERACT ION EQUAT ION EQUATION ((TENSION/TALLOM)~~ 1.000+(SHEAR/SALLOM)*~ F 000)) ~ 1.000 N(X)E TENSION SHEAR TENSION SHEAR INTERACT SAFETY ALLOM ALL(Q RATIO RATIO RAT10 FAC'TOR 10 8210. 11700. .528 .086 .614 1.628 12 8210. 11700. .162 .080 .242 4.125 38 8210. 11700. .079 .056 .134 7.435 40 8210. 11700. .001 .049 .050 20.008 111111I111*I11f*III4111000011141P4fi*11jlSOti E N 0 LOAD CASE 0

~ Ilt1111104tll000410IPllkillt14110ltl1PCOI110

~ IOitiiil1011111111100111I1110000011010114011 END POSTPROCESS I NG

~ 1001010IPOPOIOPI1114I11044110011011011101111

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I T.S, 8 PROFESSIONAL ENGINEER EM&. SAFER Y RGLA PEP/ 55l5QlC.

SE.C A-A, CAROLINA POWER & LIGHT COMPANY NUCLEAR ENGINEERING DEPARTMENT PLANT: HARRIS HUCLKhR &OPEC' UIIIT I SCALE: NOHS CHfhhlCA,L g VOl LjMG. C,OAT ROL, RAP E.l . Z3ro - CI IssvE PER PC.R &547 i sT ~> o E, R, S UP P 0 R.Y'P REV DATE DESCRIPTION WNiOSN CH OV OPE OPPE A-3-2%-I-C5-H-4400 REVS~ 8 S': 2 or Z SKETCH Np SK Ccr5%7 C i<Os 'SHT: 2 or Z

Mod Number C FR Number Calculation Affected + ~ ~+~ ~ ~~ ~~<~ Drawing Affected S<~< +> <>LC.

Reason for Change:

~crt deW r ' I sd To Ide SVPrb Ia Justification for Change Approval:

~ Minor Change (i.e., editorial, Calculations are not attached.

reference dimension, etc.), Supplementary IOther I (provide basis, attach supplementary calculations)

DPE*

%at

  • Signatures indicate design verification has been performed in accordance with NED Procedure 3.3. This form serves as the design verification record.

RQv.

(C go PP(/P ~

CALCULATION NO. 3 Z94 PAGE REV LIST OF EFFECTIVE PAGES PAGE REV PAGE REV PAGE REV L

Lc ATTACHMENTS Rev. 2 (E.C.F&/rlj)

CALCULATION NO PAGE REV TABLE OF CONTENTS Page No.

List of Effective Pages ~ ~ ~ ~ ~ ~ ~ ~ ~

Table of Contents Purpose List of References Body of Calculation Conclusions Attachments . . . . . . . . . . . . . . . . . . . . . . . Page(s)

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% 25'-wz CAROLINA POWER & LIGHT COMPANY ~

Cheeked Py< Date:

f-zz-y Pg. of Rev.

CALCULATION SHEET r I PID No.: Pile:

Pro)ect

Title:

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FORM No. 74055 REV. 10/45 Computed bv: Date: Calculation ID:

/-2e.1> CAROLINA POWER & LIGHT COMPANY Chepjced bZ: Date:

J r/PID No.: CALCULATION SHEET File.'ev.

Pg. of Pro)ect

Title:

Calculation

Title:

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CALCULATION SHEET IPID No Pile:

Title:

'ro)ect Calculation

Title:

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+ /5/g c's 25/onZws/ fc~ -,$ (std).- Zj g

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FORM No. 100SS REV. 10/SS Computed by: Date: Calculation ID:

C1 "-i 9 25 9g CAROLINA POWER & LIGHT CO~ANT c -cs-4-e~

ChectR~ by:

f Date:

27~

CALCULATION SHEET Pg. of Rev.

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FORM No. 70055 REV. 10/05 Computed by: Date: Calculation ID:

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CALCULATION SHEET r/PID No.: Pile:

Pro]ect

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FORM NO. 74055 REV. 10/$ 5 Computed by: Date: Calculation ID:

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CALCULATION SHEET Tar f PID No.: File:

Prospect

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I/ I br =9" '4y "~e ) '(>57 + leel +~os ) Roe7 'in e~ c. woe.

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FORM NO. 7$ 055 REV. 10/$ 5 Computed by' Date: Calculation ID:

T lt CAROLINA POWER ItT LIGHT COMPANY Checked I Date:

No.:

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FORM No. 70055 REV. 10/$ 5 ComPuted by: Date: Calculation ID:

~" - ala CAROLINA POWER 6 LIGHT COMPANY

-~Y'- ',~-s Checked bg: . Date:

CAL'CULATION SHEET Pg. of Reve

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Project

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R/PW/PHP NO. OWNG. NO. 0 REV.

SUBJECT

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ATTACHMENT 0

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GT1CES 3.38 92/N/24. N.36.35. PAGE 1 ~

t;ALC lf)'TrACHMENT" OF PNIE tttttttttttttt1tttttttt1tttt1tt1tttttttttttttttttttttttt1ttttttttttttttt1111ttltttltt GEORGlA lNSTlTUTE OF TECQOLOGY lNTEGRATED COMPUTER ENGlKEERlNG STSTEN GTl CES 3.38 GEORGlA TECN PRQ% lETARY PRUCT GENERATED 88/02/16. 15.25.46 DATE ~ 92/N/24.

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HARCK 1988 8701 CDC 0 2180 jbs ~

ttttttttttttttttttttttttttttttttttttttt 1111 ACTiVE UNITS - LENGTN lKIGNT ANGLE TENPERATURE Tile tttl ASS%ED TO SE INCH PtRJle RAD I AN FAHRENHEIT SECOND TYP SPA FRA UNIT IN LSS DEG JOI COO 'i 1 00.00 00.00 00.00' 2 00.00 12.00 00.00 3 00.00 20.80 00.00 4 -6.00 20.M 00.00 5 .6.00 24.00 00.00 6 00.00 12.00 14.375 7 9.375 12.00 14.375 8 9.375 12.00 17.375 9 9.375 12.00 20.37$

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5 10 11 12 13 T 'TISE80<<TS5X5X4'6 T iAISCPIPEi >P4.00XS<

NEN PRa PRIS 4 6 TO 9 15 AX 10 AY 10 AZ-10-IX 100 1Y 100 IZ 100 SY '100 SZ 100 CONSTANTS E 29+ OOE6 ALL G 11.15E6 ALL OEN 0.203 ALL QVT 0.0 NEH 4 6 TO 9 15 BETA 0 ALL POI 0.300 ALL S

STEEL ccccccccccccccccccccccccccccccccccccc>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>

ACT 1VE LNITS ikIGNT LS LENGTH INCll c

TOTAL LENGTH, lklGHT Ale VOLQK FOR SPECIFED HEHBERS c

LENGTN > 1.0975E+02 RIGHT > 1.0462E+02 VOL SE ~ 6.7795E+02 cccccccccccccccccccccccccccccccccc>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>

PLOT DEVICE PRINTER LEN 6 PLOT PLANE XY THRV 1

CAI.C N NP-PCE-4547 CT I CE$ 3.3$ %/N/24. 09.36.38. PACE 5 TCE PRLIITEE LQI 4 YZ TIRU 1

CALC NO NNP.PCR 6547 I GT CES 3+38 92/09/24. 09.36.39. PAGE 6 T I(NI; Y N(aIZONTAL SCALE ~ 3.375D IN UNITS PER INCH T

t VERTICAL SCALE ~ 3.4667 IN UNITS PER INCH

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t 14 t

6 10 1311

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PLOT INTERPRETATION:

t*ttt SiDE SELONGIKG TO ONE ELENENT SlDE SELONGIKG TO TlQ OR NORE ELENENTS FREE JOINT LOCATIONS SUPP(X(T JOINT LOCATlONS

CAI.C N0 eu -PCN-647 GTICES 3.38 %l09/24. 09.36.39+ PAGE ICE PRINTEN LEN 4 XZ TIRU 10

CALC NO NS PCR.454T QT1CES 3-3S 92/09/24. 09.36.39. PAGE S ATIINls X 2 2500 lN UNlTS PER lKCN o ~

e VERT1CAL SCALE ~ 2.2500 1N 011TS PER 1NCN 7 S 9 XttttytttttttX t

2 6 10 13 11 Xtttttttetteetttttttt5eet tteetttttttettttttttttttXttttete[ 01ttttttttttttttttXttttttlftttttttttttttttttX3*X PLOT 1NTERPRETATlINI'1DE SELOKGlKQ TO OKE ELEIKNT

+++++ S1DE SELIXIQlKQ TO TM OR ICRE ELEIKMTS X FREE AlNT LOCATLONS S SUPPORT JOlNT LOCAT 1ISS

CALC lO OP.PO.6S47 QtlCEI 3.3$ 92/09/24. 09.36AO. PAGE 9 lCE PRlllYER LKN 4 XY FANS 15

CALC NO NNP.PCR-6547 QTICES 3.38 92/N/24, 09.36.40. PAGE 18 TIOIs Y NOIIZONTAL SCALE a 1 ~ 0000 IN INIITS PER IKCN VERTICAL SCALE ~ 1.0000 IN LNITS PER INCR 14 15 16 Xt ttttttt 5 ttttttt1ttttttttttNttttttt 1 ttttttttttttttt 6tttttttttttttt1 ttttttttttttttttttttttt1ttttt ttg 1

1 14 t

13 X

PLOT INTERPRETATION!

SIDE BELONGING TO ONE ELECT SIDE QELONQINQ TO TMO OR NORE ELEKENTS FREE JOINT LOCATIONS SEAPORT JOINT LOCATIONS

CALC NO NNP.PCR 654'7 GTICES 3+3$ 92/09/24. 09.36.40. PAGE 1%

LOADS FOR JOINT 5 LOAD 'I JOI 5 LOA fOR X 174 LOAD 2 JOI 5 LOA FOR Y 341 LOAD 3 JOI 5 LOA FOR 2 154 S

t EQ. 6 LOADS FOR JOINT 5 LOAD 4 JOI 5 LOA fOR X 200 LOAD 5 JOI 5 LOA FOR Y 393 LOAD 6 JOI 5 LOA FOR 2 172 t

S S EQ. 2 LOADS FOR JOINT JS 'L4 t

LOAD 7 JOI 16 LOA FOR X 270 LOAD 8 JOI 16 LOA FOR Y 832 LOAD 9 JOI 16 LOA FIXI 2 985 L

J OA NQI X 7800 L

JOI 16 LOA HOI Y 8088 LOAD 12 JOI 16 LOA IKN 2 6780 S

S EQ. 6 LOADS FOR JOINT~ lit t

LOAD 13 JOI 16 LOA FOR X 500 LOAD 14 JOI 16 LOA FOR T 971 LOAD 15 JOI 16 LOA FOR' 1516 LOAD 16 JOI 16 LOA IKNI X 11244 LOAD 17 JOI 16 LOA IKW Y 12924 LOAD 18 JOI 16 LOA NOI 2 11076 S

DEA LOA 19 DIR Y ALL NEN S

STIFFNESS ANALYSIS SANDMIDTN INFORNATIINI BEFORE RENLWBERINQ.

CALC NO HNP-PCR 6547 GT ICES 3.38 92/09/24. 09.36.41. PAGE 12 WHI SANDMIDTN IS 4 AIS OCCURS AT JOINT 6 THE AVERAGE QANDMIOTN IS 1.357 THE STNSARO DEVIATION OF TNE SANDMIDTN IS 1 ~ 172 2.529 BNSMIDTH INFORNATION AFTER RENQOIERING.

THE NAXIJRHI SANDMIDTH IS 3 AIS OCCURS AT JOINT 6 THE AVERAGE QANDMIDTH IS 1.143 THE STANDARD DEVIATION OF THE 8ANDMIDTH IS +833 0

1,976 THE PSEISO.DIA%TER OF THE STRUCTURE IS 10 SETMEEN JOINTS 5 AJS 16 T1% FOR CONSISTENCY CHECKS FOR 16 %NBERS .44 SECONDS T1% FOR QAJSMIDTH REDUCTION .21 SECONDS TINE TO GENERATE 16 ELENENT STIF. NATRICES .30 SECONDS TIHE TO PROCESS 16 HOSER LOADS ~ 63 SECONDS TINE TO ASSENSLE THE STIFFNESS HATRIX ~ 45 SECONDS PROCESS 16 JOINTS ~ 09 SECONDS SOLVE MITH 7 PART ITIINIS .96 SECOSS T 0 PROCESS 16 JOINT DISPLACE%NTS ~ 64 SECOSS T1% TO PROCESS 16 ELE%NT DISTORTIOIS 2.20 SECONDS T1% FOR STATiCS CHECK 1.36 SECONDS S

CREATE PEAK LOAD iEO. 2'ROI 1 2 3 7 8 9 10 11 12 19 CREATE PEAK LOAD 'EQ. O'ROI 4 5 6 13 14 15 16 17 18 19 LOAD LIST 'EQ. 2'EO.

DEC 1 6'XJTPUT IXJTPUT SY NEH LIST FOR, REA ALL

CALC NO HKP.PCR-6547 GT1 CES 3.38 92/09/24 09.36.45. PAGE 13 Otter&

~RESULTS OF LATEST ANALYSES aaaeaaaeeaa PRDBLEH - PROJACR TlTLE F lLENA%44 H 4400 ACTlVE OtlTS 1NCH LB DEG DEGF SEC HEHBER FORCES NEHBER LOADTKG JOlNT /- -------.----FORCE------------------- //--------- -- ---- NNENT- -/

AXIAL SHEAR-Y SHEAR-2 TDRSlDNAL BEND lKG-T BENDlNQ 2 1 EO. 2 1 965.3 787.1 970.2 3216.3 8520.9 15872.7 2 946.3 787.1 970.2 3216.3 5227.4 8721.8 EO, 6 1 1271.9 1150.4 1444.7 4590.6 12322.8 22019.0 2 1253.0 1150.4 1444.7 4590.6 7418.8 11708.5 2 EO. 2 2 361.0 174.0 154.0 924.0 1848.0 4152.3 3 347.1 174.0 154.0 92C.O 492.8 2621.1 EO. 6 2 413.0 200.0 172.0'72.0 1032.0 2064.0 4776.3 3 399.1 200.0 1032.0 550.4 3016.3 EO. 2 3 174.0 347.1 154.0 492.8 924.0 2621.1 4 174.0 341.0 154.0 C92.$ .0 556.8 EO. 6 3 200.0 399.1 172.0 550.4 1032.0 3016.3 4 200,0 393.0 172.0 550.4 .0 640.0 EO. 2 4 3C1,0 174.0 154.0 .0 492.8 556.8 5 341.0 174.0 154.0 .0 .0 .0 EO. 6 4 393+0 200.0 172.0 .0 550.4 640.0 5 393.0 200.0 172.0 .0 .0 .0 EO. 2 2 1024.3 589.2 64C.S 5773.2 3219.0 5338.3 6 1024.3 571.3 644.S 5773.2 6648.8 3398.3 EO. 6 2 15OS.O 844.5 986.5 8312.9 4593.7 7542.6

,6 1SOSA 826.6 986.5 8312.9 10301.6 4920.5 EO 2 6 403.3 403.9 572.8 1995.$ 5182.8 4593.4 7 403.3 403.9 572.8 1995.8 860.0 241$ .2 EO. 6 6 617.3 584.0 891.9 2914.6 8047.8 6633.4 7 617.3 584.0 891.9 2914.6 1249.6 3470.7 572.$ 403.9 403.3 2418.2 860.0 1995.8

CALC KO KKP.PCR &547 GTtCES 3.38 92/09/24. 09.36.45. PAGE snA 403.9 403.3 2418.2 1163.9 1873.3 aa. s 891,9 584.0 617.3 3470.7 1249.6 2914.6 891.9 584.0 617.3 3470 7 1768.3 2756.2 8 N.2 572.8 403.9 403.3 2418.2 1163.9 1873.3 572.4 403.9 403.3 2418.2 2304.7 3050.1 N. 6 891o9 584.0 617.3 3470.7 1768.3 2756.2 891.9 5S4.0 617.3 3470.7 3542.6 4465.7 EQ. 2 9 403.3 403.9 sn.8 3050.1 2304.7 2418.2 10 403.3 403.9 sn.8 3050.1 7384.2 4593.4 EQ. 6 9 617.3 584.0 891.9 4465.7 3542.6 3470.7 10 617.3 584.0 891.9 4465.7 11491.9 6633.4 10 N. 2 6 903.1 577.8 241.2 1561.3 1567.3 2644.7 10 903.1 585.4 241i2 1561.3 2S12.7 4358.6 EQ. 6 6 1333.0 838.9 369.2 2227.4 2402.3 3807.5 10 1333.0 846.4 369.2 2227.4 4361.6 6460.4 11 N. 2 10 1024.3 579.1 644.5 5773.2 10106.2 6413.3 13 1024.3 586.9 644.5 5773.2 13779.1 9827.4 EQ. 6 10 1505.0 834.4 986.5 8312.9 15722.7 9420.3 13 1505.0 842.2 986.5 8312.9 21425.0 14363.6 12 N. 2 11 1386.2 843o4 639.4 7008.2 5277.$ 14354.1 12 1401.8 843.4 639.4 7008.2 6445.9 2%03.9 EQ. 6 11 1772.4 1354.9 912.7 10763.3 7480.6 20252.5 12 1788.0 1354.9 912.7 10763.3 9485.9 30536.9 E0.2 13 639o4 1385.4 843o4 14354.1 7383.9 5807.1 11 639e4 13S6.2 843.4 14354.1 7008.2 5277.5 EQ. 6 13 912,7 1771.6 1354.9 20252.5 11413.9 8203.7 11 912.7 1772 o4 1354.9 20252.5 10763.3 7480.6 14 EQ. 2 13 847.0 270.0 985.0 17938.0 13710.0 16777.2 14 840.9 270.0 985.0 17938.0 7800.0 15157.2 EQ, 6 13 986.0 500.0 1516.0 28084.0 20340.0 23843.2 14 979.9 500.0 1516.0 ~28084 11244.0 20843.2 15 EQ. 2 14 270.0 840.9 985,0 7800.0 17938.0 15157.2 15 270.0 840.9 985.0 7800.0 15106.1 12739.7 EQ. 6 14 500o0 979.9 1516.0 11244.0 28084.0 20843.2 15 500.0 979.9 1516.0 11244.0 23725.5 18026.0 16 EQ. 2 15 270.0 840.9 98$ .0 7800.0 15106.1 12739.'7 16 270.0 ~ 832.0 '85.0 7800.0 8088.0 6780.0 EQ. 6 15 500.0 979.9 1516.0 11244.0 23725.5 1S026.0 16 500.0 971.0 1516.0 11244.0 12924.0 11076.0 RESULTAKT JOlKT LOADS QFPOtTS JO!KT LOADI KG /- -FORCE- e//o o oeeeo og+KT /

X FORCE Y FORCE 2 FORCE X HOtEKT Y NOKKT 2 IKNEKT GLOBAL EQ. 2 787.1 970.2 8520.9 3216.3 15872.7

CALC NO NSP.PCS-6547 0T I CE$ 3+38 92/09/24. 09.36.45 PAGE 15 1150.4 1271.9 1444.7 12322.8 4590.6 22019.0 843.4 1401.8 639.4 6445.9 7008.2 20403.9 E0. 6 1354.9 1788.0 912.7 9485.9 10763.3 30536.9

CALC N OP.PCS 6547 CT ICES 3.3Q '9'/24. 09.36.45 PAGE 16 EC 3 L 1SP ALL

CALC NO NNP-PCR.6547 QT I CES 3,3B 92/09/24. 09,36.45. PAGE 12 eeeaseeeeaaoa

  • RESULTS OF LATEST ANALYSES

&101~*11 PROBLEN - PROJsPCR TITLE - FILENANE~ " 4400 ACTIVE UNITS INCH LB DEG DEGF SEC RESULTANT JOINT DISPLACENENTS SUPPORTS JOINT LOADING /---------------- DISPLACENENT-------- // - --- - - ROTATION-------------.-.-.-/

X DISPEL Y DISP. 2 Dl SP X ROT ~ Y ROT. Z ROT GLOBAL E4. 2 ,000 .000 .000 ~ 000 .000 ~ 000 EQ. 6 .000 .000 ~ 000 ~ 000 .000 ~ 000 12 GLOBAL E4. 2 .000 .OOD .000 .000 .000 .000 EQ. 6 .000 .000 .000 .000 .000 .000 RESULTANT JOINT DISPLACENENTS FREE JOINTS JOINT LOADING /---------------- DISPLACEMENT---------------- // ------- ----------ROTATION-------------------/

X DISP. Y DISP ~ 2 DISP. X ROT. Y ROT. 2 ROT.

GLOBAL EQ. 2 ,001 .000 .001 .002 .004 .009 EQ. 6 ~ 002 .000 ~ 001 .003 .006 .012 GLOBAL EQ. 2 .Na .000 .001 .003 .005 .011 EO 6 .004 .000 .002 .004 .007 .014 GLOBAL EQ+ 2 .003 .001 .002 .004 .006 .013 EQ. 6 .004 .002 .003 .005 .008 .017 GLCNAL E4. 2 .004 .001 .002 .004 .006 .013 E4. 6 ~ 005 .002 .003 .005 F005 .017 GLOBAL EQo 2 .002 .001 .001 .001 .008 .018 EO. 6 .003 .001 .001 .001 .012 .026 GLOBAL EO. 2 .002 .004 .002 .002 .009 .018 EQ. 6 .003 .005 .003 .002 .013 .026 EQ. 2 .002 .004 .002 ~ 002 .009 .019 EQo 6 .003 .005 .003 .003 .013 .027

CALO BO NO.PCB.6547 mrCES 3.3B 92/09I24. 09.36.45. ADAGE 1S

.002 .004 .002 +002 .009 .019

.003 .005 .003 .003 ~ 013 .027 10 EQ 2 .002 .001 .001 .003 .010 .019 EQ. 6 ~ 003 .001 .001 .004 .014 .027 GLOBAL EQo 2 ,003 .000 .001 .007 .016 .023 EQ. 6 .004 ~ 000 .001 .011 .024 .033 13 EQ. 2 .003 +000 .001 .008 .016 .024 EQ, 6 .004 .000 .001 .011 .025 .035 14 GLOBAL EQo 2 .007 .000 .003 .023 .057 .047 EQ. 6 ~ 010 .000 .004 .034 .ON .067 15 GLOBAL EQ. 2 .007 .003 .006 .024 .058 .048 EQo 6 .010 .004 .009 .036 .090 .069 16 GLOBAL EQ. 2 .007 .010 .014 .039 .075 .062 EQ. 6 .010 .014 .022 .057 .117 .090

CALC N OP-KR.6547 CTICRS 3.3e 92I09IZC. NIaS.AS. I uZ DEC 1 L lST 'N.

2'lST IIAX STR ALL I%II SEC FRA IN 3 0.0 0.5 1.0

CALC NO NNP.PCR-6547 OT I CES 3.3$ 92/09/24. 09.36.45 PACE 20 RESULTS OF LATEST ANALTSES ttttttttt1 tttttttttttttttttt PROBLEN - PROJtPCR TITLE - F ILENANEtCS-N.4400 ACTIVE UNITS INCR LB DEG DEQF SEC INTERNAL NOSER RESULTS IKN8ER NAXIIRM STRESS

/- STRESS NENSER NAX NORNAL A'I SECTION LOAD MIN NQRNAL AT SECTION LDID 1 2584.6 .000 FR EQ. 2 -2239.1 .000 FR EQ. 2 657.9 ~ 000 fR EQ. 2 -528.7 .000 FR EQ. 2 911.5 .000 FR EQ. 2 -814.6 ~ 000 FR EO 2 44.6 .000 FR EO. 2 23.6 F 000 FR EO. 2 5 1705.6 1.000 FR EQ 2 -1259.2 1.000 FR EO 2 6 138.1 .000 FR EO. 2 .57.4 .000 FR EQ. 2 7 87.7 1.000 FR EQ. 2 26.9 1.000 FR EO. 2 110.8 1.000 FR EQ. 2 3.7 1.000 FR EQ. 2 9 160.1 1.000 FR EQ. 2 -79.5 1 000 FR EQ. 2 10 1254.9 1.000 FR EO. 2 .861.3 1.000 FR EO. 2 11 3706.2 1.000 fR EO. 2 -3259.8 1.000 FR EQ. 2 12 4267.0 1.000 FR EO. 2 -3656.1 1.000 FR EO. 2 13 2085.6 .000 FR EQ. 2 -1806.9 .000 fR EQ. 2 14 7658.2 000 fR EQ. 2 -7186.2 .000 FR EQ. 2 15 358.0 000 fR EQ. 2 -304.0 .000 fR EQ. 2 16 6580.5 ~ 000 FR. EO. 2 .6458.0 .000 FR EO. 2

CALC R0 RRP-PCR-65Ar l GT CES 3.38 92/09/24. 09.36.45 ~ PAGE 2T IST 'EQ.

6'IST IIAX STR ALL INN SEC SRA IN 3 0+0 0.5 1,0

CALC RO RXP.PCR-6547 GT I CES 3.38 92/09/24. 09.36.47. PAGE 22 1t11*HIHI1NOIP~~4+

+RESULTS OF LATEST ANALySES 4441440tOOO~OM4140tttt+

PROBLEN - PROJPCR TITLE - FILERANCS N-4400 ACTIVE UNITS IKCH LS DM DEGF SEC INTERRAL IKNER RESULTS NBSER KAXII%A STRESS

/e STRESS ONER MAX NORMAL AT SECTION LOAD NIN RORHAL AT SECTION LOAD 1 3623.0 .000 FR EQ. 6 -3167.9 .000 FR M. 6 750.2 .000 FR N. 6 .602.4 .000 FR E4. 6 1041.3 .000 FR EQ. 6 -929.8 ~ 000 FR EO, 6 51.2 .000 fR EQ. 6 27.4 ~ 000 FR EQo 6 5 2573.9 1.000 fR EO 6 -1918.0 1.000 FR N, 6 6 208.5 .000 FR N. 6 .85.1 .000 FR EO. 6 7 134.4 1.000 FR EO+ 6 43.9 1.000 FR EOo 6 8 169.3 1+000 fR EQ. 6 9.1 1.000 FR EO. 6 9 243.0 1.000 fR EQ. 6 -119,5 1.000 FR E4, 6 10 1887.2 1.000 FR EO '6 -1306.3 1.000 FR EO 6 11 5608.4 1.000 fR EO. 6 -4952.5 1.000 FR EQ 6 12 6294.8 1 000 FR EO. 6 .5515.6 1.000 FR EQ. 6 13 3093.4 .000 fR M 6 -2695.6 ~ 000 FR EQ+ 6 14 11031.3 ~ 000 fR EOo 6 -10481.8 +000 FR EQ, 6 15 539.3 .000 FR N. 6 -439.3 .000 FR E4. 6 16 9888.3 .000 FR N. 6 -9661.4 .000 FR N. 6

CALC NO IW.PCR.6547 GTtCES 3.38 92/09/24. tN.36.47. PAGE 23 CALC NO NNP-PCR-6547 GT I CES 3,3B 92/09/24. 09.36,48. PAGE 24 DYNAMIC AREA CUWARY STATISTICS.

INITIAL POOL SIZE 4091 POOL SI2E INCRENENT 4091 NNQER OF DATA POOL INVES 255 DATA CNPACT IONS 6 LOU RELEASED 0 HIGH RELEASED 0 LQI UNRELEASED 0 LOM NCOULES 2 HIGH NCOULES 0 BLOCKS READ FROI DISK 89 BLOCKS READ FRQI ECS 20 SEtNJENTIAL READ AHEADS INITIATED 0 BLOXS READ AHEAD DISCARDED 0 ONE-PRU READ CQJNT 0 ONE-PRU IAIITE CRNT 4 BLOXS IRITTEN TO DISK 0 ONE-RID UPDATES IN ECS 0 BLOCKS RENRITTEN TO ECS 0 NAXIIRM NNGIER OF ALLOCATED lORDS 267166 NAXWM flELD LENGTH ATTAINED 36&200 NOSER OF CRASHES sr NNGIER Of FIELD LENGTN INCREASES 42 NLSSER Of FIELD LENGTH DECREASES 8 ER OF OVERFLY-ACTION CALLS 6 S

ALU IO'TTACHMENT" NE035/11 DATE 92 09 24 PAGE O*OO ~ ~ ~ 0 ~ 0 ~ ~ II@ ~ ~ ~ ~ ~ ~ ~ ~ 0 ~ P ~ ~ ~ 0 ~ ~ 0 ~ 1

~

gpss A PROJECT g STiRIP JOB NO.

CALC NO. SHT NO+

0 PREPARED BY DATE CHECKED BY DATE 0 fNchrt &i~

0 0

~ tt~ ~ ~ I ~ I ~ 1 0 ~ ~ ~ I ~ ~ 0 0 ~ 0 1 1 1*0 l ~ 0 ~ 0 ~ ~ ~ ~ ~ ~ ~ 0 ~

wcPC (

EEEEEEEEE 55555555 EE E 55 EE 55 EEEE 55555555 EE 55 EE E 55 EEEEEEEEE 55555555 VERSION E A S E D AUGUST 1989 USER NANUAL VERSION THEORETICAL NANUAL VERSION: 8 VERI F ICATION NANUAL VERSION: 10 000010 ~ I ~ ~ 0 ~ ~ 0 ~ 10000 ~ 01 ~ 0 ~ IO ~ ~ ~

IN CASE OF PROBLENS MITH I%035, CONTACT THE

~ BASEPLATE USER REPRESENTATIVES:

0 i COPYRIGHT 1984,1987 BECHTEL PQIER CORP. ALL RIGHTS RESERVED.

11 ~ OO ~ OIOO ~ ~ ~ ~ ~ 0 ~ 0 ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0 ~ ~ ~ ~ 0 ~ ~ 0 ~ ~ ~

IKQRi/11 OATE 92 09-24 PACE 2

~ ioeeeetee~~ii~tatoeaea~

NKPROCESQR @PUT DATA CARDS

  • l*tttttP1ttttOOHtltN1ttetfHe%

CARO KO 1 2= - ~ 3 4 5 6 7 12345678901234567890123456789012345678901234567890123456789012345678901234567890 8

1 3 FTLENA%~INPBP27 2 OJT Jg ~ 1/

3 CCN g~ ~ g 3000/

4 PLA 5glggbt14$ 1$ 29/

6 BPR 1,8.8E5,1.25E6,8200/8680/

7 BOL 2,2,1,1.5,1.5/

8 BOL 2,6,1 ~ 1.5,12.5/

9 BOL 4,2,1,6.5,1.5/

10 BOL 4/6/1,6.5,12.5/

11 ERO/

12 TUB 3,4,1,3.5,7.5/

13 Ele/

14 POI 3,4/

15 LOA, ~ 1,1445,-1150,1272,22019,12323,-4591/

16 EIN/

17 ERO OF JOB

~~ ERO OF INPUT DATA ~

I%035/11 DATE 92-09-24 PACE ttttttttttttttttttttttttttt PREPROCELNR lNPIJT DATA CARDS 1

ttttlllttlll*tttlllltt t>>>>ttttttttttttt>>ttttttttttttttttltttltlttttlt CARD 3 4 5 6 7 NO 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 3 F ILENANEtNNPSP27 2 OJT 0 0 1 3 CON 0 0 0 0.000 3000.000 0.000 0.000 0.000>> 0.000 4 PLA 51 7 0 8.000 14.000 1.000>> 29.0001 0.000 0.000 5 APR 0 0 1>> 6.000>> 6.000 ~ 2501 .2501 0.000>> 0+000 6 SPR 0 0 11 .880E+061 .125 E+071 ~ 820E+04>> .868E+04* 0.01 0.0 7 aOL 2 2 1.500 1.500 0.000>> 0.000>> 0.000>> 0.000 8 ROL 2 6 11 '1.500 12.500 0.000>> 0.000 0.000>> 0.000 9 ROL 4>> 2 1>> 6.500 1.500 0.000 0.000>> 0.000>> 0.000 10 ROL 4>> 6 11 6.500 12.500 0.000 0.000 0.000>> 0.000 11 END 12 TIN 3>> 4 1>> 3.SDO>> 7.SDO 0.000 0.000>>

13 END 14 POl 3>> 4 0 0.000>> 0.000 0.000>> 0.000 0.000>>

15 LOI 0 0 1* 1445.0>>'1150.01 1272.0 22019.0 12323.0 -4591.0 16 END 17 END OF JM

~ END OF lNPUT DATA DECK ~

m035/11 DATE 92 09e24 PAGE 4 ttttttttttttttt 1 ttt tttt tttttttttttt F ILEXA%tHHPQP27 ttttttttttttttt*ttt tttttttttttttttttttttttttttttttttttttttttt INPUT PARANETERS PLATE THICKNESS...". 1.000

~

PLATE X DIHENSION ~ . 8.000 Y DINENSION ~ ~ ~ ~ ~ ~ ~ 14.000 IRSULUS OF ELASTICITY ". .290E+08 C(RICHE T E IHmULUS ~ ~ ~~ ~ ~~ ~ .312E+07 CONCo CON ~ STRENGTH ~~~ ~ 3000.0 BOLT LOCATIONS BOLT I J NCOE X-COM..Y.COORD 1 2 2 9 1.500 1.500 2 2 6 13 1.500 12.500 3 4 2 23 6.500 1.500 4 4 6 27 6.500 12.500 BOLT PROPERTIES BOLT STIFFNESS (LB/IN.) ALLOMABLE FORCE (LB) eeoeeeoo eo e TENSION SHEAR TENSION SHEAR

~ 880E+06 .125E+07 8200. 868D.

2 .880E+06 .125E+07 8200. 8680.

3 .NOE+06 .125E+07 8200. 8680.

4 .880E+06 .125E+07 8200. 8680.

I%035/11 DATE 92 09 24 PAGE 5

~ ttttttttttttttttttttttttttttttttttt 1

F ILENANEtHNPSP27

~<

ttttttttttttttttttttt t*tttttttttttttttttttttttttttttttttt ATTACHNENT DATA ATTACIWENT NOSER TTPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ TLS PROPERTY NOSER 1 D DINENSION 6.000 I LINE WOOER ~ ~ ~ ~ ~~ 5

~~ ~~ ~

I DINEKSION "o ~ 6.000 J LINE NIWQER 4 HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 X COORD I NATE ~~ ~~~~ ~ 3.500 THICKNESS (T1) ~ ~ .250 Y~COORDINATE ~ ~ ~ ~ ~ ~ ~ 7.500 THICKNESS (T2) .o .250 ORIENTATION ANGLE " 0.0

I%035/11 DATE 92-09-24 t ttt tttttttttttttttttttttettttttatto F lLENANEtNKPSP27 ttttttttttttttttttttt ttttttttttttttttttttttttttttttttttttttttttttttt LOAD1KG COND 1T lONS LOADlNG CASE NO. t 1 LOADlNGS APPLlED AT INmE < 36 FOICE FX t 1445.00 FQtCE FY > -1150+00 FMCE F2 t 1272.00 NUGENT NX t 22019.00 I@KENT NY t 12323.00 INWENT NZ t -4591.00

%035/11 DATE 92.09.24 7 PACE

~ ftttnttlttttt*f14ettlit~i~

f LLENA%~27 014t101ttt404~ HOltl4tttt44ttlttlttOttftttllNtlttO BASEPLATE CONNECT i VITY ELENENT ELENENT ICE NO. JA JB JC J0 NO. JA JQ JC JO 1 1 8 9 2 2 2 9 10 3 3 3 10 11 4 4 4 11 12 5 5 5 12 13 6 6 6 13 14 7 7 8 15 16 9 8 9 16 17 10 9 10 17 18 11 10 11 18 19 12 11 12 19 20 13 12 13 20 21 14 13 15 22 23 16 14 16 23 24 17 15 17 24 25 18 16 18 25 26 19 17 19 26 27 20 18 20 27 28 21 19 22 29 30 23 20 23 30 31 24 21 24 31 ~

32 25 22 25 32 33 26 23 26 33 34 27 24 27 34 35 28

I%035/11 DATE 92-09-24 PACE 8 ttttttttttttttttttttttttttttttttttttt F 1LENA%oNXPSP27

~ ttttt1111111tttt Ottttttttttttttttttttttttttttttt KODAL COORD 1 NATES 1 J F RANE QBE X T 2 L1NE L1NE NME COORD 1 NATE COORD 1 NATE COORD1MATE 1 1 0.000 0.000 0.000 2 2 0.000 1.500 0.000 3 3 0.000 4.500 0.000 4 0.000 7.500 0.000 5 5 0.000 10.500 0.000 6 6 0.000 12.500 0.000 7 7 0.000 14.000 0.000 1 1.500 0.000 0.000 2 9 1.500 1.500 O.NO 3 10 .500 4.500 0.000 4 11 .500 7.5N 0.000 5 12 .500 10.500 0.000 6 13 1.SOO 12.500 0.000 7 14 1.500 14.000 0.000 15 3 ~ 500 0.000 0.000 2 16 3.500 1.500 0.000 3 17 3.500 4.500 0.000 4 18 3.500 7.500 0.000 5 19 3.500 10.500 0.000 6 3.500 12.5N 0.000 7 21 3.500 .14.000 O.ON 1 22 6.SOO 0.000 0.000 2 6.500 1.500 0.000 3 24 6.500 4.5N 0.000 4 25 6.SOO 7.500 0.000 5 26 6.500 10.500 0.000 6 27 6.500 12.500 0.000 7 28 6.500 14.000 0.000 1 29 8.000 0.000 0.000 2 30 $ ,000 1.500 0.000 3 31 8.000 4.500 0.000 32 8.000 7.500 0.000 5 33 8 000 10.500 0.000 6 34 8 000 12.500 0.000 7 $ .000 14.000 0.000 IKSES AT APPL1 CATlON OF LOADS 3 4(0 FFSET) 36 3.500 7.5N 500

%035/11 DATE 92-09-24 PACE 9 fQffQf~1 tilt*1t1**ttlttttttatlltO F lLENA%<NNPSP27 OIIO~t& Atll&NtfPt1ltt~t1tHtkHNPIP CONCRETE STlFFNESS DATA NODE EFFECT lVE CONCRETE NXIE EFFECTlVE CONCRETE AREA STl FF NESS AREA STTFfNESS 1 .562 .183E+06 2 1.312 .426E+06 3 1.125 .365 E+06 4 .750 .243E+06 5 .875 .284E+06 6 1.062 .345 E+06 7 .562 .183E+06 8 1.312 .426E+06 9 3.937 ~ 128E+07 10 5.250 170 E+07 11 '.250 .170E+07 12 4.375

~

~ 142E+07 13 3.062 .994E+06 14 1.312 .426E+06 15 1.875 .608E+06 16 6.000 .195E+07 17 8.625 .280E&7 18 9.000 .292E+07 19 7.250 .235E+07 20 4.625 ~ 150E+07 21 1.875 .608E+06 22 1.687 .548E+06 23 5.062 .164E+07 24 6.750 .219E+07 25 6.750 .219E+07 26 5.625 .183E+07 27 3.937 .128E+07 28 1.687 .548E+06 29 .562 .183E+06 30 1.687 .548E+06 31 2.250 .730E+06 32 2.250 730E+06 33 1.875 .608E+OS 34 1.312 .426E+06 35 .562 .183E+06 SQNAT1ON OF EffECTlVE AREAS > 112.000 PLATE AREA ~ 112.000 TOTAL COlCRETE STlFfNESS ~ 363E+05

~ 1NPUT DATA PROCESSlNO CNPLETE+ *~

I%035/IT DATE 92 09.24 PACE PLOT PLAN VIEM Of TNE BASEPLATE, MNERE TNE X AXIS (CONSTANT J LINES) ARE IKNIZONTAL, ANO TNE Y AXIS (CONSTANT I LINES) ARE VERTICAL, NJJJJJJJJJJJJNJJJJJJJJJJJJ~JNJJJJJJJJJJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJN I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I B I B I NJJJJJJJJJJJBBSJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJBBBJJJJJJJJJJJJN I I I I I I I I I I I I I I I I I

I I I I I I N JJJJJJJJJJJJJN I A I A I A I A I A I A I A I A I A I A I A I A I A I A I A NJJJ JJJJJJJJJJJJJJJJJJJJJJJJJJJAJJJJJJJJJJJJJN I A I A I A I A I A I A I A I A I A A

1.' 1 A 1 I A 1 A 1 KJ JJJJJJJJJJJJJN 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1

1 1

1

=1 1 1

1 1

1 1

1 1 1 1 I 1 1 1 1 1 1 1 1 1 1 I 1 1 1 1 1 1 1 1 I 1 1 1 1 1 1 1 1 1 1 1 1 1 1 I 1 I 1 NJJJJJJJJJJJQBSJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJSSSJJJJJJJJJJJJN 1 I 1 I 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 NJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJN

PROGRAN: NE035 SASKPLATE OMIT S9601 0110 AAH 7083 DATE< 92-09-24 RELEASE 11 NOS/VK 1.5.3 L765 TINE: 13:20:08 PAGE<

tttttttttttttttttt RESIN SOLUTION PNASE t LOA ~ CASK NOq 1 ttttttttttttttttttttttttttt TITLE: F ILERANE&RPBP27 LOAD CASE RO.

(TOP TEN VALUES)

DISPLACENENTS KODE DISPL. IRSE 0 ISPL ~

5 .336246E.02 31 -.809196E-03 6 .328099E.02 30 -.573565K-03 12 .316537E-02 24 -.351397K-03 7 .295519E-02 29 .347650K-03 4 .274493E.02 23 .324636K.03 13 .267462E-02 32 -.285248K-03 11 .255237E.02 22 -.212485K-03 14 .241440E-02 15 .345179K-04 3 .212472E.02 16 .250957E.03 20 .204698E-02 25 .256206E.03 OUADR I LATERAL PLATE PR I NC I PAL STRESSES ELENENTS + Z FACE ELEN SIGNA ELEN SIGNA EL EN SIGNA ELEN SIGNA 5 3119. 11 2907. 17 2324. 20 -1905.

23 1900. 14 -1848. 6 -1181. 13 -1052.

7 -952. 1 -871.

KLENENTS Z FACE EL EN SIGNA ELEN S1GNA ELEN SIGNA EL EN SIGNA 5 -3309. 11 -2695. 17 -2093. 20 1775.

14 1608. 23 -1490. 6 1222. 7 1039.

13 988. 1 881.

CONCRETE LOADS Nmf Z.PRESS RODE 2 PRESS IKOE Z PRESS NCOE 2 PRESS 31 -263. 30 -186. 24 -114. 29 -113.

23 -105. 32 .93. 22 -69. 35 0.

34 0. 33 0.

PROGRANs NE035 SASEPLATE Sos S9601 0110 AAll 7083 DATEs 92-09-24 RELEASE 11 NOS/VE 1.5.3 L765 TlNEs 13s20s28 PAGEs 12 NOLT LOADS N(eE X-SHEAR Y SHEAR SRSS TENS lON 9 183. -201. 272. 660.

13 543. -211. 582. 2354.

23 185. -373. 416. 0.

27 539. -3&5 651. 851 ~

DOLT lNTERACTlON EQIJATlON ENAT10Nt((TENSlON/TALL%)tt 1.000+(SHEAR/SALLOM)tt 1.000))tt 1o000 N(XSE TENS! ON SHEAR TENSTON SHEAR INTERACT SAFETY ALLOM ALLOI RAT10 RAT lO RAT10 FACTOR 9 8200. 8680..081 .031 .112 8.940 13 8200. 8680..287 .067 .354 2.824 23 8200. 8680..001 .048 ~ 049 20.432 27 8200. 8680..104 .075 .179 5.592

~ tttttttttttttttttttttttttttttttttttttttltttt t E N D L 0 A 0 CASE t ttttttttttttttttttttttttttttttttttttttttt*ttt

~ tttttttttttttttttttttttttttttttttttttttttttt t END POSTPROCESS l NQ t ttttttttttttttttttttttttttttttttttttttttttttt

CALC I IKISS/11 9Z-09-ZC PAGE 1 ATfAMNT

'ATE

~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ t~ ~ ~ ~ I~ ~ ~ 0 ~ ~ ~ ~ 0 ~ I~ ~ ~ ~ 0 ~ ~ ~ ~ ~ OF PROJECT JOB NO CALC NO. SHT NO.

PREPARED BY DATE CHECKED BY DATE e 4

~ 0 ~ 1 4 ~ P P 1 0 0 0 ~ 0 0 0 0 t1 0 ~ I~ ~ ~ ~ 0 ~ 0 ~ 1 1 ~

EEEEEEEEE 55555555 EE E 55 EE 55 EEEE 55555555 EE 55 EE E 55 EEEEEEEEE 55555555 VERSION LEASED AUGUST 1989 USER NANUAL VERS ION THEORETICAL NANUAL VERSION: 8 VER IF ICATION NANUAL VERSION: 10

~ ~ 1 ~ 010010 ~ OO ~ IO ~ ~ ~ ~ ~ ~ ~ OOO ~ ~ OOO ~

IN CASE OF PROBLEHS MITII %035/ CONTACT THE

  • BASEPLATE USER REPRESENTATIVES'

~ COPYRIGHT 1984,1987 BECHTEL POUER CORP. ALL RIGHTS RESERVED. *

~ 010 ~ 01* ~ 0 ~ 011101IOO ~ 0 ~ OO ~ 0 ~ ~ 11000 ~ ~

  • IIE035/11 DATE 92 09 24 tttttttttttttttttttttttttttttttttt PREPROCESSOR lNPUT DATA CARDS tttttt* tttttttttttttttttttttttttttttttlttttttttttttttt CARD 3 4 5 6 7 8 NO 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 3 FlLENANEtHNPBP28 2 OIT ~ ~ ~ 1/

3 CON g g ~ g 3000/

4 PLA 6,7,$ 10,10/1/29/

5 SPR g ~ 1/8.8E5,1.25E6,6020,5210/

9 SOL 5,5,1,8,8/

10 END/

11 ATT 3$ 4gg4.5,6.25/

12 JST 3,4,2,2.5,180/

13 lST 2,4,5,1,75/90/

14 1ST 2$ 5$ 6$ 75 90/

15 JST 2,6,4,5,0/

16 1ST 4,6,5,e75g270/

17 1ST 4,5,4,1.75,270/

18 lST 4,4,3,2.5,270/

1 JST 4,3,2,5,180/

T 2,3,4,2.5,90/

/

END/

23 POl 3,4/

24 LOA 1,913,-1355,1788,30537,9486,10763/

25 END/

26 END OF J08 t END OF 1NPUT DATA ~

%035/11 DATE 92 09.24 PACE 3 ttttt>>>>tttttttt>>tttt>>tttttt>>ttt>>>>

PREPROCESQS INPVT DATA CARDS ttt>>t1*ttttttt t>>tttt>>1111*11111>>ttttttttttttttt>>

CARO 1 2 =-- -3 4 5 6 7 8 No 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 3 FILENAKE>>KNPBP28 2 OJT 0 0 1 0 3 CQI 0 0 0.000 3000.000 0.000 0,000 0.000 0.000 4 PLA 6>> 7 10.000 10.000 1 ~ 000>> 29.000 0.000 0.000 5 BPR 0 0 1>> .880E+06>> .125 E+071 .602E+04>> .521 E+04'.000 0.0 0.0 6 BOL 2 2 1>> 2.000 2.000 0.000 0.000 0.000 7 BOL 2 5 1>> 2.000 8.000 0.000 0.000 0,000 0.000 8 BOL 5>> 2 1>> 8.000 2+000 0.000 0.000 0.000 0.000 9 BOL 5'>> 5 11 8,000 8.000 0.000 0.000 0.000 0.000 10 ENO 11 ATT 31 4 4.500 6.250 0.000>> 0.000 12 JST 3>> 4 2.500 180.000 0.000 13 IST 4 5 1+750>> 90.000 0.0001 14 IST 2 5 6>> .75O 90.000 0,000 15 JST 6 41 5.000 0.000 0.000 16 I ST 4 6 5>> .7501 270.000 0.000 17 IST 4 5 4* 1.750>> 270.000 O.OOO>>

18 1ST 4>> 4 3>> 2.500 270.000 0.000 1 T 4 5.000>> 180.000 0.000 2 3 4>> 2,500 90.000 0.000>>

22 END 23 Pol 3* 4 0 0.000 0.000 0.000 0.000 0.000 24 LOA 0 0 1>> 913.0 .1355.0 1788.0 30537.01 9486.0 10763.0 25 END 26 END OF JOB

~ ENO OF INPUT DATA DECK ~

NE 035/11 DATE 92-09-24 PAGE 4

~ ttttttttttttttttttttttttttttttttttt F ILENA%tHHPQP28 t

tttttttet tttttttttttttttttttttttttttttttttt INPUT PARAHETERS PLATE THICKNESS ~ ~ ~ ~ ~ ~~~ 1.000 PLATE X-DIHENSION ....... 10.000 Y OIHENSION ...... 10.MO NCOULUS OF ELASTICITY ... ~ 290E+08 CONCRETE INmULUS ~ ~ ~ ~ ~ ~ ~ ~ .312E+07 CONC. CSP. STRENGTH o." 3000.0 BOLT LOCATIONS BOLT I J NME X-COORD., Y-COORD.

1 2 2 9 2.000 2.000 2 2 5 12 2.000 8.000 3 5 2 30 8.000 2.000 4 5 5 33 8.000 8.000 BOLT PROPERTIES BOLT STIFFNESS <LB/IN.) ALLOIABLE FORCE (LB)

TENSION SHEAR TENSION SHEAR 1 .880E+06 .125E+07 6020. 5210.

2 .880E+06 .125E+07 6020. 5210.

3 .880E+06 .125E+07 6020. 5210.

.880E+06 .125E+07 6020. 5210.

I%035/11 DATE 92 09-24 PAQK 5 tttttttttttttttttttttttttttttttttttt F ILENA%iHNPSP28 t*ttttttttt ttttttlttttttttttttttttttttttttttttt ISN. STANDARD ATTACHHENT DATA ATTACHHENT IRNSER 1 SEGHENT NOBER ~ ~~ ~~ ~ ~ ~ ~ 1 TYPE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ JST HEIGHT ~ ~ ~ ~ ~ ~ ~ o~~~ ~ ~ ~ ~ ~~ 0.000 D I STANCE ~~~~~~~ ~ ~ ~ ~~ ~~ ~ 2.500 ORIENTATION ANGLE ."". 180e0 THICOESS ~o~~o~~ ~~ ~~ ~~ ~ 0.000 SKQNKNT NQIER ~~~~~~~~ ~ 2 TYPE ~~ ~~~~~~~~~~~~ ~~~~~ IST HEIGHT ~~~~~~~ ~ ~~~~~ ~ ~ ~~ 0.000 D I STANCE ~~~~~~ ~~~ ~ ~ ~~~~ 1.750 ORIENTATION ANGLE ..o" 90.0 THINESS ~~~~~~ ~ ~ ~ ~ ~~ ~ ~ 0.000 SEGNENT NSER ~~ ~ ~ ~ ~~ ~ ~ 3 TYPE ~ ~ ~ ~ ~ ~~~~~~~~~~~~~~ IST HEIGHT ~ ~ ~ e ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ .750 ORIENTATION ANGLE ~ ~ ~ ~ ~ ~ 90.0 THICOESS ~~~~~~~o~ ~~~~~ 0,000 SEQNENT NNSER ~~ ~ ~ ~ ~ ~~~ 4 TYPE ~~ ~~~ ~ ~ ~~~~~ ~~ ~~ ~~~ JST HEIGHT ~~ ~~~ ~ ~~~~~~~ ~~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 5.000 OR!ENTATION ANGLE .". ~ 0.0 THICOESS ~ ~ ~ ~ ~ ~ ~~~~~~~~ 0,000 SEGHENT IRNSER ~~~~ oooo ~ 5 TYPE ~~~~~~~o~ ooo ~~~~~~~ IST HEIGHT ~ ~ ~ ~ ~ oooooee ~ oooo 0.000 DISTANCE ~ ~ eeo ~ ~ ooo ~ ~ ~ ~ ~ .750 ORIENTATION ANGLE 270.0 THICOESS ~ ~ ~ ~ ~ ooo ~ ~ ~ o ~ e 0.000

I%035/11 DATE 92 09-24 PACK 6

~ ttttt1 11 1 1 1 1 11 1 1 1 1 ttt1 ttt1 tttttttttt1 1 tt1

~ P ILENA%tHNPSP25 11 ttt1ttttttktt1111 ttttttttttttttttttttttttttttttttttttttttttttt NON STANDARD ATTACHNENT DATA SKGNKNT NQSER "....." 6 TYPE ~ ~ ~ ~ ~~~~~~~~~~~~o~~ IST HEIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 1.750 ORIENTATION ANGLE .. 270.0 TNINESS ~~~ ~~ ~~~~ ~ oo ~~ 0 000 SKINT NSER ~ ~ ~~~ ~ ~ ~ ~ 7 TYPE ~ ~~~~~~~~ ~~~~~~~~~~ IST HEIGHT ~ ~ ~ ~ ~ ~~ ~~ ~ ~ ~~~~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 2.500 ORIENTATION ANGLE ."... 270.0 THINESS ~~~~~~~ ~~ ~~ ~ ~ ~ 0.000 SKGHKNT NQSER ~~ ~~~ ~~ ~~ 8 TYPE ~~~ ~ ~~~o~~~~~~ ~~~ ~~ JST NKIGHT ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ o ~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 5.000 ORIENTATION ANGLE .... 1SO.O THINESS ~~~~ ~~ ~~~ ~ ~ ~ ~~ 0.000 SECANT NLSOER ~~ ~~ ~~ ~~ ~ 9 TYPE ~~~~~~ ~ ~~ ~ ~~ ~~~ ~ ~ ~ ~ IST HEIGHT ~~~~~ ~~~ ~ ~o~~ ~~ ~ ~ 0.000 DISTANCE ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 2.500 ORIENTATION ANGLE ."... 90.0 THICQIESS ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 0.000

NE 035/11 DATE 92 09 24 PAGE y*~y~~yyyyiiilOPOPteltll11*OIOOtOtlOtttlOO F lLENANE<NNPBP28

~ PIIIIOIOIIPIOI ~&Ottt101111&OIPP14100111111110fii101t LOADlNG CONDlTlONS LQADlNG CASE NO. ~ 1 LOADlNGS APPLIED AT NODE ~ 43 FORCE FX > 913.00 FORCE FY ~ -1355.00 FORCE F2 ~ 1788.00 NOIENT NX ~ 30537.00 NINENT NY ~ 9486.00 lKNENT NZ ~ 10763.00

NE035/1'1 DATE 92-09-24 PACE 8 11I I ttttttlttt ttttlttltllttttltl*lltltlllttttttt F l LENA%IHNPQP28 I

Itltllltttltttt ~ tttttttttttttttttlttttttttttttttttttttttttt BASEPLATE CONNECT lVlTY ELENENT CIE ELEKENT SSE NO. JA JS JC JD NO. JA JB JC JD 1 1 8 9 2 2 2 9 10 3 3 3 10 11 4 4 4 11 12 5 5 5 12 13 6 6 6 13 14 7 7 8 15 16 9 8 9 16 17 10 9 10 17 18 11 10 11 18 19 12 11 12 19 20 13 12 13 20 21 14 13 15 22 23 16 14 16 23 24 17 15 17 24 25 1d 16 1d 25 26 19 17 19 26 27 20 18 20 27 28 21 19 22 29 30 23 20 23 30 31 24 31 . 32 25 22 25 32 33 26

~a 33 34 27 24 27 34 35 28 36 37 30 26 30 37 38 31 27 31 38 39 32 28 32 39 40 33 29 33 40 41 34 30 34 41 42 35

NE 035/11 DATE 92-09-24 PAGE 9 ititiieiii ~ tttttttttttttttttttttttttttttttttttttttttttttt t

F ILENANEtHNPSP28 t

~ titttttttttt*tttttttt ttttt*ttttttttttttt*ttttttititttit*tttt**tt*ttt lNSAL COOS I NATES I J FRANK IKSE X Y 2 LINE LINE INSE COORDINATE COORD I NATE COORDINATE 1 1 1 0.000 D.DDD 0.000 1 2 2 0.000 2.000 0.000 1 3 3 0.000 3.750 0.000 1 4 4 0.000 6.250 0.000 1 5 5 0.000 8.000 0.000 1 6 6 0.000 8.750 0.000 1 7 7 0.000 10.000 0.000 2 1 2.000 0.000 0.000 2 2 9 2.000 2.000 0.000 2 3 10 2.000 3.750 0.000 2 4 11 2.000 6.250 0.000 2 5 12 2.000 8.000 0.000 2 6 13 2.000 8.750 0.000 2 7 14 2.000 10.000 0.000 3 1 15 4.500 0.000 0.000 3 2 16 4.500 2.000 0.000 3 3 17 4.500 3.750 0.000 3 18 4.500 6.250 0.000 3 5 19 4.500 8.000 0.000 3 6 20 4.500 8.750 0.000 3 7 21 4.500 10.000 0.000 4 1 22 7.000 0.000 0.000 4 2 23 7.000 2.000 0.000 4 3 24 7.000 3.750 0.000 7 000 6.250 0.000 4 5 26 7.000 d.000 0.000 4 6 27 7.000 8.750 0.000 7 28 7.000 10.000 0.000 5 1 29 d.000 0.000 0.000 5 2 30 d.000 2.000 0.000 5 3 31 d.000 3.750 0.000 5 4 32 8.000 6.250 0.000 5 5 33 8.000 8.000 0.000 5 6 34 8.000 8.750 0.000 5 7 35 8.000 10.000 0.000 6 1 36 10.000 0.000 0.000 6 2 37 10.000 2.000 0.000 6 3 38 10.000 3.750 0.000 6 4 39 10.000 6.250 0.000

I%035/11 OATE 92-09-24 PACE 10 ttttttttttttttttttttt t ttt1 tttt1 ttttt F TLEXA%tNNPSP28 ttttttttttttttttttttttttttttttttttttttttttt11ttttttttttttt1tttttttttttttt11tttttttttt INSAL CXRD I NATES l J FRAIS INBE X Y 2 L 1NE L lKE NME COOS l NATE l COORD NATE COOROl NATE 6 5 40 10.000 8.000 0.000 6 6 41 10.000 8.750 0.000 6 7 42 10.000 10.000 0.000 INSES AT APPLlCATlON OF LOADS 3 4(OFFSET) 43 4.500 6.250 .500

m 035/11 DATE 92-09-24 PACK 11 MOO*~yrtOOot4tOt1t11000t10tttOW1 fILENA%<NNPSP28

~ t0110lttlttltOtt~tt& &ttOI1**1111t1tiltt1111114ttt11tOOtttttt1tt CONCRETE STIFFNESS DATA INSE EF FECT IVE CONCRETE INSE KFFECT I VE CONCRETE AREA STIFFNESS AREA STIFFNESS 1 1.000 .336E+06 2 1.875 .630E+06 3 2.125 .714E+06 4 2.125 .714E+06 5 1.250 .420E+06 6 1.000 .336E+06 7 .625 .21 DE+06 8 2.250 .756E+06 9 4.219 .142E+07 10 4.781 .161E+07 11 .4.78'I .161E+07 12 2.812 .946E+06 13 2.250 .756E+06 14 1.406 .473K+06 15 2.500 .840E+06 16 4.687 .158E+07 17 5.312 .179K+07 1d 5.312 .179E+07 19 3.125 .105E+07 20 2.500 .840E+06 21 1.562 .525E+06 22 1.750 .5ME+06 23 3.281 .110K+07 24 3.719 .125E+07 3.719 .125K+07 26 2.1d7 .735E+06 1.750 .588K+06 28 1.094 .368E+06 1.500 .504E+06 30 2.812 .946Ei06 31 3.187 .107E+07 32 3.187 .107E+07 33 1.875 .630E+06 34 1.500 .504E+06 35 .937 .315K+06 36 1.000 .336E+06 37 1.875 .630K+06 38 2.125 .714E+06 39 2.125 .714E+06 40 1.250 .420E+06 41 1.000 .336E+06 42 .625 .210E+06 SLNIATION Of EFFECTIVE AREAS ~ 100.000 PLATE AREA ~ 100.000 TOTAL CONCRETE STIFFNESS ~ .336E+08

~ INPIIT DATA PROCESSINQ CCHPLETE. ~

I%035/11 DATE 92 N.24 PACE P PLOT PLAN VIEN Of TME BASEPLATE'WE THE X AXIS (CONSTANT J LINES) ARE IKNI?OITAL, AMD THE Y AXIS (CONSTANT I LINES) ARE VERTICAL.

NJJJJJJJJJJJJJNJJJJJJJJJJJJ 4444JJKJJJJJJJJJJJJJJJJJJNJJJJJJJMJJJJJJJJJJJJJJN I I I I I I I I I I I I I I I I I I I I I I NJJJJJJJJJJJJJ JJJJJJJNJJJJJJJJJJJJJJM I A I A I I I A I A I I I A I A 8 I NJJJJJJJJJJJJJAJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJAJJJJJJSBBJJJJJJJJJJJJJM I A I A 8 I I A I A I I I A I A I I I A I A I I I A I A I I I A A I I A I A I I I A I A I I NJJJJJJJJJJJJ JJJJJJJJJJJJJJJJJAJJJJJJJNJJJJJJJJJJJJJJN I A I A I I I A I A I I I A A I I I A I A I I I A A I I I A I A I I I A I A I I I A I A I I I A I A I I I A I A I I I A I A I I NJJJJJJJJJJJJJ JJJJJJJMJJJJJJJJJJJJJJN I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I 8 I I 8 I NJJJJJJJJJJJJSSSJJJJJJJJJJJJJJJJJJMJJJJJJJJJJJJJJJJJJMJJJJJJBSSJJJJJJJJJJJJJM I 8 I I 8 I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I NJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJJNJJJJJJJJJJJJJJJJJJNJJJJJJJNJJJJJJJJJJJJJJM

PROGRAN: NE035 SASEPLATE SNQI: S9601 0110 AAII 7081 DATE: 92.09-24 RELEASE 11 NOS/VE 1.5.3 L765 TINE: 12:34)25 PAGE: 13 1111111111111111

~ E 0 I N S 0 L U T I 0 N P N A S E L 0 A 0 C A S E N 0:

~ ~~ttttttttttttttttttttttttttttt1111tt TITLE: FILENANEtHMPSP28 LOAD CASE NO.

(TOP TEN VALUES) 0 I S P L A C E N E N T S NME 0ISPL. NtIE 0 ISPL ~

7 .60'l470E.02 22 -.643703E 03 14 .557485E.02 15 e.637019E.03 6 .509943E.02 23 e.621235E 03 21 .501649E.02 30 -.617772E.03 13 .466271Ee02 29 -.587693E.03 5 .454994Eo02 37 -.526119E-03 28 ~ 445364E-02 36 -.474248E.03 35 .416473E-02 8 e.441528E 03 12 .411625E.02 16 e.320971E.03 20 .410428E.02 1 e.218181E 03 QUADR I LATERAL PLATE PRINCIPAL STRESSES ELENENTS + Z FACE ELEN SIGNA ELEN SIGNA ELEN SIGNA ELEN SIGNA 20 .5840. 14 5409. 8 .4144. 26 e 3632.

2 e 2977. 23 1986. 13 e 1973. 27 e 1963 24 1687. 22 1555.

ELENENTS 2 FACE ELEN SIGNA ELEN SIGNA ELEN SIGNA ELEN SIGNA ee oooo ooo 20 5998. 14 S369. 26 3725. 8 3655.

2 2464. 27 2092. 13 1858. 23 o 1694.

24 e 1548. 7 1533.

CONCRETE LOADS NtOE ZoPRESS SSE 2 PRESS NRE ZePRESS INOE Z.PRESS 22 e 216. 1S -214. 23 e 208. 30 e208.

29 e197. 37 e177. 36 e 159. 8 e 148.

16 .108. 38 e73.

PROGRAN! NESS SASEPLATE SIRRII S9601 0110 AAN 7081 DATE: 92-09 24 RELEASE 11 NOS/VE 1.5.3 L765 T INE: 12:34 46 PAGE: 14 a 0 L T LOADS N(HIE X SHEAR T SHEAR SRSS TENSlON 9 654. -761. 1004. 96.

12 -199. -792, 817. 3622.

30 652. 91. 658. 0.

33 -194. 102. 219. 2372.

80LT INTERACT lON EOUAT lON EGUATlONt((TENSlON/TALL(N)tt 1.000+(SHEAR/SALLOI)tt 1.000))tt 1.000 IKCE TENS lON SHEAR TENS lON SHEAR INTERACT SAFETY ALL(HI ALLCM RATIO RATIO RAT10 FACTOR 9 6020. 5210. .016 .193 .209 4.795 12 6020. 5210..602 .157 .759 1.318 30 6020. 5210..001 .126 .127 7.853 33 6020. 5210..394 .042 .436 2.293

~ ttttttttkttttttttttttttttttttttttttttttttttt END LOAD CASE ttttttttttttttttttttttttttttttttttttttttttttt

~ tttttttttttttttttttt*tttt**tt**tt*tttttttttt

  • END POSTPROCESS l NG 11***tttttttttt*t*t*tt*tttt*tttt*t*tttttttttt

Pile f CALC ID TTACHMENT CP!tL uNn f NED G93 ZNTERDZSCZPLZNE REVIEW REQUEST (ZRR)

ZRR fs Tos

~>/RET/ggggPCN

'nit/Subunit Ps Plant ~~

Froms j .t/Subunit, Details of Review Requests REFERENCE - PCR-6547, DELETION OP RELIEF VALVES AND ADDITION OP ORIPZCES AND STRAINERS ~

ATTACHED ARE THE SIGNED OFF SUPPORT LOAD SHEETS POR PCR-6547 AS WE KNOW IT AS OP 12s00 P.M.

ON SEPTEMBER 25, 1992 ~ PLEASE USE THESE LOADS IN YOUR SUPPORT DESIGNS AND EVALUATIONS FOR THE ABOVE MENTIONED PCR. THESE, LOADS ARE AS GOOD AS THE INFORMATION USED TO DEVELOP THEM SINCE NO APPROVED DRAWINGS HAVE BEEN RECEIVED AS OP THIS WRITING+

IP THERE ARE ANY QUESTIONS PLEASE CONTACT JOHN HOPKINS AT X-6734 ~

sponse Required Bys Responsible Supervisor/Data Authorised Man-hours Charge Number MAPS Project No.s - 7 Phases Activity:

Response/Justifications Attachments (liat) s Responsible Supervisor/Date Actual Man-hours expended Distributions NED Guideline No. E-24 Revision 4 (EO6d/rlj

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