ML20136F276
| ML20136F276 | |
| Person / Time | |
|---|---|
| Site: | Trojan File:Portland General Electric icon.png |
| Issue date: | 04/30/1984 |
| From: | ABB IMPELL CORP. (FORMERLY IMPELL CORP.) |
| To: | |
| Shared Package | |
| ML20136F274 | List: |
| References | |
| 01-0300-1291, 01-0300-1291-R00, 1-300-1291, 1-300-1291-R, NUDOCS 8601070332 | |
| Download: ML20136F276 (89) | |
Text
{{#Wiki_filter:.. . - .. . .. -. .. . . . . - . - - - . _. l Trojan Nuclear Plant Mr. Steven A. Varga
- ;- Docket 50-344 Attachment l l License NPF December 31, 1985 Reference 8
..r i TROJAN NUCLEAR POWER PLANT MODIFICATION AND STRESS ANALYSIS REPORT
. FOR THE PRESSURIZER SAFETY AND RELIEF VALVE
!' LARGE-BORE PIPING SYSTEM f 1
.i
, i f l p Submitted to . Portland General Electric Company 121 Southwest Salmon Street , Portland, Oregon 97204 <L o
- 'I
- .t
'l Prepared by Impe11 Corporation
, 350 Lennon Lane
- j. Walnut Creek, California 94598 i ! Impe11 Report No. 01-0300-1291 I Revision 0 f
, j April 1984 . l 8601070332 851231 PDR ADOCK 05000344
- p PDR
'I ~ .l - i
l O l i i M PELL 4 r APPROVALCOVERSHEET ~ i Trojan Nuclear Power Plant Modification and Stress Analysis DOCLNnent
Title:
Renort for the Pressurizer Safety and Relief Valve Lare-Bore Piping g g g 01-0300-1291 n . Portland General Electric 0300-018
, gg ,g g Project' Trojan Nuclear Power Plant 1, Revision Record -
... o.. %. , %,
W '-T A . anW g/04fd
-i-
, I i
( CERTIFICATION The undersigned, a registered Professional Engineer, competent in the field of piping stress analysis, certifies that to the best of his knowledge and belief the analysis calculations for the subject piping system as presented in this Stress Report comply with the requirements of the Design Criteria and the applicable portions of the ASME Soiler and Pressure Vessel Code, Section III, Neclear Power Plant Components. This report meeting the intent of ANSI B31.7, L Nuclear Power Piping, and ANSI B31.1, Power Piping. Piping System: Pressurizer Safety and Relief Valve Large Bore Piping System Plant: Trojan Nuclear Power Plant q@ FESS 10g7
~~
heu /(rfRsL.IbsIf84 W No.17230 Name Date A 4 Q"$# State of California Registration No.: M - '723o ke, I! I I l ll I i 11 l l
1 l TABLE OF CONTENTS O Page Report Approval Cover Sheet i Certification 11 1.0 Introduction 1-1 2.0 System Description 2-1 L 2.1 Physical Description 2-1 2.2 System Function 2-2 3.0 System Qualification Criteria 3-1 l 3.1 Applicable Codes and 3-1 3 Design-Related Requirements 3.2 Supplemental Design Requirements 3-1 4.0 Modification and Analyses Performed 4-1 p 4.1 Slug Diversion Devices 4-1
, () 4.2 Thermal-Hydraulic Analysis 4-4 4.3 Piping Analysis 4- 7 5.0 Analysis Results 5-1 5.1 Thermal-Hydraulic Analysis 5-1 a 5.2 Class 1 Piping Stress Evaluation 5-1 l 5.3 Class 3 Piping Stress Evaluation 5-6 5.4 Supplemental Design Requirements 5-7
'f 6.0 Conclusions 6-1 7.0 References 7-1 Appendix A: Mathematical Model A-1 Appendix B: Computer Programs Description B-1 Appendix C: Component Load Sumaries C-1 l l 'I LO . iii
Report No. 01-0300-1291 Revision 0
1.0 INTRODUCTION
This report, prepared by Impell Corporation, describes the modification and stress analysis for the Pressurizer Safety and Relief Valve Large Bore-Pipino ' System of the Trojan Nuclear Power Plant. The purpose of this work is to assist Portland General Electric Company (PGE) in meeting the requirements of NUREG-0737, Section II.D.1. The NUREG requires a plant-unique verification of the function and integrity of the reactor coolant system safety, relief, and block valves, in conjunction with associated piping and support systems. The verification is based on a generic test program completed by Electric Power Research Institute (References 7.7a and 7.7b). The engineering services provided by Impell do not include the verification of safety, relief, and block valves, and the support modification / design for the Pressurizer S/RV Piping System. The piping and valve resultant interface data have been transmitted to PGE for further review and verification (References 7.4f, 7.4g, and 7.4j). Sunenaries of the final as-built results are presented in Appendix C of this report. The qualification of the Pressurizer S/RV Piping System consists of thermal-hydraulic analysis, using EPRI approved computer codes RELAP5/M001 and IO REFORC2, and complete piping stress analysis, using Impell proprietary piping computer codes SUPERPIPE and TRANS2A. This qualification work was organized in the following three tasks: Task 1. Initial analyses under PGE Purchase Order N-21350: Tne original as-built piping system was evaluated by both thermal-hydraulic and piping analyses. These analyses indicated the need to modify the piping system to mitigate the effects of loop seal water discharge and related seismic qualification. Task 2. Modification and analyses under PGE Purchase Order N-24350: The original piping system was modified by Installing slug Diversion Devices (SDD's) to trap the loop seal water and provide substantial load reduction on the piping downstream of the 500's. Thermal-Hydraulic and piping analyses were performed for the modified system. The analyses results, as sumarized in Reference 7.4b, have demonstrated satisfactory qualification of the Pressurizer S/RV Large-Bore Piping System to the criteria contained in Section 3.0. Several small-bore branch lines are connected to the large-bore piping system for vent, drain, or sampling purposes. These lines were analyzed and qualified (Reference 7.4h). i 'O i~ 1-1
i
~
l Rep No 01-0300-1291 Task 3. As-built review under PGE Purchasc Order N-24350: Finally, an as-built review of the modified piping system was performed to incorporate all changes identified during the installation stage of the modification. Analysis results as sumarized in Reference 7.41 demonstrated satisfactory qualification to the criteria contained in Section 3.0. The resultant as-built loading transferred to the small-bore systems " is discussed and documented in References 7.4k and 7.41. This report sumarizes the modification, final analysis results and I qualification (Tasks 2 and 3) of the Pressurizer S/RV Large-Bore Piping I System. The initial analysis (Task 1) results have been documented elsewhere (References 7.4c and 7.4d). Section 2.0 of this report is a detailed description of the Trojan Pressurizer S/RV Piping System and its function. Section 3.0 describes the system qualification criteria: the ANSI B31.7 Code check for the Class 1 piping qualification, the ANSI B31.1 Code check for the Class 3 piping qualification, and the supplemental oesign requirements. Section 4.0 desc'.ibes the modif! cation and the thermal-hydraulic and piping analyses performed, while Section 5.0 sumarizes the analysis results. A copy of the final mathematical model and resultant component loading (requiring PGE review) are provided in the Appendices of this repnrt. The work has been performed in accordance with the Impell Quality Assurance Program, which complies fully with applicable regulatory requirements and industrial codes and standards. i e i i 1-2 ;
i Re No 01-0300-1291 2.0 SYSTEM DESCRIPTION 2.1 Physical Description The Trojan Pressurizer S/RV Pipin the pressurizer relief tank (PRT)g System
. extends from Major components of thethe pressurizer system, as to shown on the schematic drawing Figure 2.1-1, are:
. Four pressurizer nozzles, one for each discharge line.
Two power-operated relief valves (PORV), sharing a common pressurizer nozzle.
. Two motor-operated block valves, each of which is associated with a PORV.
- Three spring-loaded safety valves, each of which is connected to a
- pressurizer nozzle.
- The connecting piping which incorporates the valvis mentioned above q
and extends from the pressurizer to the PRT. ,
- The PRT nozzle which connects the common header of the piping to the PRT.
- Miscellaneous small vent, drain, and sampling lines.
l On the safety valve side, independently connected to three of the four t pressurizer nozzles are 6-inch Schedule 160 lines with one safety valve each. Downstream of the safety valves, the three discharge lines run as independent 6-inch Schedule 405 lines to three separate 12 x 12 x 6-inch . tees. A common 12-inch Tchedule 40S discharge line continues to the PRT, which has been designed to accommodate the discha'ge of the Pressurizer S/RV Piping System. On the PORV side, each PORV is connected upstream to a block valve through an independent 3-inch Schedule 160 line. These two 3-inch lines I
- are connected to the fourth pressurizer nozzle by a common 6-inch
- l Schedule 160 line. A single 6-inch Schedule 40S line connects the
- downstream PORV piping to the PRT by way of a 12-inch header, which is connon to the safety valve discharge piping.
The upstream piping of the safety and relief valves is classified as ANSI ' B31.7 Class 1 pipe and the downstream piping as ANSI B31.7 Class 3 pipe. Note that ANSI B31.7 specifies ANSI B31.1 for design and qualification O . 2-1 L_._ _
I Report No. 01-0300-1291 I Revision 0 i O of Class 3 piping. The upstream piping of the safety and relief valves is shaped to form a loop seal which collects condensate as a result of normal heat losses to the ambient enviroment. This accumula- tion of water in the loop seals prevents leckage of steam or hydrogen gas through valve seats, thereby greatly reducing valve deterioriation. On the other l hand, the discharge of the loop seal water through the valves and j downstream piping created significant thermal-hydraulic loads on the piping system. The two 3-inch PORVs, designated as PCV 46sA and PCV 456, were manufac-tured by Copes-Vulcan, Inc., and are listed as Model 0-100-160 with a design setpoint presure of 2,350 psig. The three 6-inch spring-loaded safety valves, designated as PSV 8010A, B, and C, were manufactured by Crosby Valve and Gage Company and are listed as Model HB-BP-86 (6M6) with a design setpoint pressure of 2,485 psig. The two 3-inch motor-operated block valves, designated as M0 8000A and B, were manufactured by Velan Engineering Company with a Limitorque motor operator in the vertical position. The system was modified by adding four Slug Diversion Devices. The description of the 500s is detailed in Section 4.1. 2.2 System Function The Troaa n Pressurizer S/RV Piping System is dest;ned for overpressure protection and transient pressure control of the pressurizer, through lifting of the PORVs and safety valves. The function of the PORVs is to open and relieve system pressure, when the pressure increase, caused by a change in the plant electrical load, is greater than the pressure-limiting capabilities of the Pressurizer Spray System. These valves open automatical'iy at a setpoint pressure below system design pressure. They can also be opened manually from the control room. The function of the self-actuating safety valves is to upen and relieve system pressure should the pressure continue to rise after actuation of the PORVs. Both PORVs and the safety valves also act as pressure boundaries to the RCS during normal operations. The motor-operatsd block valves isolate the PORVs should the PORVs start to leak. O' I 2-2
O O O l - { SDD (TYP.) ! 12"x 6 C 12" M h 3/4" 3/4" 6" 6" 6" 6" PSV8010C PSV8010B PSV8010A l } 6"x 3" t= 3/4" c= c= 4" p l
. T i 3= 3" l 4 3/4" y 3/4" 53/4" I ,
j PCV455 PCV455A j 6" 6" C' I M08000B MOB 000A
\\\\\
j 6 x 3- Anc a Ar PRPSSURIZ2R ! 3/4" b 6" 0 M h'T
\ M T\%
~
l \-
. ANCHOR AT FRESSURIZER (700R LOCATIONS) i, l
Figure 2.1-1: Schematic Of The Trojan Presserizer S/RV Large-bore Piping System
l l Report No. 01-0300-1291 ) Revision 0 ,1 O i 3:0 SYSTEM QUALIFICATION CRITERIA 3.1 Applicable Codes and Design-Related Requirements lhe codes of record for the Trojan Nuclear Power Plents are the ANSI B31.7, Nuclear Power Piping, 1969 Edil. ion, including all addenda through 197' for the Class 1 pipir:0 (upstream of the safety and relief valves) and the ANSI B3).1, Power Piping, 1973 Edition for the Class 3 piping l (downstream of the safety and relief valves). The computer analysis code l checking uses ASri Sotier and Pressure Vessel, Section III, ',974 Edition equations. Modification (i.e., stvess indices, etc.) to these equations have been raade to insure code of record intent has been met. u Several exceptions to the codes of record have been used, due to either unavailable code rulings for the Trojan codes of record or the relief of conservatism found in later cod 2s. These exceptions are: f, For Class I cnd Class 3 flange evaluations: the ASME Boiler and l Pressure Vessel Code, Section III, Nuclear Power Plant C aponents, i 1977 Edition, Summer '79 Addenda. For the branch connection stress intensification factor: the ASME B&PV Code, Sect 16n III, Nuclear Power Plant Components, 1974 Edition, hf ' Sumer '74 Addenda. ,
. For the buttwelding tee stress index Bl: the ASME B&PV Code, Section III, Nuclear Power Plant Components,1977 Edition, Sumer '79 Addenda.
The main desica document in the qualification of the Pressurizer S/RV Piping System is the PGE Trojan Nuclear Plant Pressurizer Blowdown Piping Analysis Design Criteria, Revision 0 (Reference 7.2a), Revision 1 (Reference 7.2b), Additional Design Criteria (Reference 7.2c), Revision 2 (Reference 7.2d)and Revision 3 (Reference 7.2e). Additional documents for design data ir. formation are referred to as appropriate throughout the report. 3.2 Supplemental Design Requirements In addition to the code stress evaluations for the piping components, there are supplemental analysis and design requirements applicable to the qualification of the piping system. These supplemental requirements involve the pipe boundary loads and displacements which have been either qualified by Impell or transmitted to PGE for further review and qualification. Those requirements qualified by Impell are: O 3-1 l
,_ . - . - . . ~ - . - . - - .-. . . . . __. . ..- _ - . .. - .. _- _ _ . . - _
Report No. 01-0300-1291 1 Revision 0 l O I - Class 1 ar.d Class 3 flange connections at the safety valves and the PRT.
- Trunnion pipe support to pipe attachments.
- Anchor to pipe interface.
- Sleeve clearance for the floor penetration.
- Small-bore brarch connection displacements.
All of the above requirements are qualified by this report except for the j small-bore branch displacements. These displacements are qualified by References 7.4k and 7.41. 1 Those loads transmitted to PGE for their review and approval are:
- Pipe support loads. <
l Valve acceleretions. n - Valve end 1 pads.
- }
i1 - Nozzle loads at the pre;surt2er and TRT. i .I. ;
- I i f
I h 8 l l Q 3-2
e Report No. 01-0300-1291 Revision 0 0 4.0 MODIFICATION AND ANALYSES PERFORMED I i 4.i Slug Diversion Devices The initial analyses (Task 1) of the Trojan Pressurizer S/RV Piping System, as documented in Referer.ces 7.4c and 7.4d, indicated unacceptably h'igh levels of stresses and support loads in a major portion of the piping system. The hydrodynarric loads induced by the impact of the loop seal water discharged following valve actuation was the major cause of the high stresses and support loads. To resolve this problem, various nptions to mitigate or eliminate the effects associated with the loop seals were investigated. These options included:
- 1. Removir.g the loop seal water by pipe routing changes.
- 2. Removing the loop seal water by continuous draining.
- 3. Heating the loop seal water by heat tracing.
. 4. Trapping the loop seal water slug by installing Slug Diversion Devices (500's). After discussing with PGE the various options, it was decided that the best option for Trojan was to trap the loop seal water slug by installing SD0's. The 500's are dead-end branches with small drain lines. They are installed at appropriate elbows downstr m m of the safety and relief valves. With these devices,the loop seal water will be driven into and tripped in the dead-end branches, thus providing substantial load reduction in the main discharge piping. PGE provided details on four SDD's to be installed at Trojan: one for both PORVs and one for each of the three safety valves. Impell then evaluated each device based on location, orientation, size, and drain pipe diame:er. These parameters rre assessed by an:lyzing the slug motion through hand calculations supplem?nted by RELAP5/M001 computer code analysis (Reference 7.4a), to ensure that the following four criteria were met:
- 1. Minimize spill entrainment of the dherted slug 1n the main flow path.
- 2. Acconinodate the 500's in existinc. space.
- 3. Generate acceptable impact loads on the deaf-end ouri,o s10wdown and stoppage of the slug.
O 41 l
Report No. 01-0300-1291 Revision 0 0
- 4. Provide adequate drain path during normal operations and valve uischarge.
i To effectively evaluate the 500's against the criteria above, a brief I~ discussion of the S/RV loop seal discharge phenomenon is warranted. 1 During the EPRI Safety and Relief Valve test program recently completed, j' the following sequence was observed for cold loop seal discharge: i j 1. The valve experienced high frequency oscillations at low lift positions (approximately 15 percent). l l 2. The loop seal was discharged at very low rates. Very little flashing occurred. j 3. The entire loop seal water was discharged into the downstream piping 4 and essentially collected there. j 4. After the loop seal was completely discharged into the downstream l piping, the valve oscillations ceased, and the valve fully opened on
- steam. The loop seal water in the discharge piping then began to l- accelerate.
Variuut 500 designs were evaluated, with the final designs shown in j Fi urt 4.1-1 and 4.1-1. Figure 4.1-1 is t pical for the safety valves i di charge region and Figure 4.1-2 is for t PG,1Vs dischar e region. The following discussion surmarizes the effectiveness of the f nalized 500's j I 'eslated to the critaria outlined above. Minimize Spill Entrainment. The key to significantty reducing the discharge piping loads is to ensure ! no high density fluid enters the piping system downstream of the SD0's. l Because of ttle volume of Trcjan's loop seal water, the loop seal frant l will be between the first and the second elbows downstream of each safety i valve before the safety valve fully opens. Therefore, the 500 for each
- safety valve region is located at the second elbow downstream of each
- safety valve. Also, in the PORVs region, the loop seal will still be l intact when it reaches the f trst elbow downstream of both PORVs due to the slow opening time of the PORVs. Therefore the 500 for the P0RVs is located at the first elbow downstream of both b Vs.
!l [ As the subcooled loop seal discharges into the 500, the fluid jet will be i nearly a constant 6-inch diameter. Since the fluid temperature is less ! than its saturation temperature at the surrounding environmental i pressure, the discharging liquid jet is characterized by a nearly constant diameter jet approximately equal to the diameter of the pipe. It will not flash and will form an incompressible fluid jet. 4-2
Report No. 01-0300-1291 Revision 0
. 9 This arrangement will result in the loop seal being discharged into and contained by the 500, with only low density fluid (less than 20 l lbm/ft 3) entering the main flow path. It will result in a significant i reduction in the hydrodynamic forces induced on the discharge piping downstream of the 500's. ;
The effective length of the 500 for eac! safety valve is 2.5 feet, with 3.0 feet for both PORVs. The effective volume of the 500's are 1.7 to 2.0 times the loop seal volume. Both the length and volume of the 500's act to prevent spill over of the high density fluid into the main flow path. The 8-inch ring located in the safety valve 500 device will eliminate the potential for spill over and subsequent entrainment of the trapped slug. The loop seal slug is driven into the 500 by high upstream pressure. The increased S00 pressure adds to the effectiveness of the 500 to minimize spill over and ensure entrainment of the diverted slug into the main flow path. 1 Accommodate the 500s in Existing Space. l Olscussions with PGE personnel and subsequent piping system walkdown by PGE personnel have indicated that the 500's illustrated in Figures 4.1-1 and 4.1-2 could be accommodated in existing space. These 500s are currently installed. Generate Acceptable Impact L.oads on 500's. The maximum hydrodynamic loads induced on the 500's were calculated to be about 30 kips. Subsequent piping analysis has demonstrated that adequate l a supports could be constructed for the 500's. Provide Adequate Drain Path. , To evaluate the adequacy of the 500 drain system which is connected directly to the PRT, analyses were performed (Reference 7.4e) using the following drain pipe options:
- 1. 3/4-inch Schedule 40S diameter pipe attached to the bottom of the 500.
- 2. 2-inch Schedule 40S diameter pipe attachment tc the bottom of the 500.
- 3. 3/4-inch Schedule 40S diameter pipe attached to the bottom of the 500, with a 1/8-inch orifice in the piping.
The results of the analysis indicate that the impact load on the 500 is directly related to the minimum cross-sectional area of the flow path. With the 2-inch drain line, the loads are about 25% lower than the drain 4-3 I, 1
4 J Report No. 01-0300-1291 1 Revision 0 l
' l i
I q , line with a 1/8-inch orifice. As expected, the amount of fluid being discharged through the drain is directly related to the minimum crosssec-tional area of the drain path. The drain rate is excessive with the ' 2-inch drain line (approximately 350 lbm/sec) and the 3/4-inch drain line . (90lbm/sec). The 1/8-inch orifice in the 3/4-inch line reduced the
; drain line flow rate to approximately 4 lbm/sec during the transient condition, and less than 1 lbm/sec during the steady state, thus meeting the minimum drain requirements. Therefore, the 3/4-inch drain line with il a 1/8-inch orifice was used in the installation.
I
; 4.2 Thermal-Hydraulic Analysis This section describes the methods used to obtain the force histories on the Pressurizer S/RV Piping System as a result of the high pressure fluid flow caused by activation of the PORVs and the safety valves. The following steps were used:
- 1. Develop thermal-hydraulic model of the system, l 2. Perform analysis to determine transient state histories at discrete locations throughout the system,
- 3. Int! grate transient state histories to develop force histories on l piping system.
4.2.1 Develop Thermal-Hydraulic Model
- I A thermal-hydraulic model was developed using control volumes, or
- a nodes, to represent the fluid in the pressurizer, the relief tank, j and the safety / relief piping system.
The number of nodes used to simulate a particular portion of the system increased as the hydrodynamic behavior to be experienced in i that region changed more rapidly. Large and small volumes were i used throughout the model, with a gradual transition in volume l sizes between the different nodalization schemes. i Following the recomendations presented in Reference 7.7e for ! water loop seal transients, the control volume size in the model is less than or equal to the loop seal water volume. This ! modeling technique for control volumes immediately downstream of
- the valves avoided underestimation of loads due to numerical smearing.
( The control volumes in the model were connected by junctions or i< flow paths. The individual control volumes and junctions were
.j described in terms of fluid state and phase parameters, geometry, O
4-4
No 01-0300-1291 and flow characteristics, with boundaries carefully selected to insure adequate representation of the fluid transient. Control junctions were located at area changes, such as the safety valves, reducers, tees, and the entrances to the pressurizer and relief tank. In addition, junction locations were specified for I' dynamic stability and force detail. Two models were developed. One to simulate PORV actuation and the other for safety valve actuation. The initial conditions for the safety valve actuation is based on the steady state conditions , resulting from PORV actuation. j 4.2.2 Perform Thermal-Hydraulic Analysis The volume / junction model described in the previous section was developed for use with the computer program RELAPS/ MODI, which is discussed in Appendix B. During the developmental stages of the RELAP5/M001 model and code input, interpretations of the technique and requirements were made which would best reflect the loop seal discharge transient and the Trojan pressurizer safety / relief system. To the extent possible, there interpretations were based on the recommendations and guidelines set forth by Intermountain Technologies, Inc., in their report on the application of RELAPS/M001 (Reference 7.7e), and by other industry users as presented during the RELAP5/M001 workshop held at EPRI on May 5, 1982 (Reference 7.7d). , In particular, the following assumptions / interpretations were l applied to the RELAP5/M001 model and code input for the Trojan system:
- a. Loop Seal Displacement Although the loop seal for the PORVs and the safety valves are physically located upstream of the valve, the loop seal water in the model was placed downstream of the valve in accordance with the recomendation in Reference 7.7e. To better represent the transient, the time required for the water slug to pass its respective valve was taken into consideration when the conditions were determined for RELAP/M001 input.
- b. Control Volume Size As recomended in Reference 7.7e and noted in Section 4.2.1, the control volume size in the areas where loads could be '
4-5
= 3 Report No. 01-0300-1291 Revision 0
- O underestimated due to numerical smearing is less than or equal to the loop seal, water volume. Since the probability of numerical smearing decreases as the water slug travels downstream, the control volume size increased gradually as the downstream piping approached the relief tank.
- c. Alternate Choking Model U The alternate choking model in RELAPS/M001 was not used in the discharge piping for the relief and safety valve transient calculations, following the recomendation in Reference 7.7e.
The choking model was however, used upstream of and at the valves since choked flow would occur in these areas.
- d. Heat Structure Model i
The condensation effects were conservatively ignored because
- 1) the uncertainties involved in defining proper heat transfer I coefficient would make the results questionable, and 2) it is l conceivable that a leaky valve would result in high pipe wall temperatures, thereby reducing the benefit that can be claimed by inclusion of wall heat transfer.
O, Valve Sequencing e. l Sequential actuation design setpoint of the to (as opposed relief and the safety simultaneous valve valves by) actuation represents a realistic transient of cold loop seal followed by a steam discharge, and was appl'ed to the RELAPS/M001 model and l code input.
- f. Relief Tank Level Under normal operation conditions, the pressurizer relief tank level is 75 percent full (Reference 7.2d). The tank level was assumed to be at the tank centerline in the load simulation analysis. The level only determines quench capacity so the short-duration transient considered in this analysis would not be sensitive to the differences in the tank level.
- g. Loop Seal Temperature Profile The temperature profile used for the safety valve loop seal was measured plant data.
The thermal-hydraulic analysis, which simulated the safety valve and relief valve discharges, was performed to observe 4-6
I Report No. 01-0300-1291 Revision 0
- 9. ! ;
i! the fluid system response unit hydraulic steady-state was achieved. ;l 4.2.3 Develop Force Histories Fluid state and flow histories generated during the thermal- ) hydraulic simulations were used by the computer program REFORC2. It integrates these parameters to determine the forces applied to the pipirig system by the fluid. REFORC2 is described in Appendix B. The general method of force history generation is to develop the total forces in the axial direction at opposing components such as I bends or tees. The analysis accounts for the wave force (due to the fluid acceleration), and the pressure and momentum at the control surface normal to the force direction. In general, the wave force component tends to accelerate the entire pipin segnent, whereas l the control surface force tends to differentia ly expand or contract the segment. The extent of such axial deformation is dependent upon the piping properties and the magnitude of the I control surface term, but is generally small for pressurizer I relief line discharge problems in nuclear piping. Total forces calculated in this fashion are intended for application at the a tangent points of each bend. Two total forces are therefore [ calculated at each direction change, or equivalently, two opposing total forces calculated for each straight segment of piping. The locations of the forcing functions are shown on Figures 4.2.3-1 and 4.2.3-2 for PORV discharge and safety valve discharge re<nectively. l 4.3 Piping Analysis The piping system was analyzed using Impell proprietary computer program SUPERPIPE, except for the Class I piping thermal transient analysis. For this analysis the Impell proprietary computer program TRANS2A was used. A description of these programs is included in Appendix B of this report. A SUPERPIPE mathematical model of the piping system was developed and is shown in Appendix A. This final as-built model was developed with the design input contained in Reference 7.2d. The model represents the mass and stiffness effects of the system, including the flexibility factors for certain piping components as defined by the code. O 4-7
Report No. 01-0300-1291 Revision 0
'O Support stiffnesses for rigid restraints, snubbers and intermediate anchors were included in the model in order to accurately account for the hydrodynamic and seismic responses. Stick models of both the pressurizer and the PRT were also included in the analysis to accurately account for dynamic and thermal expansion effects of these equipment on the piping system. All small branch lines connecting to the system with ratios of branch to pipe run size less than or equal to 1/3, were excluded from the model.
l Evaluations of all significant static and dynamic loading conditions were then performed to determine the internal forces and moments in the structural model. Radial temperature distributions and gradients, for Class 1 piping components, as a result of rapid temperature changes were I determined with TRANS2A program. All the load case results are then entered into the code stress evaluations: Class 1 evaluation for the l upstream piping of the safety and relief valves and Class 3 evaluation for the downstream piping of the safety and relief valves. 4.3.1 Load Cases Five load cases analyses were performed: two static analysis for o gravity and themal expansion loadings, one response spectrum analysis for seismic loading, one time history analysis for hydrodynamic loading, and one thermal transient analysis for Class 1 piping components experiencing rapid temperature changes. 4.3.1.1 Gravity Analysis The effect of gravity on the piping system was determined by a static analysis. The mass of the piping components, valves, pipe contents and insulation were y considered in this analysis. Two gravity computer runs were performed:
. Normal: water or steam contained only upstream of the safety and relief valves, empty pipe for downstream.
. Hydro: water contained throughout the piping system.
4.3.1.2 Thermal Expansion Analysis Thermal expansion analysis was performed for temperatures specified by selected operating modes. The operating modes were selected in such a way that the results of the thermal expansion analysis from these modes conserva-tively envelop the expected results from the remaining, 4-8
Repor No 01-0300-1291 less severe operating modes. All modes were determined in Reference 7.41 from design input in References 7.2d, 7.4a, and 7.Sa. The stress free temperature for analysis is defined to be 70*F and the ambient temperature is 108'F. Models of both the pressurizer and the PRT with associated temperatures were included in the analysis to obtain the thermal anchor movement effects of these two equipment on the piping system. Six thermal runs representing the selected operating modes were performed:
. 1005 power, all safety and relief valves closed.
- Relief valve PCV 455A open.
- Relief valve PCV 456 open.
- Both relief valves open.
- All safety and relief valves cpen.
- Cold spring for piping at three rigid hangers (data pointsC508,179,and182).
Results of the cold spring run were algebraically sunined with all other runs to represent the cold-sprung piping system at elevated temperatures of the respective operating modes. 4.3.1.3 Seismic Analysis Seismic analysis was performed by the analysis technique known as modal response spectra analysis. This utilizes response acceleration spectra as the input loading. The mass of the piping components, valves, piping contents, and insulation is considered in this analysis. All rigid restraints and snuhbers are considered while formulating I the stiffness matrix. 8 For the dynamic seismic analysis, the mass matrix is formed in addition to the stiffness matrix for the mathematical model. Once these matrices are formed, the frequencies and mode shapes for all significant modes of vibration below 33 hz are determined. The mode shapes and frequencies are solved in accordance with the following equation: l 4-9
[j -
-e, ,.
p,r s t , Report No. 01-0300-1291 Revision 0 p 8 J .
.y s
+
% 3 .
(K-w2M) u = 0 4-l , 6 , , in which: __ s
~
_ K = stiffneti matrix of the piping system s He mass raatrix for the 91 ping system i w = frequency of vibration
~
u = matrix of mode shapes After the frequency is determined for each mode, the
, corresponding model spectral acceleration is taken from the appropriate response spectrum obtained from the i
design data for the pipe. Using these spectral accelera-tions, the characteristic response for each mode is found by solving the following equation: R,SanD
- e' IY)n max" z gn,n I
ir.' wh[ch: (Yg),,x = maxfinum characteristic response of the n mode b R, - = miss participation for n mode = tMgQin Sa n
= spectral acceleration for the n th mode
= frequency of vibration for the n th mde w
n U = earthquake direction coefficient
= characteristic mass for the n th mde=1Md s-M f n Mg = mass of the ith ,,,,
fin a medal dl5 placement of the i th mass for the n th mode
. Using these results, the maximum displacement response for each mode is calculated for each mass point from the maximum characteristic response for each mode, using the following q uation:
~
O 4 10
Report No. 01-0300-1291 I Revision 0 i l Vin "# inIYnImax l I where Vin = maximum displacement response of mass i for the j n th mode The square-root-of-the-sum-of-the-squares (SRSS) method is used to combine the effects for different modes and different seismic directions, except for the closely-spaced modes. The effects for closely-spaced modes are combined by absolute sunnation, as specified by the
" grouping method" described in Regulatory Guide 1.92.
After the joint displacements are determined, the individual member forces and moments are obtained by using the member stiffness properties; and, finally the support reactions are calculated. Two seismic runs were performed:
. North-South with vertical OBE excitation g,
. East-West with vertical OBE excitation Results of these two runs are enveloped in absolute value. Results of SSE loading are obtained by multiply-ing the OBE results with a factor of 1.67 (Reference 7.2c). To reduce the conservatism, multiple support excitation (i.e., different response spectra at different support levels) instead of simple excitation (i.e., same enveloped response spectra for all supports) are specified for each seismic run. Three support levels were included:
. Support Level 1: Interpolated response spectra at or below E1. 129'-0" with 0.5% damping and applied at all supports / anchors above El. 125'-0". This spectra is interpolated from PGE Trojan Response Spectra for the Containment Structure at El.137'-6" and El.
125'-0".
. Support Level 2: PGE Trojan Response Spectra for the Containment Structure at or below E1. 125'-0" with 0.5% damping and applied at all piping supports /
anchors at or below E1. 125'-0". O 4-11
l
)
l
. i' Report No. 01-0300-1291 Revision 0 ;
4
. Support Level 3: Interpolated response spectra at or below El. 94'-0" with 2.0% damping and . applied at all pressurizer supports. This spectra is interpolated from PGE Trojan Response Spectra for the Containment Structure at El. 105'-0" and El. 93'-0".
The effects of, seismic anchor movements (SAM) was considered inlthe fnitial analysis (Task 1) by performing i an explicit computer analysis. Results of this SAM l analysis shows insignificant stresses and support loads. This was due to small relative movements for supports connected to the Containment Struiture (less than 0.05 l inch) . The SAM anal the final analysis (ysisTasks was therefore 2 and 3). not performed in I 4.3.1.4 Hydrodynamic Analysis Hydrodynamic time-history analysis was performed to obtain the structural response of the piping system following the sudden openings of the safety and relief valves. The input loads in the format of force time histories as generated from the thermal-hydraulic Ic analysis discussed in Subsection 4.2, were applied to the piping system at changes of directions (such as elbows) and at changes of flow areas (such as tees and reduces). The direct integration method of time-bistory analysis l was gpplied with a 1% damping ratio defined at the freqeencies 10 Hz and 100 Hz. These two frequencies a defira the frequency range of interest. Two time-history ,l runs are performed: Relief valves actuation
- Sc(ety values actuation
' y, ,
For the 'run with relief valve opening, the time interval u used is 0.0015 second and the time duration is 0.7 second. For the run with safety valve opening, the time interval used is 0.0015 second and the time duration is 0.6 second. 4.3.1.5 Thermal Transient Analysis Thermal transient analysis was performed to obtain the radial temperature distributions and gradients for the Class 1 piping components when system operations, such as the sudden opening of valves, result in significant i 4-12
l Report No. 01-0300-1291 Revision 0 t i changes of fluid temperatures. The analysis is done using the one-dimensional heat-transfer program TRANS2A which employs the axisymmetric equation set for unsteady I heat transfer. Maximum values of the secondary stress S , the secondary-plus-peak stress S and maximum j l -T ou put.bl are selected These fromas are used theinput TRANfor2A thecom uter fa igue analysis. Corresponding to these values are time points for which the linear temperature gradient 6T1 , the non-linear temperature gradient AT2 , and the average temperatures Ta and Tb across adjacent pipe sections for all piping components are listed. References 7.Sa and 7.5b were used to develop the thermal transient data for the Class 1 piping. Since the safety valve actuation is classified as an Emergency Condition (Reference 7.7a), the thermal transients associated with the safety valve opening need not be considered in the code stress evaluation. Several transient events result in the relief valve actuation. Review of these transient events shows that the limiting events are the Loss of Load and the Inadvertent Safety Injection. Both events involve identical temperature change (step change from l 108'F to 680'F), and flow rate (5x105 lb/hr for each ! PORV). The difference in these two events is flow duration. For the Inadvertent Safety Injection event, the flow duration is postulated to be 670 second; for the loss of Load event, 40 second. As indicated in References 7.5a and 7.5b, the total postulated l occurrences of the relief valve actuation during 40 year i plant life is 100. Piping components analyzed in TRANS2A for thermal transient loading were uniquely defined from wall thickness and inside diameter for the one-dimensional model. Special considerations are made for fittings and bends to insure conservative stress results. For tee, reducer, tapered transition joint and branch connection, PGE pipe / fitting thickress measurement data (Reference 7.5d) and two-dimensional finite element results generated in previous Impell work (Reference 7.Sc) were used to obtain the thermal transient stresses. 4.3.2. Class 1 Piping Stress Evaluation Class 1 piping stress evaluation was performed per ANSI B31.7 ! rules for the upstream piping of the safety and relief valves to ' 4-13 i ll l
p No 01-0300-1291 0 ' show that each of the stress limitations of B31.7 Divisions 1-704
" Pressure Design of Components" and 1-705 " Analysis of Piping Components" are satisfied (ANSI 831.7 Divisions 1-704 and 1-705 correspond to ASME Section III Subsubarticle NS-3640 and NB-3650, i respectively). The appliable Code Equations with corresponding service conditions and loadings are presented in Table 4.3.2-1. ,
A description of service conditions and loadings are sumarized i below (Refer to the Code isc the definition of symbols), Design Condition h For the Design Condition, the permissible pressure should not i exceed the pressure P calculated with Code Equation 2 of 1-704.1.2 and the primary stress intensity calculated with Code t Equation 9 of 1-705.1 should not exceed 1.5 Sm. The specified design pressure and temperature for the Class 1 piping are 2485 psig and 680*F, respectively. The load cases included in Code Equation 9 evaluation are:
- Weight of piping system (Normal)
- Operational Basis Earthquake (One-half the range)
- Hydrodynamic load due to relief valve opening
] ,l Normal and Upset Conditions The Normal and Upset Conditions are defined as various plant ,- events with corresponding temperatures, pressures and numbers of l occurrences. Fatigue evaluation was performed by calculating Code Equations 10, 11 and 14 of 1-705.2 through 1-705.4 j (Primary-plus-secondary stress intensity range Sn, peak stress g range S tively)p and
. Thealternative cumulativestress usageintensity factor fromSalt therespec-fatigue curves based on calculated Salt values should not exceed 1.0. In addition, if Sn from Code Equation 10 calculation exceeds the allowable stress intensity 35m, Code Equations 12 acd 13 of 1-705.4 should be satisfied. For analysis purposes the defined normal and upset plant events are enveloped and only the events which will potentially contribute to the fatigue damage are chosen for fatigue stress evaluation. The chosen events and number of occurrences for the upstream piping of relief values are listed below.
O 4-14
Report No. 01-0300-1291 Revision 0
~
0 l Plant Event Description Number of Occurrences P1 ant Heatup 200 Plant Cooldown 200 OBE 5 Relief Valve Opening (Envelope of Loss of 100 Load, Inadvertent Safety Injection and etc.) For OBE,(Reference 7.lf).10 assumed significant For stress relief valve cycles 5forsignifi-opening, each occurrence are cant stress cycles for each occurrence are assumed (Reference 7.41). The relief valve opening event causes significant hydrodynamic and thermal transient stresses. No significant thermal transient stresses are associated with plant heatup and cooldown events, for this system. Since the number of actual safety valve actuations in operating pressurized water reactors
's extremely low, the safety valve actuations has been reclassified as an Emergency Condition (References 7.7a and b).
There are no other signficant transient events defined for the upstream piping of safety valves during normal and upset conditions. Emergency Condition h For Emergency Condition, the permissible pressure should not exceed the pressure P calculated with Code Equation 2 of 1-704.1.2 by more than 50% and the primary stress intensity calculated with Code Equation 9 of 1-705.1 should not exceed , 2.25 Sm-The load cases included in Code Equation 9 evaluation are:
- Weight of piping system (Normal)
- Operational Basis Earthquake (One-half the range)
- Hydrodynamic load due to both safety and relief valve openings (Envelope of both runs)
Faulted Condition For Faulted Condition, the permissible pressure should not exceed the pressure P calculated with Code Equation 2 of 1-704.1.2 by more than 100% and the primary stress intensity calculated with Code Equation 9 of 1-705.1 should not exceed 3.0 Sm-O 4-15
Report No. 01-0300-1291 l Revision 0 j The load cases included in Code Equation 9 evaluation are:
. Weight of piping system (Nomal)
. Safe Shutdown Earthquake (One-half the range)
. Hydrodynamic load due to both safety and relief valve
- i. openings (Envelope of both runs) f 4.3.3 Class 3 Piping Stress Evaluation ,
Class 3 piping stress evaluation was performed per ANSI B31.1 rules for the piping downstream of the safety and relief values to show that each of the stress limitations of 831.1 Paragraphs 104 " Pressure Design of Components", and 102.3 " Allowable l- Stresses and Other Stress Limits" are satisfied (ANSI B31.1 Paragraph 104 corresponds to ASME Section III Subsubarticle NO-3540 and Paragraph 102.3 corresponds to NO-3650. Since the Code Equation numbers for stress evaluation are not explicitly
,l 1
mentioned in B31.1-1973 Edition, the corresponding Code Equations 8 through 11 of ASME Section III NO-3650 are used for discussions). The applicable Code Equations with corresponding service conditions and loadings are presented in Table 4.3.3-1. 10 A description of service conditions and loadings is sumarized below (Refer to the Code for the definition of symbols). Design Condition For the Design Condition, the permissible pressure should not l exceed the pressure P calculated with Code Equation 4 of 831.1 l Paragraph 104.1.2 and the stresses due to sustained loads calculated with Code Equation 8 of NO-3652.1 (corresponds to 831.1 Paragraph 102.3.2) should not exceed 1.0 Sh - The specified design pressure and temperature for the Class 3 ,y piping are 600 psig and 600*F, respectively. The load case l g included in Code Equation 8 evaluation is the weight of piping j system (Normal) only. Normal and Upset Conditions For Normal and Upset Conditions, the stress range due to thermal expansion calculated with Code Equation 10 of NO-3652.3 (corres-ponds to 831.1 Paragraph 102.3.2) should not exceed AS , or the sum of stresses due to sustain loads and stress range due to l thermal expansion calculated with Code Equation 11 of NO-3652.3 l O 1, 4-16 i !.
Report No. 01-0300-1291 Revision 0 9. (corresponds to B31.1 Paragraph 102.3.2) should not exceed the sum of Sh andAS . Additionally for Upset condition, the permissible pressure should not exceed the pressure P calculated with Code Equation 4 of B31.1 Paragraph 104.1.2 by more than 10% and the stresses due to occasional loads calculated with Code Equation 9 of ND-3652.2 (corresponds to B31.1 Paragraph 102.3.3) should not exceed 1.2 Sh - The load cases included in Code Equation 9,10 and 11 evaluations are:
- Weight of piping system (Normal) - Equation 9 and 11 - OBE (One-half the range) - Equation 9 - Hydrodynamic load due to relief valve openings - Equation 9 I - Thermal expansions (Normal and Upset) - Equations 10 and 11 :
Emergency Condition For Emergency Condition, the permissible pressure should not exceed the pressure P calculated with Code Equation 4 of 831.1 ' Paragraph 104.1.2 by more than 50% and the primary stresses due to occasional loads calculated with Code Equation 9 of ND-3652.2 (corresponds to B31.1 Paragraph 102.3.3) should not exceed 1.8 Sh-The load cases included in Code Equation 9 evaluation are:
- Weight of piping system (Normal)
- OBE (One-half the range)
- Hydrodynamic load due to both safety and relief valve openings (Envelope of both runs)
-ll Faulted Condition For Faulted Condition, the permissible pressura should not exceed l the pressure P calculated with Code Equation 4 of B31.1 Paragraph 104.1.2 by more than 100% and the primary stresses due to occasional loads calculated with Code Equation 9 of ND-3652.2 (corresponds to B31.1 Paragraph 102.3.3) should not exceed 2.4 Sh-O' l 4-17 i
; Report No. 01-0300-1291 Revision 0 lO The load cases included in Code Equation 9 evaluation are:
a
- Weight of piping system (Normal)
- SSE (One-half the range)
- Hydrodynamic load due to both safety and relief valve openings (Envelope of both runs) 1 1
j i
~
\ (a')
- I f
I o 4-18 l I- - - - - - . - - , . _ . _ _. _ _ __ _ _
Report No. 01-0300-1291 Revision 0 . TABLE 4.3.2-1 CLASS 1 PIPING CODE EQUATIONS AND LOAD COMBINATIONS B31.7 Paragraph 1-705 Service Condition Code Equation Load Combination (3)(4) Allowable Design (1) 9 Pressure (Design) + Gravity + 1.5 Sm OBE + R/V Open Emergency (1) 9 Pressure (Emer0ency) + Gravity + 2.25 Sm OBE + Envelope (R/V Open & S/V Open) Faulted (1) 9 Pressure (Faulted) + Gravity + 3.0 Sm SSE + Envelope (R/V Open & S/VOpen) Normal & Upset 10 Pressure (Normal & Upset) + OBE + 3.0 S m R/V Open + Thermal (Normal
& Upset) + Transient (oJ) &
lTa-Tl) b Normal & Upset 11 Pressure (Normal & Upset) + OBE + --- R/V Open + Therreal (Normal
& Upset) + Transient (6T1, AT2 &
lTa-Tl} b Normal & Upset 12 Thermal (Normal & Upset) 3.0 S m Normal & Upset 13 Pressure (. Normal & Upset) + 3.0 Sm Gravity + SE + R/V Open + l Transient (ITa - Tb l) Normal & Upset 14 4"2 " (K* depends on Eqn 10 Cumulative K* x l results) Usage Factor i s1.0 l NOTES: (1) Pressure checks are performed by calculating the allowable design pressure (P) with Code Eqn. 2 of B31.7 Paragraph 1-704.1.2. The limits are P for Design Condition, 1.5P for Emergency Condition t and 2.0P for Faulted Condition. I (2) Code Eqns. 12 and 13 need to be satisfied if Code Eqn. 10 stress exceeds the limit 3 Sm. l 4-19
- Report No. 01-0300-1291 '
i Revision 0 n
,U TABLE 4.3.2-1 CLASS 1 PIPING CODE EQUATIONS AND LOAD COMBINATIONS NOTES: (3) OBE and valve actuation (R/V Open or S/V Open) were sumed by the SRSS technique based on References 7.le and 7.7b.
[I (Contd) , (4) The thermal expansion associated with safety valve opening is e defined as an emergency condition by Reference 7.7.a. Therefore. it is not used for code compliance. IO I
,I l
I 1 !O 4-20 l { .
i l Report No. 01-0300-1291 ! Revision 0 i I TABLE 4.3.3-1 CLASS 3 PIPING CODE EQUATIONS AND LOAD COMBINATIONS ASME ! ND-3650(I) Service Condition Code Equation Load Combination (4) Allowable Design (2) 8 Pressure (Design) + Gravity Sh Upset (2) 9 Pressure (Upset) + Gravity + 1.2 Sh I OBE + R/V Open I Emergency (2) 9 Pressure (Emergency) + Gravity + 1.8 Sh OBE + Envelope (R/V Open & S/V Open) Faulted (2) 9 Pressure (Faulted) + Gravit 2.4 Sh SSE + Envelope (R/V Open & y + S/VOpen) Normal & Upset 10 Thermal (Normal & Upset) SA (3) Normal & Upset 11 Pressure (Design) + Gravity + S +S Thermal (Normal & Upset) h A NOTES: (1) Code Equation numbers are not explicitly mentioned in B31.1 - 1973 Edition, Paragraph 102.3. The corresponding Code Equations 8 through 11 of ASME Section III ND-3650 are used. (2) Pressure checks are performed by calculating the allowable design pressure P with Code Equation 4 of B31.1 Paragraph 104.1.2. The limits are P for Design Condition, 1.lP for Upset Condition, 1.5P for Emergency Condition and 2.0P for Faulted Condition. (3) Either Equation 10 or Equation 11 should be satisfied. (4) OBE and valve actuation (R/V Open or S/V Open) were sunined by the SRSS technique based on References 7.le and 7.7b. O 4- 21 ; I
lO s"aren t iT e si..se'-r
=5 a _1 i
' 3 3*
% l sene'-n*
3
. (!. \ t-
- = , , 7 accTions L. .J , ,
j' asciones .- i setw-r g p I 4 rat
=====.
u"
. ases I
i 1 w.p. m..m*-se t l 3 m ue. 1 VV'o=cc l t l - Figure 4.1-1: TYPICAL SAFETY VALVE SLUG DIVERSION DEVICE lO i l
, , _ _ , ,_._,,- m-_ . , _ , . - -
l i I 1 1 _2n _, et.ar-saa l
- d '
1,
,3 F ,!
h
' 't,IN --+--
=. =' -'e <, ,II' /7% .
I' _. ( - (./
+. 'N D ' ze..
29{" SECTION A-A 17" k I (+h g r - e ru= -xe f.< ;
- 16. ; F-
\;i i/ '4 f.}
23- . .t. -- - - s ,L-- _ _ T SECTION a -- ..
== ==
b ;
' ---o t-h
+-
T-SECTION g M WP EL 123"-l l q h p d'j WN Of w/ UNE onect PLAN MEW SECTION B - B l l l t Figure 4.1-2: PORV Slug Diversion Device ! l ll
)
i i
- m m --m e.- -
- O O O f 39 KEY 3
N: Positive Direction of Elbow Force N Along Axis of Pipe
@: Pipe Segment Force M. Positive
@ in Direction Opposite Steady k JF 7 .
State Flow Direction h 1 20 2
@ @' 11o 7
. 36
. A '
I 13 J L43 h 1 , 40 A h3 11 Y 42
/ 6 N4
@ g 47k/
h 5* !30g33 h 4 1s h 2g h i 1 2A q3
/ 18 /j 34 P44 48 /2s 26 y .
9 4 27 '
' 17
@ @ O U1 '19 c o -. . _ . n , .. ..-.. - ,r __,-- c..- .2--- < _ nani, n4,. u---
i O'
/
- i. @
m bI 5 1
; 5 r
al L,
. .E b
3 \ 9, i E D o, m I s ( y g n9
. 4 k/; :'
l ~ C D
/@N @ ~
i 7: g
~
f
.- r. --. = -
g O O O 53 KEY 40 ' N: Positive Direction of Elbow
\ , , 62 e' Force N Along Axis of Pipe 21
, @: Pipe Segment Force M. Positive in Directica Opposite Steady State Flow Direction h ;*
11 9 h68 10 67k 1 d 52 43 4 k
- 0 3 I
lgg u Q 2Yf 3'!32 ,, U8 9 3 8 f 2 g i70 6 38 3 3 , g [2 1r26 d 77 10 r69 { @ 1 h / Ji 16 66 34-e v 36 6y [18 ! 17 63 ri, ..ca A.9.1 7 I ncatinnc nf Fnec{nn Functinns for safety Valve Discharge 1
l
. O
. I
(
~
\
v , a
$~
+
O
}
'Y 4
h 4
- tt) h '
~
W 9 i c. W "q O
\ L e
Co
\.
D, 0 D tv M t o A G e e e . Q 1 7
,4 L' l O, i 1
l
I I Report No. 01-0300-1291 ! Revision 0 O
- 5.0 ANALYSIS RESULTS 5.1 Thermal-Hydraulic Analysis ,
Forcing functions were generated using the RELAPS/REFORC2 methods
-discussed in Section 4.2. Figures 4.2.0-1 and 4.2.3-2 show the forcing
- 4. function locations. These forces represent total (pressure, momentum and acceleration) forces acting on each half. of the pipe segment, which can be added (noting the direction convention) to generate the total I unbalanced force on the straight pipe segment.
H The force values generated repres6nt the additional forces due to tran-t n sient loading only. Loads on the pipe segment due to initial operating conditions have not been included in the force values generated in this !3 report. The general equation used to generate these forcing functions, , , l therefore, is: F = F, + Fe , - F, , where F = Total forces, lbf. F, = Wave Acceleration force, lbf. g Fe , = Control Surf ace force, lbf. I F, = Initial control surface force, lbf. Figures 5.1-1 through 5.1-13 are representative segment force history ! plots. These segment forces were used to detemine piping analysis time ! steps; however, the elbow forces were used for the piping analysis. I
' 5.2 Class 1 Piping Stress Evaluation 4
5.2.1 Pressure Design !
- ),
4 The minimum allowable internal de.iign pressure for straight pipe, as determined by Code Equation (2) of 1-704.1.2, is greater than the specified design presures. This is shown below by a compari-son of maximum pressures ratio to allowable ratio: 0 k j lO ' 5-1 l
,- . v-. -.
1 Report No. 01-0300-1291 > Revision 0 {! O Pressure Design : l Pipe Service Design Allowable Design Maximum Allowable Size Condition Pressure (psig) Pressure (psiq) Ratio Ratio 6"SCH160 Design 2485 3300 .75 1.00 Emergency (l) 2700 3300 .82 1.50 Faulted 2700 3300 .82 2.00 3"SCH160 Design 2485 3860 .64 1.00 Emergency 2700 3860 .70 1.50 Faulted 2700 3860 .70 2.00 NOTE: (1) The 6" SCH.160 inlet piping near the safety valves experiences high-frequency pressure oscillation at the instant of valve lift-up due to valve flutter and/or chatter. The peak pressure from tests reached 6300 psia (Reference 7.7c). Since the pipe temperature is essentially cold at that time, the permissible pressure at Emergency Condition is 1.5 Pa = 7131 psi (Reference 7.7b). i 5.2.2 Primary Stress Intensity The primary stress intensities as deternined by Code Equation (9) of 1-705.1 are within the code allowables. A sumary of maximum intensities and a comparison to the applicable allowable for each service condition are shown below: Maximum Primary Stress Intensity Service Stress Intensity (PSI) , location Condition Primag Allowable Ratio j Upstream of Design 23,704 24,120 .983 Relief Valves Emergency 24,134 36,180 .667 Faulted 36,332 48,240 .753 Upstream of Dasign 24,120 24,120 1.00(l) Safety Valves Emergency (2) 28,431 36,180 .786 Faulted 36,784 48,240 .763 NOTE: (1) The primary design strass intensity upstream of the Safety Valves } as calculated is slightly greater than the stress intensity allowable. The stress intensity was shown to be qualitatively conservative in Reference 7.41. I O 5-2
Report No. 01-0300-1291 Revision 0 O (2) With consideration of peak pressure at 6300 psia due to safety valve flutter and/or chatter, tiie maximum Equation 9 (Emergency) stress for the location upstceam of safty valves is 36735 psi since the pipe temperature is essentially cold, the allowable is 45000 psi (Reference 7.41). 5.2.3 Consideration of Normal and Upset Conditions The satisfaction stress intensity range of primary-plus-secondary as vetified by Code Equations stress intenstty(and (10), 11),neak I (12), and (13) of 1-705 ave within the allowables. No explicit verification of the piping upstream of the safety valves was - U required, sirce the ti.ernal transients associated with the safety valve actuation are dcfined as an emergency c:.se and relief valve transients are not applicable. A summary of the maximum stress intensity ranges and cumulative usage factors are provided below: i For each component type, the highest prir.ary-plus-secondary stress range, in comparison to the 3.0 allowable ratio, as determined by Equation (10) is shown as: !l il Maximum Primary-Plus-Secondary I ptress Intensity Range Stress Intensity Range (PSI) - i Component Type Primary / Secondary Allowable (3.0 S ,) Ratio (l) Weld to Pressurizer 58,300 55,450 3.154
! Nozzle i
Straight Pipe 143,660 60,000 7.183 4 Elbows 137,820 60,000 6.891 ll l Welds to Elbows, Valves, Tee, & Reducer, Tee, (2) (2) (2) Reducet, and at Branch Connection i NOTES: (1) Although the Equation (10) stress limit is exceeded, the results are acceptable by satisfaction of Equatiens (12) and (13). [ (2) All these component types exceed 3.0m Sm by inspection of the calculated peak primary-plus-secondary stress intensities. No '
- explicit primary-plus-secondary stress intensities were calculated.
5-3 f
- II 4
)
Report No. 01-0300-1291 Revision 0 l O The highest stress intensity ranges in comparison to the 3.0 Sm allowable, as determined by Equations (12) and (13), are shown below: Maximum Stress Intensity Range for Simplified Elastic-Plastic Discontinuity Analysis Maximum Stress Allowable Stress Component Type Integrity Range Integrity Range Ratios Equ.(12) Equ.('Q Equ.(12) Equ.(13) Weld to Pressurizer 1,440 36,890 55,450 .03 .67 Nozzle Straight Pipe 6,860 28,129 60,000 .11 .47 Elbows 12,020 20,330 60,000 .20 .34 Welds to Elbows, 5,500 57,140 60,000 .09 .95 Valves, Tee & Reducer 60,000 .27 .80 Tee 16,000 47,800 Reducer 7,750 40,440 60,000 .13 .67 Branch 3,300 59,300 60,000 .06 .99 Connection (1) NOTE: (1) For complete qualification of branch connection, see Reference 7.4k. O 5-4
Report No. 01-0300-1291 Revision 0 V,n For each component type, the highest peak primary-plus-secondary stress intensity ranges Equation (11) and the maximum cumulative usage factors are shown below: Maximum Peak Primary-Plus-Secondary Stress Intensity Ranges and Cumulative Usage Factors Sp(PSI) Salt Maximum Cumulative Cycles Component Type Equ.(ll) (PSI) Usage Factorl2) Allowed Weld to Pressurizer 100,980 59,104 .004 25,000 Nozzle Straight Pipe 205,113 341,855 1.605 62 Elbows 219,366 365,609 2.387 41 Welds to Elbows, 297,700 496,000 3.314 30 Valves, Tee & Reducer l Tee 262,900 438,000 3.587 27 I (' Reducer 257,300 428,000 4.00 25 Branch 257,300 428,000 4.00 25 i Connection (1) NOTrS: (1) For complete qualification of branch connection, see Reference 7.4k. 2 l (2) Maximum Cumulative Usage Factor is based on 100 cycles of relief valve discharge. Since the usage factor is exceeded for 100 actuations of relief d valve discharge, the number of cycles allowed to maintain the usage factor at 1.00 is shown above. It shows a maximum of 25 actuations of relief valve discharge is allowed for this system. By review of the plant history (5 actuations in 7 years to date, Reference 7.41), it is estimated the original postulated 100 actuations for 40 years of plant life is conservative. By extrapolation of the actuations to date, a revised estimate for 40 years will be close to 25 actuations. Therefore, to maintain system qualification, the number of relief g valve actuation should be monitored during the remaining plant life. 5-5 _l.
Report No. 01-0300-1291 ; Revision 0 ; O I 5.3 Class 3 Piping Stress Evaluation 5.3.1 Pressure Design The minimum allowable internal design pressure for straight pipe, as determined by Code Equation (4) of 104.1.2, is greater than the specified design pressures. This is shown below by a comparison of maximum ratio of pressures to the allowable ratio: Pipe Service (l) Design Allowable Design Maximum Allowable Size Condition Pressure (psig) Pressure (psig) Ratio Ratio 6"SCH40S Design 600 1390 .43 1.0 12"SCH40S Design 600 960 .63 1.0 NOTES: (1) The maximum pressures at Upset, Emergency and Faulted conditions are less than 600 psig. O 5.3.2 Consideration of Design Conditions The pipe stresses, as verified by Code Equations (9), (10), (11), and (12) of ND-3650, are within the allowables. A sumary of the maximum stresses and ratio of calculated to allowable stress is provided below: Code Equation / Calculated Allowable Location (DCP)(3) Service Condition Stress (PSI) Stress (PSI) Ratio 215 (8) Design 4,934 15,900 .310 183 (9) Upset 17,681 22,464 .787 20 (9) Emergency 28,361 33,696 .842 99 (9) Faulted 27,381 39,360 .696 202 (10) Normal & Upset 34,132 27,610 1.236(2) 202 (11) Normal & Upset 37,403 44,050 .849 NOTES: (1) The DCP Locations are shown in Appendix A. (2) Either Equation (10) or (11) must be satisfied. O 5-6 l > l
Report No. 01-0300-1291 Revision 0 0 5.4 Supplemental Design Requirements - 5.4.1 Impell Qualifications The following evaluations were performed in Reference 7.41 to show : complete qualification. 5.4.1.1 Class 1 and 3 Flange Joints i The pressure stresses at. flanges are acceptable based on : 4 Sections 5.2.1 and 5.3.1 summaries. Acceptable pressure ' design is met since design, upset, emergency, and faulted j pressures do not exceed the corresponding allowables. 1 The bolting was shown acceptable by meeting the require-i ments; for class 1 of Code Equations (15), (16), and (17) i of NS-3658, and for Class 3 of Code Equations (12), (13), and (14) of NO-3658. Applied moments on the bolts were based on pipe stress service level combinations. These
- calculated applied moments were compared to the allow-l ables and were found acceptable.
i o (~ 5.4.1.2 Sleeve Clearance The sleeve clearance at the single floor penetration was checked by comparing the maximum movements for each ll i service level to the measured clearance. The service level combinations are the same as for the support loads. U 5.4.1.3 Welded Attachments The trunnion and intermediate anchor attachments to the pipe, induced external local stresses on the pipe. These
- external stresses were qualified by a local stress evaluation of the attachment point. t.ocal stresses as calculated by the Welding Research Council Bulletin 107 i i (1979 Revision) were combined with the pipe membrane l stresses and compared to the pipe stress allowables. The service level combinations for the local stresses are the r
- j same as for the pipe stresses. i
'i Note that these evaluations do not include qualifications for the trunnions, anchor plates or the weld to attach-
- g s ment sizing. Qualifications of these should be included
- ' with the support evaluations.
i , !O
~
l 5-7 !l ,i _ ._ ,_. _ .~ _ _ ._ _ __ _ . _ _ _ _ _ _ _ _ _ _ _ _ _ _ . _ _ _ _ . _ _ _ _ _ _ _ .
Report N9. 01-0300-1291 Revision 0 0 5.4.2 For PGE Review and Approval The following component loadings as described were transmitted to PGE for review and approval. These component loadings are included as Appendix C, Component Load Summaries, of this report. 5.4.2.1 Support Loadings Support load combinations were based on the following table. Both plant global loading and local loading (as applicable) were calculated. SetName(I) Service Condition Load Combination I2) NORM Normal Gravity + Thermal (Normal) UPSET Upset Gravity + Thermal (Normal + Upset) + OBE + R/V OPEN EMER Emergency Gravity + Thermal (Envelop of all Thermal Cases) + OBE + Envelop (R/V OPEN + S/V OPEN) FLTD Faulted Gravity + Thermal (Envelop of all Thermal Cases) + SSE + Envelop (R/V OPEN + S/V OPEN) THM1 Thermal (Normal) Thermal (100% power, all valves closed) THMU Thermal (Normal & Thermal (Envelop of 100% power, Upset) all valves closed and three R/V open cases) NOTES: (1) Set Names correspond to those used in Appendix C. (2) OBE and valve actuation (R/V OPEN or S/V OPEN) were sumed by the SRSS technique, based on References 7.le and 7.7b. O 1 5-8 l l
l Report No. 01-0300-1291 ; Revision 0 a 5.4.2.2 Valve Accelerations Valve accelerations are based on plant global coordin-ates. The accelerations are sumarized at all DCP's on the valves (shown by Appendix A). The valve center-of-gravity for each valve are: Valve DCP II) PSV 8010A V3A PSV 80108 V2A PSV 8010C VIA PCV 455A V5A PCV 456 V6A MO 8000A V7D 1 MO 80006 V80 i NOTE: (1) The DCP locations are shown in Appendix A. l 5.4.2.3 Valve and Nozzle End Loads i Valve and nozzle loads are sumarized at attachments to the pipe. The load and moment orientations are shown in
. Appendix C (Figure C-1).
J A 1 i O 5-9 1
O E C I q V e r E
- D
- c N
- O
- I 3
1 S R
.E V
o c OlO i s N c E G C U R S L G - F H I T N d
^ c E N S i
% CI n E
. c i S S i o
I L t C A c E N n S G u I V F c R g c E 0 n i a 0 c M i I c I r o FO V R e O P e m 1
~ YN -
NG 1 4I rI 5 . MG OI e f C ", r u i lC 4 g lf i
. R1 T1 F C4 i
ER LE f EN E LL c A i c i RR _ EA 4 NE EL CC d ON N
- - - - - r.
RN LA IJ RG
- GR
- c e c c rI M o 0 e 0, g ,
4
- n 3
.. wm e w a uo u.
O
.. - . . . . .-- - -. - u.. n ., -. . .
m M. h m m m ammme w- *
,(- .aw,w ~y 4 r
,, 79 '-
.. w
'sl 5
U .7 7 i
, s [/ -
s , p " l , ,.&',
. . ^/
) . ....
*/
e 4 S ). .
, 0 .+ q; y - j NW m)
't -
/ .,
~/ l:.:s
, n p i .
.. t s, u ,,
- - . ; ; 1 v I' #
sf' .i
., 22' 2
~ .~ y) /
l , ; ,.- '
/
4 . I 4 ,s , 4&7. ~
'(
g4 f , _'e , .e - we .- -
*/
? Sn.
' ~<<
j m , i .J l o ce ,/ F
.lOCC --
-_i t
y 'A LJ ^ M g , .. A w V a x n -2447, - 4 i i 431). - , I i
- ,gg a f f f . I i 1 . I G CC to J% C 100 C.400 1 '.CC C 500 0 PSC
- IIME I SEC 1 rGRTLRNO CENERAL ELECTRIC CCMrGNY SECMENT FORCE NG . 15 i IROJ4N NOCLEGR LENERATING STGTION FORY ANALYSIS WITH "uuG DIVERSION DEVICE l
j Figure 5.1-2: PORV Forcing Function I I i
1 11 O_ E C I V i* E D
." N O
6IS 1R
.E V OID i
- N 8 E G U C L R S
. O F H T
T I N W E M i
- C S EIS C
1 S Y L C A E N S A V n I R o C 0 i
"EN 0 t c
o I n I u F g
, m i
nO c o r _ F
^c -
- YN V NG R AI O rT P MA I G F'
I, : c, 3
, r CC -
1
$ IN
'n Rl Ti 5 CG ER e -
LE r EN u E g L f. i c A F o RR EG -
's NE EL CC d
DN N AN L4 TJ
- - = RG c OR 0 j FI o Q 0 0 c;
- 0 C 0
- c C
- 0 0 0 c
- o 4 7
- *. 2 1
- - - os
- um
.e U 5 u.
O
l E C I c V
+
. o r E
- . - D c
N
. O I
S S e I
, R
~ .E V
s .
/
- I
=
. o O D o N
=
r# ' s s
=
E C . - o m C U R S L O . F H
- T T
I N W c E o H C S
~"
s
, EIS
. I S Y
- C E
S A R L N n o i I V t R c 3 r. m .
,E n IM I
0 0 F u L ' g em n
- i c
alU m m m r o
- e F t y V
R m O YN P
- N0 Al :
ri m i I. MA 4 Oi 1
- f. C 's m i ,
g CC IN 5
. RI e TT r CA u n ER g LE i EN F E
LC
= A
, RR
. - -< s ,
ER NE EL
-,. CC U
DN N AN
- LA
< TJ
- - - - n RO n OR
- 7.
4
)
1 1 O 3. 3 1 7. 4 s q c s FT 4
- 4 1 3
- n. _
o s
- - aDy -
LC e JJ s tL 3 gta. s.
].
0v .
< ' .'t I
E C I C V I C E I D
'0 4 0
1 0 $ 2 R
,E V
i 0 G 0 0
% N 0 C E U E
R S L O F H T T I N 0 E U 0 N
' Cl5 C E S I S 1 L
C A E N S A n I V o a- R i C E O t 1 4 N F c C n I I u F C r g 3 o F g V YN R 1 N0 O R1 P f rT MR : GI ES 5 i 3 CC 1 IN
.e RI 5 Ti CR e ER r LE EN u
g E i LC F 0 A
#0 RR 1
ER
-O NE EL CC J
DNt N GN LA IJ
- - ,* RO
- - ~
C OR C 0 g PT 0 3 0 0 e 0 C C C c 0 0 0
^ C 4 4 J S 4 -
- aDJ w LE e
uE
'e v
E C I c V Ier E D o N - N O 1I 2 SR
.EV c
e OlO I s N c E C U E
- R S L O
F H T Tl N m' t c n, E HS C E u I c
. I S S Y L
r C E A N r S A n i Y i o c R O t i cE c F
- c. M n I
I u F g am n m i m m m s c a c r s v. F o c U Y YN NO AI PT MA R O P OT 6 CS c - i r CG 1 o IN
. RI 5 TT CA e r
7 ER LE EN u g E i LL F e A i c RR i EA c NE - EL CC DN d N AN - LA TJ c RO __ - - - ~ - - . e n OR c e c e FT _ o c 6 _ C c c o C o c o s C 5 I o i s - 0 3 Ju5a ss
,Illl.
,1lll(lll e
S E E I io's c V E
- D 9
lI N O S
.R E
OV NI c D
- c. E i
- EC c RU CL FS .
TH NT EI HW C ES . SI S - e w.Ci Y L cE A n S N o R i I V t E R c S n M u I I F c g I o. i nO c r F o V R YN O NO P
. HI rT :
i
< MG 7 CI -
CS 1 fC i N 5 Rl Ti e CG r u ER LE g I EN i Lt E. F t se A
- RR ER NE EL CE !
i DN N Ah L5t IJ
- - - ::. RC
- - r. OR
- 7. F1 n
- 7. s 0 3
3 % u 1
- 0 J 3 58 1
- I2 Ia i wUE O
h _ r _ S E f i 0 I0 v
*. E 0 D N
0 41
= 5
.R E
OV Nl O e l 0 0 0 E CG RU OL FS TH NT
- El a
MU C
- ES SI C i S - I 0 Y 4
C L C E R S N n I R
. i o _
= V t
=
= E R c
=
=
M S n I u T F m C C g
- i n
m~ i ay m e c r o F
' V - YN NG Rl R
S Pi l J MR 8
. GT - . C LS 1 CG 5 IN Rl e _
Ti CR r A{ i ER u g LE i
- EN E F 0
l 4 LL 1 A O RR EA NE EL CC d DN N AN LA TJ O RO
- - - - - C
. . C.
GR 7 3 0 7. 7. h FT T 4 1 0 9 4- C
*. 4 1 2 7
= kED J. e dJKOL LL e
l'
i m M S E r t C i O A v E 0 D N G - 6I S
.R E
OV Nl 0 O 0 E I
' CC C RU OL FS -
TH NT 6 EI HJ C ES SI 0 i 0 S I 4 T C L C E R S N n H o I i V t E R c S n H u l F f
' g I
0 1 n i c r _. o F V R 1N S NG Rl : l ri 9 t I J HG - CI 1
/
0 FS 1 CC 5 t IN Rl e li r rG u g ER LE i EN F C E I O LC t G O RR EA NE LL CC
-- d DN N
%- RN L4 I3 O RO
- - - - C C OR 0 "1 FT
^ O 0 C 0
^ 0 0 0 0 2 *J C 0 0 C O 0 0 9 J 01 01 2 3
- $- e=t e
_ . . . . .. . _ . . _ ._ ~ - .. __ ._.., . 6 (s (-
\
,,,, I..
(v ~ 4
==
U i nce - i 1000 - i
~
u_ . um 8 { ] . a. y w .
. ia 5 ,
i u \
. g i o u- t
-100C. -
l i 2Cnc - 1* i
- i . . i . . i . i , e . . i 3nnhCCO C 100 C2 100 C.400 C '00 0 600 i
. TIME I SEC 1 l FGRILON'O CENERAL ELECTRIC COMPANY SECMENT FORCE NO . G IROJAN NUCLEDR f.ENERGilNC ST9 TION SRV RNALYSIS ulTH SLUC DIVERSION DEVICES ^
i i l Figure 5.1-10: SRV forcing Function ' i l ! 6
. .~
] O_ S E E o i I c v A E c D N O 9I S
.R E
OV NI c D o, E i CC c RU OL FS TH NT EI MW C i ES SI c I S o Y 1 S C L n cE A o S N i A t I V c R n I E S u H F l i g i e c i c i nO c r o F
, V R
S YN N0 : 41 1 r1 1 t
< M9 -
OT CS 1, CC 5 IN RI e TT r CA u ER g LE i EN F E t o LL .- t R c RR EA NE EL CC d DN N GN 1 fR iJ
- R0
~ ~ - ~ c c O6 0 C 6 F1 C 0 C
T. C 0 1 0 0 8 C 0 2 3
- J- a
$5' O
r I O S E C I 0 0 V i9 E J 0 D N 3IO 1 S R T .E O fv N O C I C E C C C R U L O S
- F T H T
N l E u H m m C S u E I m S S m C 1
- a. 0 Y I
4 C L n C E A i o
; S N A t I c V n r E R u M S F I
g O I 0 n i 0 I 1 c r o F V R m YN NO S RI 2 rT 1 I N4 - J m C 0T [ '2 CC 1 5 IN e _ Rl r Ti CA u g ER i LE F EN 0 E t 0, LC A RR EA NE EL CC d DN N AN LA TJ
- - - - RG c 0R C 0 q 3 O _
! 0I C C 0 C _ -
_'~f
; O 0 0 C .
O 0 0 0 - J 1 1 2 _" e s s. it - O _
M e_ S E C I 0 0 V 6 E C D N sG
'II S R
.E V
OI N G D
' E C L U C R O L F S T
N E H I l N u C E IS 0 i S S 0 l
. C l O E A n
S N A o I i V t E R c M S n I u I F 9 r C' r f o
' V YN R NC S Al :
- PI
'J M4 3 OI 1 c CS -
1 CC IN 5 Rl Ti CG e r A C C I ER LE EN tC G E i F u g O RR EG NE _ EL CC U ON N RN L4 I3 O RG
- - - ~ . - O G GR C c C c ! PI
- 0
- 0 C o C c 0, 0 o C 0
= 0 s 3
'J 1 -
2- r. ~
- _ i d" 5 u e_
h Re No 01-0300-1291 /
6.0 CONCLUSION
S As discussed in Section 5, all components of the large bore Pressurizer Safety and Relief Valve piping system meets the requirements of the System Qualifica-tion Criteria, and the applicable sections of the B31.7 and B31.1 Codes. The system is qualified for 25 actuations of the relief valve. To maintain system qualification the number of relief valve actuations should be monitored during the remaining plant life. The qualifics. tion of the supports, valves, and nozzles are not included in the work scope described by this report. They should be verified separately. O I i
, O 6-1
Report No. 01-0300-1291 Revision 0 I e !
7.0 REFERENCES
7.1 Codes a. ANSI throughB31.7, 1971 Nuclear (Code ofPower RecordPiping, 1969 for Class Edition,). including all addenda 1 Piping
- b. ANSI B31.1, Power Piping, 1973 Edition (Code of Record for Class 3 Piping).
- c. ASME B&FV Code, Section III, Nuclear Power Plant Components, 1974 Edition, including all addenda through Summer 74 (For Class 3 Branch Connection SIF).
- d. ASME B&PV Code, Section III, Nuclear Power Plant Components, 1977 Edition, including all addenda through Summer 79 (For Class 1 and Class 3 Flange Evaluations and Class 1 Butt-Welding Tee Stress Index B1).
- e. NUREG-0484, Methodology for Combining Dynamic Responses, Rev.1.
- f. NUREG-0800, Standard Review Plan Section 3.7.3 Seismic Subsystem Analysis, Rev. 1.
7.2 Design Criteria / Input Data O
- a. Trojan Nuclear Pressurizer Blowdown Piping Analysis Design Criteria, Revision 0, transmitted to Impell by PGE Letter RLS-415-82, dated April 2, 1982.
- b. Trojan Nuclear Plant Pressurizer Blowdown Piping Analysis Design Criteria, Rev.1, transmitted to Impell by PGE Letter RLS- 489-82, dated April 21, 1982.
- c. Trojan Nuclear Plant Pressurizer Blowdown Piping Analysis Additional Design Criteria, transmitted to Impell by PGE Letter RLS-554-82, dated May 7, 1982.
- d. Trojan Nuclear Plant Pressurizer Blowdown Pipe Analysis Design Criteria for Final Stress Report, Revision 2, transmitted by PGE Letter RLS-124-84, dated January 20, 1984. }<
- e. Trojan Nuclear Plant Pressurizer Blowdown Pipe Analsyis Design Criteria for the Final Stress Report, Revision 3 transmitted by PGE Letter ,
RLS-390-84, dated March 27, 1984 l 7-1
. . ~ - - - - - _ - - - . - - . . . . . - .- -- ..- _ _. - - - _ . - - _
I Report No. 01-0300-1291 Revision 0
/'
7.3 Final Safety Analysis Report Trojan Nuclear Power Plant, through Amendment 34. i 7.4 Impell Problem Files, Reports and Letters Related to the Pressurizer S/RV l P1 ping System
- a. Thermal-Hydraulic Analysis Calculation File No. 0300-018-1373-TH02, Revision 0.
- b. Impell Pipe Stress Analysis Calculation File No. 0300-018-RC-01, Revision 0 (as-designed results).
- c. Impell Report No. 01-0300-1216 Revision 0, " Trojan Nuclear Power Plant Load Simulation Analysis of Pressurizer Relief Piping System".
- d. Impell Letter No. 0300-017-010, dated November 5, 1982, " Summary Report on Piping Analysis Efforts for Trojan S/RV System Verification".
il l
- e. Impell Letter No. 0300-01-002, dated March 4, 1983, " Slug Diversion Devices".
lO I
- f. Impell Letters No. 0300-018-003, dated March 28, 1983, and No.
0300-018-005, dated April 19,1983, " Support Load Sumary" (as-design results).
- g. Impell Letter No. 0300-018-010, dated June 8,1983, " Valve End Load Summary" (as-design results).
i 'l l
- h. Impell Pipe Stress Analysis Calculation File No. 0300-018-RC-02 through RC-06, Revision 0 (as-design results).
i ! 1. Impell Pipe Stress Analysis Calculation File No. 0300-018-RC-01, Revision 1(as-builtresults).
- j. Impell Letter No. 0300-018-014, dated March 30, 1984, " Transmittal of I Results"(as-builtresults).
l k. Impell Pipe Stress Calculation Files No. 0300-018-RC-02 through RC-06,
- Revision 1(as-builtresults).
- 1. Impell Report No. 01-0300-1292, Revision 0, " Trojan Nuclear Power Plant l Stress Analysis Report for the Pressurizer Safety and Relief Valve i Small-Bore Piping Systems" (to be issued).
!O e 7-2 l 1
Report No. 01-0300-1291 Revision 0 1 l. 7.5 Class 1 Thermal Transient Data
- a. Westinghouse SSOC 1,3, Revisien 2, "NSSS Design Transients".
- b. Appendix A to Westinghouse SSOC 1.3, Revision 0.
- c. Impell Calculation Files 9602161-A and -B, Revision 0, "A Review of the 1-0 and 2-0 Thermal Transient Analysis for Piping Components".
- d. PGE Transmittal Form 16153, dated April 21, 1983, " Pipe / Fitting Thickness Data for RCS Pressurizer Blowdown".
7.6 Drawings
- a. Piping Layout Drawings: ,
- PGE 7108-RC-151R-1-1, Revision 11
- PGE 7108-RC-250lR-8-2, Revision 6
- PGE 7108-RC-60lR-2-1, Revision 17
- FGE 7108-RC-2501R-12-1, Revision 11
- PGE 7108-RC-2501R-8-1, Revision 8
- PGE RC-60lR-2-1-20, Revision 2
- PGE RC-60lR-2-1-21, Revision 2
- PGE RC-60lR-2-1-22, Revision 2 h
- PGE RC-60lR-2-1-23, Revision 3
- PGE RC-60lR-2-1-24, Revision 2
- b. Equipment Orawings:
- PGE C-375, Pressurizer Supports, Revision 15
- W Pressurizer Dwg. 6478-MIA(10)-4-2
- W Pressurizer Owg. 6478-MIA(10)-2-7
- 7 Pressurizer Relief Tank Owg. 6478-MIA (11)-1-5.
-{PressurizerReliefTankOwg.6478-MIA(11)-2-3.
- c. Valve Drawings: 1
- PGE 6478-MIR(2)-183-2
- PGE 6478-N25527-1-2 (Copes Vulcan Dwg. E-262539, Rev.3)
- PGE 6478-MIR(2)-054-2
- d. Other Orawings:
- PGE Pipe Support Details Listed in PGE Lettar RLS-124-84, dated January 20, 1984 0
7-3 I
Report No. 01-0300-1291 Revision 0 / O 7.7 Other References
- a. EPRI Letter (Frun A.J. Wheeler) to Utility Technical Contacts and Piping Subconnittee Members, dated November 5,1981: S/RV Piping Subconnittee, October 29, 1981, Meeting Agenda and Suggested Additional Note for the Load Combination and Acceptance Criteria Table.
- b. WCAP-10105, Mestinghouse Reoort, " Review of Pre 3surizer Safety Valve Performance and Observed in the EPRI Safety and Relief Valve Test Program", June 1982. ,
- c. EPRI NP-2628-SR, EPRI PWR Safety & Relief Valve Test Program, " Safety and Relief Valve Test Report", December 1982.
- d. Electric Power Research Institute. " Minutes of the May 5,1982 RELAPS Workshop" and attachments, May 25, 1982.
- e. Intermountain Technologies Inc., " Application af RELAP5 for Calculation of Safety and Relief Valve Discharge Piping Hydrodynamic .,
Loads", Interim Report, March 1982.
"O
[g l l l I O 7-4 i I
O I I I I 1 l l APPENDIX A ' MATHEMATICAL MODEL l l 01 O
* . a ,
j! ; 0 i: i!t y ,
=e - -
.i ,t
.d 3 !h!!
r!i ;r sl jil - , U - I': . .c m, iki O,jl!!! Illi::$i j I I! M W i :
?.
.r /\ ili liii!!
mm hil;ith p p ll3 o, ill A 1:
; lg wm .
i.!!iLj !yJ;!!!
- i>
r il :; ! e . i s/# e_. s - ii . t .,, . .... N'{ a. . ll c i ert. t + r- #s.yeerte La i 2 s..
, wig e '
i
~
@ . ,1 to h dr *' By g r .. y 'e M've4 4
fp, _ .1;
\ G :e .
"e M/M </;;&wf -
1 i $l 8, p; e(' 11 li ' W " - [ ' ) [O g'i1/ii.gitJ'*s{g.)- b s',' ; ' v o m
%ds e a i
9R ,a,K
'B ,_(.L -H '*ii,s k. A - Y .
WlS 1 o e4 s ipr t
,g p
3
-4
> . . g
[ W/ 'i E do I
*p
- 4 s h t o y *(
[*o !!
@2 0
./ M[ III I t s.,
s
~ ;.\
m: p,spQ( .. , s4
. .g p=
.e .
1e&.
!g < ..
I ji , . g= j we i, i
- i. } 4 ,
,[$
~
Ws [f6{=dIn 6 . : . i! e , s ($~i:.M)1, i! i
& e f * '
';' e, i- :: ___fl 's : if
[i il;)!gj'. i 11 $ ii 5 ii i !; El l{ j' [!! -$~$2
~~
i l il ,~-
' i; g ____41 i ! ;r I}
l 9 p!!!
! i 1 1 i7
'\ .!! !l i f- j l 3-l 1 4 E-o hl}
I 11 ; i i j 1l! l in, if*
'la!his 2 I h .a n "
_ _ _ , , . . . - * = __4 j'39pM}
\ '$
p digy B
/ (9.y k p0p at i.
-^"
%/ -
8 4 4 \g ! g ' M M qi ,j, {
\-
- 4.Sj, y -
1]1 d@h sin .
- y. sf i g ,, e T
_(Ch[!? .\ ' 38 " vg,' ; ,
- At t; ,
Jp , q
. n . v J.! ,f* 4 4.
- s x n; l 11
, % j.-qs
+ >.
/> sr , y. n .
\ ..
T
- m. .
. m , 1 t
2
- f.
a' S, @ $( thb) N/ k'! o$ 3' , I.. sr
.; i
?t f klE' ,h f' f . [,
.ef;~n//yi h,, Q,g90 g t i
> t M b s f5 .
3x 8 S&,
?tyt sN.N(a li/hhgkNj ;ie
; \N3"" rJ W i .\ 'i!
Dy.!} 1
\x i i e '*
e 4D e &
/ 1'A C i
Tph g; g j D h a?p il sn gasipppygggg gi s ,, .. .. ., 4. 2 .,
<>i e
I
- i I ! gli'-
I h: 1
; I' ___H J , ___n I ! ._
a
.- a
---lj [5 3 i !3 ,
g a i 4 ,, 3 0 -
~
fx.l l
; ; l i ll EUfi!
.. ! , , h.
- > b gj i a p, .a l I,is e
-7 l ll ll
~ 11 as s I
[ '\h \
#yhk! .i . -
b
$\
se 'l . I
- O +
't T -
l . l. I l h g j
. ,v. c .s.
k (G b' t g e O' 4. B n1, k g4 s t fg #
- 59 , 3 . .l L
- D : /
1. i
O APPENDIX B COMPUTER PROGRAMS DESCRIPTIONS I Ou 1 I I O I J
Report No. 01-0300-1 291 Revision 0 O APPENDIX B COMPUTER PROGRAMS DESCRIPTION SUPERPIPE SUPERPIPE is a general-purpose piping program which perfoms comprehensive structural analyses of linear elastic piping systems for dead weight, themal , expansion, seismic time-history or spectra, arbitrary force time-history, and other loading conditions. Analyses are perfomed to ASME mquirements for Class 1, 2, and 3 systems. The program has various features for user ease in defining the piping system. These include automatic generation of node coordinates and curved segments or elbows, automatic cartesian / polar coordinate transformation (translation / rotation), built-in data (including stress indices) for standard material : i properties, and piping schedules. The program also has various plotting > ! capabilities, and extensivo diagnostic error and warning messages aid in checking the model. In addition to the basic capabilities for perfoming dead weight, themal , expansion, seismic response spectrum, and anchor movement analyses, SUPERPIPE i offers a number of more sophisticated features for specialized piping analyses. These include: l
- a. Analysis with multiple response spectra for piping supported at numerous !
levels within a building and, therefore, subjected to independent loading ' (different spectra) at each level. l
- b. Modal superposition or direct-integration techniques of time-history analysis for shock loads associated with steam hamer and water hamer effects in piping systems, or other arbitrary fort:e time-history loadings.
- c. Analysis with multiple acceleration time history for situations in which j a pi sing system is subjected to independent motions at each support, and in witch the effect of phase relationships between these motions is important. ,
Static or dynamic equilibrium equations are fomulated using the direct stiffness method, in which the element stiffness matrices are fomed according to virtual work principles and assembled to fom a global stiffness matrix for the system, relating external fortes and moments to joint displace-ments and rotations. Six degrees-of-freedom may be specified at each joint of the global system for both static and dynamic analyses. O B-1
I 1 l Report No. 01-0300-1 291 Revision 0 9, ' I The program has a number of element types which may be used in any combina-tion. These include:
- 1. Straight pipe
- 2. Curved pipe 3 Valve
- 4. General beam
- 5. Flexible coupling
- 6. Arbitrary stiffness matrix Static equilibrium equations are solved using Gaussian reduction techniques on the compacted stiffness matrix. For dynamic problems, the equilibrium ,
equations may be solved using either step-by-step direct integrations of the I coupled equations of motion, or by first calculating natural frequencie'. and mode shapes and transforming the system into a set of uncoupled equat4ns of motion. Natural frequencies and mode shapes are calculated using the deteminant search technique. The program has been thoroughly tested and verified for a comprehensive set of l sample problems, including extensive comparison with several publicly- , available programs and ASME benchmark problems. All verification analyses have been documented in accordance with established Impell Nuclear Quality Assurance procedures. g TRANS2A TRANS2A is a computer program which detemines radial temperature distribu-tions and gradients in a pipe wall experiencing fluid temperature excursions. TRANS2A detemines these temperature distributions and gradients by solution of the unsteady one-dimensional axisymmetric heat transfer equation. For aid in Class 1 piping analysis, values of the thermal gradients,6T) andaT2 . and the average temperatures (Ta and/or Tb ) are calculated in accordance with ASME BPVC Section III, Paragraph NB-3653, and USAS 831.7, Paragraph 1-705. To be of more aid to the analyst in choosing values of the average and temperature gradient data to be input to the Code compliance analysis, TRANS2A evaluates the actual histories of the thermal stress tems, according to the equations of Section III, Paragraphs NB-3653 and 1-705, with as many as ten sets of. stress indices, and summarizes them in a table by extreme and time of occurrence. TRANS2A has been extensively tested and compared with independent result for sample problems. TRANS2A temperature distributions agree favorably with calculations using TRANSIA and the Impell proprietary finite-element program TAPAS. Calculations for thermal gradient tems6T1 andaT2 compare favorab^ly with results from TRANS1A and with the values derived from charts published by McNeill and Brock in " Engineering Data File -- Charts for Transient Temperatures in Pipes",1971. O B-2 I
i Report No. 01-0300-1291 j Revision 0 O ; k
; RELAPS Developed for the U.S. Nuclear Regulatory Cossiission by the U.S. Department of Energy's Idaho National Engineering Laboratory, RELAPS is a one-dimensional i system analysis code which provides a numerical method for detemining the l 1
transient themal-hydraulic behavior of light water mactors. It predicts the interrelated effects of coolant themal-hydraulics, system heat transfer, core I i neutronics, and system component interactions for postulated loss-of-coolant accidents (LOCA) and non-LOCA transients. The development of RELAP5 has been influenced to a great extent by the l experience gained through the development ard use of the RELAP4 code series. i The RELAP5 code, released in May 1979, was primarily a pressurized water l reactor blowdown code. The M001 version extends the M000 capabilities to include models unique to small break situations and to include capabilities for modeling certain system parameters and components.
~
The RELAP5/M001 code includes component process models for pipes, branches, abrupt flow area changes, choked flows, pumps, check valves, plant trips, control systems, steam separators, heat structures, and nuclear reactor core !I neutronics. Major new features in RELAP5/M001 include the ability to ;
- incorporate non-condensible gases, homogeneous or separated 71ows, equilibrium i or non-equilibrium effects, and small break phenomena. In addition, the code
)
is faster running and more flexible than earlier versions of RELAP. t The hydrodynamic portion of the RELAP5/M001 program uses a non-homogeneous, il non-equilibrium, two-fluid model. It consists of five field equations, including two phasic continuity equations, two phasic momentum equations, and an overall energy equation. The numerical scheme in the code applies i i finite-difference techniques to solve the five differential equations used in ! 'I the hydrodynamic model. l !' REFORC [ }' REFORC is a post-processor program develo Electric Power Researth Institute (EPRI) ped by of in support Impe11 Co@ the safety oration for the
/ relief
! system requalification effort. The code calculates forces using the i thermal-hydraulic data generated by RELAP5. i > i The total force detemined by REFORC is the sumation of the acceleration or
; wave force Fw, the control surface or blowdown force FB , and the gravity I 3
force Fg. I ; i I 1' B-3 i
Report No. 01-0300-1 291 Revision 0 N'
. 9, REFORC2, the code version released in June 1982, is an optimized code which also includes variable time steps, the sum / merge capability, junction volume sunnary table, increased volume / junction capability, improved handling of non-sequential volumes, improved output fonnat, restart capability, and a plotting package.
91 O B-4
6 O APPENDIX C COMPONENT LOAD SUMMARIES 1 I IO I
,O
Report No. 01-0300-1291 Revision 0 0 APPENDIX C COMPONENT LOAD SUMMARIES C.1 Support Load Sumary Computer Output Sequence No. 84/03/23. 11.16.16. Pages 207 through 275. C.2 Valve Accelerations Ccmputer Output Sequence No. 84/03/15. 15.31.04. Pages 161 thrcugh 163, 165, 167, 221 through 223, 225, 227. Computer Output Sequence No. 84/03/12. 12.09.36. Page 356. Computer Output Sequence No. 84/03/22. 11.35.56. Page 346. C.3 Valve and Nozzle End Loads Computer Output Sequence No. 84/03/23. 11.16.16. Pages 11 through 26. l l l 9 C-1 Il
1 ke i. S UPERP c [OS10m 150, tr#31/C?8 SvsTf"2 1pPELL - We5
...c .. p (9 set:3#23 33.3%3.
O PGE TDeJA3 muCLE03 ST3ilen ESS Ppete.tp 33ttbla ac e3 REv.1 ' Q ! PetSSumIZER St#W Lint Q aS_PUILT stentTag utTM SLus SIvtasten styICTS (S005 < O O _ o O . . O : 1 i O O.! s ' - - ** 4Q b O
* . ~
6 ., O
- O OESI6N <
/ .
~
^ ~'
-+
. i -
Q . VER I F I C A T 1 O N -2 s . O e
. e o
O SUPP04T LO.O
SUMMARY
.t * '- L 'u . SUPPO47 LEAD semeAnf F OR ALL Load CO*PINATIems ' . . FOP ALL LOAO C8mftWATIONS i
-O " . " " " " " * " -
3Ot
,O .
Ctar=1 M_f . O O 43s =0. D-SW" /-iG .
'.' O !
. ( I
~o .
CatC..Pson. me. %-8/ %-f .
'O j .
o 4
.~
.................. Oj
-{ '
,.cP..co . :
7 A , ..Tc:sg.py j g
. coce.co .: eg .. c:
44 : O - O. O 0 jO o O o
- 0 O
o L
Q IMPELL CORPOROTION CA' E 2RS ()
~
i, S UPE C')I PE VER$104 16A, !?/91/838 SYSTED IMP [LL - NOS 84/93/253 11 1631 % PGE T ROJA"] NUCLE A2 STATION g' Q EDS PP08LEP R30001R-pC-91 REV.1 PRESSL132ER S/RV LINE AS-8UILT GEOMET*T WITH SLUG DIVERSION DEVICES (5009 $ Q SUPPOR T .LO AD SUMM AR T SUPPORT LOAD SUMMART
~
s FULL (ALL SUPPORTSI
~
Q Q CHECNING R EGION INDICATOR z DETL (CETAILEO PRINTOUTS ; OUTPUT DETAIL INDICATCR COMMENTART INDICATOR s COPM (COMMENTA4Y TO PE PRINTED) , s OLOC (RE-UTE PREVIOUS CARESS O Q LOAO CASE INDICATOR' PRESSURE DISTRIMUTION INDICATOP z 4N0 nISTRIBUTIONS TO BE SPECIFIEO) O O, TEMPE9ATupE DISTRIBUTION INDICATOR s (NO DISTRIBUTIONS TO BE SPECIFIED) . t .g O DESIGN CHECK COPPENTAPY , O O Q LOAO CASE /COMBIN ATION! DESCRIPTION O' NORPAL CPAVITY: PIPE [4PTY Q Q GRAW THM1 NORMAL OPERATING THERMAL: ALL VALVES CLOSED THM2 UPSET THERMAL: RELIEF VALVE PCV 4SSA OPEN THM3 UP$ET THEPMAL: SELIEF VALVE PCW 456 OPEN O Q THM4 UPSET THERMAL: BOTH RELIEF VALVES OPEN . THu% CPERGENCY THERPAL: ALL SAFETY a RELIEF VALVE OPEN OBE SEISMIC Q
- Q OBE SSE SSE SEISMIC: 1.67*0BE FIH1 PELIEF VALVE OPENING SAFETY VALVE OPENING Q
.Q FTH2 THPU NORMAL 2 UPSET THEPPAL: PAN. RANGE
. THRM NOPMALe UPSET, & EMERGENCY THERM AL: MAN. RANGE FTHE FTH1
- FTH2 (NOTE 2 9 Q Q Av00 OBE
- FTH1 INOTE 1.1 SROB 08E
- FTHE (NOTE 1 3
, Q' SRWS $$E
- FTHE INOTE 1 3 Q NOPM N0* MAL: THP1
- GRAW UFST UPSET: THMU
- GRAW
- RVOR
[MERGENCT: THRM
- GRAW
- SR08 Q Q EMER FLTD FAULTED: THRM + GRAV
- SRVs O
O NOTES: 1. $895 SE!*FIC WITH VALVE LOAD *
- 2. ENVELOPE OF VALVE LOADS Q O
O , 0 O _ _ O__ _ _ _.
- _
*l .
'Q MPC.. .%Q S UPE APIP
,..ON RSIO4 16 As I f tt1/8!sg . Systgp 1MPttt . Not
....E 28. J p 94/03/23 11 1$.1$q g
- O Pat Tr*Jas avCitan STATToi O
- EDS PRetLEM 93 Bet 12*PC-01 revel O II IO N bE' U I' II " 8' " ""*" "' " "' O Q- LCAD $[i SPECIFICATION O
,Q SET COMB . O ' NAME TYPE LIST OF CASES IN GROUP TITLE 1 ' 0 0 NORM DFLT GRAV THMS .s-l@ UPST OFLT GPAV RVC8 THM1 THM2 THP3 THM4 D. EMER OFLT GR AW Sm08 TH49 THM2 THMS THM4 THMS FLTD DFLT GR AW SPVS THM1 THM2 THM3 ftaM4 THMS
~
jQ THMt _DFLT kHM1 O THMU DFLT THM1 THH2 THM3 THM4 % i0 - O i !0 - O i
^
lO _ O
~ '
~
iO - O O O
- O O
- O > 0
- O -
O
- O O
- O- .-
.- O
!o o i a 'O O
\
o INPELL CORPORQ1103
- PAZE 218 ([) ,4j sdPE; PIP [ WEOSIOb 16Ao it/01/n38 Sitita IMPELL - NOS *
. 84/03/23s 11.13 10. ,
e PCE T00JA3 NUCLEAR STATIO3 () EDS PR06LE2 t300818-RC-01 REU.1 P8ESSLRIZEP S/RV LINE o AS-8UILT GEOMEIRV WITH SLUG DIVERSION DCVICES 65003 d) DET AILS '0F SUPPORTS FOR THIS
SUMMARY
() SUPP SUPP N Y Z SUPP DIRN INCL, DIR. COS. WR7 GB'JBAL ARES C) CAME LOCN C00PD C00RD COORD TYPE CODC ARIS X Y Z (Fft EFT) 4FTS O 6 6 -33 112 120.250 -31.935 HANG Y () 12 12 -31 829 116.75* -31.481 SNUB V 161 16 +31.664 11R.261 -3 C.7 0 7 SNGL INCL M .7779 0.90e0 .6283 Y 6. POOP 1.CC 0 9.3000 C) 2 .6283 8.S682 .7779 16Z 16 -31 664 118.261 30.707 $ NGL INCL M .6283 8 0 Cat .7779 Y 4.4089 1. nets a.0006 C) Z .7779 a.0000 .6283 19 la -32.366 119.258 *29 841 HANG Y 25 25 -33.86u 113.833 -27.995 SNUS INCL M .7431 0.0080_ .6691 () Y f.04ng 1.g:04 p.geoe F .6691 0.CGLt .7431 28 28 -?1.792 3Et. nan -31.T84 SNUB INCL M .6293 8.0000 .7771 () Y 3 3000 1 8000 e.9000 Z .7771 9.ntfC .6293 29 29 -3u.320 114.290 -32 366 HANG Y () 30 34 -34.320 111 458 -32.366 SNUB INCL M .7772 0.00GB .6292 Y 4 9400 1 03C0 P.0000 0 Z .6292 0 0000 .7772 () 31 31 -?4.320 814.875 -32.366 SNUB Y - 32 32 -3s.792 110.125 -31 784 SNUS INCL M .629 3 0.n060 .7771 0 Y 0... . i.0. 0 0..On. c) 7 .7771 9.0GC0 .6293 354Y 35A -36.754 119 12% -2F.097 CONF Y o 41 41 -36.565 12a.251 -35.683 HANG Y () 48 4r -36 932 116.75" -37.003 SNUB Y 525 52 -37.724 118 2F1 -37.SG3 SNGL M Q) 522 52 -37.724 118.271 -37.803 SNCL 2 CD 55 55 -36.839 11".25p -37.eJ3 HANG Y 61 6f -41.214 116.583 -37.003 SNUB INCL F .8584 .0128 .9982 d) Y .A4P7 .*999 .6128 () 7 *.9983 0.tLLG .*584 63 6? -35.594 115.tr* -37.n63 Ha t:G V d) 64 64 -35.494 13 5.i' i -?.7.403 SNUB INCL u 1.'80C 9.n000 3.tP00 () Y 9.1000 1 00C0 1.0C9F 7 1. '. 3 G ; e.1ern 1. tCG B) 65 65 - 3 4 . 7 4 .' 114.2% -37.8?' SNUR Y () 67 67 -35.44* 1?n.33? -?7.'63 SNUB IUCL M 1.;936 ?.0000 ?.184 8 Y 4.1nen 1.arCr * .J L'J 1 73 7; -43.24V 13A.333 -34.41*
$ nun Y
- 5) C)
~
9 < . - .-. -- -- 9 9 _.
;()
sMPELL of~~^(ma s s CN f-~g rsel 21s -~s g) p
$1"[CPIP~ }RSION 16Ao It/31/831 SYSTEM IMPELL - NOS et/03/23c 11.16,16/
)
': (3 - PSE TalJA2 NUCLEA2 STATIE% EOS PROBLEM 8389018*PC 81 PEV.1 () PR ESS UR 1FER S/pv LINE
- ()
AS MulLT GEOMETP.Y UITH 2 LUG DIVERSION DEVICES (SOD) .. () ' f () DET AILS OF SUPPORTS FOR THIS
SUMMARY
(CONTO.8 () - () SUPP SUPP NAME LOCN COORD N Y COORD Z C00PD SUPP DIRN 1YPE CODE INCL ANIS DIA. COS. WRT GLOBAL ARES X Y CD Z j EFV1 IFil (FT3
- () () , () 71V 71 -43 243 10R.333 -?4.961 CONF Y . ()
77 77 -41.277 123.25* -33.724 NANG Y 83 83 -42.784 116.75f -33.964 SNUS Y =
' () 8FX 87 -43 250 118 261 -33.323 SNGL I ()
877 A7 -43.254 110 *%1 -33.323 SNGL F 90 96 -45.254 18 *% 2 S e -32 2e9 HANG V
. () 95 9* -45.25L If>.86* -29.834 $NUS X ()
98 98 -43.2*0 115.*Pt -36.427 HANG V 99 49 -43.230 115.0F0 -37.427 SNUS INCL x a.ngse e.gegg 1.egge . () Y a.nsee 1.nCon. c.cee0 () i 1. ness e.eers o.nese 101 1J1 -41.20R 115 009 -38.177 SNUS Y
- () 102 te2 -37 104 115.C00 -38.177 HANG Y ()
IS3 163 -37.003 11".A99 -38 177 S Nt'8 INCL 3 1 84P9 0.0009 a.0000 Y e.sace 1.seen e.9sse ' C) r n.seco e.neos 1. cons () 104 144 -36 259 114 25J -38 177 SNUB Y' 166 126 -37."Os in6 6A7 -37.177 $NUS INCL I 1 8898 8.0048 9.09b8 C) Y e.asta 1 83eo 4.nene C) i s . o .' o n e.asse 1. anne 197 107 -37.416 106 667 -3e.177 SNUS Z
- () Its 110 -43.259 1!6.467 -36 250 SNUB Y ()
111V 111 -4 3. 2
- G - 1.6.667 -35.782 CONF Y 117 117 -35.169 127.99A -27.791 SNUS F
() 120 120 -35.169 128.*98 -26 744 HANG Y () 123A 1234 -39 252 128.998 -25.671 SNUS Y 124 124 -39.752 12P.998 -25.671 SNUS F ~ () 126 126 -4. 752 128.998 -26.A71 SNUS X () 127 127 -4J.752 128.99F -27.005 HANG Y 133 133 -46.792 128.994 -31 796 HANG Y () 139 139 -39 231 126.*67 -32.963 SNUB Y () 143 143 -37. R6 126.473 -32.*63 SNur 7 144 149 -?6.795 12A.917 -32.*63 HaN6 Y . () 145 145 -36.44r 126 9h* -32 963 SNUS Y () 151 151 -e s. 752 128.24P -29.146 SNUS X 154 154 -39.71. 195.977 -29 046 $NUP 7 - ()* 155 1%5 .'9.325 124.*6* -29.r46 S Ht'R Y () 159 159 -?6.586 126.91.' -29.a46 SWt'P Y 160 16's -36.253 126.*i5 -28.w46 $NUR 7 () 164 164 -54.231 126.*F' -2*. 46 HAkG V . () 167 167 -32.669 12f.*?1 -2 9 6 3 f. SNUP Y C) () () i; i
i' ]) ICPELL C0kP6ditt03 PAGE 212 ($) i
$UPERPIPE VERSION 16Ao if/91/838 Sv5fr0 1MPELL = NOS 89/03/23e 11.13.16e '
() PGE TRIJAN NUCLEAR 57AT103 () EDS PR08LEQ 8383018-RC-91 RLVel PRES $URIl[R S/RV LINE () AS-8UILT GE0METPV WITH SLUG 01 VERSION DC11CES ($001 () () DETAILS Of SUPPORTS FOR TPIS SUMMARV (CONYD.3 () C) Suer SUee x Y r SUPE o1RN INet nit. COS. vR Gto8At ARES C) NAME LOCN COORD C0ORD C00PD 7YPE CODE ARIS X Y Z (Fil (F79 (Fil Cb () C$ 17e tre -32 669 126.831 -31 57, SNUB INCL .9848 .3736 .Pete c) Y .1736 .9848 .0800 7 .9009 8.4400 1.0000 C) 417a A178 -34.669 12a.n31 -36.e46 SNuS : () 179 179 -36 356 126.831 -37 526 SNGL Y A179 A173 -34.669 127.831 -37.526 SNUS 7 () C508 C5J8 -32.669 125.331 '7 3R0 SNGL Y () C50A C54A -32.669 126.831 -35 880 SNGL 2 SD31 $031 -32 669 123.665 -37.389 SNUS INCL X .9R&7 0.0000 .1628 () Y 0.ason 1.c95e. a.enos () 2 .1628 8.0009 .9867 1814 1818 -43 16* 126.831 -36.526 SNGL X () 192N 182A -43 16, 126.831 =27.442 SNCL M () 182Y 182A -43 169 126.A31 -27 442 SNGL Y 1822 1824 -43.169 126 931 -27.442 SNGL 2 () 182 382 -93 169 126 831 -36.234 $ NGL Y () 188V 188 -39 273 123.831 -26.276 CONF Y 192 192 -37 169 124.5A1 -26.276 $Ntl8 Y () 190 19J -37.919 123 431 -26 276 $NUS X () 194 194 -38 252 119 831 -?6 276 SNUS 7 195V 195 -41 544 119.831 -26 276 CONF Y () 196 196 -42.419 119.831 -26.276 SNGL I () 208X 2 '. R -93.169 195.*4p =26.276 SNGL E 20eV 2w8 -43 169 135.d4L -26.276 SNGL Y () 248Z 2(8 -43c169 1h5.*4* -26.276 SNGL 2 () 215V 215 -47.20e 6G.831 -26 276 CONF Y
$214 2134 -43.648 61 271 '-26 276 ShUS INCL M .8988 .43R4 .0004
() Y .4384 .8928 .0000 () 7 3603 f.CGG? 1.fC08 V6B
- V68V -35 295 I?LeP6" -32.963 HANG V
() V78 VfB -38.252 122.697 -29.ve6 SNUS INCL N .2925 .0809 9759 () Y .$164 .9767 .0792 7 .9791 0.n000 .2r32 () V7C V7C -3R.292 13:.299 -29.046 HANG Y () V88 V6B -38.252 128.619 -52.963 SNUD 7 LS LS -37.940 68."98 -31 00C ANCH GLO8 () USN M3 -37.50? 93.a58 -31 000 SNGL M () USF M3 -37.Sc. 93.a=A -31.fti RNGL 7 USY M3 -37.%Cv 9'.958 -31.8sG ENGL Y () 232 2t2 -43.169 116.123 -25.276 TNGL N () 265 2'5 -43 169 1*7.498 -?6.276 56GL F () ( O _ -_ __ O._. - _ _ O -
~ - - - -- _- - -~ _~
,Q {MPE % -f") ,.,Of ' -
.- E 2i- -
@ N SUPERPIT JR$10N 36Ao 1P/C1/838 SYSTEM IMPELL = NOS 84/93/23a 11,16 36/ \
c ,Q PGE TRiJAN NUCLEAR STATION O , EOS PR08LEN $300018-PC-91 revel PRES $URIZER S/RV LINE O AS-8UILT GEOMETRT WITH SLUG DIVERSION DEVICES (SOD) 9 lQ DETAILS OF SUPPORTS FOR TPIS
SUMMARY
(CONTD.) Q SUPP SUPP X Y F SUPP DIRN INCL DIR. COS. WRT GLO84L ANES O ' NAME LOCN C00pp COORD COORD TYPE CODE ARIS X Y Z r (FT) (Fil (Fil lc o l O 225 225 -48.41R 47 315 -29.52R ANCH GLOS O SDJ4 $0.4 -41.214 112.833 -37.003 SNUB Y SD14 %D14 -43.252 113.326 -29.834 SNUR Y . O $024 SD24 -33.860 113.641 -27.995 SNUB Y Q O . O O O O o O O g . O O O O O O O '
I MPELL CORPORail N
$UPERPIPC VERSION ISAs II/:31/R38 STStru IMPELL = NOS PAGl 214 84/85/23 11 16 16.
() .
- PGE TROJArd NUCLEAR STATIi] O
[0S PROBLEM 93rGT13*PC-31 revel PRESSURIZER $#RV LINE AS-Bull 3 GE0 METRY WITH SLUG DIVERSION DEVICES (SDD) Q S UPPOR T 'LO AD
SUMMARY
, O SUPP SUPP SUPP DIRN RESULT RESULT ARIS LDAD LOAD LOAD '
NAME LOCN ITPE CODE TYPE UNIT TYPE X-ANIS SET. T= AMIS SET Z-Ault SET O, 1 FORC (LB) GLOM -7M.58 EMER
-750.58 EMER
-750.58 FLTD 0?
-75a.54 FLTD
-75".58 NORM .
h -759.58
-75f.58 NORM UPST Q
-7 5 ft. 5 P UPSitM-9 O
DISP (IND GLOB 445 FLTDEM*) 2.855 FLTDfMel .174 FLTD(M*3
.39M EMEa 2 849 EMER .
.305 EMER
@ .33 e UPST 2.P22 .UPST .184 UPST O
.260 THMU 2 812 THMU 6
.251 THM1 2.683 THM1 Ol o .251 NOPM 2.683 NORM
.035 NORM
.035 THM1 '
o .836 THMU Q
.07 0 UPST .011 UPST .148 UPST
.070 EMER .017 EMLR .156 [MER o} .117 FLTD4M-9 .522 FLTDtM-3 .226 FLTDIM-9 O, FORC (LB3 GLOB 9386 9A FLTD(M*)
e334.P0 EMER
- 0) 3228.25 UPST O' *
-3228.25 UPtf
-8334.80 EMER
- 0) -9386.54 FLTDEM-9 Q DISP (IN) GLOB .239 FLTDiMel 2 784 FLTD(M*) .086 FLTDIM*)
() .14 6 [ pea 2 776 EMER .071 EMER O
.123 UPti 2 755 UPST .037 UPST 03% THMU 2.74u THMU Q 12 5 .THM1
.?t 7 NORM 2.609 2.6L8 THM1 Noen CI
.051 NORM Q .851 THMu O
.Pn3 NORM .'J1 NORM .051 THM1
.094 UPST .015 UPST .0RA UPST g) .31- re[R .ssa EMER .176 EMER O o O o O
_. _ _ _ _ -_ ~_.
- .-.m -
Q ILPELL c F 7as303 3 rase 213 A
\
Q ( StPERPIP 1RSIC3 164, 191811031 SYSTfM IMPELL - MOS 84#93#23s !!o16:13/ O PSE TROJA2 NUCLEAR STATIO3 Q) ' () () EDS PhoeLEM R368R1R-PC-81 Revel PRESSORIZER S#RV LINE , i () AS-BUILT Cf 0 METRY WITH SLUG DIVERSION DEVICES (S005 (D
- 6) SUPPORT LO AD
SUMMARY
(CCNTD.) CD SUPP SUPP SUPP DIRN RESULT RESULT ANIS LOAD LOAD LOAD - () NAME LOCN TYPE CODE TYPE UMfi TYPE X- A NI S SET Y-ANIS SET 2-AN13 SET CI () 12 () 6 tCONTD.) .164 FLTDEM-9 .042 FLTDtM-9 .191 FLTDtM-l
- () . (I 16N 16 SNGL *D-FORC EL89 LOCL 22R65 87 FLT0tM*)
! () 226 4 R .7 5 EMEP C)
- 6588.44 UPST 455R.55 THMU
() 4*44.32 THM1 () 4Hp5 15 NORM
-39.18 NORM
' () -FRPR.29 UPST ()
-16611 62 FMER
-16923 73 FLTDEM-1
() (I FORC (LB) GLOS 17784.41 FLTDfM*) 18579.98 FLTDtM+) 17619.40 EMER , 14437.70 EM01 () 5 863 1 F UPST 1274.42 24 62 UPST NORM C) 3 P 46.2 f ' THMU 3145.24 THM1 ! () 3115.77 NORM ()
-2516 5R NOR M
-2541 2 P THE1
() -se.4 s n0RM -2e64.3a THMU CD
=1577.86 DPST -4889 59 UPST
-12922.86 EFEP -14231 95 EMER
() -130R7 87 FLTDfM-l -19364 33 FLTDfMal () OISP IINI LOCL 004 FLTDtp+1 2 79R FLTDtM*) .903 .FLTDtM+3 C) .ee t rMER 2 7sa EMER .se3 rMER ()
.991 UPST 2.756 UPST .001 UPST .
2.725 THMU () 2 5'1 THW1 () 2 589 WORM ete! NORM C) 834 UPsi t) ,
. m.9 3 EPER .*62 FPEe .aP2 EMER
.003 FLTDEM-9 .a77 FLTDtM-9 .OR2 FLTDtM-9 Ci ()
. DISP flhi CLOB .005 FLTDEMel 2.79R FLTDtM*) 994 FLT0tMal
.a95 rwtR 2 7P4 EPEP .004 EMER
() .r42 UP5T 2.756 UPKT () () () () () i
j IMPELL CORPCR ATIO7
- PAGE 216 84/B3/23* 11+16.16e
() p L) SEPERPIPE VERS 103 16A. it/01/838 SYSTE3 iMPtLL
- NOS
]@- PGE TPIJAD buCLEAR STAT 107 () t E35 PPoeLED 3389f10-RC-T1 PEVel PRES $URIZER S/RV LINE (() l AS-8UILT GEOMETRY WITH SLUG DIVEFSION DEVICES 65003 G) l () SUPPOR T LO AD SUMMARV (CONTD.) () SUPP SUPP SUPP DIE 4 RESULT RESUL't ANIS LOAD LOAD LOAD '() NAME LOCN TYPE CODE '7YPE UNIT TYPE N-AMI S SET T= ANIS SET 7-ARIS SET () l l)( 16x (CONTO.) .891 THMU 2.725 THMU t3 () !
.003 EMER 034 UPST
.862 EMER .883 EMER
() l-l () =.004 FLTDiM-) i ..R77 FLTDiM-9 .003 FLT0tM-9 () () 162 16 $ NGL -U- () ! FORC GLD) LOCL 9665 7f FLTDEM*) R826.93 EMER () 2978.44 UPST () s 39.23 NORM
-3596.52 NORM C) -3629.75 THM1 ()
-3985.45 THPU
~6R85 4 7 UPST
() -16851 86 FMEP ()
-17690.63 FLTDtM-9 (6 FORC (LB) GLO8 11115 68 FLTDt4+1 13762 27 FLTDiMel ()
105R8.65 FPEP 13109.76 EMER 4326.4D UPST 5356.49 UPST () 2504 21 THMU 3100.45 THMU ([ ' 2280 71 THMI 2823.73 THM1 l 2256.06 N04M 2793 21 NOP M .
-30.52 NORM
() -24.65
-1871 49 UP97 NORM
-2337.08 UPST
() i
-5546.29 EMER -6866.R3 EMER i
() -6073.32 FLTDtM*) -7519 34 FLTDtM-) () D I .T P EINI LOCL .982 FLTDtMel 2.79A FLiutM*3 .004 FLTDtM*) () .en2 EMER 2.tre r=[a .so. rMER C) 2.756 uPST .est UPS7 2.725 THMU () 2.5eg inM3 () 2.589 N09M
.6?! NORM
- () .*11 UPST .P24 UPST ()
. 3c 3 EMIP . r,6 2 EMER .003 EMER
.913 FLTDEM-1 . 477 FLTDEM-l .003 FLTDtM-t
() () C) () . . O -- -- - - -- O- - - - .- O-
)
- ra.C 21e p' J Q IMPELL C SUPERPI Attt%
R$10% 164, IF/01/838 GTSTEM IMPELL - NOS C4/83/23s 11 16 16s 1 E8EFI8def.;"V5h56tRIlellf2[v.1 V \ () t () PRES $URIZER S/RV LINE n AS-RUIL1 GE0 METRY UITH SLUG DIVERSION DEVICES (SDDI II () SUPPORT LOAD
SUMMARY
(CCNTO.) SUPP SUPP SUPP DIRN RESULT RESULT ANIS LOAD LOAD LOAD NAME LOCN ITPE CODE TYPE UNIT TYPE N-ANIS SET Y* ANIS SET 2-ANIS SET () * (I 16Z DISP flND GLOS .?05 FLTDfM*) 2.148 FLTDtM*) .504 FLTDEM*)
.995 EMER 2 784 EMLR .004 EMER 2.756 UPST (),
() .002
.991 UPST THMU 2.725 THMU
.001 THP1 2 591 THM1
() .001 NORM 2.589 NORM ()
. 681 NORM
.034 UPST
() .503 EMER .462 EMER .RP3 EMER ()
.084 FLTDtM-l . 077 FLTDfM-) .083 FLTDtM-9 a
() 19 19 HANG Y FORC (LR) GLOB -1?43 15 EMER () -1363 15 EMER () ,
-1563.15 FLTD
-1562 15 FLTD
=1363.15 MORM ' ()
() -1163,15 NORM
-1363.25 UPST
-83'3 85 "'S" "-' (>
C) DISP (INI GLOS .143 FLTDtM*) P.749 FLTDfM*) .597 FLTDtM*) () . .99 4 EMER 2 761 EMER .965 EMER ()
.RR 3 UPST 2 734 UPST .054 UPST
.RG2 NORM 2.711 THMU 2.583 THM1 C)
() 2e5R3 NORM
.at t NORM .017 NORM
() .E43 THMP. -.017 THMU ()
.a6m THMU- .017 TUM1
.046 UP!T .622 UPST .071 UPSV
() ..Pe t EMIR .95r EPER .P82 EhER ()
.251 FLTDtM-9 . f 5 8, FLTO(M-9 .114 FLf3tM-3 25 25 SNUD *1.
FORT ELB3 Lf0L 5945.96 FLTDiM** , 458%.1? r"FP L) () 2717.4? UPST ,
-2T37.42 UPET C)
() () i
() IMPELL CORPORATIO3 PA:[ 218 () f SIPERPIPE VERSION 1CA. It/31/8Pt SYSTLQ IEPELL - KIS 84/03/23s 11 10 16s ,. () PGE TROJ43 NUCLTAR STATIO3 () EDS PRP.8LEM 0388018-RC-91 revel PRESSURC2ED %/RV LINE () AS-BUILT GE0M';1P.Y W11H SLUG DIVERSION DCVICES (SODI () () SUPPORT LOAD SUMMART (CCNTD.S () SUPP SUPP SUPP DIPN RESULT RESULT ANIS LOAD LCAO LOAD " () NAME LOCN TYPE CODE TYPE UNIT TYPE N-AXIS SET Y-AMIS SET F-AXIS SET C) () - 25 C) (CONID.3 -4685.17 EMER
-5999.96 FLTDIM*D FORC (LSD GLOB 441R.71 FLTDEM*l 3978.63 FLTDIM*3 3481.76 EMER 3134.99 1aER
. C) 2a34.38- UPST 1831.69 vPST ()
-2034.30 UPST -1831 69 CPST
-3481 76 EMER -3134399 LMER
- () -4418.71 FLTDEMai -3978 63 FLTDiM-9 () DISP (IN) LOCL . 02 3 FLTDtM*) 2 64R FLTDIMel .212 FLTDiM+l - () 018 EMER 2.648 EMER .212 EMER ()
.011 UPST 2 617 THMU .141 THM1 I'.616 UPST 1341 THPJ >
() 2 567 THM1 .139 UPST () 2 566 NORM .138 NORM
.211 NORM
() .211 THMU i)
.211 THM1 .001 NORM .803 EdMM
.221 UPST .052 UPS? .004 LPST
() .298 EMER .034 EMER .042 CNER ()
. .303 FLTDIM-9 . 034 FLTDiM-9 .D42 FLTDIM-9
() DISP IINI GLOB . C4 2 FLTD4M*3 2.642 FLTDiM.6 .039 FLTDEMel . ()
.04 0 EMER 2.648 EMER 83R EMER
. 31 0 UPST 2.617 THMf1 2006 UPST
- () 01? NORM 2 616 UPS7 () 2.567 THM1 2 566 NORM 002 NOMM () .24' NORM .037 THMU ()
.251 THMU .037 TRM1
.038
.251 THP1 .034 NORM NORM UPST .e02 UPST *.046 UPST
() *.25F
.362 EMER .034 TMER .099 EMER C)
.?64 FLtDeM-9 .034 FLTD8M-t .101 FLTDtM-9
' () () 28 2R SNUS +4- ' () FORC (LM t LOCL 195*1 72 FLTDtM*3 () 194*2 95 EMER 327 23 UP97 () -327.23 UPST C) O - O _ ._ __ __ O
h M N N m .. ) sMP[LL tuR"^^1ssv3 SUPERPFPE ' ,5101 16Ao 1-1/01tA38 SYSTEM IMPELL - NOS /cs\ ta== 209 89#93/23s 11e16:16e
%, d f
$ PGE TROJA1 NUCLEAR STATIO2 ()- EDS PPOMLEM 031R118-AC-01 REY.1 PRESSUP.IZER S/RV LINE AS-BUILT GEOMETRY WITH SLUG DIVERSION DEVICES 4500) 4) SUPPORT LOAD
SUMMARY
ECCNTDel II SUPP SUPP SUPP DIRh RESULT RESULT Anis LOAD LO A02 LOAD @ CAME LOCN TYPE CODE TTPE UNIT TfPE I-ARIS SET. r-ANIS SET 2-ANIS SLT C) 3 as () ECONTD.) -18492.85 EPER
-10501 72 FLTDtM-1 .
CD 3 FORC (LBl GLOB 6608.95 FLTDEM*3 8161 37 FLT0tM*) 3 'lllill blif
-6603 37 FMER
'lilill Hill
-8154.48 Et4ER c>
-66 G8.9 5 FLTDEMal -8161 37 F8TDtM-l 3 ()
DISP IINI LOCL ela3 FLTDEMel 2.45* FLTDEM*3 .142 FLTDtMel
.183 EMIR 2.459 EMER .140 EMER
} .E03 UPST 2 44d ,UPST .055 UPST () er83 NOMM Q.44P THMU .044. THMU 2.258 THM1 } 2.258 NORM .0f5 NORM ()
. . 21 9 NORM e.019 ENMU
.22R UPtf . 01 f. TH41
) .22 2 THMU .924 NORM ()
.222 THM1 .940 UP'3T
.235 F.ME R . ? 2 F. EMER .063 EMER
[) .235 FLTGtM-1 .129 FLTDtM-1 .066 FLTD4M-9 () DISP IIN) GLOB .lTS FLTDiM*) 2 45* FLTDiMel .194 FLTDtM*) [s .174 EMER 2.a59 EMER .193 EMER ()
.f32 UPST 2 44G UPST .166 Ur$T
.f22 THMU 2 440 THMU .161 ThM1
[) 2.258 THM1 .161 THMU ()
.002 NORM 2.25F NORM .156 NOPM
.154 THMU Q .154 THM1 ()
.156 NORM .005 NORM
.169 UPST .016 UPST Q .197 EMER .820 EMER .042 EMER ()
.198 FLTDtM-9 .02? FLTDEM-1 .544 FLTDtM-1 29 29 HANG V FORC (LBI GLOB -212.D7 [MER
() -2 ' ; . l. ? EMER ()
-212.r* *LTD
-212.tf FLTD l)
C) C) () () () ,
(() I MPELL CCRPOR A fl01 PAGE 228 () .; S L'PER Pi/E VERSIO1 16A, jf/31/8?l Sv5f[Q IMPELL = NOS 84/05#23 11 15.15. () PGE TROJA4 NUCLEAR STATION () EDS PR08LEM C30091R-RC-01 EEvel PRESSURIFER $/RV LIWE () AP-BUILT GEOMETRY WITH SLUG DIVERSION DEFTCES 68003 () () () SUPPORT LO AD
SUMMARY
(CONTD.3 S UPP SUPP SUPP DIRK RESULT RESULT ARIS LOAD LOAD LOAD
- C) NAME LOCN TvPE CODE Tver UNIT TvPE x-AR13 $[t v-Ax13 . SET 2-Ax S SET c)
() 29 () (CONTD.) -212.07 NORM
-212.R7 NORM
() -212.67 UPST ()
-212.07 UPsitM-1
() DISP (INS GLOB .276 FLTDiM*9 2 444 FLTDiM*9 .20P FLTD8M+3 ()
.27 3 EMER 2 444 EMER .197 EMER
.100 UPST 2 425 UPST .385 UPST
() 948 THMU 2.425 THMU .180 THM1 () 2.239 THM1 .180 THMU
.R03 NORM 2 239 NORM .374 NORM
() .12 6 THPU ()
.126 THM1
.129 NORM .006 NORM
() .14 2 UPST .018 UPST ()
. 153 EMER .018 EMEP .04T EMER
.166 FLTDtM-3 .418 FLTDiM-9 .050 FLTDtM-9
' Oi () 30 30 SNU8 -e-() FORC ILBI LOCL 5373.51 FLTDfM+3 () 5291 53 EMER 746.89 UPST () -746.99 UPST ()
-5291 53 EMER
-5373 51 FLTDIM-1 C) C)
FORC EL83 GLOB 4176 53 FLTDiM.) 3381 05 FLTDtM+) 4112.82 FMER 3329.42 EMER () 5 F O.5 2 UPST $69 94 UPST ()
-S R n.9 2 UPFT -469.94 UPST
~4112.82 FMEP -3329.92 EMIR
' () -4176.5' FLTDiM-9 -33R1 00 FLTDtM-l () DISP IIN) LOCL 02 9 FLTDiM.3 2 351 FLTDEM.) .489 FLTDiM.9 () .02 8 EPER 2 351 EMER 489 EMER ()
.*11 UP%T 2 336 UPST .254 UPST
.0J8 NORM 2 336 THMU .24R THMU
. [) 9.227 THM3 .303 NORM () 2.226 NORM
.953 NORM .D72 NORM
. () .061 THMI .075 UPST () c) ()
- e .
e . e _
= =--. e one e m. - , - - . ;() I MPELL CP"~? A T ICO .
PAGE 221 34/93#23e 11e16 16<f-() l S UPE R P1P tR$1041CAo 1P/d1/038 SYSTED' IMPELL - Net
- () @CE T ROJA3 NUCLEAR STATIO3 EDS FpetLEM 1309819-AC-91 REV.1
() PR EGS UR I2ER S/RV LINE () AS-8UILT GEDMETRY UITH SLUG DIVERSION DEVICES 4500) . (b
- () SUPPORT LO4D
SUMMARY
(CCNTO.) CD SUPP SUPP SUPP DIRN RESULT RESULT Aufs LOAD LOAD LOAD
, () NAME LOCN TYPE CODE TYPE UNIT TYPE E-ARIS SET Y-ANIS SET 2-ARIS SET ' C)
() 36 , () (CONTD.) .171 UPST , .076 THRU
.177 THMU .976 THm!
l c) .3o5 EntR .s15 EME, .12e EMER - () FLTDEM-l
.3R9 FLTDtM-9 .015 .128 FLTDEM-9 l ()
DISP (IN) GLO8 .54 4 FLTDEM*) 2.351 FLTDEM*) .139 FLTDtM*l ()
. 54 4 EMER 2 351 EMER .339 EMER
.29 3 THPU 2.336 UPST .997 THM1
! () .292 UPST 2.336 THMU .997 THMU () '
; 2.227 THM1 .093 UPST ! 2 226 NORM .089 NORM
! () .se4 NORM - . sos NORM ()
. 99 5 NORM .PR2 THMU
.000 UPFT .093 U?ST l f() . .059 .TMER .als EPEP .213 EMER () '
. 95 9 FLTDtM-9 .015 FLTDtM-1 .213 FLTDER-3
- c> <> -l 31 31 FIUB Y FORC ELB) GLOS 9959.It FLTDtMel
. () 9999.51 EPER () l!
131.55 OPST
-131.55 UPST i () -9949 51 EMER ()
-995E.10 FLTDtM-9
- () DISP IIN) SLOS .597 FLT0tM*3 2 331 FLTDEM*) .187 FLTD44*l ()
3
.59 7 EMER 2 331 EMER .107 EMER
.34 5 THMU 2 317 UPST .470 THPi
() .344 UPST 2.317 THMU 579 T MMU ()
. 83 7 THM1 2 224 THM1 .966 UPST
.n32 N0eM 2.224 NORM .062 NOWN
< () =.000 NORN () 1 .805 NORM .115 THMtl
.000 UP97 .128 UPS1:
l () .. e41 EMER .915 EMER .246 EMEp '- ()
.04 1 FLTDEM-l .?15 FLTDEM-9 .246 F L T'S 9-3
() () () () l C) l) t I () () ,
() IMPELL Come:RATIDM PAGE 222 ([) q StvtRPlPE 7E R $ 1C'J 164, It/31/R38 SYSTEM IMPELL - NOS 84/83/23 11 16.16e
- 1) PGE TRIJA: NUCLEAR STATIO7 ()
XDS PROBLE31307J18-RC-41 Revel PRES $URI2FR S/RV LINE () AS-8UILT GE0 METRY UITH SLUG DIVERSION DEVICES (SDD) () () SUPPORT LO AD SUMMART (CONTD.) () SUPP SUPP SUPP DIAN RECHLT RESULT ANIS LOAD LOAD LOAD
.(! NAME LOCN TYPE CODE TYPE UNIT TVPE R- A XI S SET T-ARIS SET 2-ARIS SET ()
() 32 32 SNUB +4- ()
- FORC (L88 LOCL 13654 18 FLTD(Mel 13649.62 EMER
() 489 96 UPST ()
-499.96 UPST
-13649.62 EMER
() -13654 18 FLTDtM-) . f) FORC EL8) GLOS 8592 91 FLTDtM*) 18611 23 FLTDiMon () 85 R9.9 4 FMER 18687.75 EMER () 3*7.77 UPST 388.07 UPST
-3 C7.7 7 UPST -388.07 UPST
() -8589.9R EMER -18607 75 EMER ()
-8592 81 FLTDtM-) ~19611 23 FLTDtK-1
() DISP flN3 LOCL .64 0 FLTDtM*) 2.193 FLTDtMel .376 FLTDtM+3 ()
.64 0 EMER 2 193 EMER .372 EMER
.39 9 UPST 2.177 UPST .219 UPST
() .343 THMU 2 376 THMU .212 THMU ()
.05 8 NORM 2 111 THM1 .077 THM1 *
.05 5 THM1 2 111 NORM .068 NORM C) .0e4 NORM ()
902 UPST '
.989 NORM
() .003 UPST .025 UPST () .'
.15* [PER .919 EMER .054 EMER
. 15 9 FLTDEM-9 .t19 FLTDtM-3 .85R FLTDEM-) i DISP (INI GLOB .69 3 FLTDEM.) 2.193 FLTDfM*) .975 FLTDtM*)
.691 FMEP 2.193 EMER .074 EMER
() .415 UPST 2 177 UPST .009 UPST ()
.496 THMU 2.176 YHMU err 6 THM1 ;
. age THut 2.111 THM1 .096 THMU
() .09 ? NOPM 2 111 NORM () ,[
.*43 NORM ,
=.009 NORM e
() .-10 4 Noen
-. 91 R UPST .003 UPST
. 165 THMU
.185 UPST
() l
.pFP EMIR .919 [MER .319 EMER
() ~. 981 FLTDfM-9 .919 FLTDEM-9 .320 FLTDiM-l () I () () C) 19 . O O O _. _ _._ .=_ _ _ _ - . _ _ -_
'Q s EPE ti. ir N .EQ .
I 22 34/03/23, 11 13.14t
) q 5%PERP1P' TRSION 164, if /01/838 SYSTED IEPELL - COS g i
-lQ O PGE TROJA3 NUCLEAR STAflic
\
O)
' O .
EDS PROBLEM #396518-RC-el pr,v.1 PRES $UR12ER S/RV LINR jQ AS-BUILT GE0METRT WITH SLUC DIVERMION DEYICES (SDDR O
.Q SUPPORT Loa 0 SUMM ARY (CONTD.8 O SUPP SUPP SUPP DIAN REsulf RESULT Anis LOAD LOAD LOAD
.Q NAME LOCN TVFE CODE TYPE UNIT TYPE N-ARIS SET 1-ARIS SET 2-ARIS SET O
'Q 35AV 354 CONF Y O FORC GL86 GLES -119.57 EMER
-179.57 EMER
,@ -179.57 FLTD O
-179.57 FLTD
-179.57 NORM l@ -179.57 NORM O
~179.57 UPST
=179.57 UPSTfM-)
DISP (IN) GLOS .333 FLTDEM+1 .643 FLTDtM*) .319 FLTDEU3
.333 EMER .640 ERIR .319 EMCR
'O .200 UPST .5R5 .UPST .910 UPSr O
.198 1HMU .563 THMU .010 THMU 82 3 NORM .464 THRi t
Q .C23 THP1 .464 NORM 4002 THMU O
.902 THM1
.004 NORM
'Q .006 NORM O
.202 UPST .923 UPST .011 UPST
. 02 9 EMER .243 EMER .195 EMER Q .02 9 FLTDtM-1 .34R FLTDtM-9 .195 FLTDtM-9 0 Q 41 41 HANG V O FORC (LDS GLOS -719.97 EMER
-719 97 EMER Q -711.97 FLTD O
-716.97 FLTD h -718.97 KOPM
'Q -71f. 97 NORM O f -71'. 47 UPST
-716.97 UPsitM-9 O O DISP (IN) 6 LOB .169 FLTDEM*l 2.R45 FLYDEM*) .1R1 FLTDfM*)
.326 EM[4 2.94L EPER .19'? EMER Q .133 UPST 2.815 UPST .300 UPST O I . .43P THMU 2.PJ4 THMU l 097 THM1 2.67f THMS Q* .43 7 NORM 2.676 NOPM O
.252 NOP M
.252 THM1 iQ .261 THMU O O O n oh
() IMPELL CORPORATIOQ PAGE 224 ()) pj
$UPERPIPE VERSIO4 tcA, it/%1/831 SYSTEQ IMPELL = NOS 84#83/23i 11 16 16e
{} PGE TP0J20 NUCLEAR STAT!02 () r, EDS PR08LE: 8300012*RC-91 Revel PR ES S UR IFER $/RV LINE AS-8UILT GE0 METRY WITH SLUG DIVf RSION DEVICES (SDDS d) () C) SUPPOR T LOAD SUMMART (CCNTD.) () SUPP SUPP SUPP DIR N RESULT SESULT ANIS LOAD LOAD LOAD X-ARIS Y-ANIS SET F-ANIS SET C) () NAME LOCN TYPE CODE . TYPE UNIT TYPE SEE () 41 () (CONTD.) . 96 5 UPST .C10 UPST .369 UPST I
. D65 EMER .019 [MER .458 EMER
() .198 FLTDiM-1 .023 FLTDtM-9 .522 FLTDEM-1 () f () 98 4R SNUB Y () FORC EL83 GLOB 8677.21 FLTDIM+) . 7399.58 EMER () 33R8 79 UPST f)
-3388.79 UPST
-7399.58 EMER C) -8677.21 .rLTDiM-9 ()
DISP (INI GLOS .137 FLTDEM*) 2 753 FLTDIM*) .118 FLTDiMel () .136 EMER 2 751 EMER .972 EMER ()
.038 UPST 2 740 UPST 471 UPST
.053 THMU 2.732 THMU .001 NORM
() . 03 3 THM1 2.681 THM1 ()
. 03 2 NORM 2.601 NORM .
.esR No$ M
() .089 THM1 ()
.021 TkMU
.00E. UPST .015 UPST .099 UPST
() e *4 5 EMER .P23 EMER .194 E MER ()
. R4 6 FLTDEM-9 .625 FLTDIM-1 .158 FLTDEM-9
() () 52N 52 $ NGL 3 FORC (LB) GLOB 19614.71 FLTDtM*l * () 19492.63 EMEP () 1734.00 Up?T 98.87 THMU () 51.91 topM () 38.39 THM1 1?.52 NORM () -1616 1e UPST ()
-2176".R4 EMEP
-21187.92 FLTDEM-9 DISP (INI GLOD .e44 FLTDtM.) 2.74" FLTDfM.) 401 FLTDtM*)
.504 EMIR 2 743 EMER
() 2.73's UPST () () () O. O O
~~ - - -- - --
( Q IMPELL Cf1 ATION PAGE 225 s @- SUPERPIP j R$104 1EAe it/C1/838 SYSTEM IMPELL
- COS 84/03/23e 11 16 1 3.x +
Q PSE TCTJA3 NUCLEA3 STA'TTIC O EDS PRO 8LEM C3sente-RC-et REv.1 PRESSURIZER S/RV LINE Q AS-RUILT GEOMET*V WITH SLUG DIVERSION DEVICES 65005 $ Q -SC7 PORT LOAD
SUMMARY
(CONTD.9 O SUPP SUPP SUPP DIAR RESULT REsteLT ANIS LOAD LOAD LOAD Q NAME LOCN TYPE CODE TYPE UNIT TYPE X=ARIS SET- Y-ANIS
- SET 2-AMIS SET O Q San O (CONTO.) 2 724 THMU 2.593 THM1 0 2.593 NORM O
.001 NORM
.001 THM1 O ..sel Tr.MU O
. ART UPST .002 UPST
.984 EMER .02n [MER .gp3 EMER O .ce4 rtTDtM-9 .n22 rtTDtM-1 .es3 rtTDEM-9 O FORC (L85 GLOR 6377 61 FLTDtM*)
4299 15 EMER Q 3549.96 UPST O 41 22 NORM
-4946.32 NORM O -* " 7 5
- inM1 O
-5433.R4 THMU
-8999 57 UPST Q -13105.43 EMER O
-15183.89 FLTDtMal Q DISP (IN) GLO8 .344 FLTDtM*) 2.f45 FLTDEMel .001 FLTDtMo O
- .004 EMER 2.f43 EMER 2.73b UPST Q 2.724 THMU O 2 593 THM1 2.593 NORM O .*tt NORM O
.get THM1
. 001 THMU O .eaf UPST .ne2 UPST O
.004 EMER .929 [MER .003 EMER
.984 FLTDiM-1 .?P2 FLTDEM-9 .003 FLTDtM-9 O O 55 55 HANG V lQ FORC tLD) GLOO -1335.37 EME# O
-1335.37 EMER
-193*.?T FLTD O -1555 57 8 0 0 0 O O
Q IMPELL CORPCRAT103 CAGE 223 84/03/23, 11 16 16
@q SUPERP1PE VERSION 164o 11/01/838 SYSTEO IRPELL = NOS
'O PGE TRIJA2 NUCLEAD STATIOc 0
- El$ P RORLE3 43S 3 018-RC-01 REV.1 UbNYbMONNVNYkN SLUG DIVERSION DCVICES 43005 g S!PPORT LOAD
SUMMARY
(CONTD.)
- SUPP SUPP SUPP DIRh RESULT RE4 ULT ANIS LOAD LOAD LOAD NAME LOCN TYPE CODE TYPE UNIT TYPE X-ANIS SET T-AMIS SET Z-AX15 SET O - O 55
~~(l (CONTD.3 -1535 37 NORM O
-1335.37 NORM
-1335.37 UPST
'O -1535.37 UPSTEM-3 O DISP (IN) GLOS .039 FLTDIM*B 2.743 FLTDfM+3 .20e FLTDfM*3 Q .03 9 EMER 2.742 EMER .159 EMER O
.n13 UPST 2 709 UPST .125 UPST .
l 2 705 THMU .859 THMU 0 O 2 575 THM1 .R49 THM1 Q
- 2 575 NORM .947 NORM
.92 4 NORM !
Q . 02 4 THM1 Ql
. 34 5 THMU *.001 NORM 8
.04 8 UPST .333 UPST .069 UPST O .116 EMER .037
.038 EM[R FLTDfM-9
- .069 EMER
.114 FLTDEM-9 O;
.11 6 FLTDtM-9 O Oj 60 6 fs SNUB ==. g FORC (L89 LOCL 2105 17 FLTDtM*3 t
-Q 1355.42 EMER O.
- 1234.89 UPST
=1234.89 UPST l
.Q -1
- u5.4 2 EMER O2
-21 ^5.17 FLTDtM-1 Q FORC (LBt GLOS 125.01 FLTDEM*) 27. ti s FLTDtM*9 2191 4R FLTDIM*) Q 76.28 [PER 16.75 EMER 1303.08 EMER 79.16 UPST 15.84 Urti 3232.68 UPST
'Q -72.16 UPST -15 84 UPST -1232.68 UPST Q
-76.2 8 EMER -16 75 [MER -1303.08 EMER
~
-123 31 FLTDfM-1 -27.00 FLTDEM-9 -2101 40 FLTDEM-3 DISP tlN) LOCL .31$ FLTDIM+3 2.636 FLTDfM*) .245 FLTDIM+)
.309 ["EP 2 636 EMER .244 [MER
'O .23 P Up*T 2.5r5 THMu .157 THMU O'
.209 THM1 2.682 UPST .155 UPST
.209 THPU 2 543 THM1 .129 THM1 Q .2P7 NOPM 2.54C NORM .125 NORM Q
.ral NOPM .PR3 NORM .004 N OR M
. 01 2 UPST .043 UPST .0M UPST
.O O O o . O - .- -. O-- - -. -- e
QTI1Q T r00C 22s ~s' M g Q IMPELL C SUPERPIP 95104 164, SP/ft/R38 SYSTEM IMPELL - NOS } 34/83/23e v 11e 13 16.V) O, O PGE TR2JA3 NUCLEAR STATIOJ EDS PROBLEM 639801a-RC-01 REV.1 PRESSURIZER S/RV LINE O Q AS-BUILT GEOMETRY WITH SLUG DIVERSION DEVICES (SDDS tc0NTD.3- O O SUPPORT LO AD SUMMART LOAD LOAD LOAD SUPP SUPP SUPP DIR N RESULT RESULT ARIS O. UNIT R-ARIS SET Y-ARIS SET 2-ANIS SET O NAME LOCN TYPE CODE TYPE TYPE O O 6e
.812 EMER .33T EMER *
*.956 EMER (CONTD.)
.01 9 FLTDtM-t . CST FLTDtM-9 .950 FLTDEM-9 DISP (IND GLOR .05 0 FLTDtM*) 2.633 FLTDtM*3 .336 FLTDtM*3
.859 EP[R 2 633 EMER .329 EMER
.006 UPST 2 602 THMU .243 UPST O Q .C64 NORM 2.608 UPST .234 THM1 2 54D THM1 .234 THMU 2.53T NORM .232 NORM 9 Q .139 NORM ,
.143 THM1
,Q .168 UPST .003 . NORM .001 NORM O
.1TO THMU .003 UPST .912 UPST
.26 4 EMER .03T EMfR .014 EMER
.264 FLTDiM-) .03T FLTLEM-3 .020 FLTDtM- O
'O -Q 63 63 HANG Y .O FOPC (LB) GLOS -2T9.99 [MER
-279.99 EMER Q -2T9.99 FLTD O
=2T9.99 FLTD
-2T9.99 NORM
-2T9 99 NORM O
-Q -2T9.99 UPST
-219.99 L*P ST (M = )
'O O DISP (IN) GLOR .tSe FLTDtM*) 2.330 FLTDise) .431 FLTDiM*)
.05 8 EMER 2 33n [MEp .266 EMER
.097 UPST 2 399 UPST .256 UPST O Q 885 NORM 2 3GR THMU .003 NORM 2 1R0 THM1 O 2 18d NORM O
.2RT NO#M .801 NORM
.20P UPST .344 THM1
.21 2 TH"U .884 THMU O Q .212 THM1 .334 UPST
.241 IMER .*P2 E P. E p .42R EMER Q .24 1 FLTDfM-9 .122 FLTDtM-3 .593 FLTDtM-3 Q O
O O O O O t
() IMPELL CORPORATION SUPERPIPE VERSION 16Ao 1E/01/838 SYSTEQ IIPELL - NOS PAGE 228 30/03/23 11 35 13. ($) ll: () PG[ TROJA3 NUCLFAR STATIOJ (D EDS PEOPLE 3 M3*Rn1R=RC-91 R[ vel PRES $tR12ER S/RV LINE () AS-MUILT GECMETRY UITH SLUG DIVERSION DEVICES 6500) G) () SUPPORT LO AD
SUMMARY
(CONTD.I () SUPP SUPP SUPP DIRN RESULT RFRULT ANIS LOAD LOAD LOAD () NAME LOCN TTPE Cone TYPE UNIT TVPE X-A NI S SET T-ANIS SET 2-ANIS SET () () 64 04 SNUS **G () FORC (L8) LOCL 8009 33 FLTDEM*3 7994.57 FMER () 365.52 UPST ()
-365.52 UPST
-7994.67 [MER
, () -800s.33 FLTDEM-9 () FORC (LB3 GLOS Gna*.33 FLTDfMel () 79*4.67 FMEP () 365.52 UPST C) :5kIki$$ Nb!btM-> () DISP (INI LOCL 36 4 FLTDEM*9 2 326 FLTDfM*3 .440 FLTDfM*3 ()' .06 4 EMER 2.326 EMER .271 EMER () 647 UPST 2 30% UPST .261 UPST
.P05 MORM 2.304 THMU .S03 NORM
() 2.175 THM1 () 2.175 NORM
.296 40n N .086 NORM
() .20R UPST .008 THM1 ()
= . 212 THMU .889 THMU
.212 THMl *.344 UPST
() .24 1 EMER .022 EMER .441 EMER ()
.24 1 FLTDtM-5 .022 FLTDtM-3 *.610 FLTDfM-3 (f DISP (INI GLOP .064 FLTDtM*) 2.326 FLTDEM*) .440 FLTDfM+3 ()
664 EMfR 2.326 EMER .271 EMER
.007 UPST 2 305 UPST .261 UPST (j .005 NORM 2.344 THMU .003 NORM ()
2.175 THM1 2 175 NORM () .246 NORM .006 NORM ()
.298 UPST .008 THM1
.21 2 THMU .089 THMU
() .21 2 THP1 e344 UPST ()
.24 1 EMEn .022 EMER .441 EMER
.241 FLTDEM-1 .??2 FLTDtM-1 .619 FLTDtM-)
() () C) C) O O O O _ _ O _
a-u-mune - ** * *** M m m e- au-p--e - - *- - - * * * = '* -s - Q IMPELL C I II'3 ry rLd 22v #q y te SUPLRPIP SILN 16Ao If/01/038 SYSTEP IPPELL N0'3
- i i O 04/03/23.11.16stSeY)I Q PGE 1poJA4 NUCLEAR STATIO3 -
O EDS PROFLEM i309Cle-RC-01 REv.1 PRES $URIZER S/RV LINE O AS-euiLT GE0 meter vlTH StuG DIVERSION DEVICES ew De o O SUProRT LOAD SuMPARv CCNTD. O SUPP SUPP SUPP DIRN RE SUL T RESULT ANIS LOAD LOAD LOAD 0 NAME LOCN TYPE CODE TYPE UNIT TYPE N-AMIS SET v-ANIS SET 2 - A N I',. SET O O 65 65 Snus v o F0PC (LB) GLOB 3011 50 FLTDfM*) 3315.73 EMER O #3.P1 UPST @
=*3.01 UPST
-3019.73 EMER Q -3011 50 FLTO(M-1 O DISP (IN) GLOS ell 2 FLTDEM*) 2.290 FLTDtM*3 .519 FLTD(Men Q .11 2 FMER 2.29P EMER .319 tMEn O
.006 UPST 2.263 UPST .388 UPST
.005 NORM 2 268 THMU .004 NORM Q 2.146 THPl O 2.146 N0kN
.21 6 NORM .949 NORM Q .21 R UPRT .953 THM1 0
.22 1 THMU .158 THM9
.221 THM1 .8Pt UPST .458 UPST O .25 3 rMER .e25 [MER .575 EMER O
.253 FLTD(M-9 .023 FLTDEM-9 .773 FLTDtM-9
.O O 67 67 KNUB *Cf FORC (LB) LOCL 80P6 39 FLTDfM*)
'O 8379.04 EM[R O 297.04 UP?T
-297.04 UPST Q -R079.a4 EMER O
-8386.3e FLTDEM-9
'O FORC ILB) GLOM 8085 39 FLTD(M* O 80T9.n4 EMER 297.04 UPST Q -297.34 U*ST Q
-8DT9.C4 FMER l -8386 3a FLTDiM-9 lO O l
DISP (IM) LOCL .397 FLTDtP*) 2 054 FLTD4M*) .587 FLTDfM*)
.397 EFER 2.P54 EMFR .364 EMER
,Q .2t9 UPFT 2 034 UPST .348 UPST O
.253 THPU 2.934 THP1 .006 NORM
.r34 NORM 2.a94 THPU Q .t 29 THP1 2.033 NORM O O O O O ,
l _ _. ._ __ ___ . _ _ _ - - - - _ _
,. e .
O o o o o o o o o o o o o o o o o o o o o C O d m e d m e a m a a m a m (
- O e O E E E E E 4 w w w w w WM Q> Em3>EQ QEME Em3>sQ OKm mEspsQ MN 4W EEEMWW MWME EEEMWM >WW EEEMWM N% OM OE2&EJ JE&O OZZ&EJ JE& ZOZhEJ M J R>>3Wh hW33 Ep>3Wh kW3 >Ep3Wh We Mo M eePeMW heed Gememd >de MMeeee he m NMfSMP edem NMeeke te N e NNommm M NNek@m OMMM NNe>PM 999 WeNNee a ee # 9 e e eeeo e e e e e e e o e o e e e o e 0 0 0 0 0 0m 8 0 0 0 cm 3 0 0 0 0 0 N 0 0 a a a a e a a 9 6 6 0 9 4 5 E E E E E E E w w w w w w w QM >EQ QEkm3E MKQ OEkkaQ QEk3Em pac 4W MWW >WMEEE MWW WWMMWW WWFEaK Ga w k ,
OM &EJ JE&ZZO EEJ JE4AEJ J E & g O =" &EJ J DWh hW3>>2 DWh kW33Wh kW3>Z> DWh M NNN eteeen NNN eeWEee ==emud Mht m ONN OOMMMM ENN M G N N o re FPEGee Wmm M OGL O&OOOO OSO e e e e e e 0000@c ECO 4 e e e e e e e e e e o e mFMMe@ e e e e e e e e 0 0 0 0 0 NNNNNW 0 0 0 donned a 6 0
> ddNNe@
0 0 t m
- a. m. )
O a. a. m. Q E E E E E e *
, = = = = w
- Q> E> EQ QEk3EmE> EQ Os>Em3E >EQ SW ar WP >WMEEEEM W> > W e & E S. 4 MWW M OM Q& Ed JEbEOZO& EJ J&&OZZO GEJ W J 23 WE kW3>2>E3 Wh kW32pm2 DWh W
=
> M. fM NN WMEMe@@M NN chMNFtM eEd W m W9 NN SPOMMNGO NN DOM =CSO mec Q M SG DO MMNNSMOS WO L O t: GCJe eJS 4 e e e e ee o e e e e e e e e e e e e o e e e 4 2 e I t l e 0 0 e O N
= .
M M E O W 2 M > e m 0 > Q m W MW e e J E G =& O O O J R 3 M> J J J W Om J (> @ @ Q
& "S M E k 6 m (U Z >
a WEWh Jp a
- a G MO Rm DM M e Z W =
Em3 MF = J w w
> EmJ W3 w M 4G > E > WODE *M Jeg>
WM%W > m DEME JW & u & M 2 O DE M E wa s e SEW m M> m O m
% DWWu o W> c h Q m 4JN O E & 3am> > l % CO J E n e Em a u EW m whM3 u EQ >
Me = mo
# WMW G QU 4 GOEM d hW44 l M > &W m E && D ME 4 3> 2 OO E Mp M mm E >M 3 GE M 42 O WW Au h OD Q 30 & 4 MJ E O a OW J e W& &W kQ O M > &E dp >
Jf\ E 34 2 JE O M3 O WW & u
&& & w E3 3 mM M ,
l W n o o o o a re n a a n a a @ a a oa o _o c i
=== m sm. --me. - - -.
f} () IMPELL L SUPER 7IP assC2
- QSION 16A, if/P1/83I SYSTEQ IMPELL - COS p ~g r..g 25.
04/03/23e 11 13 16:p s j
.) PGE TROJA3 CUCLEAR STATION ()
EDS PROBLEM 1300010-4C-01 Revel r PRESSURIZER S/RV LINE () AS-8UILT GEOMETRY WITH SLUG DIVEPSION DEVICES 15D03 () () SUPPORT LO AD
SUMMARY
(CCNTD.l () SUPP SUPP SUPP DIRh RESULT RESULT ANIS LOAD LOAD LOAD () NAME LOCN TYPE C00[ TYPE UNIT TYPE N-ANIS SET T= ANIS SET Z-ANIS SET () FORC (LBt GLO8 -201 76 EMER
-2C1.76 EMEP
' () =203 76 FL1D ()
-201.76 FLTD
-201.76 NORM l C) -2P1 76 NORM ()
=201.76 UPST
-201.76 UPSTEM-9
- C) C)
DISP (INI GLOR .96 0 FLTDtM*) .646 FLTDtM*) .028 FLTDEM*)
.052 EMER .646 EMER .027 EMER
() .032 UPST .63* .UPST .005 UPST ()
.011 NORM .635 THMU
.009 THMU .603 THM1
() 00R THM1 .603 DORM ' ()
. .003 NORM .025 THM1
.025 NORM
() . 267 THMU ()
.01 7 UpST .004 UPST .272 UPST
.e4 4 EMER .elt EMEp .441 EMER
() .05 2 FLTDtM-l .011 FLTDIM-9 .441 FLTDfM-l () () 77 77 HANG V () FORC (L83 GLOS -733.65 EMER
~733.65 EME#
() -733.65 FLTD ()
-733.65 FLTD
-733.65 NORM
() ~733.65 NORM ()
-733 65 UPST
-733.65 UPSitM-9
() .11R FLTDtMel 2.798 FLTDtM*) .273 FLTDtM*3 C) DISP (IN) GLO8 971 EMER 2.792 EMER .304 EMER () . ts 7 n UPST 2.779 UPST .303 UPST () 2 758 THMU 2.633 THMI () 2.633 NORM ()
=.174 N0a p . 109 NORM
.174 THP1 .109 THM1
() elR1 THPU .113 THMU () () L) () () i
i([j '() IMPELL CORPDA Af t"Q SUPERPIPE VERSION 16Ao 17/81/833 SYSTE3 IMPELL - Nos # PAGE 232 44/03/23. 11 16s16e
~
l () PGE TCSJA3 NUCLEAR STATION {} EDS PaogLEM n3ege13.pC=61 REV.1 PRESSLRIZER S/RV LINE AS-8UILT GEOMETRT WITH SLUG D1 VERSION DEVICES 45003 Q) () () SUPPORT LO AD
SUMMARY
(CONTD.3 () SUPP SUPP SUPP DIRN PESULT RESULT ANIS LOAD LOAD LOAD Y-ARIS 2-AXIS C) () NAME LOCN TTPE CODE TVFE UNIT TYPE N-A RI S SET SET SET () 77 () SCONTO.) .252 UPST .012 UPST .216 UPST
.311 EMER .mle EMER .264 EMER
() .35R FLTDtM-9 .524 FLTDtM-3 .333 FLTDtM-3 () () 83 83 SNUB V () FORC (L83 GLOB 1003R.91 FLTDtM*3 7613.23 EMER () 4892.74 UPST f) I
-4892 74 UPST I
-7613.23 EMER
() -18838.91 .FLTDEM-3 () DISP EIN) GLO8 .250 FLTDSM*) 2.724 FLTDeM*) .973 FLTDEM*3 () .163 EMER 2.718 EMER .359 EMER ()
.334 UPST 2 712 UPST .033 UPST
.502 NORM 2 791 THMU .991 NORM
() 2.578 THM1 () 2.577 NORM e r13 NOR" .893 NORM () . P19 THMu *.995 THM1 ()
.015 THM1 . 889 THMU
.14 5 UPST .013 UPST =.039 UPST
() .149 EMER .028 EMER .117 EMER ()
- .236 FLTOSM-9 .026 FLTDfM-9 .131 FLTDtM-9
() () 87N 87 SNGL M FORC EL83 CLO8 1n765.34 FLT0fM*3 () 7774.99 EMER () 5683.33 UPST 51 02 NORM () -3980.75 tJO R M ()
-4 D31 7 7 THM1
-4?41.43 THMU
() -8742.72 UPST ()
-16147.87 EMER
-1913R.72 FLTDfM-1 DISP IIN) GLOP .PDF FLTDtM+) 2.762 FLTDtM+1 .CO3 FLTDfMet
.*01 FMFP 2.747 EMER 003 EMER
() .021 UPST 2.733 UPST () () ()
" - a=== mamm. - -
0 IMett' '7 SUPER?,I? m a'ioa TRSION 16Ao 1C#t1/a33 SYSTEQ IMPELL - NOS n -E tu 54/93123s 11 16 16/ \ a 4*
\
N' ') () PGC TR2J20 NUCLEAR STATION () EDS PRORLEM 039001R-RC-Ol REV.1 PRESSURIZER S/RV LINE () AS-BUILT GEOMETRY UITH SLUG DIVERSION DEVIEES 45003 () () S UPPORT LO AD SUMFARY (C ON TO. 9 () SUPP SUPP SUPP dip h RESULT RESULT ANIS LOAD LOAD LOAD '(I) NAME LOCN TYPE CODE TYPE UNIT TYPE M-ARIS SET Y-AMIS SET 2-ANIS SET I) l () 875 (CONTD.9 2.784 THMU ()f. 2 584 THM1 ()j i j () 2 582 NORM l *.001 NOPM ! .692 UPST .639 UPST j () .093 [MER .045 EMER .003 EMER () !
.083 FLTDtM-9 .068 FLTOEM-9 .003 FLTDEM-9
() C) 872 87 SNGL F , FORC (LB) GLOS 17795 87 FLTDEMel () 17560 50 EMER () ' 2163 22 UPST NORM
-16 5.15,
() 5.6
-1635.44 NORM THM1 C)
-1783 17 THMU j () ~3054.98 UPST C)
-19252 17 EMER
-19487 55 FLTDEM-9
() () DISP (INI GLOS .502 FLTDEM*) 2.762 FLTOEM*) .903 FLTOEMel
.081 EMER 2.747 EMEP .903 EMER
() .001 UPST 2.733 UPST () 2 704 TMMU F.5R4 THM1 ' () 2.5R2 NORM ()
.661 NORM
.902 UPST .930 UPST
() ..es3 [PER .o45 EME= .es3 EMER ()
=.P93 FLTDtM-9 .464 FLTDfM-9 .003 FLTDiM-9
() () 90 9f HANG Y FnRC (LOS GLOR -1378 21 EMER () -1378.21 EMER ()
-1378.21 FLTD
-3378 21 FLTD
() () -137P.21 NOPM
-1378.21 NOPM i
-1978 21 UPST '
i() -137P.21 UP9ftM-9 L) '() - C) l C) () 6
Q IMPELL CCRPORATII3 PAGE 234 SUPERPIPE VERSION 11Ao 1F/01/838 SYST[Q IMPELLe= NOS 84/93/233 11 16.16e Q PGE TRIJA3 NUCLEAD STATION EDS PROBLEM C3GB018-CC-01 CEUet
$NhhNl$DEbfMH SLUG DIVERSION DEVICES (SDD)
SUPPORT LO AD
SUMMARY
(CONTD.3 O SUPP SUPP SUPP DIRK RESULT RESULT AR13 LOAD LOAD LOAD NAME LOCN TYPE CODE TYPE UNIT TYPE R-ARIS $[T Y-ARIS SET Z-ARIS SET O - 93 Q (CONTD.8
.3R9 FLTDtM+) FLTDEM*8 DISP (INI GLOS 2 770 FLTDEM*) .075
.21 7 [MER 2.763 EMER .073 EMER Q .191 UPST 2 741 UPST .022 UPST
. 05 4 THMU 2 723 THMU .912 THMU
.05 3 THM1 2 605 THM1 Q .051 NORM 2.605 NORM
.P11 THMU
.211 THM1 Q .002 NORM .311 NORM
.14 R UPST .919 UPST .821 UPST
.143 EMER .P41 EMER ' .949 EMER Q .234 FLTDiM-9 .848 .FLTDIM-9 .051 FLTDiM-9 Is 95 95 SNUS u (LB)
FORC GLOS 7927 73 FLTDEM*) 5156.24 EMER Q 45G2.33 UPST
-4532.33 UPST
-5156 24 EMER O -1927.73 FLTDtM-9 DISP EINI GLOS .334 FLTDiM*) 2.738 FLTDEM*3 .300 FLTDEM*)
Q .32 8 EMER 2.738 EMER .307 EMER
.173 UPtT 2.707 THMU .197 ThMU
.164 THMU = 2 7R5 UPST .196 UPST Q .144 THM1 2 652 THM1 .156 THM1
.143 NORM 2 650 NORM .152 NORM
.091 NORM .092 NORM .004 NORM Q .41 1 UPST .003 UPST .007 UPST
.F12 EMER .036 EMER .043 EMER
. 01 P FLTDEM-9 .036 FLTDtP-3 .344 FLTDiM-9 O
' 98 98 HANG V Q FO*C (184 GLOR -123 5B EMER
-123.50 EMER
-123.5'. FLTD Q -123.5f FLTD
-123 50 NORM
-123.5i NORM O
O . O __ .---. O O -_. 1
g; - - . . . . .
- - - - ,es - - . _ -
' () IMPELL Cp"^*3cel"/J ,
-s ,
raet aba ,q f) :1 S UPER PIP #03104 1CAe 1T161/858 SYSTEM IMPELL - CIS /
, V .
, 84/03/23e 11 16e16 V
() () .
"$ PGE TROJA3 WUCLEAR STAT 103 EDS PnCaLEM esegc1R-RC-81 PEv.1
- .. PRESSURI2ER S/RV LINE
() AS-8UILT G[0 METRY WITH SLUG DIVER
- ION DEVICES ($0D5 G)
() SUPPORT LO AD
SUMMARY
G C CNT D . 9 , {} SUPP SUPP SUPP DIRN RESULT REsttLT ANIS LOAD LOAD LOAD () NAME LOCN TYPE CODE TYPE UNIT TYPE N-A3!S SET Y-AMIS $[T 2-AXIS SET () ' () idONYb.) *123.50 UPS1 ()
-123 50 UP87tM-9
() DISP (149 GLOS .135 FLTDfM*)
. 98 3 FMER 2.[25'FLTDtM*)
2 198 EMER
.30T FLTDtM*)
.396 EMER
()fj
.881 UPST 2.168 095T .285 UPST
() .PS3 NORM 2 113 1HMU .284 THM1 () g
- 2.08T THMl .284 THMU 2.8GT ' NORM .289 WORM
() . 164 M0PM
.167 THMU
,s ()e,j
=.167 THM1 .495 NORM
' C) 2* 2 uPST .e55 .UeST .se, UPST . C) <
.2T3 EMEP .505 EMER .931 EMER !
.324 FLTDtM-9 .113 FLTDfM-9 .032 FLTDIM-l C) ()
99 99 SNUR 04-C) FORC (Lsl t0CL 83 9e.51 rLvDtM*l C) 8131.18 EMER 1549.66 UPST ,, () -1548.66 UPST () k
-8131.18 EPER _
-83*3 51 FLTDtM-9 I
() () FORC (L83 GLO8 8399.51 FLTDEM*l . 8131.1R [MER C) 15*,.66 UPST ()
-1549.66 DPST
, -8131 38s EMER
() '
-8399 51 FLTDtM-9 ()
DISP tlN) LOCL 831 FLTDIM*) 2 163 FLTDfM*l .OR1 FLTDIM*) () .030 EPER 2.134 EMER .R52 EMER () 499 UP'T 2.0*3 0857 .849 UPST
.00 5 NOPM 2 032 THMU 093 NOPM
() 1.911 NORM * () 1 911 THP1
.2T6 NORM .203 NORM
() .283 TH"U .296 THM1 ()
.2mr THM1 .211 THMU
. .24t Urt? .061 UPST .254 UPST
() () () () () }
() IMPELL CORPORATIO3 SUPERPIPE WERSION 1?Ao 19/81/838 SYST[3 IMPELL - NOS PAGE 236 84/83/23e 11 16 16e () - () PGE TROJA2 NUCLEAR STATIO3 () EDS PROBLEM 4380018*RC-01 R[ Vel PRES $URIZER 1/PV LINF
' () AS-BUILT GE0 METRY WITH SLUG DIVERSION DEVICES ($D03 ()
C) SUPPORT LO AD SUMMARv (CONTD.) () SUPP SUPP SUPP DIRN RESULT RESULT ARIS LOAD LOAD LOAD () NAME LOCN TVPE CODE TYPE UNIT TYPE I-AXIS SET Y-AXIS SET Z-AXIS SET C) () 99 () (CONTD.) .381 EPER .102 EMER .316 EMER
.332 FLTDIM-9 .131 FLTDEM-1 .345 FLTDEM-9
. (1 f)
.392 FLTDiM+)
~ DISP IIN) GLOS .tel FLTDtM*3 2.163 FLTDtM+) () ! () 1 911 NORM .288 THMU 1 911 THM1 .276 NORM
.211 THMU .385 NORM
. 254 UPST .861 UPST .009 UPST C) .31 6 E"Ea Ic2 .EMER .eSe EMER () .
.34 5 FLTDEM-9 .131 FLTDtM-9 .831 FLTDtM-9
() () 101 l 'al SNUS Y FORC (LED GLOB 375c.16 FLTDtM+) () 3671 20 EMER () 572 88 UPST
-572.88 UPST
() -3611.28 EMER ()
-3752 16 FLTDIM-9
() DISP (IN) GLOM .92 3 FLTDtM+) 1.917 FLTDtM*3 .565 FLTDIM+) ()
.92 1 EMER 1 915 E=ER .413 EMER ,
.01 1 UPsf 1.865 UPST .410 UPST
() 383 NORM 1 896 THMU .193 THM1 THMU ()* 1 706 THM1 .193 1 786 NORM .189 NORM () , ' () .225 NORM
.228 THMU .804 NORM i
.22 R THM1 .833 THMU
() .231 UPST .099 UPST .258 UPST () *
.24 2 EMER .05? [MEP .396 EMER
.244 FLTDtM-9 .061 FLTDtM-9 .544 FLTDtM-9
() () () () () () O O O .-. O - -_ O ._.
- e.- - - - -
() IMPELL C RATIO 3
( race 23s frx d) '
SUPERPI RSIO7 16Ao 1(#31/838 SYSTED IMPELL - NO2 ) 84/03/23s 11 16:16' }
}
() PGE TPrJA2 NUCLEAR STATIOJ () CDS PROBLEM R35R018-RC-61 REV.1 PRESSt*12ER S#RV LINE () AS-BUILT GECMETRY UITH SLUG DIVERSION DEVICES (SDD) () () SUPPORT LOAD SUMMART (CCNTD.) () SUPP SUPP SUPP DIRN RESULT RESULT ANIS LOAD LOAD LOAD () NAME LOCN TYPE CODE TYPE UNIT TYPE N-AN!3 SET Y-AMIS
- SET 2-AMIS SET C)
() 102 1J2 HANG Y w () FORC (LB) GLOB -313.28 EMER
-313 2R EMER
() ~313 28 FLTD ()
-313.28 FLTD
-313.28 NORM
() -313 2R NORM ()
=313 28 UPST *
-313 28 UPsitM-9
() -- 1.2SR FLTDEM*3 C) DISP (INI GLOR sn 21 FLTDEMel 1.648 'FLTDtM*) I
. 01 9 EMEP 1.646 EMEP .779 EMER
() 019 UPST 1.620 UPST .777 UPST () 003 NORM 1 614 THMU .031 THM1
.031 THMU
~
1 427 THM1 () 1.427 NORM .328 NCRM ()
.207 NORM
.211 THMU .003 NORM
() .211 THM1 .214 THMU ()
.21 3 UPST .895 UPST .965 UPST
.22 3 EPER .811 EMER -1 206 EMER
() .225 FLTDtM-9 .014 FLTDtM-9 -1 797 FLTDiM-) () () 113 133 SHUB +0L () FORC (LB) LOCL 4053.23 FLTDIMel 3652 47 EMER () !!15 6P UPST ()
-1315.6e UPST . " -3652.47 EMEP
()
~
-4G53 23 FLTDfM-9 ()
FORC (LB) GLOP 4t53 23 FLTDtM*) () 3652.47 EMER ', () 1315 68 UP!?
-1315.6 R UPST
() -3652 47 EMER
~
()
~4 353.2 3 FLTDfM-9
() DISP (IH) LOCL .321 FLTDtM*) 1.644 FLTDfM*3 1.298 FLTDEM*) ()
.01* EMER f.642 EMER .788 EMER
.Po9 UPST 1 614 UPST .786 UPST
() er43 NOPM 1.6C9 THPU .027 THMS () () b) r% () \'
() IMPELL Copp RATION - PAGE 238 34/03/233 11e16sl6e [) [' SUPERP1PE VERSlo^J 16A, 1P/91/931 STSTEM IMPELL - NOS ' () PGE TRIJA2 NUCLEAD STATIO2 (3 EDS PROPLTM C302018-RC-81 Revel PRESSUR17ER S/RV LINE () AS-BUILT GE0 METRY WITH SLUG DIVERSION DEVICES 45D0) () C) S*JPPORT LO AD
SUMMARY
(CONTDel () SUPP SUPP SUPP DIRL RESULT RfS0LT ANIS LOAD LOAD LOAD C) NAME LOCN TVPE CODE TVPE UNIT TVPE N-ANIS SEE T= ANIS $[T Z-AX15 SET () () 193 () (CONTO.) 1 421 THM1 .527 THMU 1 421 NORM .524 NORM i () .207 WORM
.21 0 THMU .883 NORM (){
.21 0 THM1 .218 THMU
. () .213 UPST .005 UPST .983 UPST ()
.223 FMER .011 EMER -1 226 EMER
.224 FLTDiM-9 .013 FLTDtM-9 -1 736 FLTDtM-9 C)
() OISP JINI GLOS .021 FLTDtM*) 1 644 FLTDtMel 1 298 FLTDIM*l ,
.01 9 [MER 1.642 EMER .788 EMER -
() .00* UPST 3 634 .UPST .786 UPST () I
.003 NORM 1 609 THMU .027 THM1 1 421 THM1 .927 YHMU
() 1 421 NORM .924 NORM () ,
.2R7 NDPM
.21 0 THMU .883 NORM
- () .21 9 THM1 a.21A THMU ()
.21 3 UPST .035 UPST .983 UPST ,
.223 EMER .n11 EMER -1 226 EMER
() .224 FLTDfM-5 .013 FLTDtM-l -1 136 FLTDIM-5 ()
- () 104 104 SNUB Y ()
FORC (LBB GLOB 304*.11 FLTDtMel , 2875.T1 EMER 75P.67 UPST () ,' () -758.67 UPST
-2875.71 EMER
' () -3049.11 FLTDtM-9 () DISP (INI GLOR .932 FLTDIM*) 1 591 FLTDiMel 1 331 FLTDIM*) () .t31 [MER 1.5*1 EMER .892 EMER () !
.007 L'o S T 1 562 UPST .800 UPST
.003 NORM 1 563 THMU .612 THM1
() 1 388 THMt .012 THMU () 1 3R7 NORM .010 NORM ,
.224 NORM
() .22 7 THMU .002 NORM ()
.22T THM1 .244 THMU
.22P UPST .043 UPST -1.036 UPST
() .242 EMER .n11 EMER -1.299 EMER () C) () O _. O._ __ _ O
- w -e.sms am - m m.
- [j[1.
() I MPtLL C SUPECPI neeION
- RSIt3 1EAe 18/01183: SYSTEM IMPELL - NOS ,.'}
. 3E 2 ,
84 #03/23s !!e1631*[,,] q) PGE TROJA2 NUCLEAR STATION () EDS PP08LEM 2309018-RC-81 REY.1 PRES 50RIZER SIRV LINE l() AS-BUILT GEOMETRY WITH SLUG DIVERSION DEVICES (SDD3 ($ l l C) SUPP0=f LOAD sUMMARv (CCnTD. CD SUPP SUPP SUPP DIPN RESULT RESULT AIts LOAD LOAD LOAD () NAME LOCN TTPE CODE TYPE UNIT TYPE X-ANIS SET T-ARIS SET Z-AMIS SET () }. l () 184 () (CONTD.3 .243 FLTDtM-1 .811 FLTDiM-9 -1 028 FLTD(M-1 () f() i 106 106 $NUO +09 FORC ELB) LOCL 4735 98 FLTDEM*) C) 4T27 44 rwER C) 225.21 UPST i -225 21 UPST C) -*727.44 EMER ()
-4735.98 FLTDEM-9 C) r0RC (ts, Gt0e 4735.,e rtTDtM.: ()
4727.44 EMER 225 21 UPST C) -225 21 UPST ()
-4727.44 EMER
-4735 9P FLT0fM-3 C) ()
DISP (IN) LOCL .237 FLTDtM.3 1 317 FLTDtM*) 419 FLTDtM*)
.237 EMER 1 316 EMER .013 EMER
() .14 1 UPST 1 303 UPST .811 UPST ()
.14 0 THPU 1.30s THMI .001 NORM 1 3CR THMU
() 1 298 NORM ()
=.039 NORM .092 NORM
.04 f THMU .893 THM1
() .e4 s THM1 . Ort NORM .419 inMu ()
.e4 9 UPST .tes UPST , .427 UPST
. P6 0 EMER .019 [MER .699 EMER C) .es e rtTDtM-i .o2a rtvDtM-> .s,6 rLibeM-i ()
DISP (IN) GLOM .237 FLTDtM*3 1 317 FLTDtM*) .319 FLTDtM*) () .237 EMER 1 316 EMER .n13 EMER ()
.14 1 UPST 1 303 UPST 611 UPST
.140 THMU 1.303 THM1 .401 NORM
() 1.300 THPU () 1 29R NORM
.G39 WOpM .692 NORM
() .54 9 THM3 .993 THM1 ()
.f t t TPol . Pct No#M .419 THMU
.:4 UPST .445 u ST .427 UPST c) .cs a ErER .nto EMEe .s9s EMER ()
() () O O ,
() IMPELL CORPORATl!3 PAGE 240 (]) % SUPERPIPE VERSION 16As 18/01/R38 SYSTEQ IMPELL - NOS e 84/03/23, 11 16.316. () PGE TROJ43 NUCLEAR STATIO3 EDS P;08LEp G3eDS12- C-81 REY.1 () PRES $URIFER S#RV LINE () AS-DUILT GEOP.ETRY WITH SLUG DIVERSICN DEVICES (SDDI d) () SUPPORT LOAD
SUMMARY
(C ON TD . ) - () SUPP SUPP SUPP DIR N RESULT REStiLT ARIS LOAD LOAD LOAD - () NAME LOCN TYPE CODE TYPE U9IT TYPE X-ANIS SET Y-ARIS SET Z-ANIS SET C) () 106 () (CONTD.9 .06 9 FLTDtM-9 .928 FLTDEM-9 .696 FLTDEM-9 () () . 107 197 SNUS 2 i FORC (LB3 GLOB 2825.54 FLTDtM*3 ,5 C) 2865 11 EMER () !
< 1441 60 UPST ;
~
- -1441 60 UPST '
- () -2s65.11 EMER ()
-2825 84 FLTDiM-9 l
() DISP (IND .21 7 FLTDiM*l 1 279 .FLTDtM*) .007 FLTDtM*l SLO 8
.21 7 [MER 1 778 EMEP .505 EMER () { ,
.128 UPST 1 266 UPST .384 UPST !
() .326 THMU 1 262 THM1 .001 NORM () g 1 262 THMU ' 1 260 NORM () .041 NORM .088 NORM ()
.04 2 THMU .RS9 THM1 ,
.94 2 THM1 .001 NORM .415 THMU
() .04 2 UPST .6D7 UPST .417 UPST ()
. 56 2 EMER .019 EMER .674 EMER
.C62 FLTDtM-9 .82n FLTDtM-9 .676 FLTDEM-9
() . () 118 lif SNUB Y () FORC (LB3 GLOB 693.48 FLTDEM*) () 607.5R EMER 303 78 UPST () -393.78 UPST ()
-6n7.58 EMER
-693.48 FLTDEM-1
() DISP (INI GLOB 924 FLTDtM*) .560 FLTDtM+) .015 FLTDtM*) C)
.02 3 EMER .55* EMEP 815 EMER
() .005 UPST .554 UPST .992 UPST ()
.558 THP1
.550 THMU
() .549 NORM ()
.851 NORM .P39 THM1
.55 2 THMU .039 NORM
() .PS 2 THP1 .317 THMU () d) () O - - - .-. O O . ,
Q IMPELL C[Q ATIo3 P*st 243 g Q j1 SUPERPIP, f RSIO3 16Ao if/41#R31 SYSTED IMPELL - NOS 84#03#23e 11e16s!6c( . () PSE TO1JA3 NUCLEA3 STATIO3 () ,' EDS PROBLFM T38PC18-*C-f t REV.1
- PRESSUR12ER $#RV LINE i C) AS-BUILT CEOMETRY WITH SLUG DIVERSION DEVICES ESDD) ()
4 , C) S UPPORT LO AD SUMMART (CONTD.3 (D
$UPP SUPP SUPP DIPN PEFULT RESULT ANIS LOAD LOAD LOAD
() NAME LOCN ITPE CODE TYPE UNIT TYPE N-ANIS SEE T=ARIS SET 2-ANIS SET ()
' Cl 110 * ()
(CONTD.3 .455 UPST .095 U*ST .318 UPST
. o8 = EMEP .s s EMER .49, EMER
- C) .n9 s rtiotM- .ett rtfotM- . 4,9 rLTDtM- ()
j () 111V 111 CCNF T () (LB9 -196 57 EPEP FOPC GLOB l -196.57 EMER
- () -196 57 FLTD ()
-196.57 FLTD
~196.57 NORM
! () -196.57 . NORM f)
-194.57 UPST
-196.57 UPSTEM-1
() (I DISP (IN) GLOB .825 FLTDEM*) .521 FLTotM.) .014 FLTDtp+3
.f24 EMER .521 EMER .014 EMER
- () .P05 UPST .514 UPST .002 UPST ()
.511 THM1
.511 THPU
,l () .511 NORM ()
. 94 7 NOPM .837 THM1
.a4 8 THPU .037 NORM l () . 64 8 THMS .382 THMU ()
.052 UPST .MOS UPST .303 UPST
.08 5 EMER .811 EMER .476 EMER
' () .08 6 FLTDtM-9 .011 FLT0tM-3 .476 FLTDtM-l ()
' () lli 117 %NUR 7 ()
FORC (LB3 GLOS 1547.17 FLTotMet 952 69 EMER
; () 952.63 UPST C)
, -952.63 UPST
- -952 63 EMER
; () -1547 17 FLTDtM-1 ()
DISP (INI GLOD .194 FLTDEM*) 3.44r FLTDiM*) .361 FLT0tM+3
, () .381 FMER 3.433 EMER .159 EMER ()
.181 UPST 3 433 UPST .159 UPST
.159 THPtl 3 421 THPU .356 THMU
- () .120 THM1 2.771 fpM1 .094 THM1 ()
() () I () ()
Q IMPELL CORPORATIE3 SUPEOPIPE VERSIO5 16A. If/Pl#p38 SYSTEM IMPELL - NOS PAGE 242 34/33/23a 11e16stSe () [;t Q POE TCTJAZ NUCLEAR STATICQ Q EDS P900LEM 33D3018-RC-81 REV.1 PRESSURIZER StRV LINE Q AS-BUILT GE0METPT WITH SLUG DIVER $10N DEVICES 45001 Q Q SEPPORT LO AD
SUMMARY
(CCNTD.) O SUPP SUPP SUPP DIRh RESULT RESULT ARIS LOAD LOAD LOAD Q NAME LOCN TYPE CODE TYPE UNIT TVPE X-ARIS $[T. T-ANIS SET Z-ARIS. SET O Q 117 O (CONTDel .32 0 NORM 2.771 NORM .894 NORM
.02 3 UPST .012 UPST .003 UPST Q .023 EMER
.036 FLTDEM-1
.n12 EMER
.819 FLTDtM-9
.333 EMEp
.996 FLTDI,M-l Q{ ,
o O! 129 120 HANG Y l FORC (L83 GLOS -372.17 EMER Q -372.17 EMER Q
. -372.17 FLTD
-372.17 FLTD Q -372.17
-372.17 NORM NORM O[,
=372.17 UPST Q -372 17 UPSTEM-l O DISP IINI GLOB .172 FLTDtM*) 3.542 FLTDIM*) .229 FLTDEMel Q .167 EMER 3 539 EMER .219 EMER O
.16 7 UPST 3 539 UPST .219 UPST
.155 THMU 3.532 THMU .205 THMU Q .11 2 THM1 2 807 THM1 .978 THM1 Q
.111 NOPM 2.947 NORM .9T8 NORM
.901 NORM Q .01 4 UPST .006 UPST .015 UPST O
.014 EMER .006 EMER .815 EMER
.02 0 FLTDtM-1 .410 FLTDIP-3 .825 FLTDEM-l O O 1234 123A SNUB Y Q FonC (LB3 GLOB 1289.19 FLTDIM*l O 895.22 EMER 8C5.22 UPET O -ets 22 UPsi O
, -805 22 EMER
-1238. 19 FLTDfM-9 O O DISP t]NI GLOB .107 FLTDtMel 2 524 FLTDtM*3 .247 FLTDEM*)
.125 Em[R 3.526 ENER .245 [MER Q .193 UPST 3.M26 UPST .245 UPST O
.t94 THM1 3.523 THMU .243 THMU
.f94 THMU 2.798 THM1 079 THM1 Q .*93 NOPM 2.797 NORM .878 NORM O O O O _. ._ _
O O
- - -- m -.
J
- r h-
'O IM*Ett sc~~ a ' a co SUPERPIP' It/C1/$35 SYSTEM tr.PELL.- NOS 34/93/23a 11e16,16e L' N.)7Q516.3 16 A . PIE T"0JAD NUCLEAR STAT 107 Q O -Q- EDS PR08LEM t3t4L18-RC-51 REV.1 PRES $LRIZER S/RV LINE !O AS-BUILT CEOMETRT WITH SLUG DIVERSION DEVICES (SDD) O {Q SUPPORT LO AD
SUMMARY
(CONTD.9 O SUPP SUPP SUPP DIRh RESULT RESULT ANIS LOAD LOAD LOAD jQ NAME LOCN TYPE CODE TYPE UNIT TYPE R-ANIS $[T Y-ANIS SET Z-ANIS SET O IQ 123A O (CONTD.) .001 NORM
.24 2 THMU / .ng! NORM
';Q .254 UPST . Pts UPST .005 UPST O
.254 FMER .805 EMER .005 EMER
.258 FLTDEM-9 .807 FLTDtM-9 .007 FLTDtM-9
- O O 124 124 SNUS 7 iQ FPRC ILB) CLOS 926 06 F L T D t 81* ) O 633.00 EMER 633.09 UPST lQ -633.R0 UPST O
-633.00 EMER '
! -926 06 FLTDEM-9 'Q i 0
. DISP flN) CLOS .194 FLTDtM+l 2.526 FLTDtM*3 .241 FLTDIM+3
.141 EMER 3.523 FMER .239 EMER
- Q .191 t 'M T 3.523 UPST .239 UPST O 99 2 THM1 3.517 THPU .238 THMU
.f92 THMU 2 794 THM1 .#79 THM1 -l
]Q .09 1 HORM 2 183 NORM .311 NORM O'
.861 WOPM
.279 THMU .591 NORM 1,Q .296 UPST .997 UPST .005 UPST O
.290 EMER .007 EMER .8P5 EMER
- .294 FLTDIM-9 .010 FLTDIM-l .006 FL) dim-9
'O O Q FORC (LP) CLOP 1413.28 FLTDtMel O 987.83 FPER 9 8 7.R 3 UPti O -987.83 UPST O
-977.R3 EMER
-1413.28 FLTDtM-l O O
, DISP tlN) GLOP .a98 FLTDEM.) 3 457 FLTDtP*) .169 FLTDtM*)
! .t93 FMER 3.44' EMER .157 EMER
'O .C93 upsi 3.449 UPST .157 UPST Q
.tRT THM1 ?.437 THMU .153 THMU
.047 THNU 2 754 THP1 .075 THM1 i /) . b8 6 NORM 2 734 NOPM 8173 NORM O i
O O O O ,
IMPELL CORPORATIC-3 P2GE 244 ($) (.
- () 84/03/23s 11 16 76.
SUPERPIPE VEGSION 164. 14/01/831 SYSTEQ IMPELL - h0S () PGE TR2JA3 CUCLEAR STAT!$3 {} EDS PR0RLFM 33**PIR-RC-91 Revel PRESSURIz[R S/RV LINE q) () AS-8UILT GECMETRY UITH SLUG OIVERSION DEVICES (SDD) () SUPPORT LO AD
SUMMARY
(CONTD.3 () SUPP SUPP SUPP DIPN RESULT RESULT ANIS LOAD . LOAD LOAD () NAME LOCN TYPE CODE TYPE UNIT TYPE I- ARI S SET , Y-AX1s SET z-AK13 SET C)
- () 126 ()
(CONTD.) *.001 NORM .982 NOR M () .324 FLTDtM-9 lli VREI
.025 FLTDiM-9 EilII fill
.051 FLTDiM-3 C) 12T 12T HAAG v ()
FORC (LBI GLOS -245.91 EMER
-245 91 EMER
- () =245.91 FLTD ()
-244.91 FLTD
-245.91 NORM
() -245.91 NORM () '
-245 91 UPST
-245.91 UPSitM-9 '
() () DISP (IN) SLOB .894 FLTDtMel 3 433 FLTDtM*3 .135 FLTDtM.)
.991 EMER 3.424 EMER .133 EMER l
() .093 UPST 3.424 UPST .133 UPST () !
.SST THM1 3 496 THMU .329 THHU 'l
.08T THMU 2.T16 THM1 .8)3 THM1 1
() .026 NORM 2.T16 NORM .rT1 NORM ()
.002 NORM
.309 THMU .966 THMU
() .31 5 UPST .018 UPST .ST3 UPST ()
.31 5 EMER .01R EMER .073 EMER
.31 8 FLTDtM-1 .026 FLTDtM-9 .975 FLTDiM-8
() , () 133 133 HANG Y C) FORC ( L B t- GLOB -259.53 EMER ()
-259.53 EMER
-259.53 FLTD
() -259.53 FLTD ()
-255.53 NORM
-2?9.53 N08M
() -259.53 UPST ()
-259.53 UPsitM-)
() DISP IINI GLOR .311 Ft700M+) 3.141 FLTDiM*) .059 FLTDtM.) ()
.11 0 emf 8 2.832 EMER .05T EMER
() () O 0
^
G _ _. e ._ _ e "
j - - - - > m -
!h IMPLLL CP ^'SmaeIO3 SUPERP!;
'IRSION 1544 It#41#R31 SYSTED IMPELL - NOS s r ra4E 2.;,
34pg3/23, 11 16:16*
, C)
\s,/ \ f
; () PSE 7ROJA3 NUCLEA3 STATIO3 *
() l EDS PP99LEM 1300018 RC-01 DEY.1 1 PRES $ UR IZER S/RV LINE () A0-BUILT GEOMETRY WITH SLUS DIVERSION DEVICES ISOD) GD 1 i () SUPPOR T LO AO
SUMMARY
(CONTD.) (I I SUPP SUPP SUPP OIRL RE S UL T RESULT ARI3 LOAO LOAD LOAD ]() NAME L OC N TYPE CODE TYPE UNIT TYPE 3-ARIS SET Y ARIS SET 2-AMIS SET CD i l() 133 (CONTD.) .11 9 UPST 3.932 UPST .357 UPST CD
.eR 7 THMU 3.918 THMU .953 TN#1
- () .975 NORM 2.439 THM1 .953 TNMU ()
, .01 5 THM1 2.439 NORM .e51 NORM 4 .eet NoR M J () .284 THfD .413 TNMU ()
1 .307 UPST .922 U#ST .421 UPST l .3 1 rME . 22 EMER .421 EMER j () .31 5 FLT0tM-9 .031 FLTOEM-1 . 423 FLTDtM-9 () () 139 139 SNU3 Y . () i FORC IL83 GLOS 1263 85 FL10tM*) 4 () llllill bill
-ss,2.es EPER j -1263 05 FLTDEM-9 i C) C)
OISP (INI GLOS .349 FL10tMel 2 636 FLTOEM*) .187 FLTOtM*) ! .137 FMER 2 636 EME# .172 EMER *
.187 UPST 2 636 UPST .372 UPST ()
j () l
.171 THMU 2 634 THMU .148 NOR M
- 2 270 THM1 .145 TNM1
! () .. se 2 NORM 2 265 NORM .145 TwMU () l .906 THP1 .PP4 WDR M
.408 N0*M j ()
j
.317 THMU .984 NORM .187 THMU ()
, . 337 UPST .011 UPST .128 UPST I .33 7 EPER .011 EMER .128 EMER l() .34 8 FLTDIM-9 .S11 FLTDfM-1 a.142 FLTOtM-9 () i () 143 143 $NUS Z () 1 FORC ILMS GLOS 467.93 FLTDtM.) i 336.51 EMER () 336 51 UPST * ()
- -336.51 UPST
-336.51 EMER
) -467.03 FL10fM-9 ()
l DISP 8tNS GLOB .195 FLTDfM*l I.4*9 FLTOEM*3 .197. FLTDtMel C) () f () C) i .
~
l (T L)
^]) I MPELL CORPOR ATION PAGE 203 3]/93/23, 11 13.30,
() - SUPERPIPE VERSION 104, 16/01/03I SYSTE3 ICPELL - NOS : () PGE TLTJLO NUrLEAR STATION () EDS PROBLEQ 0383018-AC-41 REV.1 PRES $LRIZER J/RV LINE () AS-BUILT GEOMCTRY v1TH SLUG DIVERSION DEVICES (SDOS () l C) SzPPORr t0 AD suMMARv (CCNTD.: () SUPP SUPP SUPP DIRK RESULT RESULT AMIS LOAD iCAD LOAD X-AXIS Y-ANIS
- SET Z-ARIS SET C)
() NAME LOCN TYPE CODE TYPE UNIT TVPE SET l() 343 () ~ (CONTD.) .192 [MER 2.486 [P!R .186 EMER
.192 UPST *e486 UPS1 .106 UPST
() .1TT THMU 2 465 TMMU .103 NORM () 2 131 THE1 .191 THM1 2 131 NORM . net THMU () .00 2 NORM ,.592 40RM ()
.002 NORM
.166 THMU .959 THMU
.185 UPST .022 UPST .859 UPST ()
l() .185 EMER
.18T FLTDtM-9
.022 ~EMER
.026 FLTDEM-3
.059
.060 EMER FLTDEMal l
' Cl () 144 144 HANG T () FORC (LB) GLOB -314 1R EPEP ()
-314.1R EMER
~314.30 FLTD
. () -314.16 FLTD ()
-314 18 NORM
-314.38 NOR9
, () -314 18 UPST ()
-314.1R UPSTtM )
I () OISP flN) GLOP .195 FLTDttet 2.469 FLTDEM*8 .106 FLTDEM*) ()
- .193 EMER 2.464 EHER .303 EMER
.?93 UPST 2.464 UPST .103 UPST 87T NORM () 1
- () .tTT THPU 2.442 THMU 2.113 *iHM1 .095 THM1 2 113 NORM .095 THMO .
() .001 N0pn .a02 NCAM () 0.002 N00N
.14 5 THMU .050 THMU
.364 UPST .422 UP%f .854 UPST ()
'! r) .164 EMtR .s22 EMEP .e54 EMER
.166 FLTDtM-1 .02T FLTDEM-9 .05T FLTDtM-1 '() ()
145 145 SNtl8 Y
; () F0st (LPI GLOB 89r,81 FLTDEM.3 ()
T46.19 EMER T46 19 UPST
; () -746.1* UPST ()
i O O
'O g - - .-. --
g= -. -- O
W,, --
=e N +-
2 o o o o o o o e o o o o o o o o o o o o O [N t ) t i
\d 8
en I @ea ee . e em a en a os a se
- 0 e e o E E E E E 4 .e w == en w
>M e.) > 0 m > E ese 3 T 3 e= E O O E > se 3 E E 3 e= m O QE>
rT W e4J e=taa M N E E E E M tmA > > tee M E E E E E M tmJ > > tes M N% OM .JE G.C>E E O E & E .J .J E & 1 E O O E 0. E .A 4EL M of h and 3 E p > E s=3Wm ta. tad 3 > e= E E > 3 tas k ts. tea 3 r tee to GD %
*E t M M P P P e= es. es e>>M MNNeE@NMNIWe eMe
(.h uG ** eeneeeae M e e Wt se se se O se eCMeee se > er M seOeeeee e S e G* se se se se se se M oe se seen eo e 4 e e e e e e e e e e e e eee e eee e 9 e >>> 9 9 8 9 4 0 0 0 0 9 P GI M N E **
- o. .ee.
i m e. a. a e O e 9 E E F E E w w w w w O 8= EO O ef > 3 E se D= E O O E > D E sa >EO it M taa > t=ledM E a E M too > e4J tas e e= w M E a E
- OM EJ of E d. E O E & E .J ed E & E O E b E .A
.8 eJ k as tea 3 o= X > 3 tad an. In. l.8 e*J > E > 3Wh M F we me e E e se ce M M em a'CD S F e E se ** se
** es el e art er8 ce P P 44 N d% f* @ @ grl P P NNM M e e e e e e se et de e E. N N N N Mtil s D st og de ee e ee e e e e e e e e e e e e e 0 e O- NNNNNN $ $ $ gra pt M M EU me 4 4 8
> Pe E GG e
en en sub a en en
% en e e 8 e i
j O O E E 0 E E E E t w w w e {
,% / =
M O C*
=
O r t= 3 ** K3>EO
=
O ek D= t= m O O E > ** 3 E D>EO E tr. and e= at be a= (.a til E E a E M an# t= r- and M tr toe e= a=tes M E E a M O ers .J E G. E 3 O E G. E .J .A E 0. & E .J .eE&EEO E EL E .J tea .J an, one 3 e= t= E e= 3 Ime es. te. and 3 3 tea ta. es.ImeD > > E > m3 ans ab U ee
> M weeEN es e P P ** $ e e sa en @ e ** ** es se se er. e d me
== em P P en e e N ert M e >ESe&A e $$ P E e e sum 80 e e Goa O as se we ceen e a es we se ee o e oe e e c . * *e E e e ce re ce N 4 ee e ee e o e o e se e e es d we o ee e ee oe a e E 9 4 1 0 8 e es M F5 er r1 em 8 0 4 8 O In en P= > > > trl en N se se se se N M eee M E O a.#
E ** w e em 1 0 > 0 an ED e E i tea M tmJ
.J E @ ** A. O O O O J R 3 M> d J J J l e tes O es .A es e te o o
[
*4 ** As M aC e= 8 me as U E > an e= a W o= .a e= an en om i G et a E ** 3 ** E era E s, Ima e ** 3 ME ene .A == .J WD w en w er 7
o= (1 se .J i M eo e- a
> tas e > a M .3 Se es e=
u rt % W o=
== 3 sa M E .a anJ & u e, y M E O 3 G. M u ers a rt E E tea en M> ** O me c
% D W ame 43 e imJ *= O te. f3 4 ee as .8 N O es e 3 e ** > *=
% kp O E & E o (g a 3 ee O .a las se e= en em 3 U er O as N i
' s to O w me Q l y e t J M ema e ou i e isOnM i f WJ G. taa G. 4 O i se > tm. e l er ik & P 3 i EE 4 3> E E OO L M e= to M l i
==== E
>M 3 v1 M e. E se e i
- M Lu M p
O 3O se me
.e i
I M .J l O a
.J e i
W t -+ 0. led ett O es e en e= dL E se e- art M l we se
.J a. m 3< ** E l
du o ME O I ese one A U l && & w E3 3
** M et i 'O O o o o o c 0 o o o o, o_O___o _
o o o o o o O
Q IMPELL CORPOR ATI~J PAGE 248 84/03/23= 11 16 14e O' SUPERPIPE VEOSION 11A. !!/31/038 SYSTEM IPPELL - NOS Q PGE TCTJA3 NUCLEAA 3TATION O EDS PROBLEQ 0300012-SC-81 REY.1 PRES $bRIFER S/RV LikE Q AS-8UILT GEOMETRY UIItd SLUG DIVER $10N'JEVICES 4500) O Q S ,:PPORT LOAD
SUMMARY
SCONTO.) O SUPP SUPP SUPP DIRN RESULT REStfLT 411S LOAD LOAD LOAD Q NAME LOCN ITPE CODE TYPE UNIT TYPE X ANIS SGT Y-ARIS SET Z-ARIS SET O Q 15. O (CONTL'.3 -1157.79 UPST
~1157 74 EMER Q -1897.18 FLTDEM-9 O DISP IINI GLOS .133 FLTDiMel D.200 FLTDiM*) .194 FLTDEM*3 Q .189 EPEP 3 197 [MER .389 EMER O
.109 UPST 3.197 UPST .189 UPST
. a?_5 THM1 3 149 'vHMO .183 THMU Q c 915 THMU 2 557 N049 .167 THM1 G 66 4 NORM 2.557 THM1 .166 NOMM
.iF? THMU Q .32 3 UPST .8 85- UPST .007 UPST O
.32 3 EMER .006 EMER - .e97 EMER
.34 6 FLTDtM-3 .389 FLTDeM-9 . 91) FLTDtM-5 155 155 SNU8 1 Q FORC (L89 GLO8 l*399.59 FLTDtM* O 1141 19 EMER l 114 t'.19 UPST Q -1141 19 UPS7 O .
-3141 19 EMEP
-1599.59 FLTD1M-3 O O DISP IIN3 GLO8 .134 FLTDtM*3 3.178 FLTDiM*3 .204 FLTDtM*3
. 111 EMEP J.1TS Ld[R .199 [MER Q .311 UPST 3.17" UPST .199 UP S'. O
.06 6 THM1 3.167 THMU .192 THMU 66 6 THMU 2.540 NORM .161 THM1 Q .065 NORM 2 54; THM1 .160 NOR M O
.276 THMU
.322 UPST .007 Upii .eas UPST Q .32 2 EMER .e n EMEp .ses EMER O
.34 5 FLTDtM-9 . 019 FLTDEM-9 a.012 FLTDEM-l O O 159 159 SNUM Y FORC (LM) GLOM R69.19 VLTDtM+3 Q 59R.14 (mea O 5SA.14 UPRT
-59M.14 UPST Q -578 14 EMER Q O Q
~
O .-. O.- .- - -. e
- - - ~- ,
' () iMettL SUPE PI a: ION
- E3510N 164, t r/ elf 831 SYSTER IMPELL - NOS
. SE 1,,
e4 /03 /23, R1 16,1',-,') () { i 'V () PGE TR$JA3 WUCLEAR STATION () EDS PPOPLEM 430a914-RC-01 REV.1 i PRESSURIZER S/RV LINE 4 () AS-Butti GEOMETPY UITH SLUG OIVERSION DEVICES (SDOS () () SEPPORT LOAD SUMPARY (CCNTD.) () SUPP SUPP SUP P DIRN P E SUL T ret ut ? AMIS LOAD LOAD Lose C) NAME tocN TYPE C00E TvPE Uw T TvPE x-Anis SET v-Amis SET r-Au!S SET t) * () 159 () (CONTO.) -869.15 FLTDtM-1
, () OISP (INI 6LO8 .30F FLT0fM*) 2 988 FLTOIM*) .2 96 FLTb4M*3 CD
' .1T6 EMER 2 916 EMER .281 EMER
.116 UPST 2.916 U* S T .288 UPST
() .131 THPU 2 969 Thou .256 THMU f)
. PTS TNM1 2e392 THM1 .113 NORM
.C*4 WORM 2 399 NORM elle THM1
.26e (HMu .Pe2 N0=M C)
.314 UPST .011 UPST .024 UPST () I
.314 EMER .a11 EMrR .or4 EMER
() .338 rtTotM-9 .e15 .FLTotM-9 .ste rLie M-9 ') l i C) 16e 16e SNU8 2 j FORC IL89 GLOR 3E68.19 FLTOtM*3 i 1868 56 EMER ' C) - 1868 5' UP5T C) j -1868.56 UPST j 41868.56 E ME h' () ~3868.19 FLTDPM-9 () DISP (1N) SLD8 .223 FLTDEM*3 2 958 FLTDtM*) .31T FLT0tM+n ! ()
.19 9 EMER 2.952 EMER .291 EMER ()
.199 UPST 2.952 UPST .294 UPST j .155 THMU 2.942 THMU .263 THMG
! () .016 THM1 2.313 THM1 .183 NORM ()
j .CT5 NORM 2.374 NORM .103 THM1
- .26T TMPU .4P2 NORM j f)
.31 3 UPsi .n14 UPST .031 UPST ()
.31 3 EMER .c14 EMER .931 EMEP I' .33T FLTDtM-1 .02a FLTDIN-l .958 FL10tM-9 C) C) i +
l 164 164 HANC Y l () FORC (L89 GLOB -515.04 EMER () i -91*.04 EPER
! -51c.t4 FLTD i () -516.34 FLTD ()
*Str.C4 NORM
-31r.04 NO8M i
() -51'.*4 UPST () O O
! C) C) )
7h IN'f LL CORPOR AT103 SUPEEP7" VER$10N 1CA, 1E/*1/031 SYSTEP 1MPELL - NOS PAGE 258 84/03/233 11e16 16s () U Q) PGE 107JA3 NUCLEAR STATION EDS P90RLEM G32401R.pC-91 rey.1 (] PRESSURI2ER $/RV LINE () AS-BUILT GEOMETRY WITH SLUG D1VEPSION DEVICES 650D3 C) g) S!PPORT LOAD
SUMMARY
(CONTD.3 , ()
"SUPP SUPP SUPP DIPk RESULT R EtD( T ANIS LOAD LOAD LOAD
() NAME LOCK TYPE CODE TYPE UNIT TbPE X-AXIS SET T-ARIS SET 2-AR15 SET () () 164 () (CuNTD.) -51n.c4 uPSitM-p () DISP 4INI GLOB .359 FLTDiM*3 2.834 FLTDt34) .390 FLTDEM*) ()
.334 EMER 2 809 [MER .364 EMER
.33 4 UPST 2.809 UPST .354 UPST
() .290 THMU 2.TT3 THMU .313 THMU ()
.080 THM1 2 249 THM1 .060 NORM
.591 NOPM 2 249 NORM .065 THM1
() .21 3 THMU ()
.25 9 UPST .836 UPST .e41 UPST
.259 EMER .536 EMER .841 EMER
() . 283 ( L TD t M-) .358 FLTDtM-9 a.96T FLTDtM-) () FORC C;83 GLOS 2393 39 FLTDiMel 1896.4T EMER () 1896.6T UPST ()
-1886 6T UPST
-1896 6T EMCR
() -2393 39 FLTD4M-9 () , DISP (IN) GLOS .41 2 FLTDIM.) 2 669 FLiotM.3 .342 FLTDtMel (y .392 EPER 2.605 EMER .341 EMER ()
.392 UPST 2.605 UPST .316 UPST i
.35F THMU 2.591 THMU .303 THMU C) 9T5 THM1 2.125 THr1 .526 NORM ()
.0T4 NORM 2.123 NORM .926 THM1
.19T THNU .8G2 NORM
'C; .1: 3 uPST .o19 UPST .c14 UPST c)
.14 3 EMED .019 EMER .914 EMER
.163 FLTDtMal ..R23 FLTDeM-9 .015 FLTDSM-1
- (J CI 173 1TL SNUB **t
() FORC ILet LOCL 3345.11 FLTDtM+) () 241*.54 EMEP P4?9.54 UPST (') -2434.5e UPST GD
-2 4 39.S a EPER
-9345.11 (17084-3 FCPC (LP) GLOM 3294.29 FLTutM.) Sac,MT FLTDtM*8 N) CI O .-.
O - O
-Q j
- p[4C 751 g Q
!MPELL C A T 10ag SUPECPI R$104 104, 1P/01/098 Svsfft3 IPPELA e MOS
- 04/93#23s 31 16sl6 s Q P![ TCJA3 NUCLEAR $747IE3
- Q ,e EDS P90eLEM 034881R-RC-et REv.1 PRESSURIZER $/RV LINE jQ AS-8UILT GEOMETRY WITH SLUS DIVER % ION DEVICES (SDDI O Q SUPPORT LOAD SUMPARY (CCMfD.) O SueP SUPP SUPP DIRN RESULT RESULT ANIS LOAD Lea 0 LOAD Q NAMC LOCN TYPE CODE TYPE UNIT TYPE N-ANIS $[T Y-ANIS 3ET Z-ARIS SET O '
iQ 17 O I (LDWTO.) 2432.48 EMER 423.62 ENER 24P2 48 UPST 423.62 UPST a 'O
- 32402.48 UPST -423 62 UPST O
-2407 48 EPER -412 62 EMER i
-3294.29 FLTDIM-9 -5PO.07 FLTDtM-1
-Q O i DISP (IM) LOCL .74 8 FLTDtMel 2.392 F L TO S M* P. .250 FLTD4Mel j .74 3 EPER 2.373 ftaER '
.249 [MER jQ . 74 3 UPST 2 375 UPST .238 U7sf O
.T32 TMPU 2.344 THMes .217 TMIU j .391 THM1 1 971 TMMS .919 NORM jQ .34 9 WORM 1.*66 .h09M .019 THMS Q i .CF2 NOP M .0 96 WORM '
.815 UP?T .943 UPST .013 UPST lQ .s95 EMEe .e43 EMER ..e13 EMER O ,
j .92 8 FLTOtM-9 .P56 FLTOtM-1 -.#14 FLTDiM-1 t O DISP (14) . GLOS .35 0 FLTDEMel 2.429 FLTDIA*3 .250 FLTDtMel O
. 34 5 [MER 2 416 EMER .249 EMER *
.34! UPST 2.416 UPST .238 UPST . .
,O .328 THMU 2.3ml TMMU .217 THMU O i .94 3 THM1 2 409 THM1 .319 NeRA J .84 1 NOPM 2.004 20pM 4519 TMM1 !O .stl =0,4 .ee5 m0=M O j . 91 9 UPST e644 UPST .013 UPST , i
.C19 EMER .044 EMER .813 EMER
,O .02 5 FLTDtM-3 .057 FLTDtM-9 .814 FLTDEM-9 0 1 Q A17R A178 Sh08 N ~O FORC (LB9 GLOS 1173.R5 FLTDtM.3 1 *47 1 T EMER ' O 1 G 8 7.17 UPST Q ;
-1987.17 UPST
-l a R T.17 EPER t O -1173.45 FLTDSM-9 0 DISP (INI GLOR .294 FLTDEM*l I.951 FLTDfM+) .C37 FLTDeMot
- Q .293 EPER 1.946 EMER .635 EaER O 83" '
.234 UPST 3 945 UpST UPST I .226 THPU l.92R THMU .992 NORM
,Q l.752 THP1 O ,0 , O iA tl l
} IMPELL CORPCR2110N PISE 75:
A9#83/233 13 133163 Oy
$UPEaPIPE VE4510416Ao 18tC1/a38 ETSTEQ IMPELL + meS >
0 PsE i=0aAn =UctEco STATIO= 0 EDS PROSLEM C308318-RC-81 REV.1 PRLS$0RIl[R $/PV LINE ' AS-8UILT GEOMETRY WITM SLUG DIVER $10W DEVICES 630D3 Q
.O O S f*POR T LD AD SUMM ARY (CCNTD.: O SUPP SUPP SUPP DIRK pESULT R[SULT ANIS LOAD LOAD LOAD .O NAaC L0c= iTPE C00E TTPE Unit TYPE n-A IS SET T-ANIS SET z-Ax!S SET O Q A178 O (CONTD.) 1.751 NORM o
Eilli12Y
.03 9 UPST
... 2 10RM
.02n UPST iilli M
.318 UPST O
.439 EMER .82D EMEP 333 EMER O .33 1 FLTDIM-9 .825 FLTDtM-) 319 FLTDtMal O
'O 179 179 SNCL T O FORC ELS) GLOS 1716.54 *F'.TD f M* 3 '
1716.11 EMER 17:6.11 UPST O,.
'O -151.99 NORM
-758.98 THMu
.Q -75P.98 THM1 Q
-98*.97 NORM
-2771.87 UPST Q -2771.C7 EMER Q1
-2771.55 FLTDEM-9
'Q DISP IINI GLOS .372 FLTDtM*3 .906 FLTDiM*3 .819 FLTDtM*) Q
.372 [MER .846 EMFR .[19 EMER
.299 UP%T .956 UPST 819 UPST O .269 inMu O
.*24 NORM
.G24 THM1
.O .nor THMu .1s9 n0RM 0
.0P2 THM1 . 110 THM1 l .003 NORM .354 THMU Q .831 UPST C;1 UPST .371 UPST @
. 03 1 EMER .P09 EMER .371 EMER
.831 FLTDtM-9 .OC9 FL10tM-) .372 FLTDtM-9 O O 4179 8179 SNUR 2
,'@ FORC (LB) GLOP 1290.11 FLTDtM+3 Q 1243.55 EMEP 1243 55 UPST
-1243.55 UPST Q
'@ -1243.55 LMER
-1290.11 FLTDiM-1 O O IO O e -.
e e "
-m - - c= - - -
'(p 1MPEt6 t/'"*m..stm *
./ c3 -.C 2.' . ,s f)* lj
'20SID4 164,1 r#91/83! STSTEQ IMPELL - NOS 04/93/233 11.1631S' S UPE R PI-V) i g
V V () PSC TRSJA3 NUCLECO STATION EDS PROGLcM s3ese1R-Re-si Scv.1 () PatsStairre SiRv t!Nr () AS-8UILT GEOMETRY WITH SLUS DIVER $!04 DCVICES 65003 () () SUPPORT LonD sUMMaRr tecNTD.s C) SUPP SUPP SUFe DIEN R E S bt T' RESULT AMIS Lead LOAD LSAD C) aaMc toca Tier cont Tve- UNIT TTec n-an:S Sri v-ants Scf 1-a:IS Sef () () AIT9 * ()- (CONTDel i DISP flN) GLOS .38 3 FLTDtMe) 1 839 FLTDtM*3 .9 FLTDtM*3
, C>
.3 3 <McR i.. , tMcR . . 99
. cMcR c>
- .3. UPST i.R , UPST
.27.2 ,MMU
- ..g. U,PST:U . ..
.2 N.R M
. 16T56 NORM
' (> iilli falf
. 85 1 UPST .924 UPST
?!Ill fil!
.334 UPST (r.
C) III IEII'" # III EEII'"~' III IEII'"-' C) I c588 c568 SNCL C) Y ~ FoRc tten slo 8 173T5.R3 FLTDiM*: () 17359.T5 EMER 17359.T5 UPST () 531.42 THM1 () SJ1 42 TMau
-99.18 NORM
() -634.68 NORM ()'
-1R889 54 UPST
-18089.54 [MER
() -19105.62 FLTDtM-9 () DI?' IIN) GL38 .3R 3 FLTDtM*3 .Pir FLTDtM*3 .122 FLTDtM*) () .3RR EPER .R19 [MER .115 EMER () l
.325 UPST .010 UPST .115 UPST l
.321 THMU .P99 THMU l
' () .896 NORM
.08T THM1 () I i .005 NOR M
.114 THPU
- () .146 THM1 ()
i .112 WORM .992 NORM
.122 UP4T .019 UPST .928 UPST
'() i e122 EMER
.124 FLTDtGa*
.C19
.518
[PER FLTDtM-3
.920 EMER
.026 FLTDfM-1
() jo 1 o i () () CJ C) O 0 ;
PASr 254 ,e Q i IMPELL CORP 088110N S UP:C?!PE TE;SleM 128e it#51/838 SYSTED IPPELL
- h0S e , 89/03/23s StelSel6e (C)
I () GGE TROJ43 huCLEER STATION () EDS PP08LEM (48*J1P-8C-81 RET.1 PRESSURIZER $/RV LINE () AS-8UILT GECMETRY ullH SLUG DlyER$10N DEt2CES 63003 d) () SUPPOR T LO AD SUMMART (CONTDel () SUPP SUPP SUPP DIRK RESULT RESULT Arts LOAD LOAD LOAD C) NAME LOCN TYPE CODE IVFE UNIT TYPE I- A NI S SES Y-4NIS SET Z-ARIS SET () () CLSA C5ua ShGL 2 () FORC tLLS GLOB 6984.43 FLTDiM*) 6466.56 EMER 6466 56 UPST C) () 278 76 THMU 173.28 NOR M [3 171 82 THM1 () 3 38 meRM
-371 97 THMU
() -6156 99 UPST C)
-6*56.99 EMER
-78T4.86 FLTDEM-9 DISP 61ND GLOM .384 FLTDEM*3 1.R84 FLican.3 .813 FLTDtMen
.342 EMER 1 888 EMER 912 EMER
[) .388 UPST 1 888 UPST .812 UPST ()
.298 THMH 1.865 THMU
- ) :lli VRAD I*III IIIA ()
.04 1 THM1
.04 3 NORM .882 NORM
() .e5s UPST .e19 UPST .St2 UPST ()
.45 6 rMEs .e:S EuER .8 2 EMER
.857 FLTDEM-9 .824 FLTDiM-l .813 FLTDtM-l SI
() SD31 SD31 $NUS of-() FORC (LB3 LOCL 107 t.9 0 FLTDEM*) () 966.47 EP[R 966 97 UPST () -966.97 UFST ()
-966.97 EMER
. -18 7D.9 8 FL70tM-9 FORC (LB3 GLOB 1*f6.f* FLTDEMel 174.33 FLTDtMel 954.87 FMEP 157.38 EMER
'[) 954.87 UPST 157.3R UPST ()
-954.97 UPST -157.38 UPST
-954 87 EMEp -157.38 EMER
() -1856.62 FLTDah-s -174.31 FLTDiM-1 () DISP (IND LOCL .332 FLTDEM*) 1 631 FLTDer.3 .371 FLTDtM.) C) () 1:> ()
- O O O
_ __ __ _ ._. __ __ _ m
Q 1MPELL ti e404 ' q rz.T 25) e Q y CUPERPIP! SION 1",Ao tr/01/838 SYSTE3 1MPELL = NOS 84#03/23,1116s13s('N ;- O PGE TP0JA3 NUCLEA3 STATICO O EDS PROBLEM 93taJ18-PC-01 REY.1 PRES $URIZER $1AW LINE O AS-euiti GEOMETRT vifw SLUG D1 TENSION DEVICES 4500, o Q SEPPORT LO AD SUMMART, (CCNTD.3 O SUPP SUPP SUPP D1RA p[$ ULT REtelf AN15 LOAD LOAD LOAD 9 NAME LCCN TYPE CODE TYPE UNIT TYPE X-ANIS SET Y-ARIS SET 2-A31S SET O Q S031 O (CONTD.8 .382 EPER 1 631 EMER .359 [MER
.233 THMU 1.631 UPST .359 UPST Q .229 UPST 1 61R THM1 .338 THNU O 1.618 THMU .364 THM1
.898 NORM 1 619 NORM .158 NORM Q .178 THMU O
.178 THM1
.1R6 NORM .006 NORM Q .198 UPST .514 UPST .941 UPST O
.194 FMER .014 EMER .041 EMER
.19 0 FLT0fM-9 .014 FLTDfM-) .852 FLTDtM-9 O O DISP EIN) GLOS .35 4 FLTDfM*3 1 631 FLTDtM*) .330 FLTDtM+)
.353 EPER 1.631 EMER .319 [ME R O .2s4 UPST 1 631 uPST .31, uPST O
. .244 THMU 1 618 THMI .287 THMU 1.618 THMU .198 THM1 Q .St9 NORM 1 618 !!OR M .186 NOR M O
.149 THPU
.14 9 THM1 0 .15T NORM .se4 n0R M O
.167 UPST .014 UPST .848 UPST
.167 [MER .014 EMER .948 ENER Q .169 FLTDtM-9 .014 FLTDtM-9 .951 FLTDtM-9 0
'Q 1614 181A SNGL N O FORC CLB) GLOB 5582.85 FLTDfMel s HHill Em
.16 NORM o
-127.16 T.1P 1 Q -127.32 NORM Q
-2 09.6 a THMU
-56*5.77 UPST
.Q -5615.77 FMrm O
-5642.15 FLTDEM-3
.Q DISP EIN) GLOB 86 4 FLTDtMel 915 p!TDtM*8 .514 FLTDiM*: O
. pop FMEP .915 FMER .010 EM[R
.
- na Upsi .915 UP%T .019 UPST Q O
- O . O IO O ,
I () - InsILL CORP 3aa TION PAGC #SS () % I $UPECPIPE VERSION 10A, 1f191/818 SYSTED IMPELL
- NOS 84/03/233 31 15 33
]) PSE YP0JAN NUCLE 02 STATION () '
EDS P900LEM 4380918-RC-F1 revel PsESSURIZER S#RV LINE () AS-8UILT GEOMETRY NITH SLUG DIVEPSION DEVICFS (SDD) () () $0PPORT LO AD SUMM ART (CCNTD.) () SUPP SUPP SUP P DIRh RESULT DESULT ANIS LOAD LOAD LOAD () NAME LOCN TYPE CODE TYPE UNIT TYPE N-ANIS SET Y-ANIS SET 7-ANIS SET () () talA 913 THM1 f) ' ('OMTD.3
.913 THMU
() .912 NORM ()
.9E3 NORM
.53G THM1
() ~.366 THMU ()
. 908 UPST .002 UPST e376 UPST
.t04 EMER .aP2 IMER .453 CMER
[) .088 FLTDEM-3 .aP2 FLTDtM-1 .453 FLTDtM-9 () FORC (LB) GLOS 1402 71 FLTDEMep 1385 37 EMEP 1395 37 UPST () I() 93 14 NORM 81 33 THM1 () 81 33 THMU () 11.85 NCRM , .
-907.63 THMU
() -1797.96 UPST ()
-1980 15 FMEP
~1987.4 9 FLTDEM-9 C) ()
- MOMT (LB.FT) ELOS 22915 43 FLTDiMe) 22912 24 EPEP
$) 22912 24 UPST ()
15 T f t .8 2 THM1 157P4.82 THMU [) 15615.73 NOPM ()
-89.09 NORM
-7385.60 UPST
[) -7385 66 [MER ()
-7188.79 FLTDEM-9
[) DISP GINS GLOS .094 FLTDtMel ()
.1f4 EPEP 304 UPST
[3 .)ct THMU ()
.049 UPST
. i t' 3 EMER q) ..eu? FLTDEM-9 ()
O O O g - g_. g 0 ;
' () PZ5C 2$F d) thPELL C ctION '
,/ ' e '3 SUPECPI RSION If Ae 10/01/838 SYSTE3 IMPELL - NOS ( 84/03/23e 11 16216:f i
'%) Gl
() P!E TC0JA7 NUCLEAR STATION ()' I' EOS PPD 8LEM G388018-RC-01 #EV.1 PRES $tRIZER S/RV LINE C) AS-8vItf GEOMEf ar v!Tu StuG D! VERSION DEv!CES (S005 c) , () STPPOR T LO AD
SUMMARY
(CONTDel () SUPP SUPP SUPP DIRA RESULT RESULT ANIS LOAD LOAD LOAD C) =AME LOCN TYP[ CODE TYPE UNIT TYPE I- ARI S SET Y-AXIS SET T-ARIS SET () () 182X () (CONTD.3 ROTN (RADI LOCL NESS,!GIBLE C) () 182Y 1824 SNGL Y () FORC (LP) GLOS 11893.24 FLTDtM*) () 11083.81 EMER 19564.88 UPST ' () 3312.21 THMU () !
- 2178.R3 THM1 2813.15 NORM c) -163.65 .NO,M ()
-7583.97 UPST
-7583.97 EMER
() -7584.20 FLTDtM-9 () MOMT (L8.FT) GLOS 238?.32 FLTDtM*) () 2246 99 EMER () 2286.99 UPST 16.81 NORM () -393 5m NORM ()
- -410.39 THM1
-658.44 THMU
")( -79L3.P2
-2903.82 UPST EMER
()
-2926 14 FLTDtM-9
() () DISP (IN) GLO8 944 FLTDtM*1
.0J4 EMER
() .0 14 UPST () 8.
.001 THMU
.Pe3 uPST l () .003 EMEP ()
.003 FLTDtM-9 Ii i () ROTN SPAD) LOCL NEGLIGIBLE ()
I 1822 1R2A
- NGL F d)
- () FORC EL81 GLOP 9587.81 FLTDEMel l) '( 9577.78 EM[P 9577.78 UPST () () () () () ,
3 IMPtLL CORPORAfl0N P?.GE 253 84 /83/23,11 10,13e () d SUPE.'Cist V['lS I ON 110e tr/81/833 SYSTEQ IMPELL - NOS i; [) P2C TROJA3 NUCLEIR STATION ESS P;0 BLED d3c;e18- C-81 CEO 1 () - PRESSURIl[R S/RV LINE [) AS-BUILT GE0METPY WITH SLUG DIVERSION DEVICES ISDDI (D [) SCPPCRT LOAD
SUMMARY
GCCNTD.3 () SUPP SUPP SUPP DInk RESULT R E SUL T ARIS LOAD LOAD LOAD 3 NAME LOCN TYPE CODE TYPE UNIT TYPE E-A NI S $[ T. T=ARIS SET Z-AMIS SET () ) 1822 () (CONTD.8 348.68 THMU 44.94 NORM h ) 43 75 THM1 () 1 19 NORM
-98.32 THMU
) -9525.44 UPST ()
-9525.84 EMER
-9535.87 FL104M-3
) () MOMT ELB.Fil GLOS 6816 13 FLTDtMel 6897 16 EMER ) 5813.28 UPST 3721.23 THMU () 2898 89 NORM 3 2888.89 THM1 () 6 10.88 NORM i
-2878.45 UPST i
) -2878.45 EMER
-2879 42 FLTDtM-1
() ) DISP (INI GLOS .804
.004 FLTDEM*3 EMER
()
.004 UPST
) 001 THMU ()
.803 UPST
.003 EMER 3 .r&5 FLTDtM-9 ()
ROTN (RAD) LOCL NEGLIGIBLE 3 () 182 182 SNGL Y Q FORC GL83 GLOS 43e.33 FLTDtM*) * () 432 59 EMER 432.59 UpST () -144.17 N0*M ()
-1357.34 THP1
-1501 51 NCAM
() -165?.07 T H MU ()
-2?pL.01 UPST
-2376.31 EMER
() -2371 73 FLTDEM-) () () () e 9 _ __ 9 O _.
~ - -
Q I Met ts. .ssON rist 291 p' y id S UFC'J JI RSION 153, Ett;11838 SYSTEQ IMPELL - NOS 84/93/23* 11 10.10d I r () PSE TROJA3 NUCLEAR STATION () EDS PRDPLFN 03AR11R-RC-FI revel PRESSURIFER S/RV LINE , () AS-8UILY GEOMETRY WITH SLUG DIVERSION DEVICES (SDD) () ' () SUPPORT LOAD
SUMMARY
(CONTD.3 () i SUPP SUPP SUPP OIRR RESULT RESULT ARIS LOAD LOAD LDAD l () NAME LOCN TYPE CODE TTFE UNIT TYPE I-AXIS SET Y= AMIS SET 2-ARIS SET l$ l u l () 182 () (CONTD.) DISP tint GLOM .183 FLTDtM.I .818 FLT0tM+l ^ q)
- .cs3 EMER . ele EMER CD
.993 UPST .919 UPST
.082 TMMI .937 NORM l ()
.te3 NORM .937 THM1 ()
.4t3 THMU .355 THMU
. .ee. UPST .see uPST .36. UPST
- C) .es4 EMER .es. EMER .43, EMER C)
.884 FLTDiM-l .984 FLTDtM-9 .439 FLT0tM-1
() () 188V 188 CONF T I FORC EL83 GLOS -173.23 EMER ' () -173 23 EMER ()
-175 23 FLTD
-173.23 FLTD
() l -173.23 WORM I () I
-173.23 NORM
-173 23 UPST t
I() -173.23 UPSTEM-9 () DISP (IN) GLOS .336 FLTDtM*) .203 FLTDtM*9 .132 FLT0fM*) l () .336 EPEP .203 EMER .125 EMER ()
.26 0 UPST .491 UPST .325 UPST l .203 THMU .955 THMU .965 THMU l () .824 N0*M .9P9 THMS .032 THM1 ()
+
! .R2 3 TI:M1 .9P9 NORM .539 NORM
.ect NORM
() *
*. 65 6 UPST .036 UPST .963 UPST ()
. Y16 EMER .836 EMER .063 EMER
.556 FLTDtM-9 s.R36 FLTDiM-3 .470 FLTDfM-1 l C) ()
1 192 192 SNUM Y < () f () FDPC (LMS CL OM tee 21 0* FLTDiM.9 s 13923.9R [M[R 1TG20.9A UPST
] () -1*025.9P UPST ()
~1*L2*.9R [*[e
-16c21.n9 FLTDEM-3 DISP (INI GLOM .333 FLTDtMel .!T* FLTDEM.9 .313 FLTDtM*)
O
~
4 in O 3
Q I M*[LL CORPORT. TION CASE 220 () - S UPE; PIPE VE R $ lost 164, 13/01#;38 SYSTED IMPELL - NOS 34#33/23 11e!6s162 , } PGE T;0JA'J NUCLEA) STOTION O , EDS PRORLEM J303018-RC-01 CEV.1 PRES $URIZER S/RV LINE Q AS-ButLT GEOMETRY UITH SLUG DIVERf 34 DEVICES 65003 $ SUPPORT Lead SUMMART (CCNTD.3 O Q . SUPP SUPP SUPP DIRK p[SULT RESULT ARIS LOAD LOAD LOAD NAME LOCN TYPE CODE TYPE UNIT TTPE TRIS S[i T-ARIS $[T Z-ARIS SET O Q Q 192 O (CONTD.3 .333 [MER .175 [m[R .195 [MER
.231 UPST .542 U*ST .165 UPST Q .298 THMU .R94 THM1 .376 THMU C
.82 6 NORM .084 THMU .357 THM1
.82 6 THM1 .993 404M 855 NOR M Q - .301 NORM O
.011 THMU .002 NORM
.92 2 UPST .051 UPST e833 UPST Q .122 [MER .851 [MER .R33 [MER O
.92 2 FLTDtM-9 .051 FLTDEM-3 .839 FLTDtM-9 O O 198 190 SNUS X FORC (LB3 GLOB 9793 27 FLTDER*3
-] 97*2.23 FMER Q 9702.23 UPST
-9742 23 UPST Q -9702 23 EMER O
-9703.27 FLTDtM-9 Q DISP tlN3 GLOS .401 FLTDiM*3 .384 FLTDEM*7 .145 FLTDEM*3 0
.491 FM[# .304 [MER .133 [MER
.313 UPST .146 UPST .133 UPST
.258 THMU .109 THMU .965 THMU Q Q - .t38 NORM .016 THM1 .336 THM1
.42 9 THM1 .915 NORP .034 NORM O .Ost NORM Q
.954 UPST .038 UPST .57R UPST
.054 [MER .038 EMER .870 [MER
.t54 FLTDtM-9 .938 FLTDip-3 .833 FLTDEM-3 Q Q
194 tot SMus 2 Q 3 FORC (Let Glos 761 56 FLTDEM*3 705.7R [MER Q 705.79 UPST Q
-705.70 UPST
' -705.78 [MER Q -761 56 FLTDtM-3 Q DISP (INI GLOS .22 7 FLTDfM.3 .235 FLTDip.3 .987 FLTDIM*3
() .227 [FEP .235 [MER .006 [MER Q O 3 _ e _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ e e
- - - mm e- ee w m---. .- - - _ -
Q IMPELL C 3110m eg rats. 26 h Q g S UPEtPIP SIDs l' A. 1sistis3 SYSTEa IMPELt. - m05 ( sess3r23 11 10.10e( p ) Q PSE T 'CJA"3 ffUCLE A2 ST ATI:o O EOS PRO 6LEM "3se119-RC-a1 REY.1 PRES $URIZER SrRV LINE O As-eUitt sEOMETRv viin Stus 0 VERS 0N DEv CES 45005 e O SurreRT t0A0 SuMMARv (CONTO.B O SUPP SUPP St'PP OIRN RESULT R Et t'LT ARIS LOAO L940 LOAO Q NAME LOCN TYPE CODE TYPE UNIT TVPE W-Ast S SET V-ARIS SET 2-ARIS SET O O 194 O 4 CONTO.) .175 UPST .100 UPST .486 UPST
.1SS THMU 964 THMU .001 TMMU Q . 31 7 THMt .330 THM1 .865 THM1 O
.41 7 NOR M .*09 No#M .964 te0R M
.002 ls0A M O .stl UPST .s3e UPsf .see UPST O
.02 1 EMER .P3R EMER .800 EMER
. 02 1 FLT0tM-9 .038 FLT0tM-9 .999 FLT0tM-9 195V 195 CONF Y
- F0pc (LB5 CLOS -239.31 EMER
'O -23a.31 EMER O
. -23f.31 FLTO
, -230.31 FLTD
- Q -23e.51 =0AM O,
-239.31 NORM g i
-23f.31 UPST lQ -23R.31 UrsitM-9 Ol i
.594 FLTOEM*) .173 FLT0tM*)
O DISP (INI GLOS .06 2 FLiotMel
. 96 2 EMER .599 EMER .16e EMER Ol
.e5 R UPST .334 UPST .130 UPST
.933 THMU .321 TMPU .996 THMU iQ
~
.383 THM1 .846 THM1 .086 THM1 O
.n33 NOPM .046 NORM .505 NORM
.001 WORM O
.9t t UPST .913 UPST .044 UPST Q .t17 EPER .P33 EMER .966 ENER
.t17 FLT0tM-9 .033 FLT0tM-9 .819 FLietM-9
- O O' 196 196 $ NGL E
!O FORC (LB) GLOS 12RP2 65 FLT0tM*) O 12983.33 EMER ', 12 r 96.8 7 UPST l 845.17 THMU Q lQ 1
-21 64 W0eM
-373.21 THkU
*T3.21 THP1 O
'IQ -194.8F fl0 R M
-lI 669.2 P UP'T iO O
!O O
~
O !O
() I MPELL CDR^0R ATION ' PAGE 222 84#33/23a 11 16336s () $ SUPECPIPE VERSION 10Ae if/81/033 STST[3 IMPCLL - NOS
]) PCE YpoJA3 NUCLECW STATION (}
[DS PR08L[M B343818-AC-91 REV.1 PRESSURIFER S#RV LINE () AS-8UILT GEOMETRY WITH SLUS DIVER $10W DEVICES (SDD) () () SUPPOR T LO AD SUMM ART (CCNTDel () SUPP SUPP SUPP DIP N RESULT R[SULT ANIS LOAD LOAD LOAD () NAME LCCN TYPE CODE TYPE UNIT TYPE N-AXIS $[T Y-ARIS SET 2-ARIS SET () () 196 () (CONTO.8 -11668 20 [MER
-11670.52 FLTDIM-9 DISP (IN) GLOS . 82 4 FLTDtM.) .666 FLTDfM.) .196 FLT0tM*)
.F2 P [m[R .666 [MER .379 [MER
() .819 UPST .399 UPST .354 UPST * ()
.581 THMU .3A4 THmu .100 THMU
.*56 THM1 .892 THM1
() .e5s NORM .s91 NORM C)
.991 NORM
.DI R UPST .816 UPST .052 UPST
() . 01 R [MER .434 [MER .C81 [MER ()
.C18 FLTDfM-9 .034 FLTDfM-3 .398 FLTDtM-3 C)
() 268R 239 SNGL N FORC (L83 GLOS . (M*3
}
5318 15 THMU 4869.22 THM1 () 4862.95 NORM ()
-0.27 NOFM
-1174.01 UPST
() -12282 98 [PER ()
-12 37 L .61 FLTDtM-9
() MOMT (LB.Fil GLOB 3 05 P2.4 2 FL'DEM*3 () 24854.39 [MER 17977 26 UPST () 6571.4* THMU () 4878.3R THP1 4833.54 NOPM () -44.n. NORM ()
-1149%.3P UPST
-17 4 2 p .5 3 [PfA
() -23076 56 FLTDtM-9 () DISP (INI CLOP 30% FLIDEM.) .031 FLTDiM+) () er95 [MER .*11 [MER ()
.252 Ur$T .[*6 UPST
.PGP THMU .002 THMU
() SI CD (3 9 - -. - - 9 S -
m _ m m -m
'O PA:E 263 % ;- Q pl Q ATIO4
- IMPELL C SUPE! PIP R SI L'N 16As II/91/03 SYSTEQ IMPELL - 20s e ! e4/e3/23 11 16 16. >'-
Q PGE TROJAN NUCLEA3 STATION Q EDS PROBLEM 6388?P19-RC-P1 REV.1 PRESSURIFER $1RV LINE O AS-RUILT GIOMEIRY NITH SLUG 01 VERSION DEVICES (5003 O O SUPPORT LO AO
SUMMARY
(C ON TO . ) O SUPP SUPP SUPP OIR N RESULT R EMtfL T AVIS LOAO LOAD LSAO
@ NAME LOCN TYPE CODE TTPE UNIT TYPE, E-ABIS SET Y-Atl5 SET 2=ARIS SET O O 2 *R O (CONio.9 .Rt1 TMP1 891 THM1
.891 NORM Q .005 UPST O
.48 4 F*FP .4P9 EPER
.004 FLTOtM-9 .509 FLT0fM-9 ROTN (RAO) LOCL WESLIttBLE o 298Y 2G8 $ NGL Y O
F OP. C (LBt Glos 46646 76 FLT0tM*3 " O , 465R8 13 EMER O 24211.55 UPST P415 11 THMU l Q 4661.?9 THM1 0 2031.91 NORM
-2635 93 NORM Q . -2106T.29 UPST O
-413R2.1M EMER
-414s8.94 FLTOtM-l O O MOMT tLB.Fil GLOS s213.TP FLT0tMel 6813.61 EMER Q 4242.41 UPST O
- 193D.19 NORM 999 62 THM1 Q 999.67 THPU O 38.51 NORM
, -524.34 THMU
- Q -3fA6.55 DPST O I -1317.53 EMEP
-R437.61 FLT0tM-9 EISP tlND CLOS err 5 FLTO4M*l .011 FLTOtP*l
.tp5 FMER .011 EMER i
*Q
.CO2 UPST . pts UPST O'
.'f2 THMit .402 THMU
! .f31 TDh'l 801 Thal lD .P41 N0pM Q
.0 % UPST l'
.f34 EMER .609 EMER Q .F34 FLT04P-l .nt9 FLTOtM-9 O O . O O O ,
[) IMPELL CORP: RATION PAGE 2:4 ($) q SUPE; PIPE VERSION 10Ae 1C/01/838 SYSTFQ IMPELL - NOS 44/03/233 11 10 16, ' () PGE T[0JA3 NUCLEAR STST10N (}} > [DS P00eLEM 6300818-RC-C1 REY.1 PRES $URIZER S/RV LINE [) AS-EUILT GEOMETRY WITH SLUG DIVERSION DEVICES ($003 d) [) SUPPORT LOAD SUMMART (CCNTO.3 () SUPP SUPP SUPP OIPk RESuti R[tDLT ANIS LOAO LOAD LOAD [) NAME LOCN TYPE CODE TYPE UNIT TYPE X-AMIS SET T= AMIS SET Z-AMIS $[T () [) 2887 () (CONTD.) NEGLIGISLE I ROTN (RA03 LOCL [4 () ! 2087 2W8 SNGL 7 [) FORC (LP) GLOS 6575.72 FLTDtM.) ()l' I 5398 67 EMER l 2996.58 UPST () 71 98
~6731.39 NORM NOPM
().li
-6803.29 THMU
[) -6833.29 THM1 (> l*
-9655.99 UPST
-12858 16 EMER
[) -13235 22 FLTDEM-9 Ck P0MT ELB.Fil GLCE 49348.86 FLTDtM*3 [) 46821.01 EMER () 22403.37 UPST 13664.68 THMU () ' 1127.97 NORM () 1073.63 THP1 54 34 NORM UPST () -8638.68
-25066 29 EMER C)
-27589.14 FLTDiM-3
() () DISP (IN) GLOP .a0% FLTotM*) .811 FLT0tM*3
.005 EPER .011 EMER
() .002 UPST .ar6 CPST ()
.C92 THMu .002 TMMU
.nS1 THM1 .091 THP1
() .041 h0PM ()
. .00% UFST
.na4 EPER . n r.e Erte
() . 084 FLTO(M-3 .ine FLTDIM-1 () ROTN E4401 LOCL NEGLIGIBLE () NN () CD () CD n O
- - .. m m m === - -
'Q IMPELL Cf 7 4IION rceC 263 34/05/23s II.36 36r p) M l S UPERPIP \ /,PSION tcAo 18/P1/838 SYSTE3 IMPELL - NOS ' #
\
% d l
.) - rsE TE0JA3 NUCLEA2 STATION EDS P900LEM n30gste-RC-91 REV.1 () PRESSURIZER S/RV LINE ' () AS-SUILT GEONETRY UITH SLUG OIVERSION DEVICES (SODS (D J [ () SgPPORT LO AD
SUMMARY
(C ONTD e l (D SUPP SUPP SUPP OIRE RESULT RES ULT ARIS LOAD LOAD LOAO () NAME LOC N TVPE C 00 E TTPE UNIT TYPE N* ANIS SEY T-ARIS SET ~ 2-ARIS SET (D I () - 215V 215 CONF Y (I FORC (L83 GLOS -7R7.86 EMER
-787.06 EMER
- C) -787 85 FL78 CD
-787.96 FLTD
-787.86 NORM C) -Taf.e6 =0RM ()
-797.t6 UPST
-747.06 UPSitM-9
() () DISP (INI GL OC .473 FLTDtM*1 .897 FLTDtM*) .528 FLT0tM*3
.473 EPER , .n95 EMER .391 EMER
() .237 Up%T ^
- .519 U*ST .283 UPST ()
.22 3 THMU .935 THNU
.83r THP1 .614 THM1
() . 03 8 NORM .914 NORM s, ()
.099 THM1 l
.999 WORM C) .**3 TMMU CF
.01 5 UPST .662 UPST .249 UPST -
. B9 4 EMER *1.129 EMER .356 EMER
, ()._ + -
- .094 FLTDtM-9 -1.122 FLTDtM*) .485 FLTDiM-9 () '
() 5214 213a SNus e-E , () F0hc ILB) LOCL 251 AP.17 FLTDtM*9 ; 24634.97 EMER C) 4*T6 9* UPsf ()
-4476 94 UPST '
-24f 34.9 7 EMER
() =25162 17 FL'DtM-9 () FORC GLPt GLO8 22615.61 FLTDEM*l 1103r.37 FLTDtM*3 (') 22141 77 EMER If799.26 EPER () 4 r23.8 4 U*ST 1962.56 UPST
-4973.84 UPST -1962.56 UPST
() -22141 77 FPE# -19799 26 EPER * ()
=22615 61 F (,T D t M- 9 -11638.37 FLTDtM-3
() DISP (INI LOCL 1.334 FLTDtP*1' .152 FLTDtM*3 .098 FLT0tM*) () 1.334 FPfP .191 EMER .675 E ME R
.813 UPST .?23 UPST .5P9 UPST
, () _. .804 THMU *
.378 THMU ()
s O ~- O,'
o PAGE 266 (3) J I MPELL CDRPOR ATIO] SUPERPIPE VERSION !?A, If/01/838 ST3f[Q IMPELL - NOS 30/03/23s 11 13 16. o PGE TROJA3 NUCLEA2 STATIE3 () EDS PROBLEM 439801R-RC-01 REV.1 PRES $URI2[A S/RV LINE AS-BUILT GEOMETPV UITH SLUG DIVERSION DEVICES (SDDS C) (D {D SEPPORT LO AD
SUMMARY
(CCNTD.) () SUPP SUPP SUPP DIRN RESULT RESULT ANIS LOAD LOAD
) NAME LOCN TYPE CODE TYPE UNIT TYPE I-ANIS ' LOAD SET Y-AXIS * $[1 7-AXIS SET ()
o 5214 () GCONTD.) .125 NORM .528 THM1
.124 THM1 *.001 WORM .920 NORM (D
.134 THM1 ()
.135 NORM
.812 THPU
.00 7 UPST .837 UPST .423 UPST C)
{) .04 2 EMER -1.413 EMER .5 96 EMER
.94 3 FLTDtM-9 -1 413 FLTDiM-9 .819 FLTDiM-l DIS * (IN9 GLOB .71 4 FLTDEM*) .355 FLTDfM*i .898 FLTDEM*)
.71 3 FMrs .154 EMER .675 EMER
[) .38 4 UPST .023 .UPST .500 UPST () I .36 7 THMU .378 THMU f .85 3 NORM .929 THM1 [) .053 THM1 =.9P2 NORM .923 NORM ()
.175 THM1
.176 NORM C>
-1.es2 THMU ()
1 .R17 UPST ~1 108 UPST .423 UPST f .185 EMER *1.R54 EMER .596 EMER
.186 FLTDiM-9 -14455 FLTDEM-l .819 FLTDEM-9 C)
() () V68V V60 HANG V () FORC (LM) GLOS -612.95 EMER
-612.95 EMER '
() -612.9% FLTD ()
-612.95 FLTD
-612.95 NORM
() -612.e5 NORM ()
-412.95 UPST
~612.95 UPSTfMal DISP (INI GLOS .563 FLTDfM.) 2.364 FLTDfM.) .489 FLTDiMel
.553 FMER 2 356 EMEP .244 EMER
()
.55 0 UPST 2.356 UPST .244 UPST ()
.4T3 MU 2 327 THMU
.231 T(0n N N 2.S24 THM1
*) .224 THMS 2.924 NORM .R04 NORM ()
.L93 NORM .187 THM1
.191 NORM
() .433 THPU () C3
*) .
o O O O ,
**===- - - memen a.--- sm- -. - am. - m _
gg. f () ratt 26) IMPELL CC' 1ATIC3 S UPE RPIP; ,,,R$102 1sA. 1s/sti 38 SYSTED InPELL - NOS )s a3103/23 11 16 16.(gN) ' () PSE TROJAU WWCLEA2 STAfl03 () > [0S PRO 9LEM P30*e19-RC-81 mEtt.1 PRES $tRIZER S/RV LINE
, ()
AS-8UILT GEOMETRY WITH SLUG LIVERSION DEVICES (S001 GD () SU7 PORT LOAD
SUMMARY
(C ONTD e l () SUPP SUPP SUPP DIR N R ESUL T R ESULT AEls LOAD LOAD LOAD () NAME LOCN TYPE CODE TYPE UNIT TYPE R-ANIS SEP Y*Att$ SET Z-ARIS SET () , () v6sv CD ICONTD.) .371 UPST *.829 UPST .6R5 UPST
.971 EMER .829 [MER .685 EMER
! () . 68 4 FLTDtM-1 .037 FLTDtM-3 .RSS FLT0tM-3 () l C) vis v7e SNus --* CD FORC (L89 LOCL 3987.17 FLTDtM*) 2407.31 EMER () { () 2407 31 UPST
-2407.31 UPST
-24*7 31 FMEp
' ()
-1987.17 FLTDtM-l ()
FORC ILB) GLOS 807 48 FLTDtM*3 322 6P FLTDEM*3 3891 19 FLTOtMet ! () 487.53 EME* 194.R2 EMER 2349 36 EMER CD
- 487.53 UPST 194.R2 UPST 2349.36 UPST
-487.53 UPST -194.92 UPST ~2349.36 UPST
. () -407.53 EMER -194.R? EMER -2349.36 EMER ()
-P 47.4 R FLTDtM-9 -322.68 FLTDtM-) -3093 19 FLT0tM-1 l () DISP (INI LOCL .918 FLTDfM*) 3.89A FLTDtM*) .227 FLT00Mel ()
. ee 9 FMER 3 894 EPER .201 EMER 409 UpST 3 994 UPST .281 UPST 3 987 THMU .148 THMU CD
- () 2.477 THM1
. ee 6 n0RM 2 477 n0RM
.165 THMU Ep
- () .2r e innt
.2C6 MOPM .165 THM1
. 296 THMU .165 NORM UPST .219 UPST C)
() .31 7 UPST
.31 7 EMER
.008
.P9A EMER .239 EMER
.326 FLTDtM-) .P12 FLTDEM-9 .245 FLT0tM-)
DISP IINI CLOG .24 5 FLTDtM*) 3 107 FLTDfP*) .079 FLT0tM.3
.21 8 EMER 3 193 EMEP .564 EMER
() . 21
- UPST 3 1n3 UPST .064 UPST C)
.163 M0 M 3.995 THPU .945 THMU
.162 fp i 2 4R% THP1 035 THM1 l () .162 THMU 2 4P5 NOP M 92? NOR M ()
.tn1 NOPM
.ees NonM C) t*" '""" .G42 THMU ()
() () O O
Q ICPELL CORPOP Afl03 SUPERPIPE VER$104 ItA, 16/01/R34 SYSTEC IMPELL - NOS PAGE 268 80/83/23, 11 1633.6 () p 'Q FGC Tp?JA3 NUCLEAR STATION O l EDS PRORLEM (Spaegg.sc-C1 REV.1 l PRESSLAIZER S/RV LINE Q AS*8UILT GEOMETRY UITH SLUG DIVERSION DEVICES (SDDI O Q SUPPORT LOAD
SUMMARY
(CCNTD.9 O SUPP SUPP SUPP DIRK RESULT RESULT arts LOAD LOAD LOAD Q NAME LOCN TYPE CODE TYPE UNIT TVPE R-AEIS SET Y-ARIS $[T 2-ARIS SET O I 'O V78 O (CONTD.) .203 UPST .008 UPST .873 UPST
.293 EMER . rep EMES .4T3 EMER
'O 23 8 FLTDfM-9 .812 FLTDtM-9 .888 FLTDEM-9 0 Q V7C VTC HANG Y O FORC (L88 GLOS -5F8.91 EME4
-588.91 EME3 Q -5P8.91 FLTD O
-588.91 FLTD
-588 41 NORM
@ -5e8.91 . NORM O
-Sne.91 UPST
-588.91 UPSitM-9 DISP (IN) GLOB .331 FLTDIM+l 3 187 FLTDtM*) .867 FLTDEM*)
.595 EMER 3 1P3 EMER .837 EMER Q .385 UPST 3 183 USST .437 UPST O
.24 T NORM 3.895 THMU
.24 4 THM1 2 485 THM1
.Q .24 4 THMU 2.4R5 NORM .811 NORM Q
.083 NORM .861 THM1
.472 NORM
'O .03 8 THMU .215 THMU O
.893 UPST .00m UPST .214 UPST
.89 3 EMER .59R EMER .274 EMER Q .12 0 FLTDEM-9 .011 FLTDEM-9 .384 FLTDIMal Q~
O v88 v8e SNuo 7 0 FORC (LB) GLOB 1416.47 FLTDtM+3 881 69 EMER O 881 69 UPST Q
-881.69 UPST
-881 69 EMER Q -1416 47 FLTDtM-9 Q DISP (IND GLO- .330 FLYDiM*) 2 568 FLTDtMel 427 FLTDEMel Q .32s FMED 2 566 EMER .824 [MER Q
.326 UPST 2.566 UPST .024 UPST
.3ue THMU 2.556 THMU .822 THM1
,Q .194 THM1 2 297 THM1 .022 THMU Q G O O
g _ _ g _ . - _ _ _ _ ._ _ O
Q IMPELL C IICQ (~N PXE 269 r- Q h{
$103 164. I f/01/838 SYSTEn IMPELL - N09 34#93/23s i
- S flPE
- P IP PG[ 10!JA3 NUCLEAR STATIO3 e (
O) 11 16 13N l )N () () EDS PR0eLEM 93tf018-RC-Ol REV.1 PRES $b4IFER S/RV LINE () AS-BUILI GCOMETRY WITH SLUG DIVERSION DEVICES 45003 ($ () SUPPORT LOAD
SUMMARY
(CCNTDel () SUPP SUPP SUPP DIRh RE% ULT R E S UL T ANIS LOAD LOAD LOAD () NAME LOCN TYPE CODE TYPE UNIT TYPE X-ANIS SET Y= ANIS SET 2-AII3 SET f) () V80 () (CONID.) .100 NORM 2 294 NORM .519 NORM
.814 NOPM .983 NORM
() .11 A THPU .083 NORM .268 THMU ()
.145 UPST .015 UPST .268 UPST c, ::184 ft%5 M-l ::lli FtfB.M-9 ::itt Ftf8eM-9 c),
LS LS ANCH GLOP (@ FORC (L89 GL OS 155708.81 FLTDEM*) 85897.3R FLTDfM*) 194685.83 FLTDiM*) () 94126 64 EMER 66374.67 EMER 116841 67 EMER 9399P.40 UPST 41147.93 UPST 116398.92 UPST () 1983.25 1639.37 THMU NORM 497.86 NORM () i i 1623 55 THP1 -71 45 NORM ! () 17.42 NORM -?643.6m NORM -6127.75 THM1 () j
-4141.64 THPU -6199.20 NORM -
-4141 64 TMP1 -73e7 92 TdMU
() -91971 50 UPST =44293 66 UPST -123643 79 UPST () lg
-92737.44 EMER -6952P.39 EMER ~124757.32 EMEP
-154311 61 FLTDiM-1 -88992.91 FLTDfM-9 -282681 48 FLT0tM-9 CD () l M0MT fLB.Fil GLOS 347569 69 FLTDiM*) 4a34.13 FLTDEM*) 49P190 91 FLTDtMel 269972 65 FPER 2918.3R EMER 294658.99 EMER Q) 286*31 39 UPRT 2248 15 UPST 292026.19 UPST () h 216.32 THMU 115.R3 N ORit
() -261.73 NORM 101.C5 THM1 -56.77 NORM ()
-1255*.93 THM1 14.78 NORM -5637.83 THM1
-12R21 67 NORM ~5694.69 NOMM
, C) -15144.04 THMU -320.06 THMU -7016 85 THMU ()
-22259R.9C UPST -2322.33 UPST -299155 79 UPST
-227168.0P FMER -9349 30 EMER =29950R.95 EMER l() -364757.12 FLTD(M-l -5464.75 FLTDiMai -49504P.08 FLTDtM-9 ()
DISP (INI GLOS NEGLISIBLE () () ROTN tRADS GLOP 'NEGLIGISLE () () C) L) LD L) () C)
h I MPELL CORPOR A T 103 S UPE RPIPE VERSION 164,if/81/898 SYSTED IMPELL - NOS , PAIE 2TO 84/83/23s 11e13e16e () H }) PGE TROJ13 NUCLEAR STATIO3 . () l EDS PLOBLEO 6360018-RC=C1 REV.1 PaES$URI7[R S/RV LINE y) AS-BUILT GE0MEIRV WITH SLUG DIVE 4510N DEVICES ($003 () j) SUPPORT LO AD
SUMMARY
(CCNTDel () SUPP SUPP SUPP DIRN R E SULT RESULT AXIS LOAD . LOAD LOAD
- 5) NAME LOCN ITPE CODE TYPE 04tf TYPE X-ARIS SEL T-ANIS SET 2-AXIS SET ()
- 5) USN M3 $NGt I ()
FORC ELSI GLOS 319f f 6.4 5 FLTDEM+) 192122.21 EMEP
- 5) 190655.23 UPST ()
-43.03 NORM
-3300 92 THM1
- 5) -9343.95 NORM ()
-3888.68 THuu
-194629.96 UPET -
9 -194e92.s1 EMER ()
-322547.05 FLTDEM-9 j) MOMT ELB.FT) GLOS NEGLIGISLE ()
DISP (INI GLOS .09% FLTDEM*) 1 35R FLTD4M*) .817 FLTD(Mel j) .003 EPER 1.35T EMER .011 EMER ()
.843 UPST 1 357 UPST eG10 UPST 1 357 THMU jD 1 298 NOPM () ,
1 29R THM1
.R03 UPST .019 UPST
- 5) .es3 EPER .ste EMER ()
.08 5 FLTDtM-9 .0R1 FLTDtM-1 .017 FLTDEM-3
}} ROTN tRAD) LCEL . NEGLIGISLE (). FOPC ELM) GLOB 459883.67 FLTDEM.)
- l 282095.54 EMER ,
}9 284021 61 UPST () 14236.21 THMu 12568.92 NORM }) 12529.49 THM1 () ' 39.43 NORM
-265706.54 UPST
}Q
-266534.61 EMER ()
-444242.T4 FLTDtM-) i s
}} POPT ELM.FT) GLOM NEGLIGIBLE () DISP (INI GLOB .Pim FLTDEM.) 1 358 FLTDtM.) .617 FLTDER*3 () .co3 Ente 1.35T EMtR .o11 EMER () () () O -. - --. .-. O- . - - - . - - O
-= == - -- - ~~
-Q ! MPELL Ctr^g A T ION SUPERPIP R$104 16Ao IC#ft#838 SYSTEQ IMPELL = NOS O ( PAGE 271 81/93/23a 11e16el&. Q.
'Q PSE TCOJAD CUCLEAR STATIE3 O EOS PR09LEM 030981R-RC-01 REV.1 PR ES S UR IZER URV LINE ,
O AS* BUILT GE0METpf v!TH SLUG DIVERSION DEVICES (SODI O
@ S UPPOR T LO AD SUMMART (CCNTOel O SUPP SUPP SUPP DIP N RESULT R ES ULT ANIS LOAD LOAD LOAD @ NAME LOCN TYPE CODE TYPE UNIT TYPE X-ARIS SET Y-ANIS SET 2-AK!S SET O
- G ' USz O (CONTD.9 .903 UPST 1 357 UPS? .318 UPST .
1 357 THMU O 1.29R NORM O 1 298 THM1
.983 UPST .019 UPST o .es3 rMEp
.995 FLTDEM-9 .901 FLTDfM-9
.ste EMER
.017 FLTDEM-9 O'
0 ROTa (RAol LOCL NEstisI8t[ O .Q UST M3 $ NGL Y Q FORC (LB) GLOS NEGLI61BLE Q MOMT SLM.FTl GLOS E1917 62 FLTDtM*l 0 151*0.94 EMER 11694.R1 UPST
@ 199F.18 THPu O 571.*2 NORM 494.72 THM1 .
Q 77 21 NORM O
-1 E3 3. 28 THMU
-120P9.58 UPST O -22451.*a EMER O
-2R279 28 FLT0fM-9 Q DISP tlND GLOS .505 FLTDfM*) 1 35R FLTDtM*) 317 FLYotMel O 433 EMER 1 357 EMEP .031 EMER
. u.13 UPSf 1 357 UPST .319 UPST Q 1.357 THMU O 1 29p NORM .
1.298 THMI ! o ..ses UPsf
..nt3 EMER
.ste UPST
.010 EMER o
.005 FLTDtM-9 .fal FLTDtM-l .817 FLT0fM-9 ROTN (PAD) L'O C L 'NESLIGIBLE Q O O O O O O O
PAGE 272 (5) () IMPELL CORPOR Afi13 SCPERPIPE VERS 103 16A, If/01/838 3YSTEM IMPELL = NOS 8's/43/23s 11 16:16e
- 2) PGE TROJA% NUCLEAR #TATIO] ()
[0S PP0BLEM 433031R-RC-01 REV.% PRESSDR12[P %#RV LINE () AG-8UILT GEOMETRT UITH SLUG DIVERSION DEVICFS (SDOS () () SUPPORT LO AD
SUMMARY
(C ONTO . 3 () SUPP SUPP SUPP DIP k RESULT RESULT AWIS LOAD LOAD LOAD [) NAME LOCN TYPE CODE TYPE UNIT TYPE N- A RI S SET Y-ARIS SET 2-ARIS SET C) () 202 2 82 $4GL I () l FORC (LOS GLOS 23759.5# FLTDEM*) I' 23746.95 EPER () 1203.84 UPST f) ' 36 91 NORM
-3194.31 NORM 8
() -3231 12 THM1 f)
-4745.55 THPU
-5873 78 UPST
() -29693.66 EM[a ()
-297C6 2M FLTDtM-3
() DISP (INS GLO8 .017 PLTDiM*3 .225 .FL10tM*3
.055 FLTDtM*) () ;
.03 7 EMER .225 [MER .853 EMER 002 UPST .143 UPST .838 UPST
() .136 THMU .627 THM1 () 023 THMS .927 THMU
.822 NORM .827 NORM
() .005 N0*M ()
.005 THM1
.007 THMU
() .csa UPST .e0R uPST .s 2 uPST ()
.94 7 EMER .01R EMER .027 EMER
.04 7 FLTDEM-9 .018 FLT0tM-3 .028 FLTotM-9 C) ()
205 205 SNGL 7 () FORC (L8) GLOB IR098.42 FLTDEM*) () , 17759.36 EMER a4:6.45 uPSr () 6484 16 THMU () 6449.17 THM1 6364.35 NORM () -84 82 NORM ()
-3181 94 UPST
-Il444.R5 EMER
' () -11775 91 FLTDtM-3 () DISP (IMI GLOB .C2C F L'T D E M + 3 .9*1 FLTDtM*3 .414 FLTDtMel () 82 P [MER .r91 EMER .014 EMER ()
.042 UP'T .057 UPST .007 UPST 002 t:0P M .952 THMU .005 THMU
() .is" THM1 .912 THMI .805 THM1 () O O O O O
a - yg
~
race 21a Q IMPELL of^ % ss 0J p [\ S UPER P!P' SYSTED IMPELL - NOS i 84/03/23 11 16.16e 1 Nua){RSION 16A, 10/81/838 \' , () PSE f piJAN NUCLE AR STFTIC3 . () i EDS PR09LEM 23CD618-NC-P1 PEN.1 l PRESSURIZER S/RV LINE AS-8UILT GE0METPV UITH SLUG DIVERSION DEVICES 68003 d) l () t I () SCFPORT LO AD
SUMMARY
(CCNTD.) () SUPP SUPP SUPP VIRN RESULT RESULT ANIS LOAD LOAD LOAD ( () l NANC LOCN TYPE CODE TYPE UNIT TYPE X-Alls SET Y-AMIS $[T Z-AMIS SET () l 205 C) l () .002 THMU .011 NORM .905 N0dM (CONTD.9 ! .006 UPST .982 UPST
- () = . 018 EMER . 013 EMER .099 [MER ()
.01 8 FLTDtM.) .813 FLTDtM-9 .009 FLTD4 Mal
() 225 225 ANCH GLOS II TORC (L89 GLOM 96 D 8.9 8 FLTDiM*) 35361 19 FLTDtMel 19337 63 FLTDEM*) () 8453.34 EMER 34296.86 EMER 19974.42 EMEP () 3530.11 UPST 1666 51 UPST 2095 76 UPST 243.64 THMU
- () 3s.57 NORM ()
-4.80 NDPM -721 36 NORL' 37 26 THM1
-173.25 THP1 -8128 18 THM1 1 31 NORM
() -178.15 WOPM -1849.54 NOPM ()
-994.23 THhu -6389.47 THMU
-4533.93 UPST -9498.71 UPST -1849.49 UPST
. () -9979.64 EMER -46360 68 EMER. -9693.as EMER ()
-11118.25 FLTDEM-3 -46364.93 FLTDtM-3 -9957.02 FLTDiM-l
() M0MT ILM.FT) CLOS 342943.98 FLTDtM*) 67853.95 FLTDtM.3 264185 34 FLTDEM*) () 340978.51 EMER 647ey.g1 rptp 194466 08 EMFR 66137.03 UPST IS958.P8 CPST 55499 88 U*ST () 31437 15 THPu 7602n68 THMU ()
- 10205.R8 NOPM 4770.25 N00 M 55PA.30 THM1 -19.4A NOPM 3474.26 NORR
- () 4697.57 NOPM -501 17 THMS 1290 94 THM1 ()
-523 24 NORM
.mbl3.35 THMU
() -24964.74 UPST -19R83.14 UPST -43059 60 UPET ()
=28 3 4 P9.5 6 EMER -69456 59 EMER *$79670.84 EMER
-285574.93 FLTDiM-9 -72512.64 FLTDEM-9 -189389 30 FLTDiM-5
' () ()
DISP tlND GLOS NEGLISIBLE () RotN (RADB GLOS MCGLIGIBLE () A
' () SD34 SD04 SNUR Y ()
FOPC ELPS GLOP ?7222.*1 FLTDtM*) 37223.67 EMER () 306.39 UPST C) () () () () i
PAGE 274 ]) IMPELL CORPORAT103 SUPERPIPE VERSION 104, 1C/01/838 3VST[3 IMPELL - COS
- 39/93/233 11.16s1&s () I* bj i
[) PGC TRIJA3 NUELEAR STATID3 . (} [DS GRORLEM 8392018-RC-81 REv.1 PRESSURIZER S/RV LINE ~ [D AS-8UILT GEOMETRY WITH SLUG DIVERSION DEVICES 6500) () () SCPPORT LOAD
SUMMARY
(CONTDet () i SUPP SUPP SOPP DIRN MESULT RISitLT ABIS LOAD LOAD LOAD t () NAME LOCN TYPE CODE 7VPE UNIT TYPE N-ARIS SET Y-ARIS SET Z-ARIS $[T () , () Saa4 () ".
'I C O N T D . ) -396.39 UPST
-3722%.67 EMER 8'
{} -37222.91 FLTDEM-1 () DISP EINI GLOB 855 FLTDEM*) 2.552 FLTDIM*3 .617 FLTDir+1
.05 5 [MER 2.552 [PER .475 EMER C) j}
.009 UPST 2.525 THM1 .413 UPST
.f97 NORM 2.525 THMU .260 NORM
() 2 522 UPST .259 'IHM1 () 2 522 NORM .259 THMU
=c357 wuRM
[) .16 4 uF)V ()
.364 THPU .003 NORM
.36 4 THM1 . 0P3 UPST .212 UPST
() .485 EMER .033 EMER .215 EMER ()
.406 FLTOEM-1 .a33 FLTOEM-1 =.057 FL198M-l
() (I
$014 $014 $ Nil 8 Y FORC (L83 GLOS 37422.22 FLTDEM*)
37415.89 [MER () () 515.82 UPST
=51%.R2 UPST
() -37415 89 EMER ()
-37422.22 FLTDEM-1 1 202 FLTDtM*) 2.653 FLTDtM+> .555 FLTEtM.) ()
() DISP tINI GLOB
.95* FMIR 2.663 EM[k 4550 [MER
.62 0 UPST 2 636 THM1 490 UPST
() **91 THMU 2.636 THMU s480 THMC ()
.05 1 NORM 2.634 UPST .483 THMU
. b5 0 THP1 2 634 NORM 474 NORM
.0J2 NORM .096 NORM
.527 UPST .003 UPST .021 UPST
() .s32 retr .032 rMER . set [MER ()
.632 FLTDEM-9 .053 FLTDtM-1
.88F tf(TDfM-9 C)
() C3 C)
- D C) .
O _ _ _- _ __ O _ - ._ O
- -= - - - - -
Q EMPELL ATIOJ
- PACE 275 h y y SUPERPI R$104 164 If/01/Q38 SYSTED IMPELL - NOS 84/03/233 11 16s16, )
v () PGE TROJI4 NUCLEAR STATI D C EDS PROBLEM 1300818-RC-81 REV.1 PRESSURIZER S/RV LINE Q As-BUILT GEOMETRY WITH SLUG DIVERSION DEVICES (SDDI O O SUPPORT LOAD
SUMMARY
(CCNTO.) O SUPP SUPP SUPP DIRN RESULT RESULT ANIS LOAD LOAD LOAD t Q NAME LOCN TYPE CODE TYPE UNIT TYPE N-ANIS SET Y-ANIS SET 2-ANIS SET O O S02* SDF. S=Ua v ') FORC (L8) SLOB 36720 04 FLT0tM*) 36717.4T EPER o 326 17 uPST
-326 17 UPST O
-36717 17 EMER l 0 -'672e.o. r Lio t :(- > Ol DISP EINS CLOB .368 FLTDtM+) 2 581 FLTDfM*3 .399 FLTDtM*3 l' O .231 ,EMER 2 5s1 EMER .2,s EMER O'
.21 4 UPST 2.*54 THM1 .275 UPST 2 554 THMU .197 THM1 0 2.553 UPST .197 THMu O 2.552 NORM .102 NORM l
.3R* THPU .
Q .38 9 THM1 O *
.384 NORM .9R1 N0PM .F04 NOR M
.604 UPST .007 UPST .1T7 UPST o .62 e EMER
. 75 8 FLTDEM-9
.nSe EPER
. 13P FLTotM-9
.236 EMER
. 325 FLTDfM-l O,
O O O Oj O O' O O O O O . O s l0 0 o o O O lO O. l l ____--__ __- ___--_- .
3 ...
. . l(.e t 50pse.-l , , .-l
- i.;. ! i 1#.e. e r g r t. it 6 LL ' o* pata3/15. 15 31.tu. .
3
.t- I e n.s. < e e a r t r f.f'
- 1 A ? ' Ort ~ '- ~ - '
7r - f7Tr'L: e. 5 ,ar-rc- i re v.
,*-r**t6 f ?f 9 * #pw L It E y' A%-PUILT LE0ftE TR Y W I T&f ' LUG DIVEidION DEYlCit stDDt
.'s'
*q R E S P7.f *, r e p r c g pijt. anatyegt a,n. I genEll. A P '.0L eif f GLOOAL ArCFLreaff0Pis (RULTIPLE9 or GaAylfyl [
Palhi M V 7 W-7 E-7-7
- d*' ')
tJA' L ACCfL ACCrt ACCFL ACCEL ACCE1. . Pil .?95 .16? 1 36 .385 41 7 *8' "") re1 A . n ss % .1~2 . .. :. t. .14' .es* l vq-- n n rr , .ani .ans .vn . vi r .=s 8' 2 . .' 9 7 .1&P .n*6 .?P7 41 " ' tj,j p M3 .346 .162 .124 .?P7 41 9 1.;' r; . ~i i i .i.i . 74 .;e . r.^ , ~~~-'n
! 1.612 .1r1 .218 1.'26 1 654 O "*"")
tir A 1 . 7 89 .1 (.1 ."2 3 3 72* 1. 72 7 m $ r5n 4., . .aos .saw a.acu 2. es t
. - 4.im r, i.- ' . - - - -
u 79 6 1 911 .161 .256 1 928 1 935 / ,./ h .
- v.
s "Q LS .34J 4162 000 .3PP .41 3 .* , min . im .i% . e- .a- .gir b se 1 1 612 .161 .218 1.626 1.61 gm "O 73 1 .861 9 .738 .241 1.R35 1.R51 3: 2 .
, , ..+,. ..,2 .28+ . . - . .. .. . .
!!il illi litil d "o 11 till! lilH "n. .m'.'i T . ! .
1, 7R
.. m 1.845
. 2 4 ',
.2
.36n
. . , ~
1.ela 1.934 u r c: 79 2. 47 .217 . 3 'i 8 2. r. 71 2.fRP mp ',' O
.. a 3.595 .2i2 23< 3.es5- 3.ni i m.v,4 - r yr a '> **
82 3.R36 .312 952 3.997 ' 3 . '* 6
- 4.- f. 's? ,#g. y '
' @ y R3 6,
3.698 T.
< .389
. 12
.R69
.,25 3.799 5.973 3 819 2.6i2
,c 1_ _ 4 ' on g'
u 84A 2 9P9 .798 .472 3.r26 3.120 o ** Q e5 ' 2.229 .a78 .274 2 226 2.393 y m 66 i.-^6 4^6 . a .,4 i.34i i.e56 -- g,v . ,,, jg. , yp , ,- ,- , y r .- .v - st 87 476 .A78 .*10 477 1.149 . ', (<,
. * ; Sje,.%f Q ", Q f; ;
M8 2.3* 3 .R79 .293 2.342 2.501 . p , no Z .T 3 .F70 .?;3 2 24- 25i 2
<t "
Po
!.6's .622 .2*3
.Pe4 3 642 g.642
?.654
'.644 "O
1.64 .'?2 ~
;, 2.767 . Te .2;i 3.696 3.+ i .
. . , - ,, . g y r- .
~
91 4.19? 42* .294 4.242 4e234 'i *
' ^ .*
- w.
O 92 5. 6 '. 2 .294 .f*5 5.64h 5 647 "
;3 ^ .?-4 .i- . =- i.3ii i.?i: .
14 5. '% .1 #.6 .213 5.86* 5. r6 3 g se O n '. 741 .!*6 .aa5 .747 .76* r 7% 2 . 2 7 .- .ie6 .v i 2 27i 2 2;i - - 96 4. 'a 4 .Iu .'?6 4.*** 4 . tHl ? e. g m 5011 7.165 .166 .147 7 167 7.169 o. r.ft 12 7 .-? f . .7N . .- T 19 ??4 i *.? f * ,, rnia la.** .'*' 4184 f e .5 % s. 14.55' "O 574
- fp15 la.7'e .lA6 18 . 7 ' .* IP.743 en e'
s' O 63
- - -. -. ~ ...--
- - .-- - as ====
/m .
m ~/ .o. . :. .. .r/ % fq)S sia t ' ,.s:. "
- rn- c. cry r ,
**t
- r L r t *
- 1 A 11 Or:
i..rr= i v.v.i f )I
% (%j)
*O 6 " ' ' '. I & I / e7 > ?/DV L l' r *g A' .' te lt T rJ PMr I F Y WITH ?,Lttr. P!Vr a e gop; p[y g rr$ g t n(s ) "
e. Q E SPO'68 'PICi>UM A 'f A L V' I '. N O . I 800rtle Ar'.0Li'ff CLOR'AL A ttrL[p 4 f f 0NM (8tt'L7!PLES OF GRAVITY) (CON 7D.3 nO ie P e lt. T y y 7 W=F B=Y=7 NAME ACCEL ACCEL ACCEL ACCEL ACCCL "g t s.
$ 0 i t. ? '.6 4 .166 .644 20.614 20 615 Fn11 7 165 .t'A .14? 7.167 7 169
," g 7e vr r. . s eer . 4. a. .344 a..t6P 6 rii .
n
.9,...,,.
9e 1 227 1 5?S .134 1.214 a'l
.7 al 1. f.
- 2 .333 .714 1.969 1.P 3 f.
g,,. gg i i .T=5 . su .5 erku n.ar- 'n i 1 .69R .??4 2.415 2 514 2 52* m 1 7 .696 .221 9.6*3 9.717 9.728- "g i3 w e r.
- m .cs. ,. cat ,.,nu ,.,,
l 'I 4 .6R7 , .1988 10.525 10.547 10.549 s ;r g :- g* - -
,; . n u
. w l .. ..O 1 85 .6P1 .18 P. 1 502 1 649 1 659 -5. +,[. '.
", g i 4 0- .c . .ir .u," .ses y 1 7 .64c .22.1 .*55 .6PS .71 7
- 1;h .6ps 98* 971 .684 . P9 7 *-
ng a., .ona .ase e
.vas- . ens eso - -
- y m . v.re v m- .- :. ..
Ild .6R3 .177 .014 .683 . 7n 6 N, ', o 111 .684 .166 .614 .644 .7a4 ';&[; 6 .
' "g i i .; .~r .ier . . . , .c. . ne . n 2 5 *. .ARs .166 .~47 .6At .79P 1 1 612 .161 .21R 1.626 1.6?4 *
"g av s.as, e
.nuv .< , s .na > s . e, ., - -
.n :,- e 39 1.e42 .171 . 245 1 858 1.n66 ,
< . gg g% .
. . "g 3a 1.n42 .171
; . n u, o .1~,
.24S 1.eSe s.=ra
- 1. m6 6 n.en-
. M'4).- . S' J '
,' i .' . _ U u
4- 1.RPF .164 .24H 1 844 1.851 41 1 732 .168 .247 1 751 1.75a "g
,2 , ...u .. . . .u.. ...,.. . ..5, .. . . . . .. .
i?
'!iil
. re ilil , . iip,1
. s .- s . ., - -
lill! a..-- lilli i .v e
,#, >; ,M '; ,' , ,
"o e.
40 .A77 . l f.* 1.2*2 1 4?4 1.456 4 A "" gp
.672 . 2 's 2 1.ei5i. " ,1 1 24P 1 264
.su. .2 , s.v?e s . is , -
.8 v: . . pr -r - -
m 51 .472 .? 4 .4?5 . R D f, .826 '
- c -.* . n.t.;y' '
m [g 52 .677 .?'4 . " 14 .67R .70ft -
".' se+7 .; e .i ' i . ~. e 7 i . is i I
. 6 * 't .
5!
-_. 4 .<>*9
.2 4 .FP9 1.la?
l e il4 7 1 3at 1 067 1.?ie mg j
. 3 8' "_ t n a a.av,___
.--7 .an, a . ., n a a.a, v.
% n
.6*9 .la2 1.P76 1.45P 1 461
, .6Rn ,370 3,3pq 3,a37 3,5g3 **
M g
+7 .6*+ .iti i.717 i . P* ^ i.t,, *
- r. v .'** .16? l . a 7 'a FF
?. " ' . ? . l f. ?
'a .684 .187 1. eat j , g,4 5 3,6=4 mg m
s. es e es 84 - so
'8wt 14 3 Suf'>616f V,* 8. t. 1 # 1/S'1 S V% iF.F I'FfLL - fP' 84/14/15. 15 31.C4 s e
sar T s-.Let re Nier L a a p '.TatION ' Cr* M *Lir 3: e amt a vrv.i . S pf f SLt I/rp sppy (gpr a'-PUILT GEOMETFY WITH SLl'G 01VER t10N DE VICF' 150D5 _" }'ie es R ESP 0t$r 9PECINuM A N AL Y';I '. 40. 1 ( Ott E 13 , AB00Luf[ (;LOBAL ACCCtF8A)l09fs (AHLXI>LES OF GRAVITV) "O ( C C't T D . 9 l, GOINT X Y 7 W-7 E=Y 7
- CAME ACCfL ACCEL ACCCL ACCEL ACCEL
*g a.
2 6i .6*J .167 e149 .765 .7A? 6 4 .64 .38A .003 .alA 941 n g M
- r. s
.n. .imo a.a., a.03, s. w e w --
. i ; - e.v ; [n SDt3 .679 .166 2.144 2.158 2 16 D
$092 .679 2.851 3.951 3.936
\4 4 P
,,1 ,
l""O __ __ __ _ .1_46_
~_ m :. -
o ,- eu =
.nsn . a i. r. =.v.a . .inr I,m .
FD.% .67F .166 5.41A 5.4F" '. 453 SD (. 57M .146 59'.6 F.e 3 A. cf 7 mg 5uvi .373 .ano iM i o s.a5e s e in-5 - .- . us 62 y rcy p '*yg. j n
.679 o165 1.751 1 879 1.PA6
- gj w 63 .679 .165 1.525 1.67* 1.A7P . , . g,y *?;.%- ", g r .ni, . i r. : i .m. a . i .- a.sai in h '. .se. .355 g.p54 3,qva 3.gep m A4 .AA, .165 1 749 1+A6B 1.87* "g oi . oL v .in5 a.u5, i.oai a.ac, - - -
- - w . 5 i T' 4.J ' ' % '-l ' ' P ' '"
A8 .6% .178 .P87 .686 .708 ' , 69 3678 .171 .031, .679 .704 -
*;4_
O
-ti .67; .i6 . 51 .i.- .i-T .AA, .
.1% .J31 .6A' . v t. ',
72 .6a. .l66 *
. 31 .6er .7s e "O J i, .no . ins .r51 .666 .Hi - -
- r. - m a
.e 1 1.612 .161 .21A 1 626 1 634 J ( ggc M .f y 5. ;.a.. - .i, r',' .
I e " 2 1 019 .260 .245 1.n36 1.RS4 - ~; ., ' .l hdN ' O 5 2. 4 : .276 .247 i.6 7 i.nsi [ n 5 1.84 * .276 .?*7 1.857 1.877 4 e 1.A*6 .292 .246 1.A73 1.84% ? ** Q
, i .% .5 vi - . 2ii i.666 i.565 mi
- p. . g-p + yy - - . - .-r; 1 nr m
s 6 1 867 .3t5 .25' 1 945 1.*39 7
. > . s..gT : '
r "
"O 1.A72 .310 .38'1 1.896 1.921 ') *;;7 y.
e i.F*2 ., i . = .' ; i.;;; i.;;4 e. l' ?.851 .39a 9e* 2.ng! 3. ..g g Il 2 997 .424 1.124 3 2al ang 3.22' " i^ 2.^66 .tiv i.i ? 5.W 3.i32 en 13 2.6P4
,m 1.,p .v ,,, , -5 e.
596 1.193 2.937 3.91* " 13a 0.ng 9P6 1 147 2.542 2.726- -. - M .- ti i . '.* t d* .- .m i . ii ..?ti
" O l '.i 1.12k 1.133 915 1.?95 1.674 g
- 16 . 6 7 t. . '. r p 1 318
..,n 1 133
- s. __i., .,4-___
.676
, _.c-__. - - - -
n"g 1 17 1.762 1.1*3 .*1 V.*83 ?.284 1H 2.466 428 1.513 2.P93 3. Al b
, ag i- -a+w .--- i . = t- ?. *- .*1
- 14 '.6 5 .772 1. 6 2 ** 3.*72 3 168 FF
? ?. 75 % 7.9 1.767 3.2r* 3 35a *g re u .m .m z. m e.n- .. m --
i
~
o' w l
'}
wm ^#
sw-=
,= - .--== m% am =
a.-
,- .,e a- == - *e*--== -
, , , , . . /. s , , . . .. u. . . c.,
- r a . 1 : . a . ( -- \;
(O V. . .- e a. , I* c.sa-. *esel fA6 e ta iIt "
-e, -
U'
~ ~~
5
- T r t
- g-ry -1 s--.C a e.v.i
- p -e.q2v?rr etry L l t'r ne .g e'It t 'if.0PE f
- Y W17H SLt*L P1Vr** ION DE VICre gerDs N
**/"t C C SPO N'.L ' P [ C 7 P U" A P? A L T C I ' .*p . 1 ( Ot3 L 11. At3'GLitTF GL0fl AL ACCFLEr A v l0kt (PULTIPLES OF GRAV17T1 (CON 70.1 [
PPIN7 N Y 2 F=7 W-Y-7 *
*Q 48 tir ArCIL ACCFL ACCEL ACCEL ACCEL ,
l'? .p*P .a?6 ."*4 .P=3 1.2P7 n.3 p 15? 243 .eap .ane .9am 1,3-1 P. a.i s.ni .-ar ". a , a . L ., a.ai r , a- -- 3 [ 1 ? '. . 154 .791 '
. .i ? 4 .a f.9 1.751 O n.)
13' .me. 79P .22e .nTI 1.17s iii .M 6; .. - .9 ...m- l 1 38' .Pf 5 .261 .211 . Mal 928 *.S l'* .P A to .1 ** 3 .183 .88* 9f* , i e .ssa .5i. .i .,in . 25 ; .e . n - , n 141 .n66 .516 .190 .a77 1. r1 M - "q
*~~
la2 .A6% . 7 *, 7 . J' S .PA7 1.11
- Ef. '
ie- . te .ni- . i7 . ^64 i.22 7 w 144 .sf4 .Pa9 . *36 .864 1.247 .
- i 145 iee
.863
. A ft .
9 'a f
. F. i;
. c f. 2
.i9i
.P69
.863 1 253 i.ii4 . .
l() 147 .aSa . ins .t,7 .e63 1 15s . s .'. ger6 . - es , , 34a .nst .7e .g96 .ese 1 13a - f"
,<- .w, ..,, .. . . - . ..,:- .
149 .s96 . s f r. . 33 .e4* i.ais ~~ 172 12=
.aen
.ie,
.,4.
.+i,
.2
.c+,
. 51
.i .
i.: 2 3 . i + :, - ..
*r' 15i 743 914 .le 1 .753 1 1A2 "'
. ' ;) '.,4,.
7/ .
.' ' "O 191 .845 .915 .104 .851 1.290 ,h' e ' . .
152 a . 7.= 5 .;i5 .--- i.7 5 a . - 5 .- sn 15' ?.163 .537 .'64 ?.15' 2. i'2 e , e.0'
!? 3 = ' !!" ' ;
.~
.. !. .!,' . . ,9, .. ...., *..M. , ?. , .- . .
156 2 191 .348 .P82 2 192 2.2N fl 7,),,,
; v. , ,;.,
wg 157 2.193 .35W .1 t'6 2. I 5 2.224 .
't ^^ l i! : ^ . i*^ .=44 .i24 2.i i 2 22.; .,
l ' " .19 "- .2't .141 7.1*9 P.21' * O
- 16. 2 194 .??? . I N' 2.2d( 2 211 i+i 2.i*2 .FiS . i i e. 2.1-- 2.2i ,
3 g: l[ Ic2 .1 P 8 .3a1 .2148 2 198 2.232 , . eg 163 2 18e .671 .254 2 195 2 295 a'.' t*3 -rt ^ . .; i .? ; 7 12- 2 2;= .
*fa 2.17A 771 .27a 2 1** 2.32' seg 16% 7.1'3 . "*
- 1 .127 2.177 7.?"6 A ite- i.;;i .ti; . 77 1a^4 2. i - ,
f 167 1.9 1 .33F . '.' 7 6 1.P03 n 16a 1.?42 .717 . 7* 1.244 1.PRI 1 436 4g'
- 1. 1. ~ ; 7 tre .7 . Te i.5^- ,
17 *
.*"7- .s 3a . 74 .*A 1.?75 =
"g 171 .at; .r ff . 72 56% 1.??1 1*^ .M*o .P9 .i r2 . ^31 iet*2 [
. O
.- ~ . - . _.. ..
- de
I 6 t, L L t. . s MGr if y
$UPFsrgr; g;.'g.,
c . . .
.f, f . ,, y ; 7,,,7,. ,,,,,,g , ,,, PS/f?/15. 1%.31.*4 s
( s .3 T 3 e:Ja4 fUCLFas ? T A ' I d *' .' O F Im r i. ri 5.tr.! 937rp e as y Lght
' 3--Pt- a wev.a
~
l l A '. -s D I L 1 GIONE18 V WITH MLUG OIVr #$IDH DE VICE ' (SDDI ,, i . g l RESP 0kSL %PECTRUM A8dALY?If P0. 1 (OHFil. A8 SOLUTE GLOBAL ACCELERATIONS EMULTIPLES OF GRAVITTI (CON 70.3 l l . .* , POINT M Y 2 N-2 I*Y*2 . l 8s A ME ACCEL ACCEL ACCEL ACCEL ACCEL .. 2' t 45 .tif . "*
- 6 .682 .712 88g 2it .6*. .166 .431 .6RP . 7 'l e ','
c 5 .an. .ane .6 2 . enc . ra n - v2 vs . n er. ..- n 24 48, .186 . L le7 5 8 C, 70C 7
- j'.i. Jj ,
"O 27 .684 .366 . it 02 .6Af .7f 8 - 'y cf i ;.
; A .ns .aso .G. . cd t-_ .ssu a.
2-9 .6Me .166 .ogt .6mc .700 in g 21
<si 113
.%i
.146
.zne ,. y.:,uus
.348 1.1
- 4
.,a 1.11A o w s' ln 213 .687 .366 .c80 . 692 .712 i
~ , . ' n m.7. xvyyng,1y,y. ,, m
- r 4c;.y,t .
i*. - .' - ug 213A .6sv .268 _
.r st .685 .Tes 1:;. f Np. . .jy.m.. S 4.o . n s. ..,n . ,- .... . ce .
214A .6Ad .179 .t62 .683 .7t6 mg 21* .63; .1P1 .a49 .F81 .7'S . ii. 6.. . in .vi,- .. . .e45 .
<n - cc ry , . ,
217 .68d .1h . 511 .680 .7G3
/ ;e t.' ggm.y myT7r -
s' g 218 .68J .168 .C14 .680 .701 v". ' 2,*'hg..l ' '- ' f .'ih 4.
'}
Ji; .M. .ioi .:a .66 .i. 7, 22. 221
.69
.a m ,
.167 . f.14 ei d2
.6a i .71t
- ag
.t%6 .68* .7CT $
222 .66. es&6. g m.oes :. . 6&k .i44 17- - -r puwy ., ., c w .;.ggw,, n 9 ' m,..; ma.'.: *e 223 .68d .166. ,e*US .680 .700 j' ,
; - ? ,' * * / ?
221A .68v .166 .000 .680 .750 ' t 'l' J .p ,I ,iy', ;
,"g 2 Mit - . @ .' .in .. .n
. i .- n 22e '
4 i .?F6 .33" .Fnn 70n u "g 224 . 6 8 .> .366 . J .10 .FAC .70 0 225 .oh eine- - .;.o .ooo .i.. .
-p w. - i'. r w
V I A. 2.367 1.193 1.270 2.686 2.915 = d.C. 0F'PSV- Eolod [., Nh . ' ,;' ' '
- Sg V!B 8,.757 1 133 3 769 7 737 7.819 N . * 'g. ,,
vte .894 ..'e i.7;i i . .- i. if m v?B 744 .2 . 4 3.285 *.339 3.34 5 - C. S. DP PSV - 2010 6 m g V5A '.171 879 .406 3.197 3 318 : C. G. OF PSV-80lO A " vss .tr, .m i.iei ;.rie -. 31 a . m m.w - , .m...- .< - vsA s.143 .3at 1 178 3.3sn 3 37a c C.G. or RY-9558 -
- W' '- .
.g v=n a.s ? .3at 2.a=5 5 32: s.33s . .
a i .?i .- Fe i.23 3 .- .'* i . i; 8- - l V E F: 2.?h! .7N9 1.77? 2.874 2.97a A O.S. OI D ~Db seg V7A 2.29* .3AM .377 2.Z7$ 2. 3<f ? "
- Vo 2. M . .W .,% 2.;&G 2 32 i , $
V FC 2 32* .35A .750 2.442 2.46A V70 .3N P.284 * O
?.2r1 .'m4 2 31% ; d.d. OF AfoKOOOA vna s9 -- Ft ; .
^^^
. *^ i.e*t [
V MIt ."'. . '. l i . 3 r. .a57 1.
- e 7 re j "c -
7": 1
' Mi c.c. or MogoooE, r-e. '..P' .
. L,'. .- !. ...'a- ? . ,
uy
. . . . - . . . _ _ _ _ = .. _ _.
o
, , w -
w - eep.- - um a. as . .'
- .= .,---= - - - - -
y,,
, IPPf LL (
(8 # T If6 S UPI DP ! k,m J f.6 *.If
- 1* A e 1 / 1/**1 SYSTf P ITPELL = f:03
, ;(s)
'N /
PAGE 221 83/03/15 15 '(j. ( ; Q., P f.F IPO.DH HUCLEAD STATION tb . PWUTrtTM 'ao- a n-nc= s ' ri v. s
-- ~
p. F F F'.LIrk I 2 F P 9tAV LINE g AS-0UILT GECMETRY WITH SLUG O!VCPSION CEVICE% 850D1 o l' n R ESPONSE SPECTRUM 84ALTSIS 840. 2 40BC2), Afl50 LUTE GLOBAL ACCEt[PATION$ (PULTIPLt3 0F GNAVITT) o ,, o ], PdINT X Y Z X-2 W-Y-2 * * !
, NAME ACCEL ACCEL ACCEL ACCEL ACCE L ,
o ] ,, M1 . 61 es .162 465. .43 436 o MIA 416 .162 .405 .4L5 .435 . ' g ni .' 6 :4 .ans - . sw . cr .=5r i m, , M2 .412 .162 . 406 4bF .437 ",, M3 01 4 .262 458 .458 486 . l. o s, .ss. .in-- .nis .6 n .5s 3n - MSA 1 .2P6
.3'4
.361 alf!
2 268 2.329 2 227 2.349 2 233 2.354 n>
, nS6 .5u ,
.ana s .5iw- r.aws z.5s= ,
i m, M6 .342 .161 pl ' 2e598 2.620 2.625
- e LS 000 .162 (.J jteg , 400 .432 .. ,., . ,; y,h 3 ns. . r. a a .ses .sua . m s e. m*
o .sta ]' , 1 .2% .161 2 2La 2 227 2 233 UM ', 78- .3?4 .224 2.482 2.Sf3 2.513 2m
,, 7 .M5 .23i 2.515 2.53 i .5i 5 7-E u, m,
7* .325 .239 '2 513 2.534 2.54 5 '
* -4 n 75 .314 , _ .256 ;,.~ 2.544 2.563 2.576 f* 9 , h d-
,~ so . ens .cua c.,,o c. ass cuu yy 77 .218 .292 2.396 2.4t6 2.474 r -i On o
78 ti
.297
.e83
.31F
.394 ,
2.244 i.ii5 2.264 a.t;6
?.28F 1 679 1 p%
gt 81 1 829 .344 ['1838 2 103 2.131 ... I dk 1 927 .194 o 82 . 914 -; 2 133 2.142 1 ?r. N
, 63 84 i.623 1 676
. i ^. 6
. 2 9 f-
.n6i
.R43 J.eia 1.87f 2.655 1.9tn
-~
G[;o o 84A 1.369 440 .pnS 1.5R8 1 648 Q
, 65 .ii. .5i4 v .i6. i.294 a.54 a g
^y 86 .S62 .504 ,. .779 .961 1 085 & .e o
, 87 .013 .564 . , . .778 .779 p*27 -
,, ~
.( 3
.795
^
, #6 i.;ii .57; i.26i i.3,i "3 88 1.dll .5.4 .785 1 286 1 381 89 1 .78 3 .380 .795 1.934 ? .971
, e9 -tif63 .38. - , .n a. a, 4 1rs 'y .
'q
, 90 1 9Co .357 .795 2 067 2.L97 *
,, 91 2.678 .331 .796 't .2 2 5 2.24 i .. . ,
u i 2.M i .223 .ii6 s.iF i.474
- On 93 3.213 .186 .796 3.31C 3.316 A
, 94 2.593 .le 5 .7P5 2.749 2.714 *
, 95 .ir3 .iss .ini .791 .*ti g, 95A 1. fi R 9 .166 .781 1 344 1 35E
, 94 2.w21 .166 .?R1 2.167 2 173
, 30tt S .M J .*^ .7P3 1.667 3.F6 F -
o SD12 *
.145 .It 6 .7a2 5.2
- 6 '.20h Sut* 7.2ae .tF6 .H.7 7.8.42 7.*44
-sois ~ - . m me r2, m ei -- - -. -
Vu
I MPf LL 084 Por'1 Tint' PAGE 222
, SUPfRPIPE VL k % I f,f4 lea. 1s/*!/8?l SYSTED IMFELL = C33 84/53/15. 13.31.C4.
Os , F0L TF0JAN NUCLEAR STATION *
, Lud Pr w La.n usauslu-wc -01 aty.1 Og PRESSURIF[A S/RV LINE
. AS*8UILT GEOMETRV WITH SLUG DEVER$10h DEVICES (SDD) o
. o .. R ESPONSE SPECTRUM ANALTS15 $;0. o 2 40BEP), ABSOLUTE GLOBAL ACCELEPATIONt EMULTIPLES OF CRAVITT) (CONTU.3 -Q g POINT X Y .H .3 2- X-2 E=T*7 NAME ACCEL ACCElg .] ACCEL ACCEL ACCEL o Q ,, SD16 10.34d .166 .839 10.374 10.375 o SD11 3 580 .166 .785 3.665 3.F6 8 c in aegse - . a r r 17 . e ss a.sgs a.sg v . 98 1 323 ,- .736Y. L.6 ,784 1.538 1. 78 f. f g4. Q.a. 762 1.381 , _99
,,. 843_ / R .784 1.b93 -
o av. .uoa .a,1 a . , i.1 a.=aa a.2a O.m 16 .o83 .236 3.925 3 926 3.933 lu2 .477 .179 13.191 13 191 13.193 e asa +een r. .aswu.3apousw aa.ies aa.=se '
- p. 144 , '?2 13.947 13.948 ,. , 'h. < . .L.-{ i
. r :. * .465f*I.f,,.166,g13.94[
ar 185 .838 .169 ,.al'.996 1.996 2.884 .' . fi ' , i, ,* 7. _ , a a6e .uvo .anu .sua .avs .nes Q., 137 .ub6 .2C8 .782 .782 .8G7 10s .306 .689 .784 .784 1 044 a, avi -
..vs .. ?
- I . w.181:
mn..res a s, l Le788 ersa enen c gg 110 .077 .784 .804
,.4, ,.
n -~ 111 i L . 08 5 3, .1 6 & 'J" J .78 3 .785 *
. 803 , .,y, .
m aae .paa .ses .see .sau . sv e go 206 .Jb5 .166 .780 .780 .797 a 1 .296 .141 2.20A 2 227 2.213 y ar -
-.asa .a a e <. a r g se e. sus z.waw '. - i g, 38 .329 .331- 2.584 2 525 2.54 7 . i
.331 *1 ,12 584
- 38 .329 2.525 2.54 7 -c , ,: sm
. 5, .ac. .aae <.sas e.sha c e ss e Q ,, to .298 .303 2.566 2.524 2 542
, 41 .2Aa .2A8 2.515 2.531 2.54"
, ti 265 -
.455- - ,s.55s 4.S== s.25a -
g, 43 '.326 2 448 2 469 . 2.495 - *
, 46 .107 .359
.354 f ,2.235 2.238 2.265 .
.- 2.asi
, si .i5a .svu 2. a s e. <.asr g ,, th .133 .268 1.989 1.993 P. ell
. 49 .333 .246 1 838 1 843 3.86 6
. in .aai .223: , "ra. bis 4.5i7 a.592 -
O= So .a87 .214 '1.258 1.2s3 1.272 ', ?
,, 51 52
.05U
***3
.214-
*2ih
^ l .959 *ii'
' .960 oli4
.984 m U -1
*u 53 *
. 73 .219 1 286 1.2A8 1."3J6
. 53 .a73 .215 1.?86 1.288 1.316 m 59 .ur5 .asa a.oSi s.63 a .co 5 gu 54 e r.7 3 .181 1.852 1.854 1.863
, 55 .375 .177 1.970 1 971 1 919
, ^8 .W .i;3 2.is; 7. i i ts . . iN
( . ,, 67 . - 7 .* . l A f- ?.521 2.522 2.F27
,, SH . 72 .386 '. il M .. t2 ?.*N ~
,, ~ ~ ' - - "*19 - - . M ., .u? 2.425 ..428 . .M 6 vu
.maines .uusman. em messesse w .mpanas m an - . esse em .s w
s ! c?E L L g .orailpH s ; PAGE 223 ( f
. S U?[k PI'n/Yl.6 5104 l e. A . 1 / 1/C't tYSTEM IFPFLL - M01 \# 84/C3/19 15.kdO4 i'
e
, PLF TROJAN NUCLEAR STATION y LU3 P'EDILL r' JJUUJ3n*RL "5 FLV.I g' g, P4E550AI2ER S/RV LINE At-BUILI GFOMETRY WITH SLUG DIV.ER910N DEVICES (50D) o Oa GESPONSE SPECTRUM ANALYSIS NO. 2 (00E29, o ABSOLUTE GLOBAL ACCELERAfl0NS (MULTIPLES OF GRAVITY) (CONTDel u -
() , POINT : M Y . Z X-2 X-T-2 ,'
, NAME ACCEL ACCEL ACCEL ACCEL ACCEL -
o Q ,, 60 .030 .167 .897 .89R 913 o 6uA .026 .167 1.029 1.029 1.04 3 na . a.ous
, .scu .aog s.79b . a .c a u -
-6 Qa SDc1 SD42 011 .167 ,,[: 2 52 8 2 528 2 533 ,
.011 .166 - 3 627 3.627 , 3.691 -
... < h"e . .
e 5554 .62. .i6s 5.,57 5. 55 5, C. ^ " ~ Qa Sou5 .u39 .166 6.698 6.699 6.7nt
- s. 5016 .445 .166 7.387 7.387 '7.389
, .... g .c. ., a. m a. aa x.,. .
Q, ar 62 53
.'.011 *',i.165 j g215fr
.010, ,.
165* g ;2.4661<, 2.159 2.466
- 2..'&5
~ 2.432
, gi.Mj-
- e. ,
y (
, o .usu .ana <.aiv s.a-1 <.as, Oo, 65 . ail . 65 2 92o 2.92. 2.924 66 .u06 .165 ' 2.494 2.A94 2,89*
,, si . 6 4 u ,. .ame- seau5 e.ma u ,% ,
O, 68 .001 ,198 M,.. sesw5 .773 .773 .798
,- , . 3-
.A
, 69 .091 . 1al i g~ 3788.. .793 .813 .. .,,, .__r,y y
,;7 f g
ei .a i
~
, .an, .ib .o6e .can Oo, *151 '8'1 788 .8o2 .8ea 72 .c57 .179 .708 .784 .8ap
, it ..5 --
.766 -- .1tt a i
,- 5 1 .286 -
..161 as. - - - .72.2ss y .7 6 6 - -
2 227 - Oc 2.233
' _ . ' ' 'Ei, t 2 .325 [ .183 _ '. J .J 2.4 0 0 . 2.5s1 2 508 ,
, a eaau .snu s .v ~ <.aas < oav ~
Q ,, 3 .330 .187 2 509 2.531 2 55P a 4
.339 .195 2.54u 2 562 M 7f _
.s_ _u 3 ; w u s___ ,._ _me-
, .anu___ s. ass e.ac u ,y. ..
O 6 .us .218 .
,2.41s 2.4 3 2.453
" 7 .386 .237 ' -
2 310 2.342 2.354 ^'4'
~
, 6 . i. .255 4.72s s.is? a.6i n ,, 1J 1.212 .293 .R16 1 461 1 499
", 11 1.2R6 .21C .R72 1. *L 5 4. 1.43 fi
, it iTt25 .277 68., "1TST.W i 532 g, 13 1.136. .392 .Af1 1.444 '1 A96
,, 13A .946 .%4 .877 1 290 1.402
, it .876 .6i6 .355 i. Ti i .236 s 25 3" - * ***2
O =, 16 . '.1 -e .617 .'*77 7 .777 ' . 9 9 2 g 17 .7,6 mt i- .9Yh iTt2 6 1 265 , ng 17 .7ch .617 .878 1 128 1 28? ", 18 1. u ,7 .4( 3 989 1.411 1.445
, 1R i . ,7 9eT .m ~
i.*ii i.49; g Id 1. *. 7 .4?4 1.s17 1 4?4 1 557
- 5. 1.1 '. H 4 + 1. :.5 3 1. % 1 1.( 4 y ._ . g , , ._ . _ _ , 3 3.- gpp ; , p ,, ;,9g, _ . - - . . -
torn n - . _ _ . .- U
..%- - - - - I
, IMPLLL Cokt0saitt,% PAGE 225 SUPEhPIPE VLFLION lha. 1 /.lsegg SYSTrp g FP E L L - P103 C4#13/15 15 31,04
, iGF T#0JAN MisCLIA7 %TAfloh
, wi rFOT'L r n ' ncsan-iL-La nTv a b b b k o b b N H SLUG D1WERSION DEVICES (SDDI
( . o
; ,, RESPONSE SPECThust ANALYS!! hD. 2 808f73. ABSOLUTE GLOBAL ACCELEpATIONS (MULTIPLES OF GRAVIT'8 (CONTD.8 l g POINI N Y Z F-2 W-Y-2 .-
,, NANL A{LLL AbbEL .ALLLL ALLLL ALLLL ,
6 9 ,, 132 .327 .447
.844 90% 1.81 P o saa .ana ..<a .o .w 4.u ct .
., 134 414 .372 .844 968 1.P37 a o 135 .436 .3AL .865 .969 1.04 r
. aan .cas .asi 4.aa= a.asa a.<ag ,
.. 137 .152 .313 p 1 231 1 24u 1 279 .m~
,, 138 .15u .2J2 + 1.163. 1.173 1.196 6 l
o sai .a,, .ana a.as> a.acw a.aaa 2 .} m 14d .148 .171 1 032 1.P42 1 956 L
- a. 141 .147 .242 947 .958 .979 '
a ag2 .awa .4== at- .cys . 7s o '.
- l a
.} a,. 143 .144' .,,. .308 k.use (g'._.85
.864 .91 7 , ' ' ?,f'.O % . ., .
I
- e 8 6 8'2t . ( .
144 .143
.333 879 94 0 . , ,
m a a a .a 4 .ama 7v4 .>sa .vos s }, 146 .14i, 441 9 681 97G 3 846 '
. 147 .138 .5's .971 986 1.le' essa . ins , a . .aan .5 5 r- a.aes . . -> .
.} , 148 .136 .5a5 .
'.951 461 1.125 o. c . 149 .132 .684 h . ' .45 8
- 868 1 105 .
.i l m aid .aae .nni esso .ebo a.ava .
129 .143 .46A .844 .RS6 915 }. i s ., .af, .468 .e4s .84s 94 ;- o
, ass .ii2 .,s. ,- ...,, ..s2 . +e . .
1s2 .6as 967 .nso 1.n8s 1.1:4 , )t t 153 .s95, .3a2 __.3 .ss9 . 1 241 1 2r7 i '-
. a3 .es .<a, .ao a.< , s.cos s,
} ,, 155 985 .217 .858 1 254 1 273 '
, IS6 90M .211 .865 1.2$4 1.272 ',
l i,i . vtr. .is3m W 3; a.2ws i.261 -
. c, s g ,, 158 .938 .177 .854 1.246 1 259 , 1 s.
- 159 .966 .243 .1.837 1 377 1 398 '
ir. .is; .2;; i.i;6 i.45 i.4;4 g 161 . 9 *,2 .4v6 1.278 1.564 1 616 .
.5%1
- lo? .A98 1. 3 7 f. 1. F. 3 P 1 728 g
[ -l e t 163
.o
.893
^
3 . 7%
.754
--1139i 1 391 i .6*J 5 1 653 iesii 1 817 l
164 .R9J .876 1 313 1.586 1.A12 5
,, 10 .88n i. 73 .iin i.2ie i.$5e [
p, 166 167
. f,71
.5A6 4?7
.?44
.857
.A57 1 088 1.'27 1 173 1.g57 iatt- .239 . r9 i .**ri .893 i . u9 ri ,
16a .175 64A .857 874 1 .'14 7 e 3 ,, 17e .14M .698 .856 .869 1.'l l 's #
~ . ---- t t ! .ii3 .t .676 . MAT i.i2 7 ,
g ,, i 7: .In .Le7 . n s ,. .au i.las ; h *'
- .--mmme M eme.s. -
m m- -
m ammm. ===, amm - - = b
- I a I 8FCLL . 38AfIT4. t
. 'SUPERPlhr vs.6 .Itsts 161 1. / l /f 9 8 SYSTED IPP[LL = 03*
N PAGF 227 (/ 84/~,3/15. 15 31.04. s
. PGE TF0JAN hilCLFAP %TATION
, L u s T'WOffLTM ~i3 2 p e a s = h t - v a vrt y . a
-g Pe[$5t.*RI7ER */DV LINF .
, 4'-PUILT GF0 METRY WITH SLUG DIVERSION DEVICr$ (500)
.a l R E SPuNS E SO C C T Ts H M ANALYSIS NU. 2 400E2). ABSOLUTC GLORAL ACCELEWATIOles (MULTIPLES OF GPAVITYI GCONTO.)
'Q"g FOINI NAME ACCEL N ACCEL Y 7
, ACCEL X-7 N=Y-2 ACCEL ACCEL i (. =, , 263 .9h6 .166 .812 .812 .R29
. it .4 45 .166 .788 .784 .ao5 g iv. ..u. . .. .,sa .res . ry ,
-Q. 29s 207
.045 .16s
- 7A9 .781 79 7 [
],
,, .003 .166 .. '.7e0 .7aC .797 j q
. . . . .~. .... ..., . . . . . , , ,
o: 10
!iff illt i!Hi i!!!i i!UI
.... c ...... ..c
'Q. 213A .835 C .166 i 1.721
- I.721 1.72 9 '
.'. , .,3 ,
. 214 .038 - .16 8 ' *
- 1.578 1.579 1 5A 8 far, o <sva .c.s .s.i s.ge, e.g2= s .gg s
'On 215 .639 .187 1 212 1 213 1 227
. 218 . *40 .229 .864 465 e4'4
, iii e vi . .25. ee.. .wei .e5. ---
.Or, 218 .J53 .182 , .781 .743 .804 219 .s3s
.7s1 .yn3 '.se2 ' . , ,.
... . . . .17.3
.. . ., .,.. .,.. .r.,
i~ e
'O n 221 .431 .16s .7Aa .7A1 .799 o 222 .g25 .346 .78J 7A1 79A
, f25 .eie .iee - . .iee .iei . 79 6
'Oc 223A .n14 .166
.t .7se .7ec .79 n .
2238 .see . 166 + .;no
< >.!, se .7.97 2_
., .o. .... ..
Q ,, 224 . 34,1 .146 .78. .78i, 79 7
, 225 .uhu .166 .7Aa 783 797
, v14 .isi seii .i55 i.;ii 155 '
O viu v2A s.951 .s 7 2.72; 3..c1 3.4s t. ' -- - (-.G or ps,V- 20ioC
, . .lol .215 1 626 1 629 s.s4 3 % d. C, y nV-gosos i
* .cc .c.. ,., . ,.... ,.. -
g v3a 1 412 .s 4 .e i . 3.s2n 1 7. e C,G, or psy.golo A
, V3H 4. 2 a rs . ', . 4 9 9 (. 4.316 4.34f
- vs= i.sii .351 e .e 2 3, e.-ts; e.vik -
O" v5u 2 37e .551 19.o7e 19 217 :=.225 ' - C. G. OF PCV Af 55 A ,
. v6A .459 .5 6 s.ss! 3.ns 3.74L 4 d.G. y PCV- 4 (, -
a ves .s,s .; e i.;i; s.cie e . 33 2- -
^ 5" 2'3 *'" '**'8 2 *38 O =,
, v7h l1 '. "o 7 a .193 1. t# 3 4 1 488 1 5df
. vfC 1Titi ei;5 i.4;i i. 0; i.e.4
'O = " *2" "' 2 *'3 '' d 0 N NDE8004 w '8A ' 3 2 f- *2 2 I3 *95*
, vna vs.r; .i - '.aos 8 'I 2 .;w . ;; ;
O" "'C ' 5 ? '* 3*262 Van .' 'S . 5 .2t? .857 92 94 ; C.G. OF PfogD00 8 Ou 4 o <
s > ye liPFLL CURPOJAT104 . PACE 336 o S L'P E G P I PE WLMSION IFAo 1*/81/888 S Y* T[F IPfYLL - N3* 84/03/12. 12 83.3 % ) PGE TROJAN NUCLFAR STATION c L OS P ROBLEM - 3
- C .18-P C-f'1 S TV.1 g rR L L A UR a sL M SERT LINT
) ., AF.-DUILT GECMEIPV WITH ! LUG DIVFRFION DEVICES 65003 o ) F 08CE TIME HISTORY NO. 1 (FTH1) GLOBAL ACCELCRATIONS (MULTIPLES OF GRAVITY) o ruins a v i x-7 F-Y-7 ), NAME ACCEL ACCEL ACCfL ACCEL ACCEL o " e asa 4.ses e.ags g.s u :.zia a.555 . l ).y 129 148 5 857 . 2.1s6 2 126 1.L49 4.601
".165 5.9u9 5.5F8 6.28e l 3 7_n7 . ,,, a.,a. 4.<., ,.,,a 2.ea, s.< ,
142 3 743 2.156 4.926 6.187 6.%45 )u 7.5F% 7.84 8 Z-cs 146 3.908 2.n87 6.479
, ,,, a.,aa .. .. ..< , ..< a ..,,a
)c 148 - 3 952 6 2kt 7 213 8 224 1 G. 311 ', 856 13 186 .3,418 . 9.315 16.079 16.437 ... 8l_ o ass aa.sva 4.use i s .g ns at.aen ar.ges ao yo 158 13 133 2.833 14 283 19.403 19.609 p o 161 12.869 1.#20 15.818 28.391 2f.441
, aos ac essa - z.asa an.ise <a.aus ga.gbg ;g
)r 163 12.895 13.131 18.910 22 151 25.75r a 178 14.234 9.784 18.728 17.823 28.329
.,,r r -- .~' <sw .<ne . ova .aes .arv #
). 214A 1 551 1 178 .667 1 689 2.05* m 216 1 593 .714 .P16 1 79e 1.927 o-c van s . ai .1 a... .,=< z.nea a.az a m - C*C,* OF PCA/- 456A
~
M V58 16.841 1 864 23.L34 28.069 28.131 )c
. V6A 3.482 2.699 .458 3.433 4.367 T d.C. oF A'V- 4% 9-e ..o n.1,2 <..,v ,.avv u.es, sa.us g
) ., V7A 2 723 1 773 1.746 3.2% 3.689 m m o V78 4 56u 1.770 4.073 6.114 6.365
, ,,6 ao.sga ..rs. ar.uge <a.13 < a . e s. s
) ., V7D
- 2.934 1.012 1.441 3.269 3.422 m t' 6.. Of Af0f 00(> A
. V8A 3 1st 2 428 954 3.252 4.n53 . , vRo 5.5i, 2. is a.e,7 a.rsa g.gse V6C 6.074 2.420 7.8.26 9.255 9.966
) ", V80 3.197 2.338 .308 3.395 4.122 7 d.C.OF140EOOOB e . )= ( ) *8
.e es
)= ., S. ) t.
~
. p d
) - O 1 .<* 6 m s __ uu-4. N N - M m W m armer
~
e IMPLLL CpWF SUPEOPIPE V fd N S W l'#41/3'3 S YS TEC3 IT.PELL - C0S (V PAGE 306 84/03/22 11.35 564 d (m) O-PSE TROJAN sa:CLEAp STATION EDS PROBLEM ;3D.'c18-RC '1 PEV.1 ? O PPESSLRIZEP S/8V LINE AS-BUIL7 GEOMETRY WITH MLUG DIVERSION DCVICES 8%DDI O . FORCE TIME HISTORY NO. 1 (F7H29 GLO84L ACCELEPAf!0NS (MULTIPLES OF GPAVITTI (D POIC7 X Y Z N-2 W-Y-2 - CAME ACCEL ACCEL ACCEL ACCEL ACCEL (D 84A If. 813 16 9'6 22.114 24.612 29.358
~ ~ ' ~ ~
7 87 2.729 14 417 9.6*5 9.9Ac 17 535 88 db
.4.756 3". 772 41 1C9 41.384 43.02" 89 6.196 21.518 43.689 -44.121 4*.C8 P 92 14.074 "P.580 6 C . 7 3 '. 62.339 Pt.278 i GD 49A 27.347 14 228 2 68R ~ 27.479 30.944 52 18. 936 ~ 11.945 '~~ .729 18.969 '16.212
~ ~ ~ ~ " ~
""~" ~ ~ ' ' ' ' ' '
53 45.692 9.880 .994 45.704 54 48.426 22.027 1.379 48.445 46.758 53.21e
'S 57 49.358 11.997 2 886 49.442 87.265 l 134 16 387 18 013 in.9r6 25 019 30 823 5 8 16 6 721 16.7A9 6.799 9 563 19 3ns .
17 25.345 15 341~' ~36.887* 44.696 47.25r
~ ~ " ~ ~ ~ ~ ~ ~ ~
'- ' ~~'* ~ '
18 '30 397 24.712 36.253 47.310 53.375 y 9 22 45.573 (9.453 43 559 63.042 93.79P v1 , 209 21 274 29 619 1 496 21 359 3 A.517 m 214A 6.612 15 339 7.623 IS.f92 18.361 -< (D 216 7.968 9.877 9.294 12.237 15.726 VI A - - '-v" e 14.1o7 - 77.725 se.s87- 25 2e5 3a.813m d;c. y psV-g6 toc- -- c vp. V18 37 103 17.725 54.496 r 65.928 68.269 '
^ $
V2A 10.382 1 582 27.767 < 27.722 29.616 m 6.d. or PSV-80tD8 * .
. . m V2B 72.752 10 302 4.568 72.896 73.62D V3A 5 393 12.931 24.153 24 747 27.922 ; (,.(,. Dr PSV-goto A c3 g e V3B 67.43 n 15.969 .__ 12.931 . 64.229 . 66. 178
, , . . ___ . .r3 I '
G' e m I e e t . . . . . . . . .. .. . .- .
,e e
1
$UPECPIPE VERSION l'A,10/01/838 S YS TE M IMPELL - NOS PAGE 11 (
84/03/233 11e16.163 PGE TC7JA'3 NUfLEAR STATION E35 PROBLED G300:18-7C-31 REV.I Q PRESSORIl[R S/RV LINE AS-8UILT GEOMETRY WITH SLUG OIVERSION DEVICES (500: O Q
~
. O O
................ ................. 0
. DESIGN -
Q VER IF ICAT ION . Q END LO AD SUMM AR V . . END LOAD
SUMMARY
9 '
. . Q
- CLIENT .
Q a0M NO. /9 E D C - Orr- / TCal . Q
. CALC./ PRO 8. N0. O b- [ .
G p Q PREPARE 0 BV: - p DAT[: 8 [
. CHECKED BY: gp/d DATE: 7 p[gt
- a D
0 s O b . 0 3 0
;V U O O o O C o c o o o o o o o o I
O O o o O 1 1 e 1 {
- w. *
.s
'E )
l
)
R w
& ww
. w R&
ss
- We
.wn W WW
- . s ==
w ww ukw==tww .
- b . ww .
E - 6- .. 33
- U W.. .s --
.- w I 'I w
. w w.
. u w
.s .
uus s&&..
- W L..
3 W .E BE ww 6&
)
.- - ww
. .s ww w t
R & s .s .s -o
..EI.s..
.w
===....s W
W = 0 *
- s.t**ds "
~
~ . .
.= =
-WW
= .
. ww wws.W w
.&E--E ....33W4
.33.
.s
.w wwm y
. . . =
W w
= 3
- - - a s - ..
. I.. ww
. .ww --uWW -...
..z s....
I W E R o
=
u
.sss s . t --
=
w a. w u
=
*.....W w
-ww.ww..www
. 5.
. .L Es. .
s o S w w U W
.o &W w
. :w W www
- o. . . .s s. .....w .=-UU..&hto..sas
- .o a o = s.s---. wwww ...
a -u.W-
. . . - =www... -w ssa.s.B.B
. .....gwwsm.a.== www
.S l
Y
,23"
- w. . IEttttw3:2 EEEWEE:
sw - gM%W s'"E-n.w E
,. nww.gg--
. ~ .-
a r E
- .u u. l. d.
i
.... .=
Z... - E . ws - .
- ......ww--...w.....
. w 3
I==z=z=..rse== z a ..--zzz-... g g - o
- . 6 ---....
-g9 -
o w s E U s 3 W. 3 5 s o s
,t. B w
O O O O 0 O O O O @) Gh S L Jdh & R * * * * ' '
PAGE 13 Q Q I MPELL CORPOR ATIt1 SUPERPIPE VERSION 154, 1E/81/838 SYSTEQ IMPELL - NOS 84/03/23a 11e16:16e PGE TRIJA4 NUCLEAR FTATIOQ O Q EDS PROBLEQ t30aCIE=RC-81 REV.1 PRES $L*RI2[R S/RV LINE O AS-8UILT GEOMETRY WITH SLUG OIVER$10N DEVICES ($005 0 TITLE z FLANGE AND VALVE END LOAD SUMMaAIES O, O GROUP NO. 1. SUMM4ev TYPE z FORC. O O RUN NAME OCP LIST . .. 163* 140 192+ 146 ~148+ 16 18+ 52 54* ST 89* 156 158* 161 O Q 222 G ROUP NO. SUMM AR Y .T TPE s FORC. TITLE N022LE LOAD
SUMMARY
O @ 2. OCP LIST O Q RUN NAME 221A 3* ?M* V4+ 114* O O GROUP NO. 3. SUMM AR Y T1PE
- OISP. TITLE
- SLEEVE DISPLACEMENT AT EL. 68 FT. OF 12=-RC-681-2-1 RUN NAME OCP LIST O O 211 O
O GRCUP NO. 4. SUMMAR1 TYPE DISP. TITLE z 8R ANCH DISPLACEMENT
SUMMARY
O O RUN NAME OCP LIST Q 22 13A 49A 844 123 118 209 216 92 ST 214A $O06 5033 S016 5026 Q O O
~
O O O O O O t O O O O . O O O - O O
- n_
) O O O O O o 0 -0 0 o o O o o o o o O O O O
- m. ,
e l m , em
~~
LE . d -- 2 2 2 W D u u u 2. o "3
. ==
u --
.w W E
- 1. E. I L.R m.
R R R
. W.*R W W E d
- WW W em e W- m .h &. W5 g. 3. b.
m .m W-M W
& =e
.m mo ge
- 6. o W e
.B .E E P SP me D P --
&
- e- e-- e- M. J --
e e- - Wm W- wu M W W D D > S WW
*
- UL UL db b EE W
a W 5 F. w d. L suO sw. e.v
> ew EO DS e.
t
- E W W
.E W U.
M
& J b.
W > W. h. W O W O W
- m EW-d em W
>E dL e.
b b e
>E L
JE Wb WE LL m> UU H @ d bM bM EM em -- b > c - e E > W W M EE W -
- D . O -S -O 20 O FM - W
- e - da dd JJ -d da -- d 6 W JO W. W. .O JO WW W e E. 3 ou .. EU .M GU Om E M
(% s m
. e o e e. e .a ee .. ee e , e
% e - - -- -- >- e m
w 4J -
$5 mW e
5 e FE e o
.. k.-
. .e .e -
e a me e e
/
WO .e .e .e 4 6 .e de .e .e .e .e mm O m - e e de ee we se ee mm W P. m WWW W6 WWW WW W e o e e e o e o e e e e ee m e o arm em r. m m em W - - -m -- em mm -- MO 4 W - 446 , 46 444 64
- m m -m um mm um en mm o m - U U *4 UU UUu uu I , >
g 3 3*2 *S2 22 e o e m mm e e o e e e o e e e ee . e e 00 2.". OKO 90 s W- em J w a ddd de dds ad o 5 -. m. . Ee
- e. .n m..m .m.m .m.m
- ~
% EE n .
E
- e. -Ow M. m. e. .n . m m.
- m. m. e. n. m. m. m. m.
K W m M
- m. . =--
E.E WWW WW wE WE EE W WW W % % %% %% %% %% 4 % % JJ
.J J t
-e e
.c .e .e .e . .e w
.s .
e ..
.e E
W
.e e
- d. d d
.E .E WWW WW WWW
.d .d .d
. .E WW l W
, :$ .m . " 3 WE .. ,. .. .. .. .. . . . .m . . .. ee d. de m
. e. a.
- e. e
. e.
. = .u u - m em -- m- m -- m- - m - me m -m m-m --
l l nW
.U.W.
E-.
. End.
W -
. . .. -. m. m. - m. .
. m. .
d..E E-
- d. W-
- ~
> . m... .s .. m, E e.
.e e
~~ W - ~ = = === -~n WW .,
.. ue
- m. u. m. ==
- Wm.%W ., E ar == == xx == .E - - 2:= == === ==
n SEW .5. W . e. -- -- -- -- -- 8.. . . --- -- --- --
- m. E nWW.
4dN 0 L.g5"3 E E 5 * - t t E !
- .. M. .Et. E. . , E.- . = = = =
W U- O S S "O S W W W W e WWW. B 4 pe.m O
-W
(- vi m mWh4 - E R E E 3 E E E 2 E E E E E
.E O
2 E O E E l 4 - E E E E E u o a .E .E .E .E . . a a a a = = = 6 s . 4- b r r - u w oW
==
> > a
= = a a
a e a e a a a a a
- I Eaam a a
=
a a a I & O. E M m m a m . . > - a m a b ,,. M J- E. . lea W W W W W W O O W laa 4mf 4ma i ina e-.W e h W WW E > - N m e @ W W - N 6 E
. U O 4 WE O e E E E 3 E 9 M E E S E E dh W ee > Z R R Z 2 W --E Z Z Z JE WE I E. - - - - - h b - - - -
WW D
=& 4 3 .
- en d u _- -
_ _ _ _ _ _ _ _ _ _ _ _ m m . -
D $MPELL C0aP0mafICO PACE 15 .. Q, S UPE CPIPE *ERSION 16As if/%1/Sil SYSTE3 IMPELL
- NOS
- 04#93/23 18 85 86. '
PGE TROJA2 NUCLECR STAft0N O ECS PROOLEQ 539;OIC-CC-01 CEV.1 PRESSURIFER t/R9 LINE AS-OulLT GEONETRY WITH SLUS OlVERSION DEvlCES 65003 $
- O LCA3 CASE SPECIFICATION SCONTO.!
- O CASE LOAO PRINT COMO RES8JLTS SCALE DATE TIME NAME TVPE CODE TYPE SE1 FACTOP IDENT. 10ENT. TITLE O
THMU ERPN PRIN ASUR THet 3 930 EARLIER LOAO CAtt t THno - 1 008 [ARLIER LOAO CASE O FTHE OTNU PRIN ENVA FTHI 1 981 EARLIER LOAO CASE D FTH2 8 000 EARLIER LOAO CASE O RVOS OVNU PRIN SRSS ONE 1.999 EARLIER LOAO CASE Q % FTH1 8 900 EARLIER LOA 0 CASE SR00 OTNU PRIN SR$$ OBE $.895 EARLIER LOAO CASE FTHE 1 089 EARLIER LOAO CASE O SRVS OYNU PRIN SRSS SSE 3 989 EARLIER LOAO CARE FTHE 1 889 EARLIEk LOA 0 CASE Q a O. o O O O o O O o O t o O O O O O. _ _ _ O_ __
- - , a.mmme ==== .~ m SEPL.. 29"l ...a.104 .
PAut 16 s VERS 303 IfAe 1s/?!/831 SYSTFM 1PPFLL - NOS SUPERP{ 84/03/23e 11( ;6.
~ WI. PSE TROJAN CUCLEAR STATIO3
. . EDS PR08LEM 0340818-RC-01 REV.1 '
PRES $URIZER S/RV LINF C) AS-8UILT GE0 METRY WITH SLUG DIVERSION DEVICES ($003 l r i ($ j END LOA 0
SUMMARY
FORCES AND MOMENTS FLANGE AND VALVE ENO LOAO SUMMARIES l L ,.. . _. .
@ RUN DCP LOAD FN FY FZ F YZ
- MN MY MZ MYZ _., M M Y Z RAME NAME CASE (183 (L83 (LB3 (LB) (LB.FT3 (LB.Fil (LS.F7) ,8Lt FT) (L9sFTl
~_, ,
CS fMsV-800A 87- ' o_._ HTD4 ._ -267.54.G_ .?25.15 . -15.59.. 29.55 . 8 61 -232.76 18.7 0 ,_ . 233.51 733.67 .; GRAW 6 37 51 59 ~5.31 51 92 -5.29 113 95 -22.54 116.16 116.28 + () THM1 841 13 -4109.37 1487.54 4374.32 294.84 578.84 -1729.98 1823 99 1835 46 THM2 742 02 -4309.99 1534 15 4574.98 169.03 321.42 -1521.46 1554.83 1563.99 I THM3 742 91'"'-4306.54 1541 55 4574 13 169.74 320.08 -1521.95 1554.36 1563 69 () ' THM4 _i~. THM5 742 89 i *4312 57 1536.69 4577.97 169.38 3 320.28 -1521 51 , 1554.e5 1564 05 i . . . . . . 6 23 3 6 4;28536.81.. 1238.59 ;--- 8625.4 8 419.87 - 25.59 -1558 61.. 1558 02 1614 37 . . _ OBE 846.75 2328.71 2914.41 3079 08 4847.40 938.94 6168 59 6238.44
- 790s.34
,() SSE 1934.03 3888.95 3364.06 5142.96 8895.15 1554.67 18301 55 19418 20 13193 57 e i FTH1 22.48 31.67 32.67 45 59 34.64 28. 96 13.76 32.46 47 20 FTH2 , 137 9.54 3629 14 3879 31 1651 55 4643 41 4286 84 6319 67 ~ 6531.91 C) ! THMS ' ~,841 76 1348.59. 8'*" 9.00 1541 55 1541.55 204.84 578.84 0.00 578 04 613 26
- t. ._ .. _ . - .IHM0 .u See t.M .-4312 57..... 9 00_ 4312.57 . 0.00. 0.09 p1729.98 ..1729.98 1729.98 . ..
THMU 841*.13 4312.57 1541.55 4579.81. . 294.84 578.04 1729.98 1823.99 1835 46 , () FTHE 7642 58 1370.54 3629 14 3879 31 1651.55 4643.41 4266.84 6319.67 6531.91 i RVOS 847.02 2328.93 2414.67 3179.42 4847.52 931.39 6168 61 6238.53 7908.48 l . ' SR 08 " '1689.347 " 2782.09 4158.72 4952.75 5121 82 4735.81 7511 89 8880.32 19258.92
~
! () -
.SRVS 7772.29 9
~,. 5 > 4 123.38 4948.49 6191.26 8261.91 4096 76 11157.91 12185 12 14721.97 _. -
. .: h.:... - > . . . . - ~ . .... . n . .. . . .
--..&. -~ - ......-.........A
() HYDR -2 97 -1149 19 1.2' 1149.19 -19.95 9.79 1323316 1303.20 1393.35 GRAV ~ ~ ' 87 -866.70 .57 866 78 ~23 11 -5.82 698 65 698 67 699.C5 4
, "THM1 ^19 7.9 fT*~ 841.13 77.61 844.70 1652.ee 277 96 -1223.43 1254 60 2075.93
! C) ' THM2 161 61 j 742.82 71 14 745.43 1997.58 _ 243.67 -886.50 919.38 1757.21 -
. . . . . .THMS. 2 .. 161 6 tfu;m.742.91. 71 19.. 745.42 1997.82 244.45 ~886 13 919.23 1756 72
, 71 14 e
i THM4 161 68 742.00 745 48 14*?.55 244.04 -886.34 919.32 1757.21
- () THM5 1E4.88 623.34 68.59 626.s4 1420.41 461.59 -489.24 666 18 1568.04 1 i OBE '
513.46 275.54 2843.57 2856.89 1981.47 2280.22 517 23 2338 15 2543.68
- SSE*' 857 483" 468 14 4748.76 4771.01~ 1672 46 3807 97 863.77 3904.71 4247.81
~ () FTH1 9.35 25.38 12 27 28.19 11 10 2R.71 64 73 70.01 71 68 6 _ ..%...... . F TH2.,. 14414.852ia .8328.55 699.52.__. 8357 11- 1386.96 1438.09 19266.63 _.19320 23 19369.95 : THM8 161 62 841 13 77.61 844.78 1652 88 277.96 0.00 277.96 1676 81
;qp THMO 0.9p 0.88 8.f0 0.00 n.00 Pett -1223.43 1223 43 1223.43 l THMU Ifl.62 R41.13 77.61 844 70 1652.R8 277.96 1223.43 1254 68 2475.03 FTHE 14414.05? ' 0328.55 690.52 8357 12 1386 96 1438.09 19266.63 19320 23 19369.95
- i j GD
,RVOS 513 54 276.70 2843 68 2857.P4 1801 54 2280.48 321 26 2339 22 2544 61
. . <$R08 14423 19 _.8333.14 2926.21 8831.95 1710.73 2695.83 19273.58 19461.28 19536 24
! SRVS 14439 53 8341.25 4798.71 9623.18 2172.74 4078.47 19285.99 19719.86 19838.25
' () ~.
PSV-EmoG 52-
.' HYDR -245.16 -20.35 1.79 24.43 18 59 9.82 192 22 192.47 192 77 '
- () GRAW 25.98 18.33 -42.68 46.45 2.40 -7.33 -138.87 , 139.06 139.88 !
i C) - t ILS
. .. . . t&wt 4.
SUPERPIPE VERSIO3 1&A. 10/91/438 Sv' TEM IMrELL - 4 ? 84/03/23e 11 16.16e PGE TP0JAN EUCLEA2 STATICU 3 EDS PRC'LEM 936*i10-RC-81 CEV.1 PRE 5htRI2[A S/RV LINE ~ AS-BUILT GEOMETpY WITH SLUG DIVEPKION DEVICES iSDD) $ E NO LOAD
SUMMARY
(CONTD.) F0PCES AND MOMENTS FLANGE AND VALVE ENO LOAD SUMMARIES dD RU3 DCP LOAD FM f7 FZ FYF ' MR MY MZ MYF MRYZ db CA%E NAME CASE (LB) (L8) (LB3 (L8) (L8.FT) (L8.FT) (LS.FT) _. (LO.FT) , ,,,,,t L 8.F T ) ,
- P9V-@f08 52- (CONTD.3
- S THM1 1229 11 23P.08 SP68.54 5073 75 563 53 -929 96 326 28 977.05 1127 91 THM2 1636 82 298.P8 5418.30 5422.3G 694.74 -1452.73 554 54 1554 97 1703 11 THM3 1036.69 207.57 5428.A1 5432.77 696 23 -1454.50 554.60 1556 64 1705 25 db THM4 ~1e!6.77 2f4.92 5422.23 5426.10 695 10 -1453 29 554.36 1555 43 1783.60 THPS 823.34 ~-1647.59 ~ 8750.34 8902.25 1293.35 -2407.99 " "'756.03 ~ 2523 89 " 2435.90 ~ ~
-1 OBE 41388 1442 98 3745.72 4013 73 215P.73 2120 99 198.33 2266 26 3129.07 db SSE 6*1.18 2408 28 6255.35 6742.*2 36#5.00 3542.66 1333 22 3704 66 5226 00 FTH1 10 07 19.22 39.44 43.A9 21 06 12.49 14.36 19 03 20 38 FTH2 7757.50 4043.40 919 68 4146 68 772.66 1519.51 5047.34 5271 10 5327.43 . db THMS ~ 1229 11 230.0A 5428.A1 ' 5433.68 696.23 0.00 554.G0 554 60 890.13 THMD~ 0.00 " 8 00 0 00 O.00 0 00! -1954 50' O.00 1454 59 ' 1454 50 " ~ ~ ~ ~ ~ * '
THMU 1229.11 239.08 5428.81 5433.68* 496.23 1454.5p 554.60 1556 64 1785 25 . db FTHE 7797.50 4043.40 919.68 4146 6A 772.66 1519 51 5847.34 5271 10 5327 43 l RVOS 414.s0 1442 21 3745.92 4013.97 2158 03 2121.03 798.46 2266 34 3130.00 SR08 7808.48 4292.P7 3056 97 5771.04 2292 04 2609 12 5110.09 5737 64 6178 00 db 3RVS ,_, 7828.PT,_, 4706.26 _ 6322 59 7881 88 3686.95. 3834.23 5220 45 6409 08 7463 36 , , _ , _ , PS14006 54-e HYOR -13 52 -1126.82 .83 1126.82 -9.79 10 56 1231.21 1231 46 3231 30c. , GRAV -4.P1 -847.PA ~1 47 847.09 8 78 1.63 658 51 650 52 650 57 THM1 -141 68 1229.11 121.00 1235.65 800.62 677 53 -1822.37 1226.49 1964.68 db THM2 1936.82 -4.t1 1836.83 1503.72 713.26 -556.25 904 52 1754.80 THM3 " -117.21
-117.18 ~ '1036.69 ~~ -4 24 1036.70 1565.77 '714.58 ~~ -55 6. 0 3 "* ~ 9 95.4 3 ~~~ 17 5 7. 0 3 '" '" ""~' ' "'
l THM4 -117 21 1r*6 77 -4.08 1836.78 1504.36 713.56 -536 39 904 04 1755 52 db THMS -53 53 823 34 -138.38 834.88 2442 92 1992 10 -172 19 1185 59 2601 45 OBE 78.67 266 60 829.93 R63 14 1841 60 2164.77 611 25 2249.42 2470 07 SSE 131 38 445.22 1370.96 1441.44 1739.47 3615 17 1920.79 3756 53 4139.72 GD FTH1 10.70 11 27 15.55 19 20 18.14 19.05 28.03 33.89 30.44 FTH2 14307.71 ~ 9338 94 319.21 9314.41 245.24 490.61 29930.20 '20935.99' 29930.79 " " THM8 0 00 1229 11 121 00 1235.05 1505 77 714.58 0.00 714.58 1666.73 " ' ~ ~ ~ l (D THMD *181 6R 0.00 -4 24 4.24 0 00 0.00 -1922 37 1922 37 1822 37 i THMU 191 68 1229.11 125 24 1235.4,7 1565.77 714.58 1022.37 1247.34 1955.31 FTHE 143(7.71 93rA.94 319.21 9314.41 345.24 490.61 2093p.20 20935.95 20938.79 9, RV0B 79.39 26E.P4 A?1 08 R63.35 1941.76 2164.86 611 90 2249 67 2479.17 '
'] 9
~ ~ '
14397.92 SR08 9312 7M 880.81 9354 32 2219.67 20939.12 21056.94 21085 01 SRVS 143ta.31 ?319.58 1407.63 9425 2A
'1897.33 1773.40 3648.31 2n*55.07 21270.29 21344.09 ,
- @-10l0C 16-HYDR -241.35 12.og 2g.ge 27,3e 3,g3 .gyg.15 63 66 198 12 198 16 (p GRAV 11 25 -43.72 19 19 47.74 -2 55 102 31 ~69.43 123 64 123.67 THM1 1*79.3A 550s.19 -38.e4 56C4 29 -R63 30 -677.72 1914.75 2031.15 2207.00 THM2 1326.85 6?l2.P0 -1*1 83 6012.AT -992.A4 -887.94 2530.45 2681.72 2859 60 ']dD e
G -. - - O G -
' "^
IMPLLL u seION
- PAEL 10 S UPERPI(v]7ER14/01/938 S IO2SYSTEM 16 AIMPELL e - KOS 84/83/23.Ild'~'% v.6 d4 PSE TP0JAD WUCLEA2 STATION ;
/, LDS P908LEM c388J1e-RC-41 REV.1 ,
i PR E SS L'R 12 E W S/RV LINE db AS-8UILT SEONETRV WITH SLU6 O! VERSION DEVICES (SDDI ' r i () ENO LOAD SUMMAR7 SCONTO.) FORCES AND McMENTS FLAh4E ANO VALVE END LOAD SUMMARIES C) NUN DCP LOAO FN FY F2 FY2
- MN MY M2 MYZ MRYZ CAME NAME CASE SL83 (L83 (L83 (L 8 9 (L8.FT) (LB.FT) (LO.Fil (LS.Fil ILO.FT)
(> l F5V 8000,16- tc0NTO.
- i. ._7HM3 332s.s9.__.6e12.a9 -9e.26 6e12.76 -993.,4 -ses.32 2531.07 26st.43 2e6e.65 THM4 1326 90 6C08.63 -97.25 6009.42 -992.72 -888.09 2530.15 2681 48 2859.35 l () THMS 1452 22 9602 6F ~2410.45 9988 59 -1631 54 -1122 32 3607.66 3778 20 4115.42 OBE 83e.54 2310.96 2484.55 3393.16 2478.58 1703.83 3639.97 4019.01 4717.65
$$E 1387.01 3859.31 4149.21 5666.58 4125.00 2845 48 6078.75 6711.74 7070.47
- () FTH1 24.A4 .
32.39 26 35 41 75 23 80 14.21 22.70 26.79 35.e3
. _ ..FTH2_ . 8697.38 .2 . 3914.35._ 3476 44 4536.41 2695.59 7832 02 5805.e3 , 933a.43 . 9719.78 THMS 1579 38 6G12.99 0 00 6C12.09 0.00 test 2531 07 2531.07 2531.97
{ () THMD e.n3 4.PO -101.83 Is1.A3 -993.94 -888.32 0.00 808.32 3333.05 . ! THMU 1579.38 6012.C9 101.A3 6812 99 993 94 888.32 2531.97 2682.43 2060.65 ! F T HE e697 38 ~ 2914 35 3476.44 4536.41 2695 59 7832.02' 5085 03 9338.43 9719.78 () RVOS 830.92 2311.19 2484.69 3393 42 2470.78 1793.M9 3640.04 4019.10 4717 78
. . , _ 49 0S _ _. . 8736.99,__.3719.40 , 4273.01 5665.03 3656 50 8815.21 6254.23 19166 55 19804.11 SRVS 8807.28 4836 98 5413.19 7258.73 4928 39 8332.08 7925.71 11500 36 12511 71 Psv-90 lac. 18-
' HY DA ~55.76 -1122 95 -18.77 1323.80 73.93 -13.97 1172.45 1172.93 1175.26
. () 6 RAW -17.51 -861 82 . 59 861 92 -9 93 -3.42 667.43 667 43 667 51
_ . . T HM1 ,.._-3 93.9 7_. __15 7 9. 3 8 . . 1579.43 -le73 17 -852.27 -58.67 e54.29 1371 6s , THM2 -27.41 1326.85 31.78 112 48 _. 1331 64 -1569.R4 -915 10 975.97 1337.80 2061.99
- () THM3 -87.34 1326.89 132 95 1331.69 -1569.36 -916 16 976.72 1339.15 2863 06 THM4 -87.44 ~ 1326.99 112.84 1331.69 -1568.66 -915.92 975.at 1337 71 2361 59 THM5 115.54 1952 22 223 59 1875.71 -2238.18 -1327.91 2050.95 2443.38 3313.48
; () OBE 75 18 272.47 1787 94 1888 58 471.19 1223.47 459.16 1306.79 1389 15 SSE 125 55 ._ 455.03 _ 2985.06 3029 33 786 89 2043.20 746 80. 2382.35 2319.88 ,
FTH1 9 12 13.77 46.97 49.*5 55.89 37 43 33.42 58.15 75.09 j () FTH2 19442.14 9926.74 1656.22 18463.96 1992 72 1584.52 21794.53 21852.05 21942.72 THM8 3.nn 1579 34 112.95 1583.42 0.00 4.00 976.72 976 72 976.72 THMO -303.97 0 00 0.00 0.00 -1569.36 -916 16 -58.67 918.03 1838.35
. () THmu 303 97 1579.38 112.95 1583.42 1569.36 916 16 1935.39 1382.52 2891 47 FTHE RV08 .. 19442.14 1656 22 In463.96 .1992.72 1584.52 21794.53 21052.95 23942 72 i i 15.73 ....,9926 74 ,
272.82 1788.56 1809.24 474.49 1224.63 460.41 1307.76 1391 18
- () 14442 34 SR08 9930.48 2437 17 10225 17 2047 67 2001 89 21799 36 21891 99 21986.65 '
l SRVS 14442 69 9937 16 3414.44 10507.41 2142 46 2585.68 218ve.91 21960 75 22065 01 " O l#40S8 1*8-f.49 HVOR -3.71 84.16 D4 14 5.98 ~4.48 -384.66 184.71 184.81
;* GRAV -3.76 80.13 3.n6 81.16 8 28 -4.65 -176.73 176.77 176.96 THM1 20.u0 272.P4 54.4* 274 27 22 66 -116.65 236.83 263 28 264.25 ; C)
THM2 -1917.5? $53.37 -1S*.30 556.6" -154 27 -777.32 962.#6 1236.84 1246.43
- THM3 471 16 236.09 46.59 248.65 181 22 654 12 -82.24 6C5.73 632 25 l () THM4 -223.99 367.77 -97.18 380 39 -2.32 -81.82 429.24 436.97 436.98 I C)
IMPELL CORPORATIO3 P2GE 19 (]) hj SUPERPIPE VERSION 16A, 18/01/838 SYSTEM IMPELL = NOS 80/83/23 11 16.16. PGE TRIJA3 NUCLFAR STATI03 (]^ EDS Pp08LEM L300018-RC-81 REV.1 PRESSURIZER S/RV LINE gg AS-BUILT GE0 METRY UITH SLUG OlVERSION DCVIEES 4$003 E NO LOAD
SUMMARY
ECONTD.) FORCES AND MOMENTS FLANGE ANO VALVE END L0a0 SUMMAP1ES () i CUN CCP LOAD FN FY FZ FYZ . MX MY MZ MYZ MRTZ () CAME NAME CASE ELB) SLH) (LSI (LB) (L6.Fil (L8.Fil (LB.Fil ELO.Fil (LB.Fil Moto008 140- ECONTo.3 451 97 o THMS -2!7.91 371 83 -81.83 379.94 7.33 -81.41 444.59 451 91 ODE P8 11 167.65 289.56 268.37 93 16 473.31 345 88 586.18 593.53 - () S$[ 147 14 779.97 349.97 448 1A 155 57 799.43 577.49 978.91 991 28 FTH1 4595 97 818 96 76.P7 P22.48 79.61 99.69 523.53 532.93 53A.65 FTH2 9.46 48.05 7.18 48.57 4.27 5.A6 25 88 26.46 26.88 THM8 471 16 533.37 54.49 536 15 181.22 600.12 962 86 1133.89 1148.28 () THMD -1817.52 8.89 -159.36 159.34 -154 27 -777.32 -87 24 781 66 796.73 THMU 1478.64 533 37 213.7* 574.62 335.49 1377.44 1844.29 1728.55 1768.88 FTHE 4595.97 818.96 76.87 822.48 79.61 99.69 523.53 532.93 538.85 () RV08 4596.81 835 94 222.94 865 16 122 54 483 78 627.42 792.22 881.65 SROB 4596 01 855.94 222.94 865 16 122.54 483.78 627.4* 792 22 t81 65 ) SRVS 4598 32 865.49 358 14 936.67 174.76 796.69 179.47 1114.58 1128 2J ()
) HYD4 4.87 -293 16 2.49 293 17 -51 84 -3.18 -13n.45 138 49 148.41 ()
GRAW 4.#2 -797.16 3.06 297 18 -49.54 -2.78 -118 5F 118.53 12P.47 THM1 20.08 272.88 54.49 278.27 22.66 -61 72 -39.62 73 34 76.76 ( THM2 -1017.52 533.*7 -159.38 556.65 -154.27 -937.24 424.62 1028 94 1840.44 () THM3 471 16 236.99 46.59 2 4C .65 181.22 657.58 -388.94 763 99 785 19 THP4 -223.99 ?A7.77 -47.18 3R8.39 -2.32 -187.63 -26 99 189 56 189.57 ') THM5 -2?7.90 371.03 -81 83 379.95 7.33 -169.48 -15.36 178.89 178.25 () OBE St2.06 191.11 551 46 583.82 1165.82 266 96 431.21 587.15 1271 36 SSE 504 45 319 15 921.27 974.99 1946.92 445.82 729 11 846 95 2123.16
) FTH1 5175.64 728.42 116.67 736.18 183.73 166.27 184.84 801 47 822.26 ()
FTH2 31.93 17.87 11 16 28 4C 6.98 10.88 24.89 22 44 23.58 THPB 471.16 533.37 54.49 536 15 181 22 657.58 424.62 782.76 883 46
) THMD -1C17.52 n.00 -159.38 159.38 -154.27 -937.24 -38n.94 1814.74 1826.44 ()
THMU 1488.69 ?93.37 213.79 574.62 335.49 1594.82 813.56 1790.34 1821 58 FTHE 5175 64 72A.42 106 67 736.18 183.73 166 27 784.84 Srl.47 822.26
) RV08 51P4 45 753.07 561 88 939.98 1186 21 314.51 894.79 948.45 1514.89 ()
SR00 5184.45 753.*7 561.A8 939.58 1189.21 314.51 894 79 948.45 1514.09 SRVS 5248 17 795.26 927.43 1221 71 1955.57 475.82 1864 55 1166.85 2276.83
)
() HYnR .41 -115.3% 2.49 115.38 81 84 1.70 265.15 265 16 278.17 GRAW -1.78 -1". 63 3.P6 15 93 ,
-49.54 3.21 181.22 181 25 187.90 ()
THM1 2G.01 2F2.PA 54 49 278.27 22.66 45.8% -579.42 581 23 581 67
' -627.84 1399 18 1937.66 THM2 -ta17.52 5'3.37 -159.3* 556 65 -154.27 -1259.41 THM3 471 16 P'6.a9 46.59 240.f5 181 22 77*.10 -989.57 1253.91 1266.99 ()
THM4 -223.96 367.77 -97.1R 3P'.39 -2 32 -394.83 -928.45 1401 56 1801.56 THM5 -257.93 371.65 -81.P3 379.95 7.33 -342.48 916.06 977.99 978.02 i) ORE 314.?2 ?84.14 743 17 795.64 1165.42 It61 39 431.88 1145.R9 1634.69 () 0
-~
e e e
e=== .%
- am - '
Q" INPELL C SUPERPI All8N R$10N 16A, It/SI/P38 SYSTEM IMPELL - NOS . Pa*C 23 84/93/23e 11 13.16t Q q)
- l. :
- C) PGE Tr.0JA3 NUCLEA2 5T47103 .
g= tos Pp08LEM 13Meels-RC-41 REV.1 PRESSURIZER S#RV LINE I () AS-BulLT GEOMETRY WITH SLUG DIVERSION DEVICES 45001 (g , f () ENO LSAD SU* MART (CONTD.) FORCES AND N0MENTS FLANGE AND VALVE ENO LGAO SUNNARIES () () CUN DCP LOAD FN F7 F2 F12 . NN NY M2 NY2 NETF () CAME NAME CASE (LB3 (LSI (LO) , (LSI (LS.F73 (LB.F71 (LB.FTl (LS.Fil EL8.F73 ! O P ol- W , i i46- (CONTO.1
$$E 524.75 474 52 1241 17 1328 72 1946.92- 1772 52 721 25 1913 64 2729.93 o '
4 FTH1 5173.81 e95 4R 144.97 611 88 193 73 132 22 779.31 781 58 852 48 j () FTH2 . 38.63 14.88 p.12 16.*5 6.98 7.18 16.69 18.17 19.46 ()
- THP8 471 16 533.37 54 49 536.15 1R1.22 779.18 6 88 178 1 P 791 13 THMO -1817.52 G.88 -139.38 159 30 -154 27 -1259.41 -909 57 1594 61 1682 85 i ()
- THMU 14P8.68 533,37 213.79 574.62 335.49 2C2t.51 989 57 2249 82 2274 73 ()
FTHE **73.R? 593.48 144,97 612.98 183.73 132.22 77P.31 731 58 Se2.#8 i RV0R "
.f3.tt 659.80 757.18 in84.32 1188.21 1969.59 883.12 1387.86 1821 22 ; () SR08 L '. 8 3. 3 9 659.8* 757 18 1984.32 1103 21 1869.59 SR3 12 1387.'86 1821 22 ()
SRVS 52t8.36 161 43 1249.53 1963 25 1955 57 1777.44 1855.25 2867 89 SE15.54 l lO fDI-tSG 1*8- O i HYDR -5.99 194.93 2.49 1*4.95 -51 84 4.58 288.83 288.88 287.46 l GRAV 4.68 121 12 3.06 121 15 -49.54 6.65 113.63 113.83 124 14
- () THM1 28 88 272.R8 54.49 278 27 22 66 187.65 -889.53 896.92 896 38 ()
! THM2 -1f17.52 553.37 -154 38 554.65 -129.8R -1539.92 -1386.58 2872.19 2876 28 TH43 471.16 236.69 46.59 248.69 181 22 834.74. -1334.61 1574 16 1584.56
() THM4 -223.99
- 367.77 -97 1R 384.39 -2.32 -513.87 -1433.72 1523 82 1523.02 ()
THMS -257.90 371 83 -81 83 379.95 7 33 -441.91 -1433.50 1588 97 1588.49 . 00E R18.83 264.99 962.15 997 94 1661 17 771 74 485.74 911 84 1895.18 C) SSE 1552.76 441.71 16F6.74 1666.39 2774 16 1288.88 R11 19 1522 84 3164 65 () FTH1 57E9.67 1246.32 194.25 1261.37 223.46 148.74 1348.10 1355.42 1373 72 FTH2 51.M5 34.24 5.79 34 72 4.18 4.39 35.97 36.28 36.45 j () THMS 411 16 533.37 54.49 536 15 141 22 834 74 8 80 834.74
#194 92, 851 18 ()
THMD -1*17 52 c.ed -159.30 159 38 -129.88 -153?.*2 -1433.72 2197.97
- THau 1988.68 533 37 213.79 M74.62 318.38 2374 66 1433.72 2773.91 2791 21 l() FTHE 57E9.67 1246 32 194.25 1261 37 223.46 149 74 134R.10 1355.42 1373.72 ()
Avo8 5m26.26 1274.nP 981 56 1688 33 1676.14 784.47 1432.94 1633.62 2348 54 ! SR08 5826 26 1274 8R 981.56 168R.33 1676 14 784.47 1432 94 1633 62 2348 54
- ()
SpVS 5926 13 1322 28 161R.48 2089 95 2783 15 1296 47 1573 34 2838 68 3449.95 () I 156-l()pe?-8ccctA HTDR 3 76 -74.9? .55 15.9P 58.29 -2 33 93.78 93.81 118.44 () ! Gnav 2.M3 -A3.44 .35 83.44 51 89 -2 66 111 21 111 24 122 74 i THM1 -PL.62 217.98 68.92 226 93 190 90 -224.96 711 38 746.93 792.82 j () THM2 92".8R 1"M.84 =118.37 168.2C R0.46 -568.42 345.38 665 12 669.92 g) j THM9 -6ES.29 ?%2.84 79.52 368.95
\
276 67 443.14 1121.65 1266.01 1237 34 i THM4 216 46 213 51 ~45,90 219 2P 193.24 -7.82 787.99 768.92 733.93 l () THM9 242.45 2 7."1 -49.91 213.21 191.93 7.01 677.61 677.64 784.F5 () i ORE 13F8.41 615 11 1129.32 1285.97 221.34 1142.41 1057.P3 1556.41 1571 93 i SSE 2?la.69 1827.23 18P5.97 2147 57 367.9R 1987 82 1765.24 2599.28 2625 12 I FTHI 5602.47 623.Oh 1.93 54 617 15 78 14 111.39 664.59 673 78 677.42 () I() i irT r)
1 () IMPELL CORPORSTIIC PAGE 21 83/03/23a 11 16 16. (') j' SUPERPIPE VERSION 16Ao it/01/838 SYSTED IMPELL - NOS ' rw [) PGE TP0JAC NUCLEAR STATIO3 [DS PROBLEM D380018-RC-C1 PEV.1
=
kJ PRESSURIZER S/RV L1h[ [) AS-8UILT GEOMETRY WITH SLUG DIVERSION DEVICES 65003 () , [) END LOAD
SUMMARY
ICON 10.) FORCES AND MOMENTS FLANGE AhD VALVE ENO LOAD $UMMARIES () i () RUN DCP LOAD FN FY FZ FYZ - MX MY MZ MTZ MNTZ () CAME EAME CASE (LB9 (LB) (LB) (L83 (LB.Ff) tL8.FT) (LB.Fil (LS.F7) (LB.FT3 O MOg 156- (CONTD.: O FTH2 P.73 19.r5 2 89 19.27 2.84 8.P9 15.88 17.50 17.73 THMS 925.84 352 08 79.52 360.95 276.67 443 14 1121 65 12C6.01 1237.34 () THPD -665.29 fees -118.37 118.37 P.88 -568.42 P.08 568.42 56n.42 () THPU 1591 16 352 08
- 197 89 493.88 276 67 1911.56 1121 65 1519.41 1535.54 FTHE 56L2 47 623.00 133.54 637.15 TP.14 111.39 664.58 673.78 677.42
() RV05 5771 94 875.49 1137.19 1935 16 231.24 1147 83 1248.55 1695.99 1711 68 () 5808 5771 94 875 49 1137.19 1455 16 231.24 1147.83 1248.55 1695.99 1711 68 SRVS 6t63.31 12P1 39 1898.69 2240.09 374.60 1911 07 1886 17 2685 11 2711.12 C) () pp.goooA 158 HYDR .05 105.37 .55 1C5.37 .48 -4.08 28 26 28.56 28.56 () GRAY -1 53 128.69 a.35 128.f9 -5.93 -4 19 38.56 38 78 39.23 () THM1 -ap.62 217.98 60.92 226.33 105.90 -163.75 492.09 518.62 528.35 THM2 925.88 1P8.84 -118.37 169.80 80.06 -702 91 217.92 735.92 740.26 C) THM3 -665 29 352 0R 79.52 360 95 276.67 523.05 767.68 928.93 969 25 C) THM4 216.46 219.91 -45.43 218.28 183 2R -5R.64 461.65 465 36 503 90 THMS 242 45 2n?.51 -49.01 213.21 191.03 -48.71 438.09 449.79 480.41 () OHE 572.94 376.11 9*6.98 1865.77 3988.38 1849.11 123.88 1956.39 4125.91 () SSE 956.81 6P9 11 1664.95 1779.84 6668.59 1752 02 P06.74 1764.18 6890.27 FTH1 5490.66 552.66 161 62 575 86 291 97 21P.17 661 36 693.95 752 87 {} FTHP 7.68 tw.82 4.38 11.65 6 73 7 00 11.79 13.71 15.27 () THMB 925.8A 352.C8 79.52 360.95 276.67 523.35 767.68 928.93 969.25 THMD -665.29 a.05 -118.37 118.37 0.08 -702 91 0.00 702 91 702.91 () THMU 1591 16 352.08 197 89 403 88 276.67 1225 96 767.68 1946.48 1472.70 () FTHE 5494.66 552.66 161.62 575 80 791 97 219.17 661.36 693.95 752.87 RV00 55 2t.4 7 668.84 1099.99 1211 37 3999.05 1869.96 672.85 1263.94 4194.P4 () Spon 552*4.47 66n.84 100?.99 1211.37 3499.05 1069.96 672 85 1263.94 4194.t4 () SRVS 5573 43 837 3R 1672 78 187P.67 6666.99 1764.58 692 92 1895 75 6931 28 O W-%5A 161- 0 HYDR .72 72.79 .55 72 79 .48 -5 16 -146 18 146 27 146.27 GRAW .P6 95.51 .35 95.51 -5.93 -4.P7 -1n0.3A let.45 18 C.55 () THM1 -P9.62 217.9A 60.92 226.33 115.99 -43.87 62.82 76 62 126.70 () THM2 925.RP 108.84 -118.37 160.83 R0.06 ~*66 30 -31.70 966.82 970.13 THM3 -665.29 352.a* 7a.52 361 95 276.67 679.53 74.49 683.6a 737.47 () THR4 216.46 213 51 -45.4% 219.2P 1*3.28 -159.74 -26.74 161.08 251.60 () THMS 242 45 2'7.81 -4 9. r.1 213.21 ' 191.83 -197.83 -30.98 160.84 249.75 ORE 529.26 494.18 28Pl.31 2P42. A5 3988.38 1726.93 712.04 1867.97 4404 14 () $$E 8P3.py mi8.59 4678.?? 4747.56 6669.59 2883.?8 1189.in 3119.50 7354.92 () FTH1 54*1 36 659.35 1R2.97 684.27 291 97 209.75 527 37 567.55 638.25 FTH? 7.34 a.55 4.97 13.76 6.73 3.49 1P.98 11 52 13.34 () THMB 925.48 392.f8 79.52 360.95 276.67 679 53 74.49 683 6e 737 47 () ca () O _ O _ _ _ _ O_-
D ICPELL C* A T I O's PAGE 22 SUPECPIPi%-vlRSICQ 16A, 16/41/238 SYTTEM IMPELL - 00$ - 83/03/23 11 11,,w. [) PSE TROJAN NUCLEAR STATION L. EDS PROSLEM 8308818-RC-91 #EV.1 * PRES $USIZER S/RV LINE '
) AS-8UILT GEOMETRY WITH SLUS DIVERSION DCVICES ($003 )' E NS LOAD
SUMMARY
(CONTD.) FORCES ANO MOMENTS FLANGE ANO V ALVE ENO LOAD SUMMARIES t._.. . __ [) RUN DCP LOAD FN FY F2 F YZ MN MY M2 Mv2 MNY2 CA%E NAME CASE ELB) (L83 (L89 (L8) (LS.FT3 ( LB .F il (L8.FT3 (LB.F73 8LS.FT) i D f(f % Q 161- (CONTO.3
- c. . THMO . . .-665 39 _.__ .9,00_.. -118.37 .118 37 9.00 -966.39 . -33.70 . 966 82 966.82 . ,. .. ;
THMU 1591 16 352.G8 197.89 493.R8 276.67 1645 83 196 19 - 3649.25 3672 38 D FTHE 5491 36 659 35 182.97 684.27 2*1.97 209 75 527.37 547.55 638 25 RV08 5516.81 818.f4 2007.28 2924.44 3999.05 1739.62 886 07 1952 28 4450 15 SR08 5536 81 818.04 2007 28 2924.64 3999.95 1739 62 886.07 1952.28 4450.15 .
] SRVS 5562 34 1943.34 4681 77 4796.62 6666.99 2091.60 1399.80 3170.71 7382.56 I'
.~.._.......~n.u- . . _. . . . . . . . . ..}
] HYDR 10.56 -404.74 .55 404.74 .48 ~5 74 7R.22 70.46 78.46 1 ,
I GRAW
- 8.96 -380.56 .35 388.56 -5.93 -5.26 ~ 10.80 13 30 - 12.76 THM1 -80.62 217.98 68.92 226 33 198.90 25.00 ~183.79 185 48 213.15 j THM2 925.88 198 84 -118.37 168.as 80 06 -3117 60 -175.18 3131 24 1134.87 ,
~ .7HM3 r665.2.9.___ 354 08. __.79.52 369.95 819.23 -334.34 ... est e4 947.41 __,
THht 216.46 213.51 -45.48 218 20 - . 334 193.2859 .. -217.81 -297.87 369.01 436 56
) THMS 242.45 287.51 -49.e1 213.21 191.83 -220.52 -300.40 372.65 418.76 OBE 143 58 603.44 128P.81 1415.85 2782.95 2186.06 1988 30 2441.97 3702.44
$$E 1575.78 '8837.75 2138.95 2364.46 4647.53 3650.71 1917.46 4075 10 6183 08 I FTHE 5491 53 814.42 2A1.87 861.82 310.28 159.10 1946.92 1958.94 1105.74 .
_ _ . . . .- FTH2 _ _ 10.25.. .4.46_ . . 3.31 . 5.55 4.57. ,.. 7.30 , 8.68 10.39 J THM8 925.88 352.68 79.52 360.95 5.72 338 59 .. 019.23 S.00 819 23 ._ 406.44
;) THMO -665 29 0.00 -118 37 110.37 0.00 -3117 60 -334.38 1166.55 1166 55
~
TH MU 1591.16 352.f8 197.R* 403.R8 33A.59 1936.A3 334.38 1965.40 1994.44 FTHC 5491.E3 814.42 281.A7 A61.82 338.28 359 18 1946 92 1958 94 1185.74 i
) RV08 5512.01 1813.62 1311.46 3657 53 2843 10 2191.e4 1519.11 2661.69 3864.03 SR06 5512 81... 8C13 62 ..3511 46 3657.51 2081 18 2191.e4 1518.11 2661.69 3844 03 i SRVS . 5713.14 1295 7b 2157 45 . 2516.63 4658 42 3654 18 2097.43 4213.34 6201.17 J
222-fiRESSURigh12 HYDR 402.09 -9.05 1 03 9 23 -17 03 -366.15 85 87 376.08 376.47 ,
- ) GRAV 2t3 77 -4.00 1.31 4.97 -7.62 -222.0F 48.36 227.28 227.39 i REUEF TANK THM1 1128.18 .._.373 25 . . 37.26 177.23 -Se4 58 -26es.e1 -5995.34 6536.e4 4555 4e _j THM2 6309.47 -994 23 243 64 10h3 64 -2728.46 -15069 04 -35145.74 38240 02 .30337.24
;) (A FLAMCE, vu,3 .3.,,,, .,, .,3 ,,3. . 1 ,3,s, 212 ... 1336,.c4 -35145.74 3 24e.02 38337.24
$6E SCP J334 THM4 63f9.47 -994.23 243.64 1c23.64 -2728.46 -15869.P4 -35145.74 38240.02 33337 24 FOR LOADS AT-THMS 9621 92 -1597.71 377.99 1554.3F -4158.95 -23178 24 -54158.36 58989 75 59055.81 J OBE 391 16 3393 65 1574 11 3748.95 1207.94 3800.44 4601 10 5967.70 6988.75 1RNK SytF4(E) FTH1 SSE 653.24 5667.39 262a.77 6247.38 2e37 26 6346.73 76as.e4 9966.e6 1916s.17 i 13911.88 848.74 552 05 IC12.48 2127.86 1119.08 64M.21 1209 27 2487.97
;) FTH2 87182.19 7556.13 92P9.19 11912.36 17773 53 16872.40 6474 03 30071 03 25345.97 THMS 6389.47 f.Eb 243.64 243.64 n.0f a.1R 4.60 0.99 0.08 TH40 0.30 -994.23 8.c3 994.23 -2728.46 -15269.04 -35145.74 38240.e2 38337.24 I
[] THMU 6389.47 994.25 243 64 1923.64 2728.46 15069 04 35145 74 3824C.82 30337.24
IMPELL CORPOR ATID3 SUPERPIPE VLBSION 16Ao 10/81/838 SYSTEQ I;PELL - NOS PA'E 23 84/03/23 31 16 16. Op ) P3E fp0JA3 NUCLEAR Statita O EDS P;08LEn 8384018-CC-81 CEU.1 PRESSL'AIFER $/RT LINE AS-SUILT GEDMETFT WITH SLUG O!VER$10N DEVICES 65003 g , ENO LOAD SUMMART GCONTD.) FORCES AND MOMENTS FLANGE ANO TALVE ENO LOAD SUMMARIES $ ) RUN DCP LOAD FR FY F2 FYF , MW MY MF MTZ METZ g CAIE NAME CASE (L89 (L8) IL83 (LSD (LN.Fil ELO.Fil (Lt.Fil (Ls.FT) (LB.Fil , ) 222- (CONTD.) $ FTDC 87152 19 1556 13 9209 19 31912 36 17771 53 IF472.48 6474.93 18473.53 25345.97 RV D8 11977.36 3*98.17 1668.11 3R75 54 2446.42 3961.77 4645.43 6105.38 6577 43 ) SR05 87153.L6 8283.23 9342.75 12405 95 17812.54 17295 12 7942 49 19933 67 26967.85 O SAVS 87154.43 9445 34 9577.C3 13451 17 17885.66 18926 61 19647.61 20,637.67 27369 52 > 0 > 0 ) O > 0 ) O > 0 > 0 > 0 ) O ) O > O s > 0 ) O ) O O -.- O _ O
^
~
=>-== - - - - - - - -
a j INPcLL aTIE3 r==i 29 Q'
'Q SUPctPI tRSIDW 16ae t r/91/838 SYsT[D IPPfLL - WOS D4#33/23. Stelself f-s j() p:t speaan tectran sta11oa cos eneetta e3esela-ec-e1 pcv.1
() retssuestre serv L1=r () as-eutti 6tontfev v TH sLus osvtRstom otvicts tson' db j 4
- () con tono unnnRv roRecs ano noncnts nortte Leno svanaR7 ()
l 1 () Aug ocP L0a0 FN F7 F2 FY2
- MM av. n2 Mv2 davr ()
! Cane NnME Cast tLet (Lil (LB) (L R) (LS.FT) SLB.FT) tLR.FT) ILB.FT) SLt.Fil ! () 7*- () HYD4 71 23 53.63 -27.33 60.19 23.39 75.50 14 17 76 06 88.26
- 1. ENE3bdOEbEbd Spay -249.93 -173 43 29.62 173 33 -6 14 -e.31 -71 11 71 68 71 86 i () $>E2]JEji THMt 3531.J% -2422.81 -1211.19 2789.t4 -1124.99 -3140 41 #446.62 0084.65 s162 66 ()
THM2 3592.32 -2627.88 -1292.20 2928.48 -983 95 -3469.81 7462.07 P229.34 8247.95 THMS 3543.30 -2629.08 -1244.18 2925.88 -1911 34 -3481.32 7464.49 S236.31 8298.17 () THM4 3594.59 -2630 21 -1292 14 2930.46 -907.74 -3473 46 7466.45 0234.85 4293 00 () THMS M77F.37 -5636.50 -4035.30 6441 19 4321 82 -3948 51 11634 58 122P6 27 13024 23 0FE 1498 28 4368.72 1238.73 4543.94 5328.23 1764 75 3968.17 4335 59 6469.31 i () $5E 25L2 13 7295.76 2t6R.69 7503 38 pp98 14 2947 14 6613.49 7240.43 11473.74 () FTH1 6.b6 54 28 7.11 54 74 33.23 26 37 68.36 73.27 83.46 I. FTH2 2318.11 2*75.66 1274.28 3237.02 13a?.99 3659.36 6330 71 7312.24 7442.43 l) THM8 3594 55 3.88 9.88 0.00 8.08 4.99 7454.45 1464.45 7466.45 () ] IHMD W.09 =2630.21 *1292 20 2930.49 -1A24.40 -3481.32 9 99 3431.32 3658.39 i 7HMU 35?4 55 2639.21 1292 20 2938.49 1124.48 34st.32 7056.45 8238 17 8314 55 ! () FTHE 233s'.11 2?75 66 1274 28 3237 92 13A5 99 3639 36 6330 71 7312 24 7442.43 () l Rvo8 1998.39 4?69.86 123A.75 4541 27 532A.33 1764.95 3969.76 4336.21 6869.78 SR08 2753.44 5285.95 1777 14 5576.68 5$e5.54 4062 66 7467 32 8500.95 18128 84 ! () Spys 3415.48 7879 25 2429.66 0245 36 9805.44 4699.56 9155.12 19298 42 13674.45 () I 3n. l () HTOR -23.21 -19 11 -29 28 27 97 36.52 59.74 -23 51 64 24 73.86 () ( SmaV -281 7u -143.32 26.t e 145.nl -13.33 -4.62 -65.97 66 14 67.46 ! THM1 4311.7tl -2738.42 -828.76 20f3.42 -1378.53 -6918.82 9466.02 11387.43 11470.54 I THM2 4469 28 -11*6.43 -923.00 3244.65 *1523 91 -61P4.47 89A7.22 19864 37 19970.45 ()
) () THM3 THMe 44 76 2R 4473 46
-3133.f1
-31*p.79
-925.68
-924.90 3244.49 3243 99
-1524 89
-1513.44
-6111 83
-6193.39 8*99 74 8?91 91 19874.53 19866 98 19994.87 19971a79
! ; () THMS 6321 56 -5316 19 -34kl.it 6321.e5 2993.31 -6133.69 11645.65 13179.89 13515 53 () OBE 411 79 3961.48 1888.99 4197.!? 3243 56 1878.27 C111 6* 5245.68 P147.40 SSE 687 53 6613.22 1848.61 6858 72 5416.74 1967 71' 8536.44 976f.29 18299.70 FTH1 7.39 Steen 25.27 M6.45 34.67 23.67 65.83 64.34 78.C6 () l() { FTH2 T H P9 2741.96 4 4 74.2 A 3644.92 C.a9 1806.41 0.4N 3781 31 4.93 1494.43 4.80 2121 55 0 00 6864.'98 9666.p2 7233.m4 9666.92 7266.73 9666.02 () THMo D.*u ~3113.81 -926.94 324a.se -1524.a3 -6111 93 Dett 6111 8.'3 6299.16 () l T H Mil 4476.28 3113 81 926.90 3248.84 1924.88 6311 83 9666.83 184?A.06 11536.86
- FTHE 2741.96 3644.92 10P6.41 37a1.31 1994.43 2121.55 6P78.90 7131 04 1286.73 I () RVOS 411.76 3968.34 1989 28 4117 41 3743.74 1178 54 5112.96 5246 15 6167.98 ()
SPOR 2772 70 53R2 11 F392.pt 5542 64 g 3571 27 2426.70 9514.37 J853 27 9546.43 Sevs 2826 45 7'*l.37 2078.51 7832.ft 5619.11 2A93 59 19919.3V 11294 28 12434.67 i () l () 3-HYDR 29 15 27.49 26 26 38.91 -14.98 -66.64 -9.68 67.16 68.99
; () s 4v -Pe .in -296.r9
-71.6 3 ,4 . c , -12 41 24.19 -62.36 66.99 64.e3 ()
() () ! () ., () , i i '
a IMPELL CORPORAT103 PAGE 25 (")
" "l q SUPERPIPE VER$10N 10A, 18/01/031 SYST[3 IMPELL - hos. 94/03/23 11 16.15. -
- PIE TROJ 3 NULLEAR STAT 101 () -
EDS PROALEM 039t019-PC-81 REY.1 PP ESS URIZER S/RV LINE
- AS-BUILT CE09[Tpi WITH SLUG DIVERSION DCVICES 45909 - () t s END LOAD
SUMMARY
tCONTO.3 FOPCES AND MOMENTS N022LL LOAD $UMMARY () o RUN DCP LOAD FN TV FZ FYZ
- RX M7 M7 M72 MEVZ ()
NAME NAME CASE (L8) (L83 (LB) (L8) (LS.Ffi (LB.FTl (LS.Fil (LB.F73 (L8.FT3 . 3- (CONTD.) () THM1 4922 51 -2A25 05 1284.29 3071 03 298.58 6887.75 9898 62 12887 88 12018.59 THM2 Sa37.2n 3274.20 1349.57 3541 43 455 49 6818.43 9t55 81 11535.72 11344 87 o THP3 5t28.95 -3275.96 1338.27 3538.77 491 29 6831 29 9C58.67 11345.75 11356.38 () THM4 5635 68 -3272.48 1344.3? 3537.87 468.84 6823.79 9052.91 11334.42 11344.48 THMS 6954.e95 -563A.94 4354.29 7124.43 ~4868.45 6942.24 11849.31 13713 81 14551 59 OBE 1t12 69 2725.44 2023.58 3394.54 5756.96 1907.22 2257.25 2659.*0 6341 78 () SSI 1691 28 4551 48 337?.37 5668.A7 9614 12 2358.06 3769 27 4441 87 1859c.64 FtH1 12 37 35.19 31 54 47.26 97.48 33.92 41 19 53 33 75 41 FTH2 2955 29 3787.38 1845.35 4213 43 1793.*7 4553.76 7482.39 8698.92 8874.14 () THM8 5438.95 P.00 1349.5F 1349.57 491.29 6R31.29 9898.62 12028 44 12838.47 THMO 8.Se -3275 96 8.00 3275.96 8.88 P.80 0.08 8.08 0.88 0 THMU 50?8 15 3275.96 1349.57 3543 06 491.29 6831 29 9n9t.62 12020 44 12038.47 () FTHE 2955 23 3767 38 1845 35 4213 83 1793.97 4553.76 7492 39 8699.92 8874.14 Avo8 1c12s77 2725.67 2023.82 3394.06 5757.25 1407.63 2257.42 2668.34 6342 18 i SROS 3123 93 4666.98 2738.65 5418.44 6838.88 4766.25 7738.84 9888 82 18987.23 () SpVS 34c4 90 5*21 17 3858.39 7462 98 978s.87 5124.48 8306.79 9768 24 13817.89 [) 114- () HYDE 238.83 222 19 .94 222.19 -3 35 11 32 179.19 178.57 179.68 6RAV 194.E6 186.59 2.43 186 68 6.19 6.24 144.16 144.30 144.43
- 5) THM1 397.04 297 46 108 67 316.69 1t86.47 -1118 11 -2544.88 2779.67 2984.46 ()
THM2 272 75 641.la -99.79 653.78 1736 16 1339.56 -711 57 1516.82 2385 43 THM1 42a.89 416.42 221.33 971 5A 1418.38 -1989.29 -2315.27 3*49.24 3359 59 O THM4 338.J2 4 P6 18 -87.41 493.98 257 78 388.74 *1632.66 1677.72 1697 41 () THMS 329.52 th1.94 -74.s6 en6.61 494.98 449.50 -1695.16 1753.75 1822 26 Out 431.47 151.41 117.21 276.49 1454.32 1931.64 2739 78 3352 28 3654 16 () SSE 728.58 41n.19 195.73 461 75 2428.71 3225 91 4575.44 559A.32 6102 44 () fiHI 22?6 19 4 t 5.79 218.35 456.37 32P.41 335.88 423.a1 549.77 628.56 FIH2 213.34 183.11 41.58 187.77 99.12 146.49 225.39 268.82 286 51 () THM8 429.89 643.18 221.33 680 13 1736.16 1339 56 0.00 1339.56 2192.87 () THMD 0.CG 0.s8 =*9.79 99 79 C.48 -1984.29 -2544 88 3227.85 3227.05 THMU 4 2e.n* 643 11 321.13 719 82 1736.1A 3323.86 2544.R8 4196.22 4531.*6 () FTNE 22?6 19 of).75 218.35 456.37 320.41 335.88 423.81 540 77 628.56 () RV08 2277.44 472.56 247.81 533.59 14R9.28 196e.67 2772 37 3395.62 3787.82 5408 2277.44 472 56 247.81 533.59 1449.28 1869.67 2772.37 3395.62 3707 82 () SRVS 2349 41 579.21 293.23 649.21 2449.76 3243.35 4595.82 5624.37 6134.73 () 223A-() HYDR 985.29 -9.as 3,p3 g.23 -17.J3 *63.13 97.84 376.66 377.04 () 51DD7JOD3d GPAv 721.36 -4.8* 1 31 4.97 -7.32 -220.34 54.72 227.83 227 13 THE1 1128 18 -173.25 '7.26 177.21 k S94.58 -2553.49 -5763.07 6305 27 6325 42 THM2 65m9.47 a*4.23 243.64 1t25.64 -2728.46 -19731.93 -33770 12 36843.68 36944.49 () () bLC (8611C77704K DCP ttz O M W "G O AT FIA@d j O -- - O .-. -.- .- ._. - e - .-.
8NPELL Sant:34 9 - -
' ~
...! 2 ,))
($) D4#93/23e 11.16e ,, S UPEOP VE3510N 164e 11/95/038 $757E3 IPPELL - NOS r () PSE 7ptJA3 NUCLE 23 STA71SW - () EDS PeteLEN 03SS018-pC-91 REV.1 PetSSUA12ER S/RV LINE I () AS-tulL7 GEORETRY UITN SLus OlvtRSION DEVICES 45003 () () ENO LSAD
SUMMARY
(CON TD.1 FDACES Aun RomENTS N0ZZLE LDAD SURNART () SUN DCP LOAD FN FY F2 F72 . NN PT M2 pf2 REVZ () i () (LSI (LBI (LB.F73 (LB.FID (LB.F73 (LO.Fil (LS.F7) NAME NAME CASE EL8 3 ELSI l 223A- (CONTO.) () ! () THr.3 63m9.47 -994.23 243 64 1925 64 -2728.46 -14731.93 -33770 12 36e43 49 36944.49 THne 6349.47 -994.23 243.64 1921.64 -272P.46 -14731.93 -33770 12 36043.60 36944.49 l 9631 32 -1547.71 377.99 1554.37 -4159.95 -22641.35 -52416 85 56738.88 56882.46 () () THMS Ost 416.33 34a3.91 1694 23 3882.24 1297.94 5*64 62 9099.42 19899.48 19946.93 SSE 695.26 5684.54 2029.37 6349 75 2017 26 9?69 91 15196.93 18169.75 19281.37 () FTH1 13*14.29 948 36 726 39 1894.50 2127.06 1935.69 1814.36 2653.07 3400.97 f) i FTH2 87124.11 7734.85 9533.68 12276.28 17771 53 29363.99 16549 5e 33765 74 38103 87 t THn8 63ee.47 e.es 243 44 243.64 e.es e.se s.so s.ee e.80 () THN0 8.ed -994.23 4.60 994.23 -2720 46 -14731.93 -33779 12 36843.49 36944.49 () THpU 6389.47 994.23 243 64 1e23.64 2728.46 14731 93 33770 12 36843 68 36944.49 FTHE 87124 11 7734.t5 9533.6* 12276.28 17771 53 29363.*9 16549.50 33795.74 38103.87 i ! () RV08 139pe.49 3533.55 1843.39 3985 48 2446.82 6270.85 9278.54 11198.08 11463.96 () SR05 87125 10 8449.98 9682 90 12851 55 17812.54 2*962 77 18086 12 35418 26 39645 17 SRVS 871P6 88 959A.41 9944.59 13821 16 17805.66 31496.63 22467 87 30291.28 42262 43 i () () I CD C) . C) () C) () . c) !c; () () I g . g) () () ()
- C) .
() !o - o i I
1 1 O I I VALVE AND N0ZZLE END LOADS I 4pQl GLO8AL AXIS M; Le'x GLOBAL AXIS I XdZ y b $0ZZLE ( DCPS 16, 52, 87 DCP 223A
- 1) 1)
(1 APER)A DCPS 18, 54, 89, 142, DCPS 140, 146, 156, 161 1 148, 158, & 163 i Z (IN PAPER) NOTES: (1) SEE ATTACHMENT A FOR l X & Z GLOBAL ORIENTATION - A AND N0ZZLE LOCATIONS. X Y
}Y (2)LOADSANDMOMENTSARE ACTING ON THE N0ZZLE N0Z GLOCAL OR VALVE END.
AXIS (1) (3) CASES OBE, FTH1, AND FTHE DCPS 3, 38, 74, 114 ARE UNSIGNED AND SHOULD BE , CONSIDERED BOTH PLUS AND l MINUS. Figure C-1: LOAD AND MOMENT END LOAD ORIENTATIONS O
. _ . _ . . . _ . .-. - _ . , _ . _ _ _ _ _ _ _ . . . _ _ . _ _}}