ML18024A413: Difference between revisions

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: a. Permissible Deformation,DPAnalyzedDeformationCausing Loss of Function, DL
: a. Permissible Deformation,DPAnalyzedDeformationCausing Loss of Function, DL


09.minSF   b. Permissible  Deformation,  DP Experimental  DeformationCausing  Loss of Function,  DE
09.min SF   b. Permissible  Deformation,  DP Experimental  DeformationCausing  Loss of Function,  DE


1.0SFmin where DP = permissible deformation under st ated conditions of normal, upset, emergency, or faulted DL = analyzed deformation which woul d cause a system loss of function (1)  DE = experimentally determined formation which would cause a system loss of function(1)   
1.0 SFmin where DP = permissible deformation under st ated conditions of normal, upset, emergency, or faulted DL = analyzed deformation which woul d cause a system loss of function (1)  DE = experimentally determined formation which would cause a system loss of function (1)   
(1)  "Loss of Function" can only be defined quite generally until attention is focused on the component of interes
(1)  "Loss of Function" can only be defined quite generally until attention is focused on the component of interes
: t. In cases of interest, where deformation limits can affect the f unction of equipment and components, they will be specifically delineated. From a practical viewpoint, it is convenient to interchange some deformation condition at which function is assured with the loss of function condi tion if the require d safety margins from the functioning condition can be achieved. Therefore, it is often unnecessary to determine the actual loss of function condition because this interchange procedure produces conservative and safe designs. Examples where deformation limits apply are:  control rod drive alignment and clearances for proper insertion, core support deformation causing fuel disarrangement, or excess leakage of any component.
: t. In cases of interest, where deformation limits can affect the f unction of equipment and components, they will be specifically delineated. From a practical viewpoint, it is convenient to interchange some deformation condition at which function is assured with the loss of function condi tion if the require d safety margins from the functioning condition can be achieved. Therefore, it is often unnecessary to determine the actual loss of function condition because this interchange procedure produces conservative and safe designs. Examples where deformation limits apply are:  control rod drive alignment and clearances for proper insertion, core support deformation causing fuel disarrangement, or excess leakage of any component.
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Any One of (No More than One Required)  General Limit  
Any One of (No More than One Required)  General Limit  
: a. Elastic Evaluated Primary Stresses,PEPermissible Primary Stresses, PN          2.25minSF b. Permissible Load,LP                        Largest Lower Bound Limit Load, CL  1.5SFmin c. Elastic Evaluated                    Primary Stress, PEConventional ultimate strengthat Temperature, US    075.minSF d. ElasticPlastic EvaluatedNominal Primary Stress, PEConventional ultimate strengthat Temperature, US
: a. Elastic Evaluated Primary Stresses,PEPermissible Primary Stresses, PN          2.25min SF b. Permissible Load,LP                        Largest Lower Bound Limit Load, CL  1.5 SFmin c. Elastic Evaluated                    Primary Stress, PEConventional ultimate strengthat Temperature, US    075.min SF d. ElasticPlastic EvaluatedNominal Primary Stress, PEConventional ultimate strengthat Temperature, US


09.minSF e. Permissible Load, LP      Plastic Instability Load, PL    09.minSF f. Permissible Load, LP     
09.min SF e. Permissible Load, LP      Plastic Instability Load, PL    09.min SF f. Permissible Load, LP     


Ultimate Load From Fracture Analysis, UF  09.minSF g. Permissible  Load,  LP                  Ultimate  Load  or  Loss  of  FunctionLoad  from  Test,  LE
Ultimate Load From Fracture Analysis, UF  09.min SF g. Permissible  Load,  LP                  Ultimate  Load  or  Loss  of  FunctionLoad  from  Test,  LE


1.0SFmin BFN-27 Sheet 2 Table C.2-2 (continued) PRIMARY STRESS LIMIT
1.0 SFmin BFN-27 Sheet 2 Table C.2-2 (continued) PRIMARY STRESS LIMIT


where  
where  
Line 45: Line 45:
LP = Permissible load under stated c onditions of emergency or faulted.  
LP = Permissible load under stated c onditions of emergency or faulted.  


CL = Lower bound limit load wi th yield point equal to 1.5 S m, where S m is the tabulated value of allowable stre ss at temperature of the ASME III code or its equivalent. The "lower bound limit load" is here defined as that produced from the analysis of an ideal ly plastic (nonstrain harde ning) material where deformations increase with no further increase in applied load. The lower bound load is one in which the material everywhere satisfies equilibrium and nowhere exceeds the defined material yield strength using either a shear theory or a strain energy of distortion theory to r elate multiaxial yielding to the uniaxial case.  
CL = Lower bound limit load wi th yield point equal to 1.5 S m , where S m is the tabulated value of allowable stre ss at temperature of the ASME III code or its equivalent. The "lower bound limit load" is here defined as that produced from the analysis of an ideal ly plastic (nonstrain harde ning) material where deformations increase with no further increase in applied load. The lower bound load is one in which the material everywhere satisfies equilibrium and nowhere exceeds the defined material yield strength using either a shear theory or a strain energy of distortion theory to r elate multiaxial yielding to the uniaxial case.  


US = Conventional ultimate strength at temper ature or loading that would cause a system malfunction, whichever is more limiting.
US = Conventional ultimate strength at temper ature or loading that would cause a system malfunction, whichever is more limiting.
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: a. Permissible Load, LP              Code Normal Event PermissibleLoad, PN
: a. Permissible Load, LP              Code Normal Event PermissibleLoad, PN


2.25minSF       b. Permissible  Load, LP        Stability Analysis Load, SL    09.minSF c. Permissible Load, LP                Ultimate Buckling Collapse Loadfrom Test, SE    1.0SFmin where:
2.25 min SF       b. Permissible  Load, LP        Stability Analysis Load, SL    09.min SF c. Permissible Load, LP                Ultimate Buckling Collapse Loadfrom Test, SE    1.0 SFmin where:
LP = Permissible load under stated c onditions of emergency or faulted.
LP = Permissible load under stated c onditions of emergency or faulted.
PN = Applicable code norm al event permissible load.  
PN = Applicable code norm al event permissible load.  
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SE = Ultimate buckling collapse load as determined from ex periment. In using this method, account s hall be taken of the dimensional tolerances which may exist betw een the actual part and the tested part. The guide to be used in each of these areas is that the experimentally determined load shall be adjusted to account for material property and dimension va riations, each of which has no greater probability t han 0.1 of being exceeded in the actual part.
SE = Ultimate buckling collapse load as determined from ex periment. In using this method, account s hall be taken of the dimensional tolerances which may exist betw een the actual part and the tested part. The guide to be used in each of these areas is that the experimentally determined load shall be adjusted to account for material property and dimension va riations, each of which has no greater probability t han 0.1 of being exceeded in the actual part.
BFN-27 Table C.2-4 FATIGUE LIMIT General Limit Summation of mean fatigue(1) a. Fatigue cycle usage usage including emergency or      from analysis    0.05 faulted events with design and operation loads following      b. Fatigue cycle usage Miner hypotheses....        from test    0.33 either one (not both)  
BFN-27 Table C.2-4 FATIGUE LIMIT General Limit Summation of mean fatigue(1) a. Fatigue cycle usage usage including emergency or      from analysis    0.05 faulted events with design and operation loads following      b. Fatigue cycle usage Miner hypotheses....        from test    0.33 either one (not both)  
  (1) Fatigue failure is defined here as a 25% area reduction for a load carrying member which is required to function or excess leakage causing loss of function, whichever is more limiting. In the fatigue evaluation, the methods of linear elastic stress analysis may be used when the 3S m range limit of ASME Code, Se ction III has been met. If 3Sm is not met, account will be tak en of (a) increases in local strain concentration, (b) strain ratcheting, and (c) redistribution of strain due to elastic-plastic effects. The January 1969 draft of the USAS B31.7 Piping Code may be used where applicable, or detailed elastic-plastic methods may be used. With elas tic-plastic methods, strain hardening may be used not to exceed in stress for the same strain the steady-state cyclic strain hardening meas ured in a smooth low cycle fatigue specimen at the average te mperature of interest.  
  (1) Fatigue failure is defined here as a 25% area reduction for a load carrying member which is required to function or excess leakage causing loss of function, whichever is more limiting. In the fatigue evaluation, the methods of linear elastic stress analysis may be used when the 3S m range limit of ASME Code, Se ction III has been met. If 3S m is not met, account will be tak en of (a) increases in local strain concentration, (b) strain ratcheting, and (c) redistribution of strain due to elastic-plastic effects. The January 1969 draft of the USAS B31.7 Piping Code may be used where applicable, or detailed elastic-plastic methods may be used. With elas tic-plastic methods, strain hardening may be used not to exceed in stress for the same strain the steady-state cyclic strain hardening meas ured in a smooth low cycle fatigue specimen at the average te mperature of interest.  


BFN-27                   
BFN-27                   
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Max (Peak) Pressure + M BE = M(E2,VT,WH,JI) 5,6,8,11  Sustained + Fluid Transient    (9E) + (DBE or Jet Impingement)     
Max (Peak) Pressure + M BE = M(E2,VT,WH,JI) 5,6,8,11  Sustained + Fluid Transient    (9E) + (DBE or Jet Impingement)     


PDDDiMZSioiAh222075.  ()PDDDiMMZSmioiABUh22207512++.. ()PDDDiMMZSmioiABEh22207518++..
PD DD iM Z S i oi A h 2 22075.  ()PD DDiMM Z S mi oiABU h 2 22075 12++.. ()PD DDiMM Z S mi oiABE h 2 22075 18++..
BFN-27                 
BFN-27                 


Line 86: Line 86:
Faulted (Max (Peak) Pressure + M BF = M(E2,VT,WH,JI) 6,8    (9F) Sustained + DBE + Fluid Transient + Jet Impingement)
Faulted (Max (Peak) Pressure + M BF = M(E2,VT,WH,JI) 6,8    (9F) Sustained + DBE + Fluid Transient + Jet Impingement)
Normal and Upset (Secondary)
Normal and Upset (Secondary)
Thermal Expansion +  M C = M(Ti,SD,S1)3,4,7    (10) Thermal Anchor Movement +
Thermal Expansion +  M C = M(T i ,SD,S1)3,4,7    (10) Thermal Anchor Movement +
Seismic Anchor Movement OR  Design Pressure + Sustained +    (11)
Seismic Anchor Movement OR  Design Pressure + Sustained +    (11)
Thermal Expansion + Thermal Anchor Movement + Seismic Anchor Movement Differential Settlement  
Thermal Expansion + Thermal Anchor Movement + Seismic Anchor Movement Differential Settlement  
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Differential Settlement M D = M(BS)   
Differential Settlement M D = M(BS)   


  ()PDDDiMMZSmioiABFh2220752++..4iMZScA PDDDiMZiMZSSioiACAh222075+++. iMZSDC3 BFN-27                 
  ()PD DDiMM Z S mi oiABF h 2 22075 2++..4 iM Z S c A PD DD iM Z iM Z SS i oi AC Ah 2 22075+++. iM Z S D C3 BFN-27                 


Sheet 3 of 8 TABLE C.3-1B LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA OF CLASS I PIPING FOR REACTOR RECIRCULATION (RRS) MAIN STEAM (MS) AND FEEDWATER (FW) SYSTEMS 9  Plant Conditions Moment Constituents 2                            NC-3652 1 Concurrent Loads  From Load Sources  Equations and Stress Limits Eq. No.
Sheet 3 of 8 TABLE C.3-1B LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA OF CLASS I PIPING FOR REACTOR RECIRCULATION (RRS) MAIN STEAM (MS) AND FEEDWATER (FW) SYSTEMS 9  Plant Conditions Moment Constituents 2                            NC-3652 1 Concurrent Loads  From Load Sources  Equations and Stress Limits Eq. No.
Line 105: Line 105:
Design Pressure +  M' C = M(Ti,SD)  (11)  Sustained + Thermal      Expansion + Thermal Anchor Movement  
Design Pressure +  M' C = M(Ti,SD)  (11)  Sustained + Thermal      Expansion + Thermal Anchor Movement  


PDDDiMZSioiAh222075.  ()PDDDiMMZSioiABUh22207512++.. PDDDiMiMZSSioiACAh222075++.'
PD DD iM Z S i oi A h 2 22075.  ()PD DDiMM Z S i oiABU h 2 22075 12++.. PD DDiMiM Z SS i oi AC Ah 2 22075++.'
BFN-27                                                                                          Sheet 4 of 8 TABLE C.3-1B LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA OF CLASS I PIPING FOR REACTOR RECIRCULATION (RRS) MAIN STEAM (MS) AND FEEDWATER (FW) SYSTEMS 9  Plant Conditions Moment Constituents 2                            NC-3652 1 Concurrent Loads  From Load Sources  Equations and Stress Limits    Eq. No.
BFN-27                                                                                          Sheet 4 of 8 TABLE C.3-1B LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA OF CLASS I PIPING FOR REACTOR RECIRCULATION (RRS) MAIN STEAM (MS) AND FEEDWATER (FW) SYSTEMS 9  Plant Conditions Moment Constituents 2                            NC-3652 1 Concurrent Loads  From Load Sources  Equations and Stress Limits    Eq. No.
Upset (Primary + Secondary)
Upset (Primary + Secondary)
Design Pressure + M C = M(Ti,SD,S1) 3,4,7  (9U+10) Sustained + Thermal    Expansion & Thermal Anchor Movement + OBE + SAM Emergency (Primary)
Design Pressure + M C = M(Ti,SD,S1) 3,4,7  (9U+10) Sustained + Thermal    Expansion & Thermal Anchor Movement + OBE + SAM Emergency (Primary)
Design Pressure + M BE = M(E2,VT,WH,JI)5,6,8,11  (9E)  Sustained + Fluid Transient    + (DBE or Jet Impingement)    Max. (Peak) Pressure + M BE' = M(E1,VT,WH) 6,8  (9E)' Sustained + OBE + Fluid      Transient Max. (Peak) Pressure +      Sustained + Fluid Transient    (9E)" + (DBE or Jet Impingement)
Design Pressure + M BE = M(E2,VT,WH,JI)5,6,8,11  (9E)  Sustained + Fluid Transient    + (DBE or Jet Impingement)    Max. (Peak) Pressure + M BE' = M(E1,VT,WH) 6, 8  (9E)' Sustained + OBE + Fluid      Transient   Max. (Peak) Pressure +      Sustained + Fluid Transient    (9E)" + (DBE or Jet Impingement)
Faulted Primary Max (Peak) Pressure + M BF = M(VT,E2,WH,JI) 6,8    (9F) Sustained + Fluid Transient  + DBE + Jet Impingement  
Faulted Primary Max (Peak) Pressure + M BF = M(VT,E2,WH,JI) 6,8    (9F) Sustained + Fluid Transient  + DBE + Jet Impingement  
  ()()PDDDiMMiMZSSioiABUChA22207512+++..()PDDDiMMZSioiABEh22207518++..()PDDDiMMZSmioiABEh22207515++.'.()PDDDiMMZSmioiABEh22207520++..()PDDDiMMZSmioiABFh2220752++..4 BFN-27                   
  ()()PD DDiMMiM Z SS i oiABUC hA 2 22075 12+++..()PD DDiMM Z S i oiABE h 2 22075 18++..()PD DDiMM Z S mi oiABE h 2 22075 15++.'.()PD DDiMM Z S mi oiABE h 2 22075 20++..()PD DDiMM Z S mi oiABF h 2 22075 2++..4 BFN-27                   


Sheet 5 of 8 TABLE C.3-1C LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA FOR CONTROL ROD DRIVE HYDRAULIC PIPING Plant Conditions Moment Constituents 2                            NC-3652 1 Concurrent Loads  From Load Sources  Equations and Stress Limits Eq. No.
Sheet 5 of 8 TABLE C.3-1C LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA FOR CONTROL ROD DRIVE HYDRAULIC PIPING Plant Conditions Moment Constituents 2                            NC-3652 1 Concurrent Loads  From Load Sources  Equations and Stress Limits Eq. No.
Line 126: Line 126:


     (11)
     (11)
PDDDiMZSioiAh222075.()P DDD0.75i MMZ1.2Sni2o2i2ABUh++iMZScA1PDDDiMiMZSSnioiACAh2221075++.
PD DD iM Z S i oi A h 2 22075.()P D DD0.75i MM Z 1.2S ni 2 o 2 i 2ABU h++iM Z S c A 1PD DDiMiM Z SS ni oi AC Ah 2 22 1075++.
BFN-27                   
BFN-27                   


Sheet 6 of 8 TABLE C.3-1C LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA FOR CONTROL ROD DRIVE HYDRAULIC PIPING Plant Conditions Moment Constituents 2                              NC-3652 1 Concurrent Loads  From Load Sources  Equations and Stress Limits  Eq. No.
Sheet 6 of 8 TABLE C.3-1C LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA FOR CONTROL ROD DRIVE HYDRAULIC PIPING Plant Conditions Moment Constituents 2                              NC-3652 1 Concurrent Loads  From Load Sources  Equations and Stress Limits  Eq. No.
Max Operating Pressure +  MC2 = M(Ti,SD) 7  Sustained + Abnormal Scram    OR  (10) Thermal Expansion and Anchor
Max Operating Pressure +  M C2 = M(Ti,SD) 7  Sustained + Abnormal Scram    OR  (10) Thermal Expansion and Anchor


Movement          (11)  
Movement          (11)  
Line 136: Line 136:
Emergency (Primary)
Emergency (Primary)
Max Operating Pressure +
Max Operating Pressure +
MDE = M(E2,VT,WH,JI) 6,8,11    Sustained + Fluid Transient        (9E)  
M DE = M(E2,VT,WH,JI) 6,8,11    Sustained + Fluid Transient        (9E)  
+ (SSE or Jet Impingement) 5      Faulted (Primary)
+ (SSE or Jet Impingement) 5      Faulted (Primary)
Max Operating Pressure +
Max Operating Pressure +
MDF = M(E2,VT,WH,JI) 6,8    Sustained + Fluid Transient        (9F) + SSE + Jet Impingement iMZSCA2 PDDDiMiMZSSnioiACAh2222075++.()PDDDiMMZSnioiADEh22207518++..()PDDDiMMZSnioiADFh2220752++..4 BFN-27                                                            Sheet 7 of 8 TABLE C.3-1A, 1B, 1C (Cont'd)  
M DF = M(E2,VT,WH,JI) 6,8    Sustained + Fluid Transient        (9F) + SSE + Jet Impingement iM Z S C A 2 PD DDiMiM Z SS ni oi AC Ah 2 22 2075++.()PD DDiMM Z S ni oiADE h 2 22075 18++..()PD DDiMM Z S ni oiADF h 2 22075 2++..4 BFN-27                                                            Sheet 7 of 8 TABLE C.3-1A, 1B, 1C (Cont'd)  


Nomenclature P = Design Pressure, psi.
Nomenclature P = Design Pressure, psi.
Pm = Max (Peak) Pressure, psi.  
P m = Max (Peak) Pressure, psi.  


Pn = Maximum operational or scram pressure for the Hydraulic System Pump Pressure for CRDH    System only.  
P n = Maximum operational or scram pressure for the Hydraulic System Pump Pressure for CRDH    System only.  


Do = Outside Pipe Diameter, in.  
D o = Outside Pipe Diameter, in.  


Di = Nominal Inside Pipe Diameter, in.  
D i = Nominal Inside Pipe Diameter, in.  


i = Stress Intensification Factor from B31.1.0 - 1967.  
i = Stress Intensification Factor from B31.1.0 - 1967.  


Sh = Basic material allowable stress at maximum operating temperature.
S h = Basic material allowable stress at maximum operating temperature.
Sc = Basic Material Allowable Stress at Ambient Temperature.  
S c = Basic Material Allowable Stress at Ambient Temperature.  


SA = Allowable expansion stress defined in B31.1.0 - 1967.  
S A = Allowable expansion stress defined in B31.1.0 - 1967.  


U,E,F = Added Suffixes for differentiation between Upset, Emergency, and Faulted.  
U,E,F = Added Suffixes for differentiation between Upset, Emergency, and Faulted.  
Line 191: Line 191:
: 10. Additional stresses caused by hydrostatic testing weight are evaluated when applicable.  
: 10. Additional stresses caused by hydrostatic testing weight are evaluated when applicable.  
: 11. Fire events are evaluated as separate emergency loading conditions. No dynamic loads are postulated to occur simultaneously with these events. Piping is evaluated for pressure plus deadweight effects of the events.
: 11. Fire events are evaluated as separate emergency loading conditions. No dynamic loads are postulated to occur simultaneously with these events. Piping is evaluated for pressure plus deadweight effects of the events.
BFN-27  TABLE C.3-2 Sheet 1 of 5 LOAD COMBINATIONS AND ALLOWABLE STRESSES FOR CLASS I PIPE AND TUBING SUPPORTS Support Category Load Condition Direction Design Load Combinations 1,2,9 Allowable 3 Stresses Linear Type Support Normal +  
BFN-27  TABLE C.3-2 Sheet 1 of 5 LOAD COMBINATIONS AND ALLOWABLE STRESSES FOR CLASS I PIPE AND TUBING SUPPORTS Support Category Load Condition Direction Design Load Combinations 1,2,9 Allowable 3 Stresses Linear Type Support Normal + - DW + Ti+ DW + Ti- 1.0S AISC  Hydrotest  DW 1.0S AISC  Upset + DW + Ti
- DW + Ti+ DW + Ti- 1.0S AISC  Hydrotest  DW 1.0S AISC  Upset + DW + Ti
+ + SRSS[VT+, WH+, E1, S1] 1.33S AISC 4  - DW + Ti
+ + SRSS[VT
+, WH+, E1, S1] 1.33S AISC 4  - DW + Ti
- - SRSS [VT
- - SRSS [VT
-, WH-,  -E1, -S1]
-, WH-,  -E1, -S1]
Line 219: Line 217:
BFN-27  TABLE C.3-2 (CONTINUED)
BFN-27  TABLE C.3-2 (CONTINUED)
Sheet 2 of 5 Support Category Load Condition Direction Design Load Combinations 1,2,9 Allowable 3 Stresses Snubbers    Hydraulic      Upset +/- Same as Linear VLR  Emergency  
Sheet 2 of 5 Support Category Load Condition Direction Design Load Combinations 1,2,9 Allowable 3 Stresses Snubbers    Hydraulic      Upset +/- Same as Linear VLR  Emergency  
+/- Same as Linear 1.2 VLR  Faulted  
+/- Same as Linear 1.2 VLR  Faulted +/- Same as Linear 1.2 VLR Mechanical    Pre-NF Upset  
+/- Same as Linear 1.2 VLR Mechanical    Pre-NF Upset  
+/- Same as Linear VLR  Emergency  
+/- Same as Linear VLR  Emergency  
+/- Same as Linear The lesser of 1.33 VLR or LCD Level 'C'  Faulted  
+/- Same as Linear The lesser of 1.33 VLR or LCD Level 'C'  Faulted +/- Same as Linear The lesser of 1.33 VLR or LCD Level 'C' Post-NF Upset  
+/- Same as Linear The lesser of 1.33 VLR or LCD Level 'C' Post-NF Upset  
+/- Same as Linear LCD Level 'B'  Emergency  
+/- Same as Linear LCD Level 'B'  Emergency  
+/- Same as Linear LCD Level 'C'  Faulted  
+/- Same as Linear LCD Level 'C'  Faulted +/- Same as Linear LCD Level 'C' BFN-27  TABLE C.3-2 (CONTINUED)
+/- Same as Linear LCD Level 'C' BFN-27  TABLE C.3-2 (CONTINUED)
Sheet 3 of 5 Support Category Load Condition Direction Design Load Combinations 1,2,9 Allowable Stresses 3,5,6 Standard Support Components Normal +/- Same as Linear S 58  Hydrotest  Same as Linear 2.0S 58 8 Upset +/- Same as Linear 1.2S 58  Emergency  
Sheet 3 of 5 Support Category Load Condition Direction Design Load Combinations 1,2,9 Allowable Stresses3,5,6 Standard Support Components Normal +/- Same as Linear S 58  Hydrotest  Same as Linear 2.0S 588 Upset +/- Same as Linear 1.2S 58  Emergency  
+/- Same as Linear (See Note 7)  Faulted +/- Same as Linear (See Note 7)
+/- Same as Linear (See Note 7)  Faulted  
+/- Same as Linear (See Note 7)
BFN-27  TABLE C.3-2 (CONTINUED)
BFN-27  TABLE C.3-2 (CONTINUED)
Sheet 4 of 5 Notes:  1. Signs for Load Evaluation  DW - Carries the actual analysis signs. Ti - Thermal load shall be evaluated for both hot and cold conditions. 2. Design value for (+) direction is the larger of zero and the value calculated; (-) direction is the smaller of zero and the value calculated. 3. S AISC =  The basic allowable stresses defined in Part I of the AISC Specification for the Design, Fabrication, and Erection of Structural Steel for Buildings, November 1978.  (Excluding the 1.33 factor).
Sheet 4 of 5 Notes:  1. Signs for Load Evaluation  DW - Carries the actual analysis signs. Ti - Thermal load shall be evaluated for both hot and cold conditions. 2. Design value for (+) direction is the larger of zero and the value calculated; (-) direction is the smaller of zero and the value calculated. 3. S AISC =  The basic allowable stresses defined in Part I of the AISC Specification for the Design, Fabrication, and Erection of Structural Steel for Buildings, November 1978.  (Excluding the 1.33 factor).
S58   =  The basic allowable load as defined by the vendor in accordance with MSS SP-58, 1967 edition, Pipe Hangers and Supports.
S 58   =  The basic allowable load as defined by the vendor in accordance with MSS SP-58, 1967 edition, Pipe Hangers and Supports.
Fy   =  The minimum yield stress of support member at elevated sustained temperature (i.e., normal operating temperature exceeds 150
F y   =  The minimum yield stress of support member at elevated sustained temperature (i.e., normal operating temperature exceeds 150
°F). VLR  = The basic load rating supplied by the vendor. LCD  = Load capacity data sheet as levels supplied by the vendor.  
°F). VLR  = The basic load rating supplied by the vendor. LCD  = Load capacity data sheet as levels supplied by the vendor.  
: 4. Linear Allowables shall not exceed 0.9F y for tension or 0.9F y/3 = 0.52F y for shear. 5. Load rated allowables established according to ASME section III subsection NF are acceptable using the appropriate load level. 6. Linear support allowables may be used for detailed analysis of standard support components.
: 4. Linear Allowables shall not exceed 0.9F y for tension or 0.9F y/3 = 0.52F y for shear. 5. Load rated allowables established according to ASME section III subsection NF are acceptable using the appropriate load level. 6. Linear support allowables may be used for detailed analysis of standard support components.
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Primary Stress Limit - ASME Boiler Normal and upset condition loads General membrane 26,700  and Pressure Vessel Code, Sect. III 1. Dead weight defines stress limit for SA 302 2. Operating Basis Earthquake Gr. B Emergency condition loads General membrane 40,000 For normal and upset condition 1. Dead weight  
Primary Stress Limit - ASME Boiler Normal and upset condition loads General membrane 26,700  and Pressure Vessel Code, Sect. III 1. Dead weight defines stress limit for SA 302 2. Operating Basis Earthquake Gr. B Emergency condition loads General membrane 40,000 For normal and upset condition 1. Dead weight  


SM = 26,700 psi 2. Design Basis Earthquake  
S M = 26,700 psi 2. Design Basis Earthquake  


For emergency condition Faulted condition loads General membrane 53,400 Slimit = 1.5 SM = 1.5 X 26,700 =  1. Dead weight 40,000 psi 2. Design Basis Earthquake  
For emergency condition Faulted condition loads General membrane 53,400 Slimit = 1.5 S M = 1.5 X 26,700 =  1. Dead weight 40,000 psi 2. Design Basis Earthquake  
: 3. Jet reaction forces For faulted condition   
: 3. Jet reaction forces For faulted condition   


Slimit = 2.0 SM = 20 X 26,700 = 53,400 psi  
Slimit = 2.0 S M = 20 X 26,700 = 53,400 psi  


BFN-27    Sheet  2 Table C.4-1 (Continued)
BFN-27    Sheet  2 Table C.4-1 (Continued)
Line 263: Line 257:
Shroud leg Support Primary Stress Limit - ASME Boiler Normal and upset condition loads Tensile 23,300  and Pressure Vessel Code, Sect. III 1. Operating Basis Earthquake defines allowable primary membrane 2. Pressure drop across shroud stress SB-168 material.    (normal)  
Shroud leg Support Primary Stress Limit - ASME Boiler Normal and upset condition loads Tensile 23,300  and Pressure Vessel Code, Sect. III 1. Operating Basis Earthquake defines allowable primary membrane 2. Pressure drop across shroud stress SB-168 material.    (normal)  
: 3. Subtract dead weight  
: 3. Subtract dead weight  
: 1. Tensile Loads For normal and upset condition Emergency condition loads Tensile 35,000 SM = 23,300 psi 1. Design Basis Earthquake  2. Pressure drop across shroud For emergency condition    (normal)  
: 1. Tensile Loads For normal and upset condition Emergency condition loads Tensile 35,000 S M = 23,300 psi 1. Design Basis Earthquake  2. Pressure drop across shroud For emergency condition    (normal)  


Slimit = 1.5 SM   3. Subtract dead weight        = 1.5 X 23,300 = 35,000 psi  Faulted condition loads Tensile 46,600  For faulted condition 1. Design Basis Earthquake  
Slimit = 1.5 S M   3. Subtract dead weight        = 1.5 X 23,300 = 35,000 psi  Faulted condition loads Tensile 46,600  For faulted condition 1. Design Basis Earthquake  


Slimit = 2.0 SM 2. Pressure drop across shroud        = 2.0 X 23,300 = 46,600 psi    during faulted condition  
Slimit = 2.0 S M 2. Pressure drop across shroud        = 2.0 X 23,300 = 46,600 psi    during faulted condition  
: 3. Subtract dead weight  
: 3. Subtract dead weight  
: 2. Compressive Loads For normal and upset condition Normal and upset condition loads Compressive 14,000 SA = 0.4 Sy 1. Operating Basis Earthquake    = 0.4 X 35,000 = 14,000 psi 2. Zero pressure drop across shroud For emergency condition 3. Dead weight  
: 2. Compressive Loads For normal and upset condition Normal and upset condition loads Compressive 14,000 S A = 0.4 S y 1. Operating Basis Earthquake    = 0.4 X 35,000 = 14,000 psi 2. Zero pressure drop across shroud For emergency condition 3. Dead weight  


Slimit = 0.6 Sy           = 0.6 X 35,000 = 21,000 psi Emergency condition loads Compressive 21,000  1. Design Basis Earthquake For faulted condition 2. Subtract operating pressure  
Slimit = 0.6 S y           = 0.6 X 35,000 = 21,000 psi Emergency condition loads Compressive 21,000  1. Design Basis Earthquake For faulted condition 2. Subtract operating pressure  


Slimit = 0.8 Sy     drop across shroud        = 0.8 X 35,000 = 28,000 psi 3. Dead weight  
Slimit = 0.8 S y     drop across shroud        = 0.8 X 35,000 = 28,000 psi 3. Dead weight  


Faulted condition loads Compressive 28,000  1. Design Basis Earthquake  
Faulted condition loads Compressive 28,000  1. Design Basis Earthquake  
Line 285: Line 279:
For normal and upset condition Emergency condition loads* General membrane plus 38,081  Stress Intensity 1. Design Basis Earthquake bending  
For normal and upset condition Emergency condition loads* General membrane plus 38,081  Stress Intensity 1. Design Basis Earthquake bending  


SA = 1.5 Sm = 1.5 X 16.925 = 25,388 psi 2. Weight of structure  
S A = 1.5 S m = 1.5 X 16.925 = 25,388 psi 2. Weight of structure  


For emergency condition  
For emergency condition  


Slimit = 1.5 SA = 1.5 X 25,388        = 38,081 psi Faulted condition loads* General membrane plus 50,775  (Same as emergency condition) bending For faulted condition  
Slimit = 1.5 S A = 1.5 X 25,388        = 38,081 psi Faulted condition loads* General membrane plus 50,775  (Same as emergency condition) bending For faulted condition  


Slimit = 2SA = 2 X 25,388 = 50,775 psi  
Slimit = 2S A = 2 X 25,388 = 50,775 psi  


Top Guide Beam End Connections Primary Stress Limit - ASME Boiler Normal and upset condition loads* Pure shear 10,155  and Pressure Vessel Code, Sect. III 1. Operating Basis Earthquake defines material stress limit for 2. Weight of structure Type 304 stainless steel  
Top Guide Beam End Connections Primary Stress Limit - ASME Boiler Normal and upset condition loads* Pure shear 10,155  and Pressure Vessel Code, Sect. III 1. Operating Basis Earthquake defines material stress limit for 2. Weight of structure Type 304 stainless steel  


For normal and upset condition Stress Intensity Emergency condition loads* Pure shear 15,232 SA = 06 Sm = 0.6 X 16,925 = 10,155 psi 1. Design Basis Earthquake  2. Weight of structure For emergency condition  
For normal and upset condition Stress Intensity Emergency condition loads* Pure shear 15,232 S A = 06 S m = 0.6 X 16,925 = 10,155 psi 1. Design Basis Earthquake  2. Weight of structure For emergency condition  


Slimit = 1.5 SA       = 1.5 X 10,155 = 15,232 psi Faulted condition loads* Pure shear  20,310  (Same as emergency condition) For faulted condition  
Slimit = 1.5 S A       = 1.5 X 10,155 = 15,232 psi Faulted condition loads* Pure shear  20,310  (Same as emergency condition) For faulted condition  


Slimit = 2SA = 2 X 10,155 = 20,310 psi  
Slimit = 2S A = 2 X 10,155 = 20,310 psi  


*Note:  Normal, upset, and accident top guide hydraulic loads are upward. These are not included in the stress analysis since they counteract the effect of the structure weight.  
*Note:  Normal, upset, and accident top guide hydraulic loads are upward. These are not included in the stress analysis since they counteract the effect of the structure weight.  
Line 329: Line 323:
Fuel Channels  
Fuel Channels  


Primary Stress Limit - The allowable Normal and Upset condition loads Membrane and bending 28,230 Sm for Zircaloy determined according 1. Operating Basis Earthquake to methods recommended by ASME 2. Normal pressure load Boiler and Pressure Vessel Code, Sect. III. Allowable moment Emergency condition loads Membrane and bending 42,350  determined by calculating limit 1. Design Basis Earthquake moment using Table C.2-2                    2. Normal pressure load equation (b), then applying SFmin  for applicable loading conditions. Faulted condition loads Membrane and bending 56,500  1. Design Basis Earthquake 2. Loss-of-coolant accident (Sm = 9,270 psi, 1.5 S m = 13,900 psi)    pressure  
Primary Stress Limit - The allowable Normal and Upset condition loads Membrane and bending 28,230 S m for Zircaloy determined according 1. Operating Basis Earthquake to methods recommended by ASME 2. Normal pressure load Boiler and Pressure Vessel Code, Sect. III. Allowable moment Emergency condition loads Membrane and bending 42,350  determined by calculating limit 1. Design Basis Earthquake moment using Table C.2-2                    2. Normal pressure load equation (b), then applying SFmin  for applicable loading conditions. Faulted condition loads Membrane and bending 56,500  1. Design Basis Earthquake 2. Loss-of-coolant accident (S m = 9,270 psi, 1.5 S m = 13,900 psi)    pressure  


Emergency limit load = 1.5 X Normal limit load calculated using 1.5 Sm =  yield BFN-27    Sheet  6 Table C.4-1 (Continued)
Emergency limit load = 1.5 X Normal limit load calculated using 1.5 S m =  yield BFN-27    Sheet  6 Table C.4-1 (Continued)
REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES  
REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES  


Line 347: Line 341:
BFN-27    Sheet 7 Table C.4-1 (Continued)
BFN-27    Sheet 7 Table C.4-1 (Continued)
REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Criteria  Loading Location Allowable Stress (psi)
REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Criteria  Loading Location Allowable Stress (psi)
CRD Housing Support "Shootout Steel"  
CRD Housing Support "Shootout Steel" Primary Stress Limit - AISC specification Faulted Condition loads Beams (top cord)  33,000  for the design, fabrication 1. Dead weight  33,000 and erection of structural steel 2. Impact force from failure Beams (bottom cord)  33,000  for buildings    of a CRD housing  33,000   
 
Primary Stress Limit - AISC specification Faulted Condition loads Beams (top cord)  33,000  for the design, fabrication 1. Dead weight  33,000 and erection of structural steel 2. Impact force from failure Beams (bottom cord)  33,000  for buildings    of a CRD housing  33,000   
 
For normal and upset condition (Dead weights and earthquake Grid structure  41,500 Fa = 0.60 F y (tension) loads are very small as  27,500 Fb = 0.60 F y (bending) compared to jet force.)
Fv = 0.40 F y (shear)


For normal and upset condition (Dead weights and earthquake Grid structure  41,500 F a = 0.60 F y (tension) loads are very small as  27,500 F b = 0.60 F y (bending) compared to jet force.)
F v = 0.40 F y (shear)
For faulted conditions  
For faulted conditions  


Fa limit = 1.5 F a (tension)
F a limit = 1.5 F a (tension)
Fb limit = 1.5 F b (bending)
F b limit = 1.5 F b (bending)
Fv limit = 1.5 F b (shear)
F v limit = 1.5 F b (shear) F y = Material yield strength  
Fy = Material yield strength  


Recirculating Pipe and Pump Pipe Rupture Restraints Primary Stress Limit - Structural Faulted condition loads Brackets on 28 in. pipe  33,000  Steel:  AISC specification for the 1. Jet force from a complete design, fabrication and erection    circumferential failure Cable on pump restraints  99,000  of structural steel for buildings.    (break) of recirculation line  
Recirculating Pipe and Pump Pipe Rupture Restraints Primary Stress Limit - Structural Faulted condition loads Brackets on 28 in. pipe  33,000  Steel:  AISC specification for the 1. Jet force from a complete design, fabrication and erection    circumferential failure Cable on pump restraints  99,000  of structural steel for buildings.    (break) of recirculation line  


For normal or upset conditions Fa = 0.60 F y (tension)  
For normal or upset conditions F a = 0.60 F y (tension)  


For faulted conditions  
For faulted conditions  


Fa limit = 1.5 F a (tension)
F a limit = 1.5 F a (tension)
Fy = yield strength Cable (wire rope)
F y = yield strength Cable (wire rope)
For faulted conditions  
For faulted conditions  


Fa = 0.80 F u (tension)
F a = 0.80 F u (tension)
Fu = ultimate strength BFN-27    Sheet  8 Table C.4-1 (Continued)
F u = ultimate strength BFN-27    Sheet  8 Table C.4-1 (Continued)
REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES  
REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES  


Line 378: Line 368:
Control Rod Drive Housing  
Control Rod Drive Housing  


Primary Stress Limit - The allowable      Normal and upset condition loads Maximum membrane  16,925  primary membrane stress is based on 1. Design pressure stress intensity occurs the ASME Boiler and Pressure Vessel 2. Stuck rod scram loads at the tube to tube Code Sect. III, for Class A vessels  3. Operating Basis Earthquake weld near the center of for Type 304 stainless steel  the housing for normal upset and emergency For normal and upset condition  conditions Sm = 16,925 psi at 575 oF For emergency conditions Emergency condition loads  25,100 Slimit = 1.5 Sm = 1.5 X 16,925=25,400 psi 1. Design pressure 2. Stuck rod scram loads 3. Design Basis Earthquake  
Primary Stress Limit - The allowable      Normal and upset condition loads Maximum membrane  16,925  primary membrane stress is based on 1. Design pressure stress intensity occurs the ASME Boiler and Pressure Vessel 2. Stuck rod scram loads at the tube to tube Code Sect. III, for Class A vessels  3. Operating Basis Earthquake weld near the center of for Type 304 stainless steel  the housing for normal upset and emergency For normal and upset condition  conditions S m = 16,925 psi at 575 o F For emergency conditions Emergency condition loads  25,100 Slimit = 1.5 S m = 1.5 X 16,925=25,400 psi 1. Design pressure 2. Stuck rod scram loads 3. Design Basis Earthquake  


Control Rod Drive  
Control Rod Drive  


Primary Stress Limit - The allowable Normal and upset condition loads Maximum stress intensity  26,060  primary membrane stress plus Maximum hydraulic pressure occurs at a point on the bending stress is based on ASME from the control rod drive Y-Y axis of the indicator Boiler and Pressure Vessel Code Supply pump. tube Sect. III for SA-212 TP 316 NOTE - Accident conditions tubing do not increase this loading Earthquake loads are negligible For normal and upset condition SA = 1.5 Sm = 1.5 X 17.375 = 26,060 psi BFN-27      Sheet  9 Table C.4-1 (Continued)
Primary Stress Limit - The allowable Normal and upset condition loads Maximum stress intensity  26,060  primary membrane stress plus Maximum hydraulic pressure occurs at a point on the bending stress is based on ASME from the control rod drive Y-Y axis of the indicator Boiler and Pressure Vessel Code Supply pump. tube Sect. III for SA-212 TP 316 NOTE - Accident conditions tubing do not increase this loading Earthquake loads are negligible For normal and upset condition S A = 1.5 S m = 1.5 X 17.375 = 26,060 psi BFN-27      Sheet  9 Table C.4-1 (Continued)
REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Criteria  Loading Location Allowable Stress (psi)
REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Criteria  Loading Location Allowable Stress (psi)
Control Rod Guide Tube (pre-uprate)  
Control Rod Guide Tube (pre-uprate)  
Line 390: Line 380:
For normal and upset conditions  
For normal and upset conditions  


Sm = 16,925 psi For faulted condition Slimit = 1.5 Sm = 1.5 X 16,925 - 25,400  
S m = 16,925 psi For faulted condition Slimit = 1.5 S m = 1.5 X 16,925 - 25,400  


Control Rod Guide Tube (uprate)*    Allowable loads (lbs)        Pressure differential (psi)  
Control Rod Guide Tube (uprate)*    Allowable loads (lbs)        Pressure differential (psi)  
Line 405: Line 395:
For normal and upset conditions  
For normal and upset conditions  


Sm = 16,925 psi at 575 oF For emergency condition (N + A M) Slimit = 1.5 Sm = 1.5 X 16,925 = 25,400 psi  
S m = 16,925 psi at 575 o F For emergency condition (N + A M) Slimit = 1.5 S m = 1.5 X 16,925 = 25,400 psi  


*The component did not change as a result of increasing power but represents the parameters that were reevaluated as part of the power uprate analysis.
*The component did not change as a result of increasing power but represents the parameters that were reevaluated as part of the power uprate analysis.
Line 416: Line 406:


Loads: where: t = 4.888 in. t  = minimum thickness, inches    Design pressure and temperature    d  = diameter or short span, in.
Loads: where: t = 4.888 in. t  = minimum thickness, inches    Design pressure and temperature    d  = diameter or short span, in.
Design bolting load    C  = attachment factor Gasket load    S  = allowable stress, psi    W  = total, bolt load, lb hG = gasket moment arm, in.
Design bolting load    C  = attachment factor Gasket load    S  = allowable stress, psi    W  = total, bolt load, lb h G = gasket moment arm, in.
Ci = corrosion allowance, in. Primary Stress Limit:
C i = corrosion allowance, in. Primary Stress Limit:
Allowable working stress per  
Allowable working stress per  


ASME Section VIII tPdSPC=+15212..tdCPSWhSdCG=++1783121./
ASME Section VIII t Pd SP C=+15212..td CP S Wh Sd C G=++178 3 12 1./
BFN-27                  Sheet 2 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Isolation Valves (Continued)  
BFN-27                  Sheet 2 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Isolation Valves (Continued)  


Line 433: Line 423:
2 Seismic load - Design Basis vertical seismic forces shall be applied at  Earthquake the mass center of the valve operator assum- ing that the valve body is rigid and anchored. Flange Stress Limits:  
2 Seismic load - Design Basis vertical seismic forces shall be applied at  Earthquake the mass center of the valve operator assum- ing that the valve body is rigid and anchored. Flange Stress Limits:  


SH, SR, ST 1.5 Sm per ASME Nuclear Pump and Valve Code, Class I.
S H , S R , S T 1.5 S m per ASME Nuclear Pump and Valve Code, Class I.
BFN-27        Sheet 3 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Isolation Valves(Continued)
BFN-27        Sheet 3 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Isolation Valves(Continued)
Criteria Method of Analysis                        Allowable Stress
Criteria Method of Analysis                        Allowable Stress
: 5. Valve Disc Thickness       
: 5. Valve Disc Thickness       


Loads: where: S = 17,800 lb/in 2  Sr = radial stress, psi    Design pressure and temperature  S t  = tangential stress Primary bending stress limit:    v  = Poisson's ratio    P  = design pressure, psi Allowable working stress per    R  = radius of disc, inches ASME Section VIII    t  = thickness of disc, inches  
Loads: where: S = 17,800 lb/in 2  S r = radial stress, psi    Design pressure and temperature  S t  = tangential stress Primary bending stress limit:    v  = Poisson's ratio    P  = design pressure, psi Allowable working stress per    R  = radius of disc, inches ASME Section VIII    t  = thickness of disc, inches  
: 6. Valve Operator Supports The valve assembly shall be analyzed assuming  that the rigid mass and that the valve body  Loads: is an anchored, rigid mass and that the specified vertical and horizontal seismic  Design pressure and temperature              forces are applied at the mass center of the      S = 18,000 lb/in 2 Stem operational load                        operator assembly, simultaneously with Equipment dead weight                      operating pressure plus dead weight plus Seismic load-Design Basis                    operational loads. Using these loads,                                                      stresses and deflections shall be determined Support Rod Stress Limit:                    for the operator support components.               
: 6. Valve Operator Supports The valve assembly shall be analyzed assuming  that the rigid mass and that the valve body  Loads: is an anchored, rigid mass and that the specified vertical and horizontal seismic  Design pressure and temperature              forces are applied at the mass center of the      S = 18,000 lb/in 2 Stem operational load                        operator assembly, simultaneously with Equipment dead weight                      operating pressure plus dead weight plus Seismic load-Design Basis                    operational loads. Using these loads,                                                      stresses and deflections shall be determined Support Rod Stress Limit:                    for the operator support components.               


Line 444: Line 434:


ASME Section VIII  
ASME Section VIII  
()SS33vPR8trt22==+
()SS33vPR 8t rt 2 2==+
BFN-27      Sheet 4 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves Criteria        Method of Analysis Allowable Stress              Minimum Dimension Required  
BFN-27      Sheet 4 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves Criteria        Method of Analysis Allowable Stress              Minimum Dimension Required  
: 1. Inlet Nozzle Wall Thickness
: 1. Inlet Nozzle Wall Thickness
Line 457: Line 447:
°F W  =  shear load, lb  A  =  shear area, in.
°F W  =  shear load, lb  A  =  shear area, in.
2 Diagonal Shear Stress Limit: P  =  1.1 X design pressure, lb/in.
2 Diagonal Shear Stress Limit: P  =  1.1 X design pressure, lb/in.
A1 =  disc area, in.2 0.6  x allowable stress intensity and: as defined by ASME Standard Code  A  =  S (R + R1) for Pumps and Valves for Nuclear  S  =  slope of frustrum of shear cone, in. Power R1 =  radius at base of cone, in. R  =  radius at top of cone, in.  
A 1 =  disc area, in.2 0.6  x allowable stress intensity and: as defined by ASME Standard Code  A  =  S (R + R 1) for Pumps and Valves for Nuclear  S  =  slope of frustrum of shear cone, in. Power R 1 =  radius at base of cone, in. R  =  radius at top of cone, in.  
: 3. Inlet Flange Bolt Area Total bolting loads and stresses shall be  calculated in accordance with procedures of Loads:  Para. 1-704.5.1 Flanged Joints, of B31.7 S b = 27,700 lb/in.
: 3. Inlet Flange Bolt Area Total bolting loads and stresses shall be  calculated in accordance with procedures of Loads:  Para. 1-704.5.1 Flanged Joints, of B31.7 S b = 27,700 lb/in.
2  Nuclear Piping Code. Design pressure and temperature Gasket load Operational load Design Basis Earthquake  
2  Nuclear Piping Code. Design pressure and temperature Gasket load Operational load Design Basis Earthquake  


Bolting Stress Limit: Allowable stress intensity, S m, as defined by ASME Standard Code for Pumps and Valves for Nuclear Power tPRSEPC=+0.6SsWAPAA==1 BFN-27        Sheet 5 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves (Continued)  
Bolting Stress Limit: Allowable stress intensity, S m, as defined by ASME Standard Code for Pumps and Valves for Nuclear Power t PRSEP C=+0.6 Ss W A PA A==1 BFN-27        Sheet 5 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves (Continued)  


Criteria Method of Analysis  Allowable Stress    4. Inlet Flange Thickness Flange thickness and stresses shall be  S H= 27,300 lb/in.
Criteria Method of Analysis  Allowable Stress    4. Inlet Flange Thickness Flange thickness and stresses shall be  S H= 27,300 lb/in.
Line 467: Line 457:
2      Loads:                          Para. 1-704.5.1 Flanged Joints, of B31.7  S T= 27,300 lb/in.
2      Loads:                          Para. 1-704.5.1 Flanged Joints, of B31.7  S T= 27,300 lb/in.
2                                              Nuclear Piping Code.      Design pressure and temperature Gasket load Operational load Seismic load-Design Basis Earthquake Flange Stress Limits:
2                                              Nuclear Piping Code.      Design pressure and temperature Gasket load Operational load Seismic load-Design Basis Earthquake Flange Stress Limits:
SH, SR, ST 1.5 S m per ASME Nuclear Pump    and Valve Code  Set Point  5. Valve Spring-Torsional Stress                          S = 82,500 lb/in 2      Loads: where:  Smax = torsional stress, lb/in 2 Maximum Lift        W1 =  Set point load P = W 1 or W2 = spring load,      W2 =  Spring load at maximum D = means diameter of coil, in. S = 112,500 lb/in.
S H , S R , S T 1.5 S m per ASME Nuclear Pump    and Valve Code  Set Point  5. Valve Spring-Torsional Stress                          S = 82,500 lb/in 2      Loads: where:  S max = torsional stress, lb/in 2 Maximum Lift        W 1 =  Set point load P = W 1 or W 2 = spring load,      W 2 =  Spring load at maximum D = means diameter of coil, in. S = 112,500 lb/in.
2  lift, lb d = diameter of wire, in. C =  D  = correction factor            d Torsional Stress Limit 0.67 X torsional elastic limit when subjected to a load of W
2  lift, lb d = diameter of wire, in. C =  D  = correction factor            d Torsional Stress Limit 0.67 X torsional elastic limit when subjected to a load of W
: 1.
: 1.
0.90 X torsional elastic limit when subjected to a load of W
0.90 X torsional elastic limit when subjected to a load of W
: 2. SPDdCCCmax.=+8414406153 BFN-27        Sheet 6 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves (Continued)
: 2. S PD d C CCmax.=+841 440615 3 BFN-27        Sheet 6 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves (Continued)
Criteria Method of Analysis  Allowable Stress          Minimum Dimension Required
Criteria Method of Analysis  Allowable Stress          Minimum Dimension Required
: 6. Yoke Rod Area                                                    Loads:      where:
: 6. Yoke Rod Area                                                    Loads:      where:
Spring load at maximum lift A = required area per rod, in 2  A = 0.852 in.
Spring load at maximum lift A = required area per rod, in 2  A = 0.852 in.
2 F = total spring load, lb Primary Stress Limit: S m = allowable stress, lb/in.
2 F = total spring load, lb Primary Stress Limit: S m = allowable stress, lb/in.
2    Allowable stress intensity, S m, as      defined by ASME Standard Code for Pumps and Valves for Nuclear Power.  
2    Allowable stress intensity, S m , as      defined by ASME Standard Code for Pumps and Valves for Nuclear Power.  
: 7. Yoke Bending and Shear Stresses Sb = 18,200 lb/in.
: 7. Yoke Bending and Shear Stresses S b = 18,200 lb/in.
2 Loads: where:  S s = 10,900 lb/in.
2 Loads: where:  S s = 10,900 lb/in.
2      Spring load at maximum lift S b = bending stress, lb/in.
2      Spring load at maximum lift S b = bending stress, lb/in.
2        Ss = shear stress, lb/in.
2        S s = shear stress, lb/in.
2      Bending and Shear Stress Limits:      M  = bending moment, in.-lb Z  = section modulus, in.
2      Bending and Shear Stress Limits:      M  = bending moment, in.-lb Z  = section modulus, in.
3      Bending-allowable stress intensity, V  = vertical shear, lb      Sm, per ASME Nuclear Pump and Valve    A  = shear area, in.
3      Bending-allowable stress intensity, V  = vertical shear, lb      S m, per ASME Nuclear Pump and Valve    A  = shear area, in.
2      Code Shear - 0.6 X allowable stress intensity, 0.6 S m, per ASME Nuclear      Pump and Valve Code.  
2      Code Shear - 0.6 X allowable stress intensity, 0.6 S m, per ASME Nuclear      Pump and Valve Code.  
: 8. Body Minimum Wall Thickness     
: 8. Body Minimum Wall Thickness     
Line 489: Line 479:
2    P = primary service pressure, 150 lb/in 2  Inlet Nozzle        Primary Stress Limit: d = inside diameter of valve at                                              t = 0.231 in.              section being considered, in.
2    P = primary service pressure, 150 lb/in 2  Inlet Nozzle        Primary Stress Limit: d = inside diameter of valve at                                              t = 0.231 in.              section being considered, in.
Allowable stress, 7,000 lb/in 2,  Outlet Nozzle      in accordance with USAS B16.5.                                                                                            t = 0.2823 in.
Allowable stress, 7,000 lb/in 2,  Outlet Nozzle      in accordance with USAS B16.5.                                                                                            t = 0.2823 in.
AFSm=2SMZSVAbs==,tPdSPC=+1521..2 BFN-27    Sheet 7 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves
A F S m=2 S M Z S V A bs==, t Pd SP C=+15 21..2 BFN-27    Sheet 7 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves


Criteria  Method of Analysis Allowable Stress            Load Limit
Criteria  Method of Analysis Allowable Stress            Load Limit
Line 506: Line 496:
4      L  =  length of spindle in compression, in.
4      L  =  length of spindle in compression, in.
0.2 X critical buckling load  
0.2 X critical buckling load  
: 11. Spring Washer Shear Area    Ss = 15,960 lb/in.
: 11. Spring Washer Shear Area    S s = 15,960 lb/in.
2 Loads where:  
2 Loads where:  


Spring load at maximum lift  S s = shear stress, lb/in.
Spring load at maximum lift  S s = shear stress, lb/in.
2      F  = spring load, lb  Shear Stress Limit:  A  =  shear area, in.
2      F  = spring load, lb  Shear Stress Limit:  A  =  shear area, in.
2  0.6 X allowable stress intensity, 0.6Sm, per ASME Nuclear Pump and  Valve Code.
2  0.6 X allowable stress intensity, 0.6S m, per ASME Nuclear Pump and  Valve Code.
SFFAMMZ=+++1212FEILc=22SFAs=
S FF A MM Z=+++1212 F EI L c=2 2 S F A s=
BFN-27      Sheet 8 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Relief Valves
BFN-27      Sheet 8 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Relief Valves


Line 530: Line 520:
t  =  minimum required thickness, in.            Pilot Base:      Design pressure and temperature  d  = diameter or short span, in.      Gasket load  C  = attachment factor, ASME            t = 2.117 in.
t  =  minimum required thickness, in.            Pilot Base:      Design pressure and temperature  d  = diameter or short span, in.      Gasket load  C  = attachment factor, ASME            t = 2.117 in.
Section VIII Primary Stress Limit:  P  = design pressure, lb/in.
Section VIII Primary Stress Limit:  P  = design pressure, lb/in.
2    Sm = allowable stress, lb/in.
2    S m = allowable stress, lb/in.
2      Allowable stress intensity, Sm,  W  = total bolt load, lb as defined by ASME Standard  h g  = gasket moment arm, in.      Code for Pumps and Valves  C 1  = corrosion allowance, 0.12 in.      for Nuclear Power. t1.5 PD2S1 2PC=+tdCPSWhGSdCmm=++1783121./
2      Allowable stress intensity, Sm,  W  = total bolt load, lb as defined by ASME Standard  h g  = gasket moment arm, in.      Code for Pumps and Valves  C 1  = corrosion allowance, 0.12 in.      for Nuclear Power. t1.5 PD2S1 2P C=+td CP SWhG Sd C m m=++178 3 12 1./
BFN-27      Sheet 9 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Relief Valves (Continued)  
BFN-27      Sheet 9 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Relief Valves (Continued)  


Criteria Method of Analysis Allowable Stress Minimum Dimension Required       
Criteria Method of Analysis Allowable Stress Minimum Dimension Required       
: 3. Flange Bolt Area - Inlet Flange, Total bolting loads and stresses shall be  Body to Base:
: 3. Flange Bolt Area - Inlet Flange, Total bolting loads and stresses shall be  Body to Base:
Outlet Flange, Body to Bonnet, calculated in accordance with procedures Bonnet to Base of Para. 1-704.5.1 Flanged Joints, of A b = 10.26 in 2  Ab = 2.854 in.
Outlet Flange, Body to Bonnet, calculated in accordance with procedures Bonnet to Base of Para. 1-704.5.1 Flanged Joints, of A b = 10.26 in 2  A b = 2.854 in.
2            B31.7 Nuclear Piping Code Loads:    Bonnet to Cap:  
2            B31.7 Nuclear Piping Code Loads:    Bonnet to Cap:  


Design pressure and temperature  A b = 1.452 in.
Design pressure and temperature  A b = 1.452 in.
2 Ab = 0.995 in.
2 A b = 0.995 in.
2  Gasket load        Operational load    Inlet Flange Design Basis Earthquake          Ab = 13.9 in.
2  Gasket load        Operational load    Inlet Flange Design Basis Earthquake          A b = 13.9 in.
2 Ab = 6.25 in.
2 A b = 6.25 in.
2  Bolting Stress Limit:
2  Bolting Stress Limit:
Outlet Flange:
Outlet Flange:
Allowable stress intensity, S m as  Ab = 12.2 in 2    defined by ASME Standard Code for    A b = 5.5 in.
Allowable stress intensity, S m as  A b = 12.2 in 2    defined by ASME Standard Code for    A b = 5.5 in.
2  Pumps and Valves for Nuclear Power.  
2  Pumps and Valves for Nuclear Power.  
: 4. Flange Thickness - Inlet, Outlet, Flange thickness and stresses shall be    Bonnet Flanges calculated in accordance with procedures S H = 26,250 lb/in.
: 4. Flange Thickness - Inlet, Outlet, Flange thickness and stresses shall be    Bonnet Flanges calculated in accordance with procedures S H = 26,250 lb/in.
Line 556: Line 546:
Flange Stress Limits:  
Flange Stress Limits:  


SH, SR, ST     1.5 Sm per ASME Nuclear  Pumps and Valve Code.  
S H , S R , S T     1.5 S m per ASME Nuclear  Pumps and Valve Code.  


BFN-27      Sheet 10 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Relief Valves (Continued)  
BFN-27      Sheet 10 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Relief Valves (Continued)  
Line 563: Line 553:
: 5. Valve Disc. Thickness and Stress  Disc Stress:                                                       
: 5. Valve Disc. Thickness and Stress  Disc Stress:                                                       


Loads: where:  S m = 15,800 lb/in 2    Design pressure and temperature    S r = radial stress, lb/in 2        St =  tangential stress, lb/in 2  Primary Stress Limit:    v  =  Poisson's ratio P =  design pressure, lb/in 2  Allowable stress intensity, S m    R =  radius of disc, in. as defined by ASME Standard Code for    t  =  thickness of disc, in.
Loads: where:  S m = 15,800 lb/in 2    Design pressure and temperature    S r = radial stress, lb/in 2        S t =  tangential stress, lb/in 2  Primary Stress Limit:    v  =  Poisson's ratio P =  design pressure, lb/in 2  Allowable stress intensity, S m    R =  radius of disc, in. as defined by ASME Standard Code for    t  =  thickness of disc, in.
Pumps and Valve for Nuclear Power.
Pumps and Valve for Nuclear Power.
Inlet Nozzle Diameter Thickness          and Stress  Inlet Nozzle Stress:               
Inlet Nozzle Diameter Thickness          and Stress  Inlet Nozzle Stress:               


Loads: where: S = 26,250 lb/in 2      S  =  combined bending and tensile  Design pressure and temperature        stress, lb/in 2  Operational load  F 1 = vertical load due to design pressure, lb  Design Basis Earthquake  F 2 =  vertical component of reaction              thrust, lb Primary Stress Limit:  A  = cross section area of nozzle, in 2      M1 = moment resulting from horizontal  1.5 X allowable stress intensity,        reaction, in.-lb 1.5 Sm as defined by ASME  M 2 = moment resulting from horizontal  Standard Code for Pumps and  seismic force at mass center of  Valves for Nuclear Power.        valve, in.-lb  
Loads: where: S = 26,250 lb/in 2      S  =  combined bending and tensile  Design pressure and temperature        stress, lb/in 2  Operational load  F 1 = vertical load due to design pressure, lb  Design Basis Earthquake  F 2 =  vertical component of reaction              thrust, lb Primary Stress Limit:  A  = cross section area of nozzle, in 2      M 1 = moment resulting from horizontal  1.5 X allowable stress intensity,        reaction, in.-lb 1.5 S m as defined by ASME  M 2 = moment resulting from horizontal  Standard Code for Pumps and  seismic force at mass center of  Valves for Nuclear Power.        valve, in.-lb  


   ()SSvPRtrt==+33822SFFAMMZ=+++1212 BFN-27                      Sheet 11 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Pumps
   ()SSvPR t rt==+33 8 2 2 S FF A MM Z=+++1212 BFN-27                      Sheet 11 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Pumps


Criteria Method of Analysis  Allowable Stress      Minimum Dimension Required
Criteria Method of Analysis  Allowable Stress      Minimum Dimension Required
Line 578: Line 568:
Design pressure and temperature            S r = 15,075 psi                                                                                                      Primary Bending Stress Limit:   
Design pressure and temperature            S r = 15,075 psi                                                                                                      Primary Bending Stress Limit:   


1.5 Sm per ASME code for        Pumps and Valves for    S t = 15,075 psi  Nuclear Power Class I     
1.5 S m per ASME code for        Pumps and Valves for    S t = 15,075 psi  Nuclear Power Class I     


where:
where:
Sr =  radial stress at outer edge, psi        St =  tangential stress at inner edge, psi        w =  pressure load, psi        W = uniform load along inner edge, lb          t =  disc thickness, in.
S r =  radial stress at outer edge, psi        S t =  tangential stress at inner edge, psi        w =  pressure load, psi        W = uniform load along inner edge, lb          t =  disc thickness, in.
m =  reciprocal of Poisson's ratio a =  radius of disc, in.
m =  reciprocal of Poisson's ratio a =  radius of disc, in.
b = radius of disc hole, in.  
b = radius of disc hole, in.  
()()()()()Sr3W4t2a22b2b4m14b4m1ln aba2b2m1a2m1b2m1=++++++/()()()++++3W2pt212mb22b2m1lnaba2m1b2 m1/()()()St3Wm214mt2a4b44a2b2ln aba2m1b2m1=+++/()()()()()3W2pmt21ma2m1mb2m12m21a2ln aba2m1b2m1++++/tPRSE06PC=+-
()()()()()S r 3W 4t 2 a 2 2b 2 b 4m14b 4m1ln aba 2 b 2 m1 a 2m1b 2 m1=++++++/()()()++++3W 2pt 2 12mb 2 2b 2m1lnab a 2m1b 2 m1/()()()S t3Wm 2 14mt 2 a 4 b 4 4a 2 b 2ln ab a 2m1b 2 m1=+++/()()()()()3W2pmt 2 1 ma 2m1mb 2m12m 2 1a 2ln ab a 2m1b 2 m1++++/t PRSE06P C=+-
BFN-27      Sheet 12 Table C.4-2 (Continued)
BFN-27      Sheet 12 Table C.4-2 (Continued)
PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Pumps (Continued)  
PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Pumps (Continued)  
Line 630: Line 620:


The effect of the remaining energy on the vertical columns is analyzed. Equivalent static load tests are made on the structure to assure that the criteria are met.
The effect of the remaining energy on the vertical columns is analyzed. Equivalent static load tests are made on the structure to assure that the criteria are met.
BFN-27                Sheet 16 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RHR Pumps
BFN-27                Sheet 16 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RHR Pumps Criteria            Method of Analysis                                Allowable Stress       
 
Criteria            Method of Analysis                                Allowable Stress       
: 1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be      25,000 psi    contain the internal design pressure      calculated in accordance with the "Rules of the pump casing without exceeding      for Bolted Flange Connections," ASME the allowable stress of the bolting      Boiler and Pressure Vessel Code, material. Allowable stresses at      Section VIII, Appendix II.
: 1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be      25,000 psi    contain the internal design pressure      calculated in accordance with the "Rules of the pump casing without exceeding      for Bolted Flange Connections," ASME the allowable stress of the bolting      Boiler and Pressure Vessel Code, material. Allowable stresses at      Section VIII, Appendix II.
design temperature shall be in accordance with ASME Boiler and      Pump Design Pressure                450 psig pressure Vessel Code, Section VIII.      Maximum Design Temperature    350
design temperature shall be in accordance with ASME Boiler and      Pump Design Pressure                450 psig pressure Vessel Code, Section VIII.      Maximum Design Temperature    350
°F  2. The minimum wall thickness of the 2. Stress in the pump casing shall be      14,000 psi    pump shall limit stress to the      calculated at the point of maximum allowable stress when subjected to      internal pump diameter by the formula design pressure and temperature. Allowable stresses shall be in  accordance with ASME Boiler and Pressure Vessel Code, Section VIII. where  Sc =  calculated stress, psi P  =  pump design pressure, psi D  =  maximum pump internal diameter t  =  actual minimum metal thickness less corrosion allowance, 0.080 in.  
°F  2. The minimum wall thickness of the 2. Stress in the pump casing shall be      14,000 psi    pump shall limit stress to the      calculated at the point of maximum allowable stress when subjected to      internal pump diameter by the formula design pressure and temperature. Allowable stresses shall be in  accordance with ASME Boiler and Pressure Vessel Code, Section VIII. where  S c =  calculated stress, psi P  =  pump design pressure, psi D  =  maximum pump internal diameter t  =  actual minimum metal thickness less corrosion allowance, 0.080 in.  
  ()SPDttc=+02.2 BFN-27                Sheet 17 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RHR Pumps (Continued)  
  ()SPDt t c=+0 2.2 BFN-27                Sheet 17 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RHR Pumps (Continued)  


Criteria Method of Analysis and Allowable Nozzle Loads     
Criteria Method of Analysis and Allowable Nozzle Loads     
Line 656: Line 644:
°F  2. The minimum wall thickness of the 2. Stress in the pump casing shall be    14,000 psi  pump shall limit stress to the allow-  calculated at the point of maximum able stress when subjected to design    internal pump diameter by the formula pressure and temperature. Allowable                        stresses shall be in accordance with ASME Boiler and Pressure Vessel Code, Section VIII.   
°F  2. The minimum wall thickness of the 2. Stress in the pump casing shall be    14,000 psi  pump shall limit stress to the allow-  calculated at the point of maximum able stress when subjected to design    internal pump diameter by the formula pressure and temperature. Allowable                        stresses shall be in accordance with ASME Boiler and Pressure Vessel Code, Section VIII.   


where Sc = calculated stress, psi 17,500 psi allowable for 216 WCB X    P  = pump design pressure, psi 0.8 (quality factor) = 14,000 psi    D  = maximum pump internal diameter t  =  actual minimum metal thickness less corrosion allowance, 0.080 in.  
where S c = calculated stress, psi 17,500 psi allowable for 216 WCB X    P  = pump design pressure, psi 0.8 (quality factor) = 14,000 psi    D  = maximum pump internal diameter t  =  actual minimum metal thickness less corrosion allowance, 0.080 in.  
  ()SPDttc=+02.2 BFN-27                                                                          Sheet 19 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Core Spray Pumps (Continued)
  ()SPDt t c=+0 2.2 BFN-27                                                                          Sheet 19 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Core Spray Pumps (Continued)
Criteria                                Method of Analysis and Allowable Nozzle Loads  Representative Results
Criteria                                Method of Analysis and Allowable Nozzle Loads  Representative Results
: 3. Application of forces and moments by 3. Stresses will not be excessive if the  attaching pipe on pump nozzles under      maximum resultant force when taken with the  combined maximum thermal expansion      maximum resultant moment falls below the line. Operating Basis Earthquake loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel    Code, Section VIII. Suction          OBE                  DBE Fintercept    66,686 lb      104,955 lb  
: 3. Application of forces and moments by 3. Stresses will not be excessive if the  attaching pipe on pump nozzles under      maximum resultant force when taken with the  combined maximum thermal expansion      maximum resultant moment falls below the line. Operating Basis Earthquake loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel    Code, Section VIII. Suction          OBE                  DBE Fintercept    66,686 lb      104,955 lb  
Line 676: Line 664:
Volute stress shall be calculated by the Boost Pump    following formula          14,000 psi  The maximum stress in the pump          Roark casing when subjected to design  p. 307 Case 26 pressure shall not exceed the allow-                    able working stress of the material.
Volute stress shall be calculated by the Boost Pump    following formula          14,000 psi  The maximum stress in the pump          Roark casing when subjected to design  p. 307 Case 26 pressure shall not exceed the allow-                    able working stress of the material.
The allowable stress shall be in    and R = a - 0.5b accordance with ASME Boiler and Pressure Vessel Code, Section III.  
The allowable stress shall be in    and R = a - 0.5b accordance with ASME Boiler and Pressure Vessel Code, Section III.  
  ()SPDtETh=+02.2SPbRaRvt=+2 BFN-27            Sheet 21 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES HPCI Pumps (Continued)  
  ()SPDt ET h=+0 2.2 SPbRa R v t=+2 BFN-27            Sheet 21 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES HPCI Pumps (Continued)  


Criteria                            Method of Analysis and Allowable Nozzle Loads                               
Criteria                            Method of Analysis and Allowable Nozzle Loads                               
Line 691: Line 679:
Pipe Design Pressure Suction    =  150 psig Discharge  = 1500 psig  
Pipe Design Pressure Suction    =  150 psig Discharge  = 1500 psig  


BFN-27                                      Sheet 22 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RCIC Pump
BFN-27                                      Sheet 22 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RCIC Pump Criteria                                        Method of Analysis                          Allowable Stress   
 
Criteria                                        Method of Analysis                          Allowable Stress   
: 1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be      contain the internal design pressure    calculated in accordance with the "Rules of the pump casing without exceeding    for Bolted Flange Connections," ASME    20,000 psi      the allowable stress of the bolting    Boiler and Pressure Vessel Code, Section material. Allowable stresses at  VIII, Appendix II.
: 1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be      contain the internal design pressure    calculated in accordance with the "Rules of the pump casing without exceeding    for Bolted Flange Connections," ASME    20,000 psi      the allowable stress of the bolting    Boiler and Pressure Vessel Code, Section material. Allowable stresses at  VIII, Appendix II.
design temperature shall be in accordance with ASME Boiler and  Pump Design Pressure      1500 psig Pressure Vessel Code, Section VIII.   
design temperature shall be in accordance with ASME Boiler and  Pump Design Pressure      1500 psig Pressure Vessel Code, Section VIII.   
: 2. The minimum wall thickness of the 2. Stress in the pump casing shall be    14,000 psi      pump shall limit stress to the allow-    calculated at the point of maximum able stress when subjected to design  internal pump diameter by the formula pressure and temperature. Allowable stresses shall be in accordance with ASME Boiler and Pressure Vessel Code, Section VIII.
: 2. The minimum wall thickness of the 2. Stress in the pump casing shall be    14,000 psi      pump shall limit stress to the allow-    calculated at the point of maximum able stress when subjected to design  internal pump diameter by the formula pressure and temperature. Allowable stresses shall be in accordance with ASME Boiler and Pressure Vessel Code, Section VIII.
S C = 0.8Sa  
S C = 0.8Sa The maximum stress in the pump  Volute stress shall be computed by the    14,000 psi casing when subjected to design    following formula:
 
The maximum stress in the pump  Volute stress shall be computed by the    14,000 psi casing when subjected to design    following formula:
pressure shall not exceed the    allowable working stress of the    Roark p. material. The allowable stress    225 Case No. 36 shall be in accordance with ASME Boiler and Pressure Vessel Code,  Section III.      = factor from Roark      a = volute length    b = volute width  
pressure shall not exceed the    allowable working stress of the    Roark p. material. The allowable stress    225 Case No. 36 shall be in accordance with ASME Boiler and Pressure Vessel Code,  Section III.      = factor from Roark      a = volute length    b = volute width  
()SPDttEc=+.022SPtbb=22 BFN-27                                                                              Sheet 23 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RCIC Pump (Continued)
()SPDt tE c=+.02 2 S P t b b=2 2 BFN-27                                                                              Sheet 23 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RCIC Pump (Continued)
Criteria                              Method of Analysis and Allowable Nozzle Loads         
Criteria                              Method of Analysis and Allowable Nozzle Loads         
: 3. Application of forces and moments by 3. Stresses will not be excessive if the    attaching pipe on pump nozzles under  maximum resultant force when taken with the  combined maximum thermal expansion    maximum resultant moment falls below the line. and Operating Basis Earthquake loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel  Code, Section VIII. Suction          OBE    DBE  
: 3. Application of forces and moments by 3. Stresses will not be excessive if the    attaching pipe on pump nozzles under  maximum resultant force when taken with the  combined maximum thermal expansion    maximum resultant moment falls below the line. and Operating Basis Earthquake loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel  Code, Section VIII. Suction          OBE    DBE  
Line 727: Line 711:
: 1. Application of forces and moments by 1. Stresses will not be excessive if the attaching pipe on pump nozzles under  loads on the pump nozzles do not  combined maximum thermal expansion  exceed the following values: and Operating Basis Earthquake loading reaction plus load due to Condition          F(Axial)        F(Vertical)      F(Lateral)        M(Torsion)        M(Vertical)        M(Laterial)  internal pressure shall not produce Normal              6,211 lb        6,888 lb          3,882 lb          5,552 ft-lb        17,499 ft-lb      10,419 ft-lb an equivalent bending and torsional Upset                9,110 lb        8,970 lb          5,103lb            8,790 ft-lb        19,218 ft-lb        13,006 ft-lb stress in the nozzles in excess  of Emergency      12,010 lb      11,052 lb          6,984 lb          12,047 ft-lb        30,527 ft-lb        15,593 ft-lb the allowable stress as defined b BFN-50-C-7106 Table 3.1-1 for  Active Pumps.   
: 1. Application of forces and moments by 1. Stresses will not be excessive if the attaching pipe on pump nozzles under  loads on the pump nozzles do not  combined maximum thermal expansion  exceed the following values: and Operating Basis Earthquake loading reaction plus load due to Condition          F(Axial)        F(Vertical)      F(Lateral)        M(Torsion)        M(Vertical)        M(Laterial)  internal pressure shall not produce Normal              6,211 lb        6,888 lb          3,882 lb          5,552 ft-lb        17,499 ft-lb      10,419 ft-lb an equivalent bending and torsional Upset                9,110 lb        8,970 lb          5,103lb            8,790 ft-lb        19,218 ft-lb        13,006 ft-lb stress in the nozzles in excess  of Emergency      12,010 lb      11,052 lb          6,984 lb          12,047 ft-lb        30,527 ft-lb        15,593 ft-lb the allowable stress as defined b BFN-50-C-7106 Table 3.1-1 for  Active Pumps.   


BFN-27              Sheet 26A Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RHR Service Water Pumps A1, B1, D1, D2, D3 Criteria Method of Analysis and Allowable Nozzle Loads  
BFN-27              Sheet 26A Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RHR Service Water Pumps A1, B1, D1, D2, D3 Criteria   Method of Analysis and Allowable Nozzle Loads  
: 1. Application of forces and moments by attaching pipe on pump nozzles under combined maximum thermal expansion and Operating Basis Earthquake loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel Code, Section VIII.
: 1. Application of forces and moments by attaching pipe on pump nozzles under combined maximum thermal expansion and Operating Basis Earthquake loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel Code, Section VIII.
For Design Basis Earthquake stress shall be less than 1.5 of allowable stress..  
For Design Basis Earthquake stress shall be less than 1.5 of allowable stress..  
Line 793: Line 777:
Loads: Total bolting loads and stresses  4 in. (Discharge Bypass Valve) shall be calculated in accordance Design pressure and temperature with "Rules for Bolted Flange Con-  Sallow = 29,000 lb/in.
Loads: Total bolting loads and stresses  4 in. (Discharge Bypass Valve) shall be calculated in accordance Design pressure and temperature with "Rules for Bolted Flange Con-  Sallow = 29,000 lb/in.
2  Gasket load nections," ASME Boiler and Pressure  Stem operational load Vessel Code, Section VIII, Appendix Design Basis II, except that the stem operation-Earthquake al load and seismic loads shall be included in the total load carried by bolts. The horizontal and    vertical seismic forces shall be  applied at the mass center of the valve operator assuming that the valve body is rigid and anchored.  
2  Gasket load nections," ASME Boiler and Pressure  Stem operational load Vessel Code, Section VIII, Appendix Design Basis II, except that the stem operation-Earthquake al load and seismic loads shall be included in the total load carried by bolts. The horizontal and    vertical seismic forces shall be  applied at the mass center of the valve operator assuming that the valve body is rigid and anchored.  
()tPSPyd=+1522101..
()t PSPy d=+15221 01..
BFN-27                            Sheet 34 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Valves - Units 1 and 2 (Continued)  
BFN-27                            Sheet 34 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Valves - Units 1 and 2 (Continued)  


Line 823: Line 807:


Vessel Code, Section VIII, Appendix II, 1968 Edition.  
Vessel Code, Section VIII, Appendix II, 1968 Edition.  
()t1.5Pd2S2P1y0.1
()t1.5Pd2S2P1y0.1=+
=+
BFN-27                      Sheet 37 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Valves - Unit 3 (Continued)
BFN-27                      Sheet 37 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Valves - Unit 3 (Continued)
Criteria        Method of Analysis Allowable Stress   
Criteria        Method of Analysis Allowable Stress   
Line 832: Line 815:
2 (Tangential Stress)    Boiler and Pressure Vessel Code,  Design pressure and temperature Section VIII, Appendix II, except Gasket load that the stem operational load and  Stem operational load seismic loads shall be included in  Seismic Loads - the total load carried by the flange.
2 (Tangential Stress)    Boiler and Pressure Vessel Code,  Design pressure and temperature Section VIII, Appendix II, except Gasket load that the stem operational load and  Stem operational load seismic loads shall be included in  Seismic Loads - the total load carried by the flange.
Design Basis The horizontal and vertical seismic Earthquake forces shall be applied at the mass center of the valve operator as- Flange Stress Limits; suming that the valve body is rigid.
Design Basis The horizontal and vertical seismic Earthquake forces shall be applied at the mass center of the valve operator as- Flange Stress Limits; suming that the valve body is rigid.
SH,SR,ST: Sm per ASME Boiler and Pres- sure Vessel Code, Section VIII, Appendix II, 1968 Edition.  
S H ,S R ,S T: S m per ASME Boiler and Pres- sure Vessel Code, Section VIII, Appendix II, 1968 Edition.  
: 4. Valve Operator Support Bolts The valve assembly is analyzed assum- S b allowable = 20,000 lb/in.
: 4. Valve Operator Support Bolts The valve assembly is analyzed assum- S b allowable = 20,000 lb/in.
2 ing that the valve body is an anchored, Loads: rigid mass and that the specified vertical and horizontal seismic forces Design pressure and temperature are applied at the mass center of the Stem operational load operator assembly, simultaneously with Equipment dead weight operating pressure plus dead weight  Seismic load -  plus operational loads. Using these Design Basis loads, stresses and deflections are Earthquake determined for the operator support components. Yoke and Yoke Bolt Stress Limits:
2 ing that the valve body is an anchored, Loads: rigid mass and that the specified vertical and horizontal seismic forces Design pressure and temperature are applied at the mass center of the Stem operational load operator assembly, simultaneously with Equipment dead weight operating pressure plus dead weight  Seismic load -  plus operational loads. Using these Design Basis loads, stresses and deflections are Earthquake determined for the operator support components. Yoke and Yoke Bolt Stress Limits:
Allowable working stress per ASME Section VIII.
Allowable working stress per ASME Section VIII.
BFN-27    Sheet 1 of 1 TABLE C.5-1 DRYWELL-LOADING CONDITIONS AND ALLOWABLE STRESSES Loading          Allowable Stress Intensity (ksi) Condition    Loading Components          (Notes 1 and 2)
BFN-27    Sheet 1 of 1 TABLE C.5-1 DRYWELL-LOADING CONDITIONS AND ALLOWABLE STRESSES Loading          Allowable Stress Intensity (ksi) Condition    Loading Components          (Notes 1 and 2)
Initial and Final    Dead Loads    P m < Sm = 17.5 Test Condition    Test Pressure    P L < 1.5 Sm = 26.3 Vent Thrusts    P L + Pb < 1.5 Sm = 26.3 OBE    P L + Pb + Q < 3.0 S m = 52.5  Normal and Upset Dead Loads P m < Sm = 17.5 Operating Condition Vent Thrusts P L < 1.5 Sm = 26.3 OBE PL + Pb < 1.5 Sm = 26.3 Accident Temperature P L + Pb + Q < 3.0 S m = 52.5 Accident Pressure Emergency Condition Dead Loads Region not Backed by Concrete (Note 3)          Accident Pressure P m < 0.9 Sy = 30.3 Accident Temperature P L < 0.9 Sy = 30.3 Vent Thrusts          OBE          Region Backed by Concrete Jet Loads P m < Sy = 33.7            P L < 1.5Sy = 50.6  Flooded Condition Dead Loads P m < Sy = 38.0 Hydrostatic Pressure  P L < Sy = 38.0 From Flooded DryWell P L + Pb < Su = 70.0 DBE PL + Pb + Q < Su = 70.0 NOTE:  1. Stress intensities are based on ASME Boiler and Pressure Vessel Code, Se ction III, Subsection B of Reference 17.  
Initial and Final    Dead Loads    P m < S m = 17.5 Test Condition    Test Pressure    P L < 1.5 S m = 26.3 Vent Thrusts    P L + P b < 1.5 S m = 26.3 OBE    P L + P b + Q < 3.0 S m = 52.5  Normal and Upset Dead Loads P m < S m = 17.5 Operating Condition Vent Thrusts P L < 1.5 S m = 26.3 OBE P L + P b < 1.5 S m = 26.3 Accident Temperature P L + P b + Q < 3.0 S m = 52.5 Accident Pressure Emergency Condition Dead Loads Region not Backed by Concrete (Note 3)          Accident Pressure P m < 0.9 S y = 30.3 Accident Temperature P L < 0.9 S y = 30.3 Vent Thrusts          OBE          Region Backed by Concrete Jet Loads P m < S y = 33.7            P L < 1.5S y = 50.6  Flooded Condition Dead Loads P m < S y = 38.0 Hydrostatic Pressure  P L < S y = 38.0 From Flooded DryWell P L + P b < S u = 70.0 DBE P L + P b + Q < S u = 70.0 NOTE:  1. Stress intensities are based on ASME Boiler and Pressure Vessel Code, Se ction III, Subsection B of Reference 17.  
: 2. Definition of symbols are as follows:    Pm = Primary membrane stress,    PL = Primary local membrane stress,    Pb = Primary bending stress, Q = secondary stress.  
: 2. Definition of symbols are as follows:    P m = Primary membrane stress,    P L = Primary local membrane stress,    P b = Primary bending stress, Q = secondary stress.  
: 3. The 1965 ASME Code does not address accident conditions. Therefore, this design criteria utilizes the 1968 ASME Code with addenda through the summer of 1969 to establish design allowables for the accident condition for that portion of the vessel backed by concrete.}}
: 3. The 1965 ASME Code does not address accident conditions. Therefore, this design criteria utilizes the 1968 ASME Code with addenda through the summer of 1969 to establish design allowables for the accident condition for that portion of the vessel backed by concrete.}}

Revision as of 04:06, 6 July 2018

Browns Ferry Nuclear Plant Updated Final Safety Analysis Report (Ufsar), Amendment 27, Appendix C Table - Structural Qualification
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Text

BFN-27 Table C.2-1 DEFORMATION LIMIT

Either One of (Not Both) General Limit

a. Permissible Deformation,DPAnalyzedDeformationCausing Loss of Function, DL

09.min SF b. Permissible Deformation, DP Experimental DeformationCausing Loss of Function, DE

1.0 SFmin where DP = permissible deformation under st ated conditions of normal, upset, emergency, or faulted DL = analyzed deformation which woul d cause a system loss of function (1) DE = experimentally determined formation which would cause a system loss of function (1)

(1) "Loss of Function" can only be defined quite generally until attention is focused on the component of interes

t. In cases of interest, where deformation limits can affect the f unction of equipment and components, they will be specifically delineated. From a practical viewpoint, it is convenient to interchange some deformation condition at which function is assured with the loss of function condi tion if the require d safety margins from the functioning condition can be achieved. Therefore, it is often unnecessary to determine the actual loss of function condition because this interchange procedure produces conservative and safe designs. Examples where deformation limits apply are: control rod drive alignment and clearances for proper insertion, core support deformation causing fuel disarrangement, or excess leakage of any component.

BFN-27 Sheet 1 Table C.2-2 PRIMARY STRESS LIMIT

Any One of (No More than One Required) General Limit

a. Elastic Evaluated Primary Stresses,PEPermissible Primary Stresses, PN 2.25min SF b. Permissible Load,LP Largest Lower Bound Limit Load, CL 1.5 SFmin c. Elastic Evaluated Primary Stress, PEConventional ultimate strengthat Temperature, US 075.min SF d. ElasticPlastic EvaluatedNominal Primary Stress, PEConventional ultimate strengthat Temperature, US

09.min SF e. Permissible Load, LP Plastic Instability Load, PL 09.min SF f. Permissible Load, LP

Ultimate Load From Fracture Analysis, UF 09.min SF g. Permissible Load, LP Ultimate Load or Loss of FunctionLoad from Test, LE

1.0 SFmin BFN-27 Sheet 2 Table C.2-2 (continued) PRIMARY STRESS LIMIT

where

PE = Primary stresses evaluated on an elasti c basis. The effective membrane stresses are to be averaged through t he load carrying section of interest.

The simplest average bending, shear or torsion stress distribution which will support the external loading will be added to membrane stresses at the section of interest.

PN = Permissible primary stress levels under normal or ups et conditions under applicable industry code.

LP = Permissible load under stated c onditions of emergency or faulted.

CL = Lower bound limit load wi th yield point equal to 1.5 S m , where S m is the tabulated value of allowable stre ss at temperature of the ASME III code or its equivalent. The "lower bound limit load" is here defined as that produced from the analysis of an ideal ly plastic (nonstrain harde ning) material where deformations increase with no further increase in applied load. The lower bound load is one in which the material everywhere satisfies equilibrium and nowhere exceeds the defined material yield strength using either a shear theory or a strain energy of distortion theory to r elate multiaxial yielding to the uniaxial case.

US = Conventional ultimate strength at temper ature or loading that would cause a system malfunction, whichever is more limiting.

EP = Elastic-plastic evaluated nominal pr imary stress. St rain hardening of the material may be used for the actual m onotonic stress str ain curve at the temperature of loading or any approximation to the actual stress strain curve which everywhere has a lower stress fo r the same strain as the actual monotonic curve may be used. Either t he shear or strain energy of distortion flow rule may be used.

PL = Plastic instability load. The "plastic instability load" is defined here as the load at which any load bearing section begins to diminish its cross-sectional area at a faster rate than the strain hardening c an accommodate the loss in area. This type analysis requires a true stress-true strain curve or a close approximation based on monot onic loading at the tem perature of loading.

BFN-27 Sheet 3 Table C.2-2 (continued) PRIMARY STRESS LIMIT

UF = Ultimate load from fracture analyses. For components that involve sharp discontinuities (loc al theoretical stress conc entration > 3) the use of a "fracture mechanics" anal ysis where applica ble, utilizing measurements of plain strain fracture toughness may be applied to compute fracture loads. Corre ction for finite plastic zones and thickness effects as well as gr oss yielding may be necessary. The methods of linear elastic stress analysis may be used in the fracture analysis where its use is clearly conservative or supported by experimental evidence. Examples where "fracture mechanics" may be applied are for fillet welds or end of fatigue life crack propagation.

LE = Ultimate load or loss of func tion load as determined from experiment.

In using this method account s hall be taken of the dimensional tolerances which may exist between the actual part and the tested part or parts as well as differences which may exist in the ultimate tensile strength of the actual part and the tested parts. The guide to be used in each of these areas is that the experimentally determined load shall use adjusted values to account fo r material properties and dimension variations, each of which has no gr eater probability than 0.1 of being exceeded in the actual part.

BFN-27 Table C.2-3 BUCKLING STABILITY LIMIT

Any One of (no more than one required) General Limit

a. Permissible Load, LP Code Normal Event PermissibleLoad, PN

2.25 min SF b. Permissible Load, LP Stability Analysis Load, SL 09.min SF c. Permissible Load, LP Ultimate Buckling Collapse Loadfrom Test, SE 1.0 SFmin where:

LP = Permissible load under stated c onditions of emergency or faulted.

PN = Applicable code norm al event permissible load.

SL = Stability analysis load. The ideal buckling analysis is often sensitive to otherwise minor deviations from ideal geometry and boundary conditions. These effects shall be accounted for in the analysis of the buckling stability loads.

Examples of this are ovality in externally pressurized shells or eccent ricity of column members.

SE = Ultimate buckling collapse load as determined from ex periment. In using this method, account s hall be taken of the dimensional tolerances which may exist betw een the actual part and the tested part. The guide to be used in each of these areas is that the experimentally determined load shall be adjusted to account for material property and dimension va riations, each of which has no greater probability t han 0.1 of being exceeded in the actual part.

BFN-27 Table C.2-4 FATIGUE LIMIT General Limit Summation of mean fatigue(1) a. Fatigue cycle usage usage including emergency or from analysis 0.05 faulted events with design and operation loads following b. Fatigue cycle usage Miner hypotheses.... from test 0.33 either one (not both)

(1) Fatigue failure is defined here as a 25% area reduction for a load carrying member which is required to function or excess leakage causing loss of function, whichever is more limiting. In the fatigue evaluation, the methods of linear elastic stress analysis may be used when the 3S m range limit of ASME Code, Se ction III has been met. If 3S m is not met, account will be tak en of (a) increases in local strain concentration, (b) strain ratcheting, and (c) redistribution of strain due to elastic-plastic effects. The January 1969 draft of the USAS B31.7 Piping Code may be used where applicable, or detailed elastic-plastic methods may be used. With elas tic-plastic methods, strain hardening may be used not to exceed in stress for the same strain the steady-state cyclic strain hardening meas ured in a smooth low cycle fatigue specimen at the average te mperature of interest.

BFN-27

Sheet 1 of 8 TABLE C.3-1A LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA FOR CLASS I PIPING AND TUBING (PIPING OTHER THAN RRS, MS, FW AND CRDH SYSTEMS) 9 Plant Conditions Moment Constituents 2 NC-3652 1 Concurrent Loads From Load Sources Equations and Stress Limits Eq. No.

Design and Normal Design Pressure + Sustained M A = M(DW)10 (8)

Upset Max (Peak) Pressure + M BU = M(E1,VT,WH) 3,6 Sustained + OBE + Fluid (9U)

Transient Emergency

Max (Peak) Pressure + M BE = M(E2,VT,WH,JI) 5,6,8,11 Sustained + Fluid Transient (9E) + (DBE or Jet Impingement)

PD DD iM Z S i oi A h 2 22075. ()PD DDiMM Z S mi oiABU h 2 22075 12++.. ()PD DDiMM Z S mi oiABE h 2 22075 18++..

BFN-27

Sheet 2 of 8 TABLE C.3-1A LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA FOR CLASS I PIPING AND TUBING (PIPING OTHER THAN RRS, MS, FW AND CRDH SYSTEMS) 9 Plant Conditions Moment Constituents 2 NC-3652 1 Concurrent Loads From Load Sources Equations and Stress Limits Eq. No.

Faulted (Max (Peak) Pressure + M BF = M(E2,VT,WH,JI) 6,8 (9F) Sustained + DBE + Fluid Transient + Jet Impingement)

Normal and Upset (Secondary)

Thermal Expansion + M C = M(T i ,SD,S1)3,4,7 (10) Thermal Anchor Movement +

Seismic Anchor Movement OR Design Pressure + Sustained + (11)

Thermal Expansion + Thermal Anchor Movement + Seismic Anchor Movement Differential Settlement

Differential Settlement M D = M(BS)

()PD DDiMM Z S mi oiABF h 2 22075 2++..4 iM Z S c A PD DD iM Z iM Z SS i oi AC Ah 2 22075+++. iM Z S D C3 BFN-27

Sheet 3 of 8 TABLE C.3-1B LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA OF CLASS I PIPING FOR REACTOR RECIRCULATION (RRS) MAIN STEAM (MS) AND FEEDWATER (FW) SYSTEMS 9 Plant Conditions Moment Constituents 2 NC-3652 1 Concurrent Loads From Load Sources Equations and Stress Limits Eq. No.

Design and Normal (Primary)

Design Pressure + M A = M(DW)10 (8) Sustained

Upset (Primary)

Design Pressure + M BU = M(E1,VT,WH) 3,6 (9U) Sustained + Occasional

Normal (Primary + Secondary)

Design Pressure + M' C = M(Ti,SD) (11) Sustained + Thermal Expansion + Thermal Anchor Movement

PD DD iM Z S i oi A h 2 22075. ()PD DDiMM Z S i oiABU h 2 22075 12++.. PD DDiMiM Z SS i oi AC Ah 2 22075++.'

BFN-27 Sheet 4 of 8 TABLE C.3-1B LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA OF CLASS I PIPING FOR REACTOR RECIRCULATION (RRS) MAIN STEAM (MS) AND FEEDWATER (FW) SYSTEMS 9 Plant Conditions Moment Constituents 2 NC-3652 1 Concurrent Loads From Load Sources Equations and Stress Limits Eq. No.

Upset (Primary + Secondary)

Design Pressure + M C = M(Ti,SD,S1) 3,4,7 (9U+10) Sustained + Thermal Expansion & Thermal Anchor Movement + OBE + SAM Emergency (Primary)

Design Pressure + M BE = M(E2,VT,WH,JI)5,6,8,11 (9E) Sustained + Fluid Transient + (DBE or Jet Impingement) Max. (Peak) Pressure + M BE' = M(E1,VT,WH) 6, 8 (9E)' Sustained + OBE + Fluid Transient Max. (Peak) Pressure + Sustained + Fluid Transient (9E)" + (DBE or Jet Impingement)

Faulted Primary Max (Peak) Pressure + M BF = M(VT,E2,WH,JI) 6,8 (9F) Sustained + Fluid Transient + DBE + Jet Impingement

()()PD DDiMMiM Z SS i oiABUC hA 2 22075 12+++..()PD DDiMM Z S i oiABE h 2 22075 18++..()PD DDiMM Z S mi oiABE h 2 22075 15++.'.()PD DDiMM Z S mi oiABE h 2 22075 20++..()PD DDiMM Z S mi oiABF h 2 22075 2++..4 BFN-27

Sheet 5 of 8 TABLE C.3-1C LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA FOR CONTROL ROD DRIVE HYDRAULIC PIPING Plant Conditions Moment Constituents 2 NC-3652 1 Concurrent Loads From Load Sources Equations and Stress Limits Eq. No.

Design and Normal (Primary)

Design Pressure + M A = M(DW)10 Sustained (8)

Upset (Primary)

Max Operating Pressure + M BU = M(E1,VT,WH) 3,6 (9U) Sustained + Occasional (9U)

Upset (Primary + Secondary)

Max Operating Pressure + M C1 = M(Ti,SD,S1) 3,7 OR Sustained + Normal Scram (10)

Thermal Expansion and Anchor Movement + SAM (OBE)

(11)

PD DD iM Z S i oi A h 2 22075.()P D DD0.75i MM Z 1.2S ni 2 o 2 i 2ABU h++iM Z S c A 1PD DDiMiM Z SS ni oi AC Ah 2 22 1075++.

BFN-27

Sheet 6 of 8 TABLE C.3-1C LOAD COMBINATIONS AND ALLOWABLE STRESS CRITERIA FOR CONTROL ROD DRIVE HYDRAULIC PIPING Plant Conditions Moment Constituents 2 NC-3652 1 Concurrent Loads From Load Sources Equations and Stress Limits Eq. No.

Max Operating Pressure + M C2 = M(Ti,SD) 7 Sustained + Abnormal Scram OR (10) Thermal Expansion and Anchor

Movement (11)

Emergency (Primary)

Max Operating Pressure +

M DE = M(E2,VT,WH,JI) 6,8,11 Sustained + Fluid Transient (9E)

+ (SSE or Jet Impingement) 5 Faulted (Primary)

Max Operating Pressure +

M DF = M(E2,VT,WH,JI) 6,8 Sustained + Fluid Transient (9F) + SSE + Jet Impingement iM Z S C A 2 PD DDiMiM Z SS ni oi AC Ah 2 22 2075++.()PD DDiMM Z S ni oiADE h 2 22075 18++..()PD DDiMM Z S ni oiADF h 2 22075 2++..4 BFN-27 Sheet 7 of 8 TABLE C.3-1A, 1B, 1C (Cont'd)

Nomenclature P = Design Pressure, psi.

P m = Max (Peak) Pressure, psi.

P n = Maximum operational or scram pressure for the Hydraulic System Pump Pressure for CRDH System only.

D o = Outside Pipe Diameter, in.

D i = Nominal Inside Pipe Diameter, in.

i = Stress Intensification Factor from B31.1.0 - 1967.

S h = Basic material allowable stress at maximum operating temperature.

S c = Basic Material Allowable Stress at Ambient Temperature.

S A = Allowable expansion stress defined in B31.1.0 - 1967.

U,E,F = Added Suffixes for differentiation between Upset, Emergency, and Faulted.

Z = Pipe section modulus (in 3).

DW = Deadweight.

E1 = Operating Basis Earthquake (OBE) Inertia Effect.

E2 = Design Basis Earthquake (DBE) Inertia Effect.

WH = Steam/Water Hammer.

Ti = Thermal mode i (i = mode number).

SD = Thermal Anchor Movements.

S1 = OBE Seismic Anchor Movements.

BS = Differential movement between the soil and building structure for buried piping or relative differential building settlement for piping attached to two buildings.

VT = Valve Thrust (Main Steam Relief Valve Actuation).

JI = Jet Impingement.

BFN-27 Sheet 8 of 8 TABLE C.3-1A, 1B, 1C (Cont'd)

Notes 1. ASME Boiler and Pressure Vessel Code,Section III, Division 1, 1971 edition, through Summer 1973 Addenda and Code Case 1606-1. Material allowables and SIFs from USAS B31.1.0 -

1967 2. The sequence of events, consistent with the system operational requirements, is considered in establishing which load sources are taken as acting concurrently.

3. Seismic anchor movements are included in the evaluation of either equation (9) or equation (10), but need not be included in both.
4. All secondary load sources resulting from plant normal or upset conditions are identified and evaluated for the limiting operating modes of the system. The effects of these load sources are used in evaluating equipment loading, support loading, and type.
5. The largest loads from either DBE or Je t Impingement are used. Jet impingement loading requirements for piping inside and outside of containment are described in Appendix M.
6. If more than one dynamic load source is involved, such as earthquake, valve thrust, and water hammer, the SRSS method will be used to combine resultant moments from individual load sources. In the event that the dynamic load sources are determined to act nonconcurrently, then they can be considered independently.
7. For M c, the effects of Ti and corresponding SD are combined algebraically first, and then combined absolutely with S1.
8. Only inertia term of earthquake effect to be considered.
9. Exceptions from the requirements in Table C.3-1A, -1B, and -1C may be allowed with proper justification and NRC concurrence.
10. Additional stresses caused by hydrostatic testing weight are evaluated when applicable.
11. Fire events are evaluated as separate emergency loading conditions. No dynamic loads are postulated to occur simultaneously with these events. Piping is evaluated for pressure plus deadweight effects of the events.

BFN-27 TABLE C.3-2 Sheet 1 of 5 LOAD COMBINATIONS AND ALLOWABLE STRESSES FOR CLASS I PIPE AND TUBING SUPPORTS Support Category Load Condition Direction Design Load Combinations 1,2,9 Allowable 3 Stresses Linear Type Support Normal + - DW + Ti+ DW + Ti- 1.0S AISC Hydrotest DW 1.0S AISC Upset + DW + Ti

+ + SRSS[VT+, WH+, E1, S1] 1.33S AISC 4 - DW + Ti

- - SRSS [VT

-, WH-, -E1, -S1]

Emergency + DW + Ti

+ + SRSS [VT

+, WH+, E2, S2] 1.5S AISC 4 or DW + Ti

+ + SRSS [VT

+, WH+] + PR+ or DW + Ti

+ (fire event)

- DW + Ti

- - SRSS [VT

-, WH-, -E2, -S2]

or DW + Ti

- - SRSS [VT

-, WH-] + PR- or DW + Ti

- (fire event)

Faulted + DW + Ti

+ + SRSS [VT

+, WH+, E2, S2] + PR

+ 1.5S AISC 4 - DW + Ti

- - SRSS [VT

-, WH-, -E2, -S2] +PR

-

BFN-27 TABLE C.3-2 (CONTINUED)

Sheet 2 of 5 Support Category Load Condition Direction Design Load Combinations 1,2,9 Allowable 3 Stresses Snubbers Hydraulic Upset +/- Same as Linear VLR Emergency

+/- Same as Linear 1.2 VLR Faulted +/- Same as Linear 1.2 VLR Mechanical Pre-NF Upset

+/- Same as Linear VLR Emergency

+/- Same as Linear The lesser of 1.33 VLR or LCD Level 'C' Faulted +/- Same as Linear The lesser of 1.33 VLR or LCD Level 'C' Post-NF Upset

+/- Same as Linear LCD Level 'B' Emergency

+/- Same as Linear LCD Level 'C' Faulted +/- Same as Linear LCD Level 'C' BFN-27 TABLE C.3-2 (CONTINUED)

Sheet 3 of 5 Support Category Load Condition Direction Design Load Combinations 1,2,9 Allowable Stresses 3,5,6 Standard Support Components Normal +/- Same as Linear S 58 Hydrotest Same as Linear 2.0S 58 8 Upset +/- Same as Linear 1.2S 58 Emergency

+/- Same as Linear (See Note 7) Faulted +/- Same as Linear (See Note 7)

BFN-27 TABLE C.3-2 (CONTINUED)

Sheet 4 of 5 Notes: 1. Signs for Load Evaluation DW - Carries the actual analysis signs. Ti - Thermal load shall be evaluated for both hot and cold conditions. 2. Design value for (+) direction is the larger of zero and the value calculated; (-) direction is the smaller of zero and the value calculated. 3. S AISC = The basic allowable stresses defined in Part I of the AISC Specification for the Design, Fabrication, and Erection of Structural Steel for Buildings, November 1978. (Excluding the 1.33 factor).

S 58 = The basic allowable load as defined by the vendor in accordance with MSS SP-58, 1967 edition, Pipe Hangers and Supports.

F y = The minimum yield stress of support member at elevated sustained temperature (i.e., normal operating temperature exceeds 150

°F). VLR = The basic load rating supplied by the vendor. LCD = Load capacity data sheet as levels supplied by the vendor.

4. Linear Allowables shall not exceed 0.9F y for tension or 0.9F y/3 = 0.52F y for shear. 5. Load rated allowables established according to ASME section III subsection NF are acceptable using the appropriate load level. 6. Linear support allowables may be used for detailed analysis of standard support components.

BFN-27 TABLE C.3-2 (CONTINUED)

Sheet 5 of 5 Notes: 7. Allowable stress shall not exceed the lesser of 2.05 58 or the linear support allowance. However, the lesser shall not exceed available LCD Level 'D' limits. 8. Maximum allowable stress for hydrotest condition shall not exceed 0.8F

y. 9. SRSS combinations shall be consistent with the provisions of Section C.3.1.2.

BFN-27 Sheet 1 Table C.4-1 REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES

Criteria Loading Primary Stress Type Allowable Stress (psi)

Stabilizer Bracket and Adjacent Shell Primary Stress Limit - ASME Boiler Normal and upset condition loads Membrane and bending 40,000 and Pressure Vessel Code, Sect. III 1. Operating Basis Earthquake defines primary membrane plus 2. Design pressure primary bending stress intensity limit for SA 302 - Gr. B Emergency condition loads Membrane and bending 60,000

1. Design Basis Earthquake For normal and upset condition 2. Design pressure Stress limit = 1.5 X 26,700 = 40,000 psi Faulted condition loads Membrane and bending 80,000 For emergency condition 1. Design Basis Earthquake Stress limit = 1.5 X 40,000 = 60,000 psi 2. Jet reaction forces
3. Design pressure For faulted condition Stress limit = 2.0 X 40,000 = 80,000 psi

Vessel Support Skirt

Primary Stress Limit - ASME Boiler Normal and upset condition loads General membrane 26,700 and Pressure Vessel Code, Sect. III 1. Dead weight defines stress limit for SA 302 2. Operating Basis Earthquake Gr. B Emergency condition loads General membrane 40,000 For normal and upset condition 1. Dead weight

S M = 26,700 psi 2. Design Basis Earthquake

For emergency condition Faulted condition loads General membrane 53,400 Slimit = 1.5 S M = 1.5 X 26,700 = 1. Dead weight 40,000 psi 2. Design Basis Earthquake

3. Jet reaction forces For faulted condition

Slimit = 2.0 S M = 20 X 26,700 = 53,400 psi

BFN-27 Sheet 2 Table C.4-1 (Continued)

REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Criteria Loading Primary Stress Type Allowable Stress (psi)

Shroud leg Support Primary Stress Limit - ASME Boiler Normal and upset condition loads Tensile 23,300 and Pressure Vessel Code, Sect. III 1. Operating Basis Earthquake defines allowable primary membrane 2. Pressure drop across shroud stress SB-168 material. (normal)

3. Subtract dead weight
1. Tensile Loads For normal and upset condition Emergency condition loads Tensile 35,000 S M = 23,300 psi 1. Design Basis Earthquake 2. Pressure drop across shroud For emergency condition (normal)

Slimit = 1.5 S M 3. Subtract dead weight = 1.5 X 23,300 = 35,000 psi Faulted condition loads Tensile 46,600 For faulted condition 1. Design Basis Earthquake

Slimit = 2.0 S M 2. Pressure drop across shroud = 2.0 X 23,300 = 46,600 psi during faulted condition

3. Subtract dead weight
2. Compressive Loads For normal and upset condition Normal and upset condition loads Compressive 14,000 S A = 0.4 S y 1. Operating Basis Earthquake = 0.4 X 35,000 = 14,000 psi 2. Zero pressure drop across shroud For emergency condition 3. Dead weight

Slimit = 0.6 S y = 0.6 X 35,000 = 21,000 psi Emergency condition loads Compressive 21,000 1. Design Basis Earthquake For faulted condition 2. Subtract operating pressure

Slimit = 0.8 S y drop across shroud = 0.8 X 35,000 = 28,000 psi 3. Dead weight

Faulted condition loads Compressive 28,000 1. Design Basis Earthquake

2. Zero pressure drop across shroud
3. Dead weight BFN-27 Sheet 3 Table C.4-1 (Continued)

REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Criteria Loading Primary Stress Type Allowable Stress (psi)

Top Guide Longest Beam

Primary Stress Limit - The allowable Normal and upset condition loads* General membrane plus 25,388 primary membrane stress plus bending 1. Operating Basis Earthquake bending stress is based on ASME Boiler and 2. Weight of structure Pressure Vessel Code, Sect. III for Type 304 stainless steel plate.

For normal and upset condition Emergency condition loads* General membrane plus 38,081 Stress Intensity 1. Design Basis Earthquake bending

S A = 1.5 S m = 1.5 X 16.925 = 25,388 psi 2. Weight of structure

For emergency condition

Slimit = 1.5 S A = 1.5 X 25,388 = 38,081 psi Faulted condition loads* General membrane plus 50,775 (Same as emergency condition) bending For faulted condition

Slimit = 2S A = 2 X 25,388 = 50,775 psi

Top Guide Beam End Connections Primary Stress Limit - ASME Boiler Normal and upset condition loads* Pure shear 10,155 and Pressure Vessel Code, Sect. III 1. Operating Basis Earthquake defines material stress limit for 2. Weight of structure Type 304 stainless steel

For normal and upset condition Stress Intensity Emergency condition loads* Pure shear 15,232 S A = 06 S m = 0.6 X 16,925 = 10,155 psi 1. Design Basis Earthquake 2. Weight of structure For emergency condition

Slimit = 1.5 S A = 1.5 X 10,155 = 15,232 psi Faulted condition loads* Pure shear 20,310 (Same as emergency condition) For faulted condition

Slimit = 2S A = 2 X 10,155 = 20,310 psi

  • Note: Normal, upset, and accident top guide hydraulic loads are upward. These are not included in the stress analysis since they counteract the effect of the structure weight.

BFN-27 Sheet 4 Table C.4-1 (Continued)

REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Criteria Loading Primary Stress Type Allowable Stress (psi)

Core support (pre-uprate)

Primary Stress Limit - The allowable Normal and Upset condition loads General membrane plus 25,388 primary membrane stress plus bending 1. Normal operation pressure drop bending stress is based on ASME Boiler and 2. Operating Basis Earthquake

Pressure Vessel code, Sect. III for Type 304 stainless steel plate Emergency condition loads General membrane plus 38,081 1. Normal operation pressure drop bending For allowable stress see top guide 2. Design Basis Earthquake longest beam above Faulted condition loads General membrane plus 50,275 1. Pressure drop after recircu- bending lation line rupture

2. Design Basis Earthquake Core support (uprate)* Allowable pressure For power uprate the allowable differential differential (psid) loading is based on the ratio of applied pressure to buckling pressure.

For normal and upset: Normal and Upset condition loads Buckling 28.0 allowable ratio = 0.40 1. Normal operation pressure drop 2. Operating Basis Earthquake

For emergency: Emergency condition loads Buckling 42.0 allowable ratio = 0.60 1. Normal operation pressure drop

2. Design Basis Earthquake

For faulted: Faulted condition loads Buckling 56.0 allowable ratio = 0.80 1. Pressure drop after main steam line rupture.

2. Design Basis Earthquake Allowable Stress (psi)

Core Support Aligners

Primary Stress Limit - ASME Boiler Normal and upset condition load Pure shear 10,155 and Pressure Vessel Code, Sect. III 1. Operating Basis Earthquake defines material stress limit for Type 304 stainless steel Emergency condition load Pure shear 15,232 1. Design Basis Earthquake For allowable shear stresses, see top guide beam end connections Faulted condition load Pure shear 20,310 above 1. Design Basis Earthquake

  • The component did not change as a result of increasing power but represents the parameters that were reevaluated as part of the power uprate analysis.

BFN-27 Sheet 5 Table C.4-1 (Continued)

REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Moment Limit Accounting Criteria Loading Primary Stress Type for Pressure Loads (in-lb)

Fuel Channels

Primary Stress Limit - The allowable Normal and Upset condition loads Membrane and bending 28,230 S m for Zircaloy determined according 1. Operating Basis Earthquake to methods recommended by ASME 2. Normal pressure load Boiler and Pressure Vessel Code, Sect. III. Allowable moment Emergency condition loads Membrane and bending 42,350 determined by calculating limit 1. Design Basis Earthquake moment using Table C.2-2 2. Normal pressure load equation (b), then applying SFmin for applicable loading conditions. Faulted condition loads Membrane and bending 56,500 1. Design Basis Earthquake 2. Loss-of-coolant accident (S m = 9,270 psi, 1.5 S m = 13,900 psi) pressure

Emergency limit load = 1.5 X Normal limit load calculated using 1.5 S m = yield BFN-27 Sheet 6 Table C.4-1 (Continued)

REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES

Criteria Loading Location Allowable Stress (psi)

RPV Stabilizer

Primary Stress Limit - AISC specification Upset condition Rod 130,000 for the construction, fabrication 1. Spring preload Bracket 22,000 and erection of structural steel for 2. Operating Basis Earthquake 14,000 buildings Emergency condition Bracket 33,000 For normal and upset conditions 1. Spring preload 21,000 AISC allowable stresses, but without 2. Design Basis Earthquake the usual increase for earthquake loads Faulted condition Bracket 36,000 For emergency conditions 1. Spring preload 21,500 1.5 X AISC allowable stresses 2. Design Basis Earthquake 3. Jet reaction load For faulted conditions Material yield strength

RPV Support (Ring Girder)

Primary Stress Limit - AISC specification Normal and upset condition Top flange 27,000 for the design, fabrication and erection 1. Dead loads of structural steel for buildings 2. Operating Basis Earthquake Bottom Flange 27,000 3. Loads due to scram Vessel to girder bolts 60,000 For normal and upset conditions 22,500 AISC allowable stresses, but without the usual increase for earthquake loads

For faulted conditions Faulted condition Top flange 45,000 1.67 X AISC allowable stresses for 1. Dead loads Bottom flange 45,000 structural steel members 2. Design Basis Earthquake Vessel to girder bolts 125,000 Yield strength for high strength 3. Jet reaction load 75,000 bolts (vessel to ring girder)

BFN-27 Sheet 7 Table C.4-1 (Continued)

REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Criteria Loading Location Allowable Stress (psi)

CRD Housing Support "Shootout Steel" Primary Stress Limit - AISC specification Faulted Condition loads Beams (top cord) 33,000 for the design, fabrication 1. Dead weight 33,000 and erection of structural steel 2. Impact force from failure Beams (bottom cord) 33,000 for buildings of a CRD housing 33,000

For normal and upset condition (Dead weights and earthquake Grid structure 41,500 F a = 0.60 F y (tension) loads are very small as 27,500 F b = 0.60 F y (bending) compared to jet force.)

F v = 0.40 F y (shear)

For faulted conditions

F a limit = 1.5 F a (tension)

F b limit = 1.5 F b (bending)

F v limit = 1.5 F b (shear) F y = Material yield strength

Recirculating Pipe and Pump Pipe Rupture Restraints Primary Stress Limit - Structural Faulted condition loads Brackets on 28 in. pipe 33,000 Steel: AISC specification for the 1. Jet force from a complete design, fabrication and erection circumferential failure Cable on pump restraints 99,000 of structural steel for buildings. (break) of recirculation line

For normal or upset conditions F a = 0.60 F y (tension)

For faulted conditions

F a limit = 1.5 F a (tension)

F y = yield strength Cable (wire rope)

For faulted conditions

F a = 0.80 F u (tension)

F u = ultimate strength BFN-27 Sheet 8 Table C.4-1 (Continued)

REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES

Criteria Loading Location Allowable Stress (psi)

Control Rod Drive Housing

Primary Stress Limit - The allowable Normal and upset condition loads Maximum membrane 16,925 primary membrane stress is based on 1. Design pressure stress intensity occurs the ASME Boiler and Pressure Vessel 2. Stuck rod scram loads at the tube to tube Code Sect. III, for Class A vessels 3. Operating Basis Earthquake weld near the center of for Type 304 stainless steel the housing for normal upset and emergency For normal and upset condition conditions S m = 16,925 psi at 575 o F For emergency conditions Emergency condition loads 25,100 Slimit = 1.5 S m = 1.5 X 16,925=25,400 psi 1. Design pressure 2. Stuck rod scram loads 3. Design Basis Earthquake

Control Rod Drive

Primary Stress Limit - The allowable Normal and upset condition loads Maximum stress intensity 26,060 primary membrane stress plus Maximum hydraulic pressure occurs at a point on the bending stress is based on ASME from the control rod drive Y-Y axis of the indicator Boiler and Pressure Vessel Code Supply pump. tube Sect. III for SA-212 TP 316 NOTE - Accident conditions tubing do not increase this loading Earthquake loads are negligible For normal and upset condition S A = 1.5 S m = 1.5 X 17.375 = 26,060 psi BFN-27 Sheet 9 Table C.4-1 (Continued)

REACTOR VESSEL, REACTOR VESSEL INTERNALS AND SUPPORTS CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Criteria Loading Location Allowable Stress (psi)

Control Rod Guide Tube (pre-uprate)

Primary Stress Limit - The allowable Faulted condition loads The maximum bending 25,400 primary membrane stress plus 1. Dead weight stress under faulted bending stress is based on the ASME 2. Pressure drop across guide loading conditions Boiler and Pressure Vessel Code tube due to failure of occurs at the center of Sect III for Type 304 stainless steam line the guide tube steel tubing 3. Design Basis Earthquake

For normal and upset conditions

S m = 16,925 psi For faulted condition Slimit = 1.5 S m = 1.5 X 16,925 - 25,400

Control Rod Guide Tube (uprate)* Allowable loads (lbs) Pressure differential (psi)

(vertical)

The allowable loading is based on Faulted condition loads The maximum loading 35,200 84 the ratio of applied load to bucklling 1. Dead weight conditions occur at the load 2. Pressure drop across guide center of the guide tube tube due to failure of length For normal and upset: steam line allowable ratio = 0.40 3. Design Basis Earthquake

For faulted: allowable ratio = 0.80

Incore Housing Allowable Stress (psi)

Primary Stress Limit - The allowable Emergency condition loads Maximum membrane 25,400 primary membrane stress is based on 1. Design pressure stress intensity occurs ASME Boiler and Pressure Vessel 2. Design Basis Earthquake at the outer surface of Code, Sect. III, for Class A vessels the vessel penetration for Type 304 stainless steel

For normal and upset conditions

S m = 16,925 psi at 575 o F For emergency condition (N + A M) Slimit = 1.5 S m = 1.5 X 16,925 = 25,400 psi

  • The component did not change as a result of increasing power but represents the parameters that were reevaluated as part of the power uprate analysis.

BFN-27 Sheet 1 Table C.4-2 PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES MAIN STEAM ISOLATION VALVES Criteria Method of Analysis Minimum Dimension Required

1. Body Minimum Wall Thickness Minimum wall thicknesses in the cylindrical Body wall thickness portions of the valve shall be calculated Loads: using the following formula: t = 1.83 in. at 23-in. diameter Design pressure and temperature Primary Membrane Stress Limit:

S = 7,000 lb/in.

2 per ASA B16.5 where: S = allowable stress of 7000 psi P = primary service pressure, 655 psi d = Inside diameter of valve at section being considered, in.

C = corrosion allowance of 0.12 in.

2. Cover Minimum Thickness Valve cover thickness

Loads: where: t = 4.888 in. t = minimum thickness, inches Design pressure and temperature d = diameter or short span, in.

Design bolting load C = attachment factor Gasket load S = allowable stress, psi W = total, bolt load, lb h G = gasket moment arm, in.

C i = corrosion allowance, in. Primary Stress Limit:

Allowable working stress per

ASME Section VIII t Pd SP C=+15212..td CP S Wh Sd C G=++178 3 12 1./

BFN-27 Sheet 2 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Isolation Valves (Continued)

Allowable Stress or Criteria Method of Analysis Actual Dimension

3. Cover Flange Bolt Area Loads: Total, bolting loads and stresses shall be Flange Bolt Stress calculated in accordance with "Rules for Loads: Bolted Flange Connections" - ASME Boiler S = 30,900 lb/in.

2 and Pressure Vessel Code,Section VIII, at 575

°F Design pressure and temperature Appendix II, except that the stem operational Gasket load load and seismic loads shall be included in Stem operational load the total load carried by bolts. The Seismic load-Design Basis Earthquake horizontal and vertical seismic forces shall be applied at the mass center of the valve Bolting Stress Limit: operator assuming that the valve body is rigid and anchored.

Allowable working stress per ASME Nuclear Pump & Valve Code, Class I

4. Body Flange Thickness and Stress Flange thickness and stress shall be calcu- Body Flange Stress lated in accordance with "Rules for Bolted Loads: Flange Connections" = ASME Boiler and Pressure Vessel Code,Section VIII, Appendix II, except Design pressure and temperature that the stem operational load and seismic S H = 26,700 lb/in.

2 Gasket load loads shall be included in the total load S R = 26,700 lb/in.

2 Stem operational load carried by the flange. The horizontal and S T = 26,700 lb/in.

2 Seismic load - Design Basis vertical seismic forces shall be applied at Earthquake the mass center of the valve operator assum- ing that the valve body is rigid and anchored. Flange Stress Limits:

S H , S R , S T 1.5 S m per ASME Nuclear Pump and Valve Code, Class I.

BFN-27 Sheet 3 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Isolation Valves(Continued)

Criteria Method of Analysis Allowable Stress

5. Valve Disc Thickness

Loads: where: S = 17,800 lb/in 2 S r = radial stress, psi Design pressure and temperature S t = tangential stress Primary bending stress limit: v = Poisson's ratio P = design pressure, psi Allowable working stress per R = radius of disc, inches ASME Section VIII t = thickness of disc, inches

6. Valve Operator Supports The valve assembly shall be analyzed assuming that the rigid mass and that the valve body Loads: is an anchored, rigid mass and that the specified vertical and horizontal seismic Design pressure and temperature forces are applied at the mass center of the S = 18,000 lb/in 2 Stem operational load operator assembly, simultaneously with Equipment dead weight operating pressure plus dead weight plus Seismic load-Design Basis operational loads. Using these loads, stresses and deflections shall be determined Support Rod Stress Limit: for the operator support components.

Allowable working stress per ASME

ASME Section VIII

()SS33vPR 8t rt 2 2==+

BFN-27 Sheet 4 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves Criteria Method of Analysis Allowable Stress Minimum Dimension Required

1. Inlet Nozzle Wall Thickness

Loads: t = 0.183 in. where: 1.1 X Design pressure at 600

°F T = min. required thickness, in. S = allowable stress, lb/in.

2 Primary Membrane Stress Limit: P = 1.1 X design pressure, lb/in.

2 R = internal radius, in.

Allowable stress intensity as defined E = joint efficiency by ASME Standard Code for Pumps and C = corrosion allowable, in. Valves for Nuclear Power

2. Valve Disc Thickness Loads: where: S s= 20,190 lb/in.

2 1.1 X Design pressure at 600

°F W = shear load, lb A = shear area, in.

2 Diagonal Shear Stress Limit: P = 1.1 X design pressure, lb/in.

2 A 1 = disc area, in.2 0.6 x allowable stress intensity and: as defined by ASME Standard Code A = S (R + R 1) for Pumps and Valves for Nuclear S = slope of frustrum of shear cone, in. Power R 1 = radius at base of cone, in. R = radius at top of cone, in.

3. Inlet Flange Bolt Area Total bolting loads and stresses shall be calculated in accordance with procedures of Loads: Para. 1-704.5.1 Flanged Joints, of B31.7 S b = 27,700 lb/in.

2 Nuclear Piping Code. Design pressure and temperature Gasket load Operational load Design Basis Earthquake

Bolting Stress Limit: Allowable stress intensity, S m, as defined by ASME Standard Code for Pumps and Valves for Nuclear Power t PRSEP C=+0.6 Ss W A PA A==1 BFN-27 Sheet 5 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves (Continued)

Criteria Method of Analysis Allowable Stress 4. Inlet Flange Thickness Flange thickness and stresses shall be S H= 27,300 lb/in.

2 calculated in accordance with procedures of S R= 27,300 lb/in.

2 Loads: Para. 1-704.5.1 Flanged Joints, of B31.7 S T= 27,300 lb/in.

2 Nuclear Piping Code. Design pressure and temperature Gasket load Operational load Seismic load-Design Basis Earthquake Flange Stress Limits:

S H , S R , S T 1.5 S m per ASME Nuclear Pump and Valve Code Set Point 5. Valve Spring-Torsional Stress S = 82,500 lb/in 2 Loads: where: S max = torsional stress, lb/in 2 Maximum Lift W 1 = Set point load P = W 1 or W 2 = spring load, W 2 = Spring load at maximum D = means diameter of coil, in. S = 112,500 lb/in.

2 lift, lb d = diameter of wire, in. C = D = correction factor d Torsional Stress Limit 0.67 X torsional elastic limit when subjected to a load of W

1.

0.90 X torsional elastic limit when subjected to a load of W

2. S PD d C CCmax.=+841 440615 3 BFN-27 Sheet 6 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves (Continued)

Criteria Method of Analysis Allowable Stress Minimum Dimension Required

6. Yoke Rod Area Loads: where:

Spring load at maximum lift A = required area per rod, in 2 A = 0.852 in.

2 F = total spring load, lb Primary Stress Limit: S m = allowable stress, lb/in.

2 Allowable stress intensity, S m , as defined by ASME Standard Code for Pumps and Valves for Nuclear Power.

7. Yoke Bending and Shear Stresses S b = 18,200 lb/in.

2 Loads: where: S s = 10,900 lb/in.

2 Spring load at maximum lift S b = bending stress, lb/in.

2 S s = shear stress, lb/in.

2 Bending and Shear Stress Limits: M = bending moment, in.-lb Z = section modulus, in.

3 Bending-allowable stress intensity, V = vertical shear, lb S m, per ASME Nuclear Pump and Valve A = shear area, in.

2 Code Shear - 0.6 X allowable stress intensity, 0.6 S m, per ASME Nuclear Pump and Valve Code.

8. Body Minimum Wall Thickness

Loads: where: Body Bowl t = required thickness, in t = 0.3312 in Primary service pressure S = allowable stress, 7,000 lb/in.

2 P = primary service pressure, 150 lb/in 2 Inlet Nozzle Primary Stress Limit: d = inside diameter of valve at t = 0.231 in. section being considered, in.

Allowable stress, 7,000 lb/in 2, Outlet Nozzle in accordance with USAS B16.5. t = 0.2823 in.

A F S m=2 S M Z S V A bs==, t Pd SP C=+15 21..2 BFN-27 Sheet 7 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Safety Valves

Criteria Method of Analysis Allowable Stress Load Limit

9. Inlet Nozzle Combined Stress S = 27,300 lb/in.

2

Loads: where:

S = combined bending and tensile Spring load at maximum lift stress, lb/in.

2 Operational load F 1 = maximum spring load, lb Seismic load-Design Basis Earthquake F 2 = vertical component of reaction thrust, lb Combined Stress Limit:

A = cross section area of nozzle, in.

2 1.5 X allowable stress intensity, M 1 = moment resulting from horizontal 1.5 S m, per ASME Code for Pumps component of reaction, lb-in. and Valves for Nuclear Power. M 2 = moment resulting from horizontal seismic force, in.-lb

10. Spindle Diameter Load limit (0.2F c)

Loads: where: F = 30,210 lb Spring load at Maximum lift F c = critical buckling load, lb E = modulus of elasticity, lb/in.

2 Spindle Column Load Limit: I = moment of inertia, in.

4 L = length of spindle in compression, in.

0.2 X critical buckling load

11. Spring Washer Shear Area S s = 15,960 lb/in.

2 Loads where:

Spring load at maximum lift S s = shear stress, lb/in.

2 F = spring load, lb Shear Stress Limit: A = shear area, in.

2 0.6 X allowable stress intensity, 0.6S m, per ASME Nuclear Pump and Valve Code.

S FF A MM Z=+++1212 F EI L c=2 2 S F A s=

BFN-27 Sheet 8 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Relief Valves

Criteria Method of Analysis Minimum Dimension Required

1. Body Minimum Wall Thickness Main Body:

Loads: where: t = 0.625 in.

Design pressure and temperature t = minimum required thickness, in. Bonnet:

S = allowable stress, 7,000 lb/in.

2 Primary Membrane Stress Limit: P = primary service pressure, 655 t = 0.287 in. d = inside diameter of valve at section Allowable working stress as being considered, in. defined by USAS B16.5 (7,000 C = corrosion allowance, 0.12 in.

psi at primary service pressure).

2. Bonnet Cap and Pilot Base Bonnet Cap:

Minimum Thickness t = 0.612 in.

Loads: where:

t = minimum required thickness, in. Pilot Base: Design pressure and temperature d = diameter or short span, in. Gasket load C = attachment factor, ASME t = 2.117 in.

Section VIII Primary Stress Limit: P = design pressure, lb/in.

2 S m = allowable stress, lb/in.

2 Allowable stress intensity, Sm, W = total bolt load, lb as defined by ASME Standard h g = gasket moment arm, in. Code for Pumps and Valves C 1 = corrosion allowance, 0.12 in. for Nuclear Power. t1.5 PD2S1 2P C=+td CP SWhG Sd C m m=++178 3 12 1./

BFN-27 Sheet 9 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Relief Valves (Continued)

Criteria Method of Analysis Allowable Stress Minimum Dimension Required

3. Flange Bolt Area - Inlet Flange, Total bolting loads and stresses shall be Body to Base:

Outlet Flange, Body to Bonnet, calculated in accordance with procedures Bonnet to Base of Para. 1-704.5.1 Flanged Joints, of A b = 10.26 in 2 A b = 2.854 in.

2 B31.7 Nuclear Piping Code Loads: Bonnet to Cap:

Design pressure and temperature A b = 1.452 in.

2 A b = 0.995 in.

2 Gasket load Operational load Inlet Flange Design Basis Earthquake A b = 13.9 in.

2 A b = 6.25 in.

2 Bolting Stress Limit:

Outlet Flange:

Allowable stress intensity, S m as A b = 12.2 in 2 defined by ASME Standard Code for A b = 5.5 in.

2 Pumps and Valves for Nuclear Power.

4. Flange Thickness - Inlet, Outlet, Flange thickness and stresses shall be Bonnet Flanges calculated in accordance with procedures S H = 26,250 lb/in.

2 of Para. 1-704.5.1 Flanged Joints, of S R = 26,250 lb/in.

2 Loads: B31.7 Nuclear Piping Code S T = 26,250 lb/in.

2 Design pressure and temperature

Gasket load Operational load Design Basis Earthquake

Flange Stress Limits:

S H , S R , S T 1.5 S m per ASME Nuclear Pumps and Valve Code.

BFN-27 Sheet 10 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Main Steam Relief Valves (Continued)

Criteria Method of Analysis Allowable Stress

5. Valve Disc. Thickness and Stress Disc Stress:

Loads: where: S m = 15,800 lb/in 2 Design pressure and temperature S r = radial stress, lb/in 2 S t = tangential stress, lb/in 2 Primary Stress Limit: v = Poisson's ratio P = design pressure, lb/in 2 Allowable stress intensity, S m R = radius of disc, in. as defined by ASME Standard Code for t = thickness of disc, in.

Pumps and Valve for Nuclear Power.

Inlet Nozzle Diameter Thickness and Stress Inlet Nozzle Stress:

Loads: where: S = 26,250 lb/in 2 S = combined bending and tensile Design pressure and temperature stress, lb/in 2 Operational load F 1 = vertical load due to design pressure, lb Design Basis Earthquake F 2 = vertical component of reaction thrust, lb Primary Stress Limit: A = cross section area of nozzle, in 2 M 1 = moment resulting from horizontal 1.5 X allowable stress intensity, reaction, in.-lb 1.5 S m as defined by ASME M 2 = moment resulting from horizontal Standard Code for Pumps and seismic force at mass center of Valves for Nuclear Power. valve, in.-lb

()SSvPR t rt==+33 8 2 2 S FF A MM Z=+++1212 BFN-27 Sheet 11 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Pumps

Criteria Method of Analysis Allowable Stress Minimum Dimension Required

1. Casing Minimum Wall Thickness t = 2.68 in. Loads: Normal and Upset Condition where:

Design pressure and temperature t = minimum required thickness, in. P = design pressure, psig Primary Membrane Stress Limit: R = maximum internal radius, in. S = allowable working stress, psi Allowable working stress per E = joint efficiency ASME Section III, Class C C = corrosion allowance, in.

2. Casing Cover Minimum Thickness Loads: Normal and Upset Condition

Design pressure and temperature S r = 15,075 psi Primary Bending Stress Limit:

1.5 S m per ASME code for Pumps and Valves for S t = 15,075 psi Nuclear Power Class I

where:

S r = radial stress at outer edge, psi S t = tangential stress at inner edge, psi w = pressure load, psi W = uniform load along inner edge, lb t = disc thickness, in.

m = reciprocal of Poisson's ratio a = radius of disc, in.

b = radius of disc hole, in.

()()()()()S r 3W 4t 2 a 2 2b 2 b 4m14b 4m1ln aba 2 b 2 m1 a 2m1b 2 m1=++++++/()()()++++3W 2pt 2 12mb 2 2b 2m1lnab a 2m1b 2 m1/()()()S t3Wm 2 14mt 2 a 4 b 4 4a 2 b 2ln ab a 2m1b 2 m1=+++/()()()()()3W2pmt 2 1 ma 2m1mb 2m12m 2 1a 2ln ab a 2m1b 2 m1++++/t PRSE06P C=+-

BFN-27 Sheet 12 Table C.4-2 (Continued)

PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Pumps (Continued)

Criteria Method of Analysis Allowable Stress Minimum Dimension Required

3. Cover and Seal Flange Bolt Areas Bolting loads, areas and stresses shall be calculated in accordance with "Rules for Loads: Normal and upset conditions Bolted Flange Connections" - ASME 20,000 psi Section VIII, Appendix II Design pressure and temperature Design gasket load 20,000 psi Bolting Stress Limit:

Allowable working stress per ASME Section III, Class C

4. Cover Clamp Flange Thickness Flange thickness and stress shall be Flange Thickness calculated in accordance with "Rules 8.9 in.

Loads: Normal and upset condition for Bolted Flange Connections" -ASME Section VIII, Appendix II Design pressure and temperature Design gasket load Design bolting load

Tangential Flange Stress Limit:

Allowable working stress per ASME Section III, Class C

5. Pump Nozzle Stress Pipe Stress is compared to allowable 21,708 psi of 0.9 (Yield stress of pump nozzle)

Loads: Normal, Upset and Faulted Condition Sheet 13 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Pumps (Continued)

Criteria Method of Analysis Allowable Stress

6. Mounting Bracket Combined Stress Bracket vertical loads shall be determined BFN-27 summing the equipment and fluid weights Loads: and vertical seismic forces. Pump Lug Bracket horizontal loads shall be determined Flood weight by applying the specified seismic force at 17,280 psi Design Basis Earthquake mass center of pump-motor assembly (flooded). Combined Stress Limit: Horizont al and vertical loads shall be applied simultaneously to determine Yield Stress tensile, shear and bending stresses in Motor Lug the brackets. Tensile shear, and bending stress shall be combined to determine 21,000 psi

maximum combined stresses.

BFN-27 Sheet 14 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Pumps (Continued)

Criteria Method of Analysis Allowable Stress

7. Stresses Due to Seismic Loads The flooded pump-motor assembly shall Motor Bolt Tensile Stress: be analyzed as a free body supported by Loads: constant support hangers from the pump 11,200 psi brackets. Horizontal and vertical seismic Operating pressure and forces shall be applied at mass center of Pump Cover Bolt Tensile Stress: temperature assembly and equilibrium reactions shall Design Basis Earthquake be determined for the motor and pump 32,000 psi brackets. Load, shear, and moment Combined Stress Limit: diagrams shall be constructed using live Motor Support Barrel loads, dead loads, and calculated snubber Combined Stress: Yield stress reactions. Combined bending, tension and shear stresses shall be determined 22,400 psi for each major component of the assembly including motor, motor support barrel, bolting and pump casing. The maximum combined tensile stress in the cover bolting shall be calculated using tensile stresses determined from loading diagram plus tensile stress from operating pressure.

BFN-27 Sheet 15 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Fuel Storage Racks

Criteria Loading Location Allowable Stress

Stresses due to normal, upset, or emergency Emergency condition At column to base welds 11,000 psi(1) loading shall not cause the racks to fail "A" loads so as to result in a critical fuel array 1. Dead loads At base hold down lug 20,000 psi(2) 2. Full fuel load in rack (casting)

3. Design Basis Earthquake Primary Stress Limit-Paper numbers 3341 and 3342, Proceedings of the ASCE, Journal Emergency condition of the Structural Division, December 1962 "B" loads (see below) (task committee on lightweight alloys) (Aluminum)

Emergency Conditions Stress limit = yield strength at 0.2% offset.

(1) Load testing shows that the structure will not yield when subjected to simulated emergency condition "A" loads. Strain gages mounted on the welds show that calculated stresses are conservative. (2) Calculated stresses compare very well with test results.

Emergency Condition "B"

Loading In addition to the loading conditions given above, the racks are tested and analyzed to determine their capability to safely withstand the accidental, uncontrolled drop of the fuel grapple from its full retracted position into the weakest portion of the rack.

Method of Analysis

The displacement of the vertical columns at the ends of the racks is determined by considering the effect of the grapple kinetic energy on the upper structure. The energy absorbed shearing the rack longitudinal structural member welds is determined.

The effect of the remaining energy on the vertical columns is analyzed. Equivalent static load tests are made on the structure to assure that the criteria are met.

BFN-27 Sheet 16 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RHR Pumps Criteria Method of Analysis Allowable Stress

1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be 25,000 psi contain the internal design pressure calculated in accordance with the "Rules of the pump casing without exceeding for Bolted Flange Connections," ASME the allowable stress of the bolting Boiler and Pressure Vessel Code, material. Allowable stresses at Section VIII, Appendix II.

design temperature shall be in accordance with ASME Boiler and Pump Design Pressure 450 psig pressure Vessel Code,Section VIII. Maximum Design Temperature 350

°F 2. The minimum wall thickness of the 2. Stress in the pump casing shall be 14,000 psi pump shall limit stress to the calculated at the point of maximum allowable stress when subjected to internal pump diameter by the formula design pressure and temperature. Allowable stresses shall be in accordance with ASME Boiler and Pressure Vessel Code,Section VIII. where S c = calculated stress, psi P = pump design pressure, psi D = maximum pump internal diameter t = actual minimum metal thickness less corrosion allowance, 0.080 in.

()SPDt t c=+0 2.2 BFN-27 Sheet 17 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RHR Pumps (Continued)

Criteria Method of Analysis and Allowable Nozzle Loads

3. Application of forces and moments by 3. Stresses will not be excessive if the attaching pipe on pump nozzles under maximum resultant force when taken with combined maximum thermal expansion the maximum resultant moment falls below and Operating Basis Earthquake the line.

loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel Code,Section VIII. Suction OBE DBE Fintercept 88,000 lb 146,000 lb (M=0)

For Design Basis Earthquake stress Mintercept 1,200,000 in.-lb 1,800,000 in.-lb shall be less than 1.5 of allowable (F=0) stress. Discharge

Fintercept 68,000 lb 126,000 lb (M=0)

Mintercept 760,000 in.-lb 1,300,000 in.-lb (F=0)

Pipe Design Pressure Suction = 150 psig Discharge = 450 psig

BFN-27 Sheet 18 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Core Spray Pumps

Criteria Method of Analysis Allowable Stress

1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be 20,000 psi contain the internal design pressure calculated in accordance with the "Rules of the pump casing without exceeding for Bolted Flange Connections," ASME the allowable stress of the bolting Boiler and Pressure Vessel Code, Section material. Allowable stresses at VIII, Appendix II.

design temperature shall be in accordance with ASME Boiler and Pump Design Pressure 500 psig Pressure Vessel Code,Section VIII. Maximum Design Temperature 210

°F 2. The minimum wall thickness of the 2. Stress in the pump casing shall be 14,000 psi pump shall limit stress to the allow- calculated at the point of maximum able stress when subjected to design internal pump diameter by the formula pressure and temperature. Allowable stresses shall be in accordance with ASME Boiler and Pressure Vessel Code,Section VIII.

where S c = calculated stress, psi 17,500 psi allowable for 216 WCB X P = pump design pressure, psi 0.8 (quality factor) = 14,000 psi D = maximum pump internal diameter t = actual minimum metal thickness less corrosion allowance, 0.080 in.

()SPDt t c=+0 2.2 BFN-27 Sheet 19 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Core Spray Pumps (Continued)

Criteria Method of Analysis and Allowable Nozzle Loads Representative Results

3. Application of forces and moments by 3. Stresses will not be excessive if the attaching pipe on pump nozzles under maximum resultant force when taken with the combined maximum thermal expansion maximum resultant moment falls below the line. Operating Basis Earthquake loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel Code,Section VIII. Suction OBE DBE Fintercept 66,686 lb 104,955 lb

(M=0)

For Design Basis Earthquake stress Mintercept 564,193 in.-lb 880,105 in.-lb shall be less than 1.5 of allowable (F=0) stress. Discharge

Fintercept 35,105 lb 65,982 lb (M=0)

Mintercept 266,479 in.-lb 463,492 in.-lb (F=0)

Pipe Design Pressure Suction = 125 psig Discharge = 500 psig

BFN-27 Sheet 20 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES HPCI Pumps

Criteria Method of Analysis Allowable Stress

1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be Main Pump contain the internal design pressure calculated in accordance with the "Rules of the pump casing without exceeding for Bolted Flange Connections," ASME 20,000 psi the allowable stress of the bolting Boiler and Pressure Vessel Code, Section material. Allowable stresses at VIII, Appendix II. Boost Pump design temperature shall be in accordance with ASME Boiler and Main Pump Design Pressure 1500 psig 20,000 psi Pressure Vessel Code,Section VIII. Boost Pump Design Pressure 450 psig
2. The minimum wall thickness of the 2. Stress in the pump casing shall be Main Pump pump shall limit stress to the allow- calculated at the point of maximum able stress when subjected to design internal pump diameter by the formula 14,000 psi pressure and temperature. Allowable stresses shall be in accordance with ASME Boiler and Pressure Vessel Code,Section VIII.

Volute stress shall be calculated by the Boost Pump following formula 14,000 psi The maximum stress in the pump Roark casing when subjected to design p. 307 Case 26 pressure shall not exceed the allow- able working stress of the material.

The allowable stress shall be in and R = a - 0.5b accordance with ASME Boiler and Pressure Vessel Code,Section III.

()SPDt ET h=+0 2.2 SPbRa R v t=+2 BFN-27 Sheet 21 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES HPCI Pumps (Continued)

Criteria Method of Analysis and Allowable Nozzle Loads

3. Application of forces and moments by 3. Stresses will not be excessive if the attaching pipe on pump nozzles under maximum resultant force when taken with the combined maximum thermal expansion maximum resultant moment falls below the line. and Operating Basis Earthquake

loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel Code,Section VIII. Suction OBE DBE

Fintercept 33,000 lb 43,000 lb (M=0)

For Design Basis Earthquake stress Mintercept 500,000 in.-lb 700,000 in.-lb shall be less than 1.5 of allowable (F=0) stress. Discharge

Fintercept 32,000 lb 47,000 lb (M=0)

Mintercept 250,000 in.-lb 460,000 in.-lb (F=0)

Pipe Design Pressure Suction = 150 psig Discharge = 1500 psig

BFN-27 Sheet 22 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RCIC Pump Criteria Method of Analysis Allowable Stress

1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be contain the internal design pressure calculated in accordance with the "Rules of the pump casing without exceeding for Bolted Flange Connections," ASME 20,000 psi the allowable stress of the bolting Boiler and Pressure Vessel Code, Section material. Allowable stresses at VIII, Appendix II.

design temperature shall be in accordance with ASME Boiler and Pump Design Pressure 1500 psig Pressure Vessel Code,Section VIII.

2. The minimum wall thickness of the 2. Stress in the pump casing shall be 14,000 psi pump shall limit stress to the allow- calculated at the point of maximum able stress when subjected to design internal pump diameter by the formula pressure and temperature. Allowable stresses shall be in accordance with ASME Boiler and Pressure Vessel Code,Section VIII.

S C = 0.8Sa The maximum stress in the pump Volute stress shall be computed by the 14,000 psi casing when subjected to design following formula:

pressure shall not exceed the allowable working stress of the Roark p. material. The allowable stress 225 Case No. 36 shall be in accordance with ASME Boiler and Pressure Vessel Code, Section III. = factor from Roark a = volute length b = volute width

()SPDt tE c=+.02 2 S P t b b=2 2 BFN-27 Sheet 23 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RCIC Pump (Continued)

Criteria Method of Analysis and Allowable Nozzle Loads

3. Application of forces and moments by 3. Stresses will not be excessive if the attaching pipe on pump nozzles under maximum resultant force when taken with the combined maximum thermal expansion maximum resultant moment falls below the line. and Operating Basis Earthquake loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel Code,Section VIII. Suction OBE DBE

Fintercept 9,000 lb 13,500 lb (M=0) For Design Basis Earthquake stress Mintercept 54,000 in.-lb 69,000 in.-lb shall be less than 1.5 of allowable (F=0) stress. Discharge Fintercept 9,000 lb 13,500 lb (M=0)

Mintercept 54,000 in.-lb 69,000 in.-lb (F=0)

Pipe Design Pressure Suction = 150 psig Discharge = 1500 psig

BFN-27 Sheet 24 Table C.4-2 (Continued)

PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Standby Liquid Control Pumps Criteria Method of Analysis Allowable Stress

1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be Stuffing Box Bolts contain the internal design pressure calculated in accordance with the "Rules of the pump without exceeding the for Bolted Flange Connections," ACME 25,000 psi allowable working stress of the Boiler and Pressure Vessel Code, Section bolting material. Allowable stresses VIII, Appendix II. Cylinder Head Bolts shall be in accordance with ASME Boiler and Pressure Vessel Code. 25,000 psi
2. The maximum stress in the pump 2. Stress in the pump fluid cylinder shall be 16,500 psi fluid cylinder when subjected to calculated at the point of maximum stress design pressure shall not exceed by the pressure area method.

the allowable working stress of the material. The allowable stress Pump Design Pressure 1400 psig shall be in accordance with ASME Boiler and Pressure Vessel Code,Section VIII.

3. The stresses in the motor mounting 3. The seismic forces acting on the motor to Tension bolts when the motor is subjected subject the bolting to shear or tension to the Design Basis Earthquake shall are considered. The motor is isolated 16,500 psi not exceed 0.9 of yield stress and from the pump and nozzle forces by the twice the allowable shear stress for flexible coupling. Shear bolting material in accordance with the ASME Boiler and Pressure Vessel 10,000 psi Code,Section VIII.

BFN-27 Sheet 25 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Standby Liquid Control Pumps (Continued)

Criteria Method of Analysis and Allowable Nozzle Loads

4. The stresses in the pump mounting bolts 4. The maximum force taken with the maximum due to the combination of Operating resultant moment shall fall below the line on the Basis Earthquake acting on the flooded force-moment diagram: pump plus the attaching pipe reactions under combined maximum thermal expan-

sion plus Operating Basis Earthquake shall not exceed the allowable shear

and tensile stresses for the bolting material in accordance with the ASME Boiler and Pressure Vessel code,Section VIII. The attaching pipe reaction plus the load due to internal pressure shall not produce an equivalent bending and torsional stress in OBE nozzles in excess of the allowable Discharge M = 2.3 (342-F) stress. not to exceed 283 ft-lb The stresses in the pump mounting bolts Suction M = 4.59 (711-F) due to the combination of the Design not to exceed 1385 ft-lb Basis Earthquake acting on the flooded DBE pump plus the attaching pipe reactions Discharge M = 2.3 (684-F) under combined maximum thermal expan- not to exceed 444 ft-lb sion plus Design Basis Earthquake shall Suction M = 4.59 (1422-F) not exceed 0.9 times the yield stress not to exceed 2060 ft.lb in tension and twice the allowable shear stress for the bolting material Where M is maximum moment (ft-lb) in in accordance with the ASME Boiler and any direction and F is maximum force Pressure vessel Code,Section VIII. (lb) in any direction.

The attaching pipe reaction plus the load due to internal pressure shall not produce an equivalent bending and tor-sional stress in nozzles in excess of 1.5 times allowable stress.

BFN-27 Sheet 26 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RHR Service Water Pumps A2, A3, B2, B3, C1, C2, C3 Criteria Method of Analysis and Allowable Nozzle Loads

1. Application of forces and moments by 1. Stresses will not be excessive if the attaching pipe on pump nozzles under loads on the pump nozzles do not combined maximum thermal expansion exceed the following values: and Operating Basis Earthquake loading reaction plus load due to Condition F(Axial) F(Vertical) F(Lateral) M(Torsion) M(Vertical) M(Laterial) internal pressure shall not produce Normal 6,211 lb 6,888 lb 3,882 lb 5,552 ft-lb 17,499 ft-lb 10,419 ft-lb an equivalent bending and torsional Upset 9,110 lb 8,970 lb 5,103lb 8,790 ft-lb 19,218 ft-lb 13,006 ft-lb stress in the nozzles in excess of Emergency 12,010 lb 11,052 lb 6,984 lb 12,047 ft-lb 30,527 ft-lb 15,593 ft-lb the allowable stress as defined b BFN-50-C-7106 Table 3.1-1 for Active Pumps.

BFN-27 Sheet 26A Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RHR Service Water Pumps A1, B1, D1, D2, D3 Criteria Method of Analysis and Allowable Nozzle Loads

1. Application of forces and moments by attaching pipe on pump nozzles under combined maximum thermal expansion and Operating Basis Earthquake loading reaction plus load due to internal pressure shall not produce an equivalent bending and torsional stress in the nozzles in excess of the allowable stress as defined by the ASME Boiler and Pressure Vessel Code,Section VIII.

For Design Basis Earthquake stress shall be less than 1.5 of allowable stress..

1. Stresses will not be excessive if the maximum resultant force when taken with the maximum resultant moment falls below the line.

Pump is a vertically mounted deep-well type with submerged suction.

Discharge OBE DBE Fintercept 45,200 lb 73,000 ob (M=0) Mintercept 336,000 in.-lb 536,500 in.-lb (F=0) Pipe Design Pressure Discharge = 185 psig

BFN-27 Sheet 27 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RCIC Turbine Criteria Method of Analysis Allowable Stress

1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be 20,000 psi contain the internal design pressure calculated in accordance with the "Rules of the turbine casing without for Bolted Flange Connections," ACME exceeding the allowable working Boiler and Pressure Vessel Code, Section stress of the bolting material. VIII, Appendix II.

Allowable stresses shall be in accordance with ASME Boiler and Pressure Vessel Code,Section VIII.

2. The maximum wall thickness of the 2. Stresses in the various pressure contain- 17,500 psi turbine casing shall be based on ing portions of the turbine casing shall that to limit stress to the allowable be calculated according to the rules of working stress when subjected to Part UG,Section VIII, of the ASME Boiler design pressure plus corrosion and Pressure Vessel Code.

allowance. Allowable stresses shall be in accordance with ASME Boiler and Pressure Vessel Code,Section VIII.

BFN-27 Sheet 28 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RCIC Turbine (Continued)

Criteria Method of Analysis and Allowable Nozzle Loads

3. The forces and moments imposed by the 3. The total resultant of the forces and the total attached piping on the turbine inlet resultant of the moments on both the inlet and and exhaust connections shall satisfy the exhaust connections of the turbine shall the following conditions: satisfy the following equations:
a. The resultant force and moment For the combination of dead weight and maximum from the combination of dead thermal expansion, weight, and thermal expansion shall be less than that stipulated Inlet F = (2620-M)/3.0 by the equipment vendor. Exhaust F = (6000-M)/3.0
b. The resultant force and moment For the combination of dead weight, maximum from the combination of dead thermal expansion, and Operating Basis Earth-weight, thermal expansion, and quake.

Operating (or Design) Basis Inlet F = (3000-M)/2.5 Earthquake shall be less than Exhaust F = 3.0 (6000-M), but not that demonstrated acceptable to exceed 8,370 lb by detailed seismic analysis of the equipment. For the combination of dead weight, maximum thermal expansion, and Design Basis Earthquake

Inlet F = (4500-M)/2.5 Exhaust F = 3.0 (9000-M), but not to exceed 12,555 lb Where "F" is the resultant force in lb and "M" is the resultant moment in ft-lb Typical acceptable area on the force-moment diagram is indicated below:

BFN-27 Sheet 29 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES RCIC Turbine (Continued)

Criteria Method of Analysis

4. The stresses in the turbine anchor 4. Vertical forces on the anchor bolts shall be bolts (turbine to baseplate) due to the sum of the following: the combination of the Operating Basis Earthquake acting on the a. Weight of the turbine assembly times the turbine while running plus the total vertical component of acceleration, piping loads (weight, thermal & OBE) b. The vertical pipe force reactions, shall not exceed the allowable tensile c. The pipe moment reactions tending to tip the stress nor the allowable shear stress turbine and subject the bolting to tension. for the bolting materials as specified in the ASME Boiler and Pressure Horizontal forces on the anchor bolts, Vessel Code,Section VIII. subjecting them to shear, shall be the sum of the following:
a. Weight of the turbine assembly times the horizontal component of acceleration,
b. The horizontal pipe force reactions, c. The effect of pipe moment reactions causing horizontal loading at the anchor bolts NOTE: Friction shall not be considered to be restrictive
5. The stresses in the turbine anchor 5. Same as analysis under 4, above. bolts (turbine to baseplate) due to the combination of Design Basis Earthquake acting on the turbine in standby plus the total piping loads (weight, thermal, and DBE) shall not exceed 0.9 times the yield stress in tension, nor twice the allowable shear stress for the bolting materials as specified in the ASME Boiler and Pressure Vessel Code,Section VIII.

BFN-27 Sheet 30 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES HPCI Turbine Criteria Method of Analysis Allowable Stress

1. Closure bolting shall be designed to 1. Bolting loads and stresses shall be 20,000 psi contain the internal design pressure calculated in accordance with the "Rules of the turbine casing without for Bolted Flange Connections," ASME exceeding the allowable working Boiler and Pressure Vessel Code, Section stress of the bolting material. VIII, Appendix II.

Allowable stresses shall be in accordance with ASME Boiler and

Pressure Vessel code,Section VIII.

2. The minimum wall thickness of the 2. Stresses in the various pressure 17,500 psi turbine casing shall be based on that containing portions of the turbine casing to limit stress to the allowable work- shall be calculated according to the rules ing stress when subjected to design of Part UG,Section VIII, of the ASME pressure plus corrosion allowance. Boiler and Pressure Vessel Code.

Allowable stresses shall be in accordance with ASME Boiler and Pressure Vessel Code,Section VIII.

BFN-27 Sheet 31 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES HPCI Turbine (Continued)

Criteria Method of Analysis and Allowable Nozzle Loads

3. The forces and moments imposed by the 3. The total resultant of the forces and the total attached piping on the turbine inlet of the moments on both the inlet and and exhaust connections shall satisfy the connections of the turbine shall the following conditions: satisfy the following equations:
a. The resultant force and moment For the combination of dead weight and from the combination of dead maximum thermal expansion, weight and thermal expansion shall be less than that stipulated Inlet F = (7570-M)/3.0 by the equipment vendor. Exhaust F = (9930-M)/3.0
b. The resultant force and moment For the combination of dead weight, maximum from the combination of dead thermal expansion, and Operating Basis Earthquake weight, thermal expansion, and Inlet F = (20,000-M)/2.5 but not Operating (or Design) Basis to exceed 5000 lb Earthquake shall be less than Exhaust F = (20,000-M)/0.8, but not that demonstrated acceptable to exceed 11,500 lb by detailed seismic analysis of the equipment For the combination of dead weight, maximum thermal expansion, and Design Basis Earthquake, Inlet F = (30,000-M)/2.5, but not to exceed 17,250 lb Exhaust F = (30,000-M)/0.8, but not to exceed 17,250 lb Where "F" is the resultant force in lb and "M" is the resultant moment in ft-lb Typical acceptable area on the force-moment diagram is indicated below:

BFN-27 Sheet 32 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES HPCI Turbine (Continued)

Criteria Method of Analysis

4. The stresses in the turbine anchor 4. Vertical forces on the anchor bolts shall be the bolts (turbine to baseplate) due to sum of the following: the combination of the Operating Basis Earthquake acting on the turbine while a. Weight of the turbine assembly times the running plus the total piping loads vertical component of acceleration, (weight, thermal and OBE) shall not b. The vertical pipe force reactions, exceed the allowable tensile stress c. The pipe moment reactions tending to tip the nor the allowable shear stress for turbine and subject the bolting to tension. the bolting materials as specified in the ASME Boiler and Pressure Horizont al forces on the anchor bolts, subjecting Vessel Code,Section VIII. them to shear, shall be the sum of the following:
a. Weight of the turbine assembly times the horizontal component of acceleration,
b. The horizontal pipe force reactions, c. The effect of pipe moment reactions causing horizontal loading at the anchor bolts NOTE: Friction shall not be considered to be restrictive
5. The stresses in the turbine anchor 5. Same as analysis under 4, above. bolts (turbine to baseplate) due to the combination of Design Basis Earthquake acting on the turbine in standby plus the total piping loads (weight, thermal and OBE) shall not exceed 0.9 times the yield stress in tension, nor twice the allowable shear stress for the bolting materials as specified in the ASME Boiler and Pressure Vessel Code,Section VIII.

BFN-27 Sheet 33 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Valves - Units 1 and 2

Criteria Method of Analysis Allowable Stress Minimum Dimension Required

1. Body Minimum Wall In Pipe Run Codes and Standards 2 in. (Equalizer Bypass Valve) 1. USAS B31.1.0 1967 t = 0.253 in.

2 in. Equalizer Bypass Valve 2. Manufacturers Standards 4 in. (Discharge Bypass Valve) 4 in. Discharge Bypass Valve Society MSS-SP.66 t = 0.405 in.

22 in. Equalizer Valve 28 in. Suction Valve 22 in. (Equalizer Valve) 28 in. Discharge Valve t = 1.520 in.

Loads: where:

Design Pressure t = minimum wall thickness, in. 28 in. (Suction Valve) Design Temperature P = design pressure, psig t = 1.938 in.

d = minimum diameter of flow passage, but not less than 28 in (Discharge Valve)

Primary Membrane Wall 90% of inside diameter at t = 1.938 in. Thickness welding end, in. S = allowable working stress, psi y = plastic stress distribution factor, 0.4

2. Body-to-Bonnet Bolt Area Loads ASME Boiler and Pressure Vessel 2 in. (E qualizer Bypass Valve) Code,Section VIII, Appendix II, 2 in. Equalizer Bypass Valve 1968 Edition. Sallow = 29,000 lb/in.

2 4 in. Discharge Bypass Valve

Loads: Total bolting loads and stresses 4 in. (Discharge Bypass Valve) shall be calculated in accordance Design pressure and temperature with "Rules for Bolted Flange Con- Sallow = 29,000 lb/in.

2 Gasket load nections," ASME Boiler and Pressure Stem operational load Vessel Code,Section VIII, Appendix Design Basis II, except that the stem operation-Earthquake al load and seismic loads shall be included in the total load carried by bolts. The horizontal and vertical seismic forces shall be applied at the mass center of the valve operator assuming that the valve body is rigid and anchored.

()t PSPy d=+15221 01..

BFN-27 Sheet 34 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Valves - Units 1 and 2 (Continued)

Criteria Method of Analysis Allowable Stress

3. Flange Stress ASME Boiler and Pressure Vessel 2 in. (Equalizer Bypass)

Code,Section VIII, Appendix II, 2 in. Equalizer Bypass Valve 1968 Edition. S H S R S T 4 in. Discharge Bypass Valve 20,100 3,426 13,426 Loads: Flange thickness and stress shall be calculated in accordance with 4 in. (Discharge Bypass) Design pressure and temperature "Rules for Bolted Flange Connec- Gasket load tions," ASME Boiler and Pressure 20,100 13,426 13,426 Stem operational load Vessel Code,Section VIII, Appen-Seismic load - dix II, except that the stem Design Basis operational load and seismic loads Earthquake shall be included in the total load carried by the flange. The horizontal and vertical seismic forces shall be applied at the mass center of the valve operator assum-ing that the valve body is rigid.

4. (A) Body and Bonnet Flange ASME Boiler and Pressure Vessel Primary Stresses Stress Code,Section III, Article 4 Membrane Stress Allowable = (B) Body Neck Wall Stress Primary, secondary, and peak 15,800 psi stresses were analyzed in accordance 22 in. Equalizer Valves with ASME Section III using finite Local Membrane Stress Allowable = 28 in. Suction Valves element computer analysis. The 23,700 psi 28 in. Discharge Valves model was verified by strain gage Primary Plus Secondary Stresses tests Loads: Code Allowable - 3S m = Design pressure and 47,400 psi Design temperature

BFN-27 Sheet 35 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Valves - Units 1 and 2

Criteria Method of Analysis Allowable Stress

5. Body to Bonnet Bolting Under operating conditions

Loads: 67,000 psi Design Pressure Maximum conditions Design Temperature 100,500 psi

6. Valve Operator Support Bolting The valve assembly is analyzed S b allowable = 20,000 lb/in.

2 assuming that the valve body is an 2 in Equalizer Bypass Valve anchored, rigid mass and that the 4 in. Discharge Bypass Valve specified vertical and horizontal 22 in. Equalizer Valve seismic forces are applied at the 28 in. Suction Valve mass center of the operator assembly, 28 in. Discharge Valve simultaneously with operating pres- sure plus dead weight plus opera- Loads: tional loads. Using these loads, stresses and deflections are deter- Design Pressure and Temperature mined for the operator support Stem operational load components.

Equipment dead weight Seismic load

Design Basis Earthquake BFN-27 Sheet 36 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Valves - Unit 3

Criteria Method of Analysis Allowable Stress Minimum Required Dimensio n

1. Body Minimum Wall In Pipe Run 22 in. Valve - t = 1.52 in. Loads: 4 in. Valve - t = 0.405 in.

Design pressure and temperature where: 2 in. Valve - t = 0.253 in. t = minimum wall thickness, in. Primary Membrane Stress Limit: P = design pressure, psig 28 X 24 X 28 in. Valve - d = minimum diameter of flow t = 1.677 in. (Suction) Allowable working stress per passage but not less than 90%

ASME Section 1 of inside diameter at welding 28 X 24 X 28 in. Valve -

end, in. t = 1.938 in. (Discharge) S = allowable working stress, psi y = plastic stress distribution factor, 0.4

2. Body-to-Bonnet Bolt Area Total bolting loads and stresses Flanged Bolt Stress shall be calculated in accordance Loads: with "Rules for Bolted Flange Sallow = 29,000 lb/in.

2 Connections," ASME Boiler and Design pressure and temperature Pressure Vessel Code,Section VIII, Gasket load Appendix II, except that the stem Stem operational load operational load and seismic loads Seismic load - shall be included in the total load Design Basis Earthquake carried by bolts. The horizontal and vertical seismic forces shall Bolting Stress Limit: be applied at the mass center of the valve operator assuming that Allowable working stress per the valve body is rigid and anchored. ASME Boiler and Pressure

Vessel Code,Section VIII, Appendix II, 1968 Edition.

()t1.5Pd2S2P1y0.1=+

BFN-27 Sheet 37 Table C.4-2 (Continued) PRIMARY SYSTEM COMPONENTS - CRITICAL LOAD COMBINATIONS, LOCATIONS, AND ALLOWABLES Recirculation Valves - Unit 3 (Continued)

Criteria Method of Analysis Allowable Stress

3. Flange Stress Flange thickness, and stress shall be S H: 20,100 lb/in.

2 (Hub Stress) calculated in accordance with "Rules S R: 13,426 lb/in.

2 (Radial Stress) Loads: for Bolted Flange Connections"-ASME S T: 13,426 lb/in.

2 (Tangential Stress) Boiler and Pressure Vessel Code, Design pressure and temperature Section VIII, Appendix II, except Gasket load that the stem operational load and Stem operational load seismic loads shall be included in Seismic Loads - the total load carried by the flange.

Design Basis The horizontal and vertical seismic Earthquake forces shall be applied at the mass center of the valve operator as- Flange Stress Limits; suming that the valve body is rigid.

S H ,S R ,S T: S m per ASME Boiler and Pres- sure Vessel Code,Section VIII, Appendix II, 1968 Edition.

4. Valve Operator Support Bolts The valve assembly is analyzed assum- S b allowable = 20,000 lb/in.

2 ing that the valve body is an anchored, Loads: rigid mass and that the specified vertical and horizontal seismic forces Design pressure and temperature are applied at the mass center of the Stem operational load operator assembly, simultaneously with Equipment dead weight operating pressure plus dead weight Seismic load - plus operational loads. Using these Design Basis loads, stresses and deflections are Earthquake determined for the operator support components. Yoke and Yoke Bolt Stress Limits:

Allowable working stress per ASME Section VIII.

BFN-27 Sheet 1 of 1 TABLE C.5-1 DRYWELL-LOADING CONDITIONS AND ALLOWABLE STRESSES Loading Allowable Stress Intensity (ksi) Condition Loading Components (Notes 1 and 2)

Initial and Final Dead Loads P m < S m = 17.5 Test Condition Test Pressure P L < 1.5 S m = 26.3 Vent Thrusts P L + P b < 1.5 S m = 26.3 OBE P L + P b + Q < 3.0 S m = 52.5 Normal and Upset Dead Loads P m < S m = 17.5 Operating Condition Vent Thrusts P L < 1.5 S m = 26.3 OBE P L + P b < 1.5 S m = 26.3 Accident Temperature P L + P b + Q < 3.0 S m = 52.5 Accident Pressure Emergency Condition Dead Loads Region not Backed by Concrete (Note 3) Accident Pressure P m < 0.9 S y = 30.3 Accident Temperature P L < 0.9 S y = 30.3 Vent Thrusts OBE Region Backed by Concrete Jet Loads P m < S y = 33.7 P L < 1.5S y = 50.6 Flooded Condition Dead Loads P m < S y = 38.0 Hydrostatic Pressure P L < S y = 38.0 From Flooded DryWell P L + P b < S u = 70.0 DBE P L + P b + Q < S u = 70.0 NOTE: 1. Stress intensities are based on ASME Boiler and Pressure Vessel Code, Se ction III, Subsection B of Reference 17.

2. Definition of symbols are as follows: P m = Primary membrane stress, P L = Primary local membrane stress, P b = Primary bending stress, Q = secondary stress.
3. The 1965 ASME Code does not address accident conditions. Therefore, this design criteria utilizes the 1968 ASME Code with addenda through the summer of 1969 to establish design allowables for the accident condition for that portion of the vessel backed by concrete.