ML19290E583: Difference between revisions

From kanterella
Jump to navigation Jump to search
(Created page by program invented by StriderTol)
 
(Created page by program invented by StriderTol)
Line 20: Line 20:
Attachment 1 Safety Evaluation for Preposed Technical Specifications Chance : o. 28 North Anna Power Station Unit No. 1 suos e 2 3 6
Attachment 1 Safety Evaluation for Preposed Technical Specifications Chance : o. 28 North Anna Power Station Unit No. 1 suos e 2 3 6


. .
SAFETY lliALYSIS FOR REVISED CONTROL ROD INSERTION LIMITS FOR NORTil ANNA CMIT 1 1.0 Introduction and Summary A quadrant power tilt ana localized power distribution asymmetry was observed during the later portions of North Anna Unit 1, Cycle 1 operation. A safety assessment was made and no adverse impact on continued operations was predicted. The characterization of this quadrant power tilt and potential mechanisms causing the tilt were discussed with Nuclear Regulatory Commission Staf f personnel on August 21, 1979. During the refueling for Cycle 2, the fuel, burnable poison, and control rods were inspected and no anomalies were observed.      In addition, analytical investigations were undertaken to better understand and represent the observed end of Cycle 1 tilt and to assess any impact on Cycle 2.      The result of these investigations was that no significant impact was pre-dicted for Cycle 2.
SAFETY lliALYSIS FOR REVISED CONTROL ROD INSERTION LIMITS FOR NORTil ANNA CMIT 1 1.0 Introduction and Summary A quadrant power tilt ana localized power distribution asymmetry was observed during the later portions of North Anna Unit 1, Cycle 1 operation. A safety assessment was made and no adverse impact on continued operations was predicted. The characterization of this quadrant power tilt and potential mechanisms causing the tilt were discussed with Nuclear Regulatory Commission Staf f personnel on August 21, 1979. During the refueling for Cycle 2, the fuel, burnable poison, and control rods were inspected and no anomalies were observed.      In addition, analytical investigations were undertaken to better understand and represent the observed end of Cycle 1 tilt and to assess any impact on Cycle 2.      The result of these investigations was that no significant impact was pre-dicted for Cycle 2.
However, during the low power physics testing of North Anna 1, Cycle 2, che local power distribution and reactivity in the southwest quadrant were determined to be significantly greater than those of the other quadrants in the core. Further, measurements of radial peaking f actors at very low core power levels indicated that adjustments to the control rod insertion limits were needed in order to maintain F aH          "
However, during the low power physics testing of North Anna 1, Cycle 2, che local power distribution and reactivity in the southwest quadrant were determined to be significantly greater than those of the other quadrants in the core. Further, measurements of radial peaking f actors at very low core power levels indicated that adjustments to the control rod insertion limits were needed in order to maintain F aH          "
Line 26: Line 25:
Additional analytical simulation of the tilted condition in Cycle 2 was performed in order to a) provide a basis for revising the control rod insertion limits and b)        generate core physics input re-quired to support a safety evaluation of the impact of the power tilt on the postulated accidents presented in Chapter 15 of the FSAR.      Based on this analytical simulation, a new and very conservative set of control
Additional analytical simulation of the tilted condition in Cycle 2 was performed in order to a) provide a basis for revising the control rod insertion limits and b)        generate core physics input re-quired to support a safety evaluation of the impact of the power tilt on the postulated accidents presented in Chapter 15 of the FSAR.      Based on this analytical simulation, a new and very conservative set of control


. .
rod insertion limits was developed and administratively imposed. These new limits were verified by measurement at several power levels during the unit startup physics testing program. In addition, these newly in-posed limits were developed consistent with the commitment made in Reference 1.
rod insertion limits was developed and administratively imposed. These new limits were verified by measurement at several power levels during the unit startup physics testing program. In addition, these newly in-posed limits were developed consistent with the commitment made in Reference 1.
The remaining sections present a summary of both the results of the analytical Cycle 2 flux tilt simulation, and the evaluation per-formed to assess the impact of the core tilt and the proposed control rod insertion limits on the conclusions stated in the FSAR regarding core safety. It has been concluded, based on this safety assessment, that the presence of the observed and predicted core tilt in Cycle 2 does not invalidate the conclusions presented in the FSAR. In addition, a company task force has been established to continue to investigate the basic underlying causes for the observed tilt.
The remaining sections present a summary of both the results of the analytical Cycle 2 flux tilt simulation, and the evaluation per-formed to assess the impact of the core tilt and the proposed control rod insertion limits on the conclusions stated in the FSAR regarding core safety. It has been concluded, based on this safety assessment, that the presence of the observed and predicted core tilt in Cycle 2 does not invalidate the conclusions presented in the FSAR. In addition, a company task force has been established to continue to investigate the basic underlying causes for the observed tilt.
Line 34: Line 32:
To represent the effect of the end of Cycle 1 burnup asymmetry on Cycle 2, a full core shuffle was made.      Then, full core Cycle 2 calcu-lations at various power and burnup conditions were made assuming that the thermal imbalance still existed.      The quadrant power tilts calculated with this model are compared to tne measured tilts during the Cycle 2 power ascension in Table 2.    (Note that all of the values in Table 2 are average quadrant tilts. The maximum measured tilt values, which are compared to the Technical Specifications limits, are based on octants where the core is represented in radial quadrants and divided into octants by the core midplane).
To represent the effect of the end of Cycle 1 burnup asymmetry on Cycle 2, a full core shuffle was made.      Then, full core Cycle 2 calcu-lations at various power and burnup conditions were made assuming that the thermal imbalance still existed.      The quadrant power tilts calculated with this model are compared to tne measured tilts during the Cycle 2 power ascension in Table 2.    (Note that all of the values in Table 2 are average quadrant tilts. The maximum measured tilt values, which are compared to the Technical Specifications limits, are based on octants where the core is represented in radial quadrants and divided into octants by the core midplane).


.
The calculated quadrant power tilts during the Cycle 2 deple-tion at full power are presented in Table 3.      As shown in this table, the full power tilts are less than 1% during the depletion through Cycle 2.
The calculated quadrant power tilts during the Cycle 2 deple-tion at full power are presented in Table 3.      As shown in this table, the full power tilts are less than 1% during the depletion through Cycle 2.
Th is table also includes tilt values calculated during a power coastdown of Cycle 2 which is allowed for in the Cycle 2 reload safety evaluation (Reference 2).
Th is table also includes tilt values calculated during a power coastdown of Cycle 2 which is allowed for in the Cycle 2 reload safety evaluation (Reference 2).
Line 41: Line 38:
: 2. The major dif ference between the results generated with the Westinghouse and Vepco models was a larger tilt projected by Westinghouse at hot zero power, end of Cycle 2. The Westinghouse analytical model, which included the impact of this larger tilt, was used to evaluate the impact of the observed and projected tilt on the safety analysis parameters as discussed in the following sections. Westinghouse concluded, based on their review, that the use of their analytical representation of the tilt for the safety evaluation would bound the inpact of results obtained with the Vepco model.
: 2. The major dif ference between the results generated with the Westinghouse and Vepco models was a larger tilt projected by Westinghouse at hot zero power, end of Cycle 2. The Westinghouse analytical model, which included the impact of this larger tilt, was used to evaluate the impact of the observed and projected tilt on the safety analysis parameters as discussed in the following sections. Westinghouse concluded, based on their review, that the use of their analytical representation of the tilt for the safety evaluation would bound the inpact of results obtained with the Vepco model.


                                                                        .
3.0 Imoact on Core Safety An explicit assessment of the impact of the observed (beginning of life) and analytically predicted (end of life) Cycle 2 core power tilt on all of the accidents postulated in Chapter 15 of the FSAR (Reference 4) has been made. This assessment assumes operation within the revised control rod insertion limits shown in Figure 1.        In addition, the impact of a postulated coolant flow and temperature imbalance (a potential cause of the tilt) was determined.
3.0 Imoact on Core Safety An explicit assessment of the impact of the observed (beginning of life) and analytically predicted (end of life) Cycle 2 core power tilt on all of the accidents postulated in Chapter 15 of the FSAR (Reference 4) has been made. This assessment assumes operation within the revised control rod insertion limits shown in Figure 1.        In addition, the impact of a postulated coolant flow and temperature imbalance (a potential cause of the tilt) was determined.
3.1 Impact of Core Power Tilt Core physics analyses have demonstrated that the observed and predicted flux asymmetry will have negligible impact on core average reactivity parameters (e.g., temperature coefficients and control rod bank worths). These conclusions have been confirmed by startup physics test results. Calculations have also indicated that core peaking factors associated with routine steady state operation over the power range will remain within appropriate design limits.      This conclusion has been supported by all core power distribution measurements performed to date.
3.1 Impact of Core Power Tilt Core physics analyses have demonstrated that the observed and predicted flux asymmetry will have negligible impact on core average reactivity parameters (e.g., temperature coefficients and control rod bank worths). These conclusions have been confirmed by startup physics test results. Calculations have also indicated that core peaking factors associated with routine steady state operation over the power range will remain within appropriate design limits.      This conclusion has been supported by all core power distribution measurements performed to date.
Since F H w      e ma n a ne wt n        e ec n cal Specifications limits with the proposed control rod insertion limits, the basis assumed in the safety analysis for transients sensitive to F          (e.g., rod with-g drawal and loss of flow) remains valid.      The remaining potential core physics related impact of the tilt concerns the reactivity worth cf postulated stuck, misaligned, dropped and ejected rods and their associated peaking factors. These parameters have a potential impact on core shutdown margin and the following accidents:        all cases of the Rod Ejection Accident (i.e., from HZP and from HFP at BOL and EOL), Rod Misalignment, Dropped Rod, and the Main Steam Line Break Accident.
Since F H w      e ma n a ne wt n        e ec n cal Specifications limits with the proposed control rod insertion limits, the basis assumed in the safety analysis for transients sensitive to F          (e.g., rod with-g drawal and loss of flow) remains valid.      The remaining potential core physics related impact of the tilt concerns the reactivity worth cf postulated stuck, misaligned, dropped and ejected rods and their associated peaking factors. These parameters have a potential impact on core shutdown margin and the following accidents:        all cases of the Rod Ejection Accident (i.e., from HZP and from HFP at BOL and EOL), Rod Misalignment, Dropped Rod, and the Main Steam Line Break Accident.
                  .


The stuck and ejected rod worths and their corresponding local peaking f actors have been examined over the Cycle 2 range of power and core burnup. It has been concluded that even if the current rod insertion limits were used, the observed and predicted flux tilt will have negligible impact on the stuck and ejected rod worths and peaking factors in most cases. This results from the f act that the orientation of the flux tilt (which is along the S.W./N.E. core diagonal) is such that the limiting locations for stuck and ejected rods for this cycle (i.e. ,
The stuck and ejected rod worths and their corresponding local peaking f actors have been examined over the Cycle 2 range of power and core burnup. It has been concluded that even if the current rod insertion limits were used, the observed and predicted flux tilt will have negligible impact on the stuck and ejected rod worths and peaking factors in most cases. This results from the f act that the orientation of the flux tilt (which is along the S.W./N.E. core diagonal) is such that the limiting locations for stuck and ejected rods for this cycle (i.e. ,
Line 52: Line 47:
The Main Steam Line break is potentially impacted by increased local peaking factors in the vicinity of the assumed stuck rod and by any decrease in the core shutdown margin. The orientation of the observed flux imbalance is such that the stuck rod worth and local peaking factors in the core location which are most limiting for the Main Steam Line Break accident are not significantly impacted.      The Technical Specifications shutdown margin requirement has been confirmed for Cycle 2.      Thus, all of the original core physics assumptions made and values of parameters used
The Main Steam Line break is potentially impacted by increased local peaking factors in the vicinity of the assumed stuck rod and by any decrease in the core shutdown margin. The orientation of the observed flux imbalance is such that the stuck rod worth and local peaking factors in the core location which are most limiting for the Main Steam Line Break accident are not significantly impacted.      The Technical Specifications shutdown margin requirement has been confirmed for Cycle 2.      Thus, all of the original core physics assumptions made and values of parameters used


.
in the safety analysis for this accident remain valid.
in the safety analysis for this accident remain valid.


.
3.2 Impact of a Postulated Core Thermal / Hydraulic Imbalance While a detailed review of plant performance data is underway, preliminary results indicate only a small loop thermal-hydraulic imbalance.
3.2 Impact of a Postulated Core Thermal / Hydraulic Imbalance While a detailed review of plant performance data is underway, preliminary results indicate only a small loop thermal-hydraulic imbalance.
However, the impact of a significant flow imbalance (% 6%) and the associated temperature imbalance on the thermal-hydraulic bases of the safety analysis has also been evaluated.      Thermal hydraulic imbalances have a potential i= pact on postulated transients which result from changes in primary coolant system flow rate (such as a Complete Loss of Flow, or Locked Rotor and the loss of offsite power Main Steam Line Break (MSLB) t rans ient cases). The mixing assumptions for the MSLB are also potentially affected. In addition, the core thermal limit curves, which form the basis for some reactor protection system setpoints (:    1 particular, the overpower and overtemperature LT trips), are potentially impacted by a thermal-hydraulic imbalance.
However, the impact of a significant flow imbalance (% 6%) and the associated temperature imbalance on the thermal-hydraulic bases of the safety analysis has also been evaluated.      Thermal hydraulic imbalances have a potential i= pact on postulated transients which result from changes in primary coolant system flow rate (such as a Complete Loss of Flow, or Locked Rotor and the loss of offsite power Main Steam Line Break (MSLB) t rans ient cases). The mixing assumptions for the MSLB are also potentially affected. In addition, the core thermal limit curves, which form the basis for some reactor protection system setpoints (:    1 particular, the overpower and overtemperature LT trips), are potentially impacted by a thermal-hydraulic imbalance.
Line 62: Line 55:
The Main Steam Line Break transient could potentially be impacted by an initial flow imbalance due to changed flow coastdown characteristics and flow mixing assumptions. Both potential impacts have been assessed and
The Main Steam Line Break transient could potentially be impacted by an initial flow imbalance due to changed flow coastdown characteristics and flow mixing assumptions. Both potential impacts have been assessed and


. .
found to be negligible and therefore, the current Main Steam Line Break analyses remain conservative.
found to be negligible and therefore, the current Main Steam Line Break analyses remain conservative.
These evaluations have demonstrated that the impact of a potential loop flow and temperature imbalance for North Anna Unit ' does not invalidate the conclusions of the FS AR, provided the flow in all loops is equal to the thermal design flow or greater. As discussed previously, measurements indicate substantial cargins to the thermal design flow rate in all loops.
These evaluations have demonstrated that the impact of a potential loop flow and temperature imbalance for North Anna Unit ' does not invalidate the conclusions of the FS AR, provided the flow in all loops is equal to the thermal design flow or greater. As discussed previously, measurements indicate substantial cargins to the thermal design flow rate in all loops.
Line 69: Line 61:
Si gnif ic an t changes in the value of tilt will be detectable by the EXCORE and INCORE monitoring sys tems.
Si gnif ic an t changes in the value of tilt will be detectable by the EXCORE and INCORE monitoring sys tems.


.
   ".0 References
   ".0 References
: 1. Letter from C. M. Stallings (Vepco) to H. R. Denton (NRC),
: 1. Letter from C. M. Stallings (Vepco) to H. R. Denton (NRC),
Line 80: Line 71:
NS-TMA-2167, November 28, 1979.
NS-TMA-2167, November 28, 1979.


  .
Figure 1 FULLY WITEDPEG 228 ,'                            - - - - - -
Figure 1
.
FULLY WITEDPEG
                                                                                                      .
                                                                                ..
                                                                                                            .                  -
                                        -          . ,          , .,        ,
228 ,'                            - - - - - -
                                                                          ,
                                                                                           ;      :_-__n g _g= =
                                                                                           ;      :_-__n g _g= =
220 ;                                                                                  -
220 ;                                                                                  -
_              _
_-              .
_.
5
5
              .
               ;                                                                                  ,
               ;                                                                                  ,
                                                                                                                 .=.            ..
                                                                                                                 .=.            ..
p 200
p 200 (1.194)k              -
              !
(1.194)k              -
t r                                                                                                                    -----
t r                                                                                                                    -----
180 ;
180 ;
Line 109: Line 85:
5                                                                                        y                                      :
5                                                                                        y                                      :
               ),                                                                                    '
               ),                                                                                    '
                                                                                            ',-                                  .              .
160                                                                        /
160                                                                        /
                                                                                        -
                                                                                                                                                  '
l
l
                -
                                                                                -
                '                                                              -
                                                                            -
                                                                      -
                >
                                                                 /                                        -                              ---
                                                                 /                                        -                              ---
     --  140                                                                            --
     --  140                                                                            --
5
5 t
    -
n                                    -
t n                                    -
f'                    BANS D                                                              ,
f'                    BANS D                                                              ,
H
H s'
                '
                ,
s'
     ~                                    /                                                                                                -
     ~                                    /                                                                                                -
     "  120 6
     "  120 6
                                    -
                                      '
9
9
    -
                 ;
                 ;
                              ,-
                                -'                                                                                              -
                                                                                                                                                  -
e c          1      '
e c          1      '
                          -                                                                                                -
p          h 100    '  '
p          h 100    '  '
G                                                                                                                           *
G
                                                                                                                                              "
* _          C'    (0, 100)
_          C'    (0, 100)
     ;;
     ;;
n          s
n          s
                    -
_.          ..          _
                                                                                                                                                  ,
     =          >
     =          >
5    SO r            .                        -_                                                            ___ _ _.                        .
5    SO r            .                        -_                                                            ___ _ _.                        .
c          )                                                                                  -                      _
c          )                                                                                  -                      _
9
9 r                                                                                        .
    -
:
r                                                                                        .
_
60 ;
60 ;
i t    _
i t    _
                                                                                                                                                  -
_.
                                                                                                                                                -
                 ,  ==
                 ,  ==
40 r          -
40 r          -
                                                                                                                                          -
s,                                                                                                                      -.-
s,                                                                                                                      -.-
t                                                                                                -
t                                                                                                -
* t
* t P
                                                                                                                                          --
90
P 90
          .      ,                                                                                                                _
                 ;r                                                                                                                        .-_.
                 ;r                                                                                                                        .-_.
                  .
a                                                                    _
a                                                                    _
                  -              ,                                                                                      --
                                                        - . - - - - -                    --...              --
_
0        .1      .2        .3          4            .5        .6          .7            .3            .9            1.0 FULLY INSERTED FRACTION OF RATED THEFF.AL POWER Fi;ura 3.1-1 Rod Group Insertion Limits Versus Thermal Po<ier NORTH AN':A-UNIT 1                                        3/4 1-26
0        .1      .2        .3          4            .5        .6          .7            .3            .9            1.0 FULLY INSERTED FRACTION OF RATED THEFF.AL POWER Fi;ura 3.1-1 Rod Group Insertion Limits Versus Thermal Po<ier NORTH AN':A-UNIT 1                                        3/4 1-26
                                                                                                                .


.
TABLE 1 CALCULATED AND MEASURED SUADRANT BURNUP TILT NORTN ANNA. UNIT NO. 1. CYCLE 1 Calculated Tilt    (%)
TABLE 1 CALCULATED AND MEASURED SUADRANT BURNUP TILT NORTN ANNA. UNIT NO. 1. CYCLE 1 Calculated Tilt    (%)
Core Average                Measured        (Temperature Burnup          Sundrant    Tilt (%)        Imbalance 6 F) 15900              SW        -
Core Average                Measured        (Temperature Burnup          Sundrant    Tilt (%)        Imbalance 6 F) 15900              SW        -
Line 190: Line 126:
0.1
0.1


.                                    TABLE 2 CALCULATED AND MEASURED QUADRANT POWER TILT RAMP UP TO POWER NORTH ANNA UNIT NO. 1, CYCLE 2
.                                    TABLE 2 CALCULATED AND MEASURED QUADRANT POWER TILT RAMP UP TO POWER NORTH ANNA UNIT NO. 1, CYCLE 2 Calculated Calculated                                          Tilt (%)      -
                        *    *        *
              '
* Calculated Calculated                                          Tilt (%)      -
Core Average                            Measured    (Temperature Burnup              Power  Quadrant    Tilt (%)    Imbalanc 6 P) 0                    0        SW        + 8.1        + 6.0 NE        - 8.6        - 5.4 MW        + 0.6        - 2.3 SE        -
Core Average                            Measured    (Temperature Burnup              Power  Quadrant    Tilt (%)    Imbalanc 6 P) 0                    0        SW        + 8.1        + 6.0 NE        - 8.6        - 5.4 MW        + 0.6        - 2.3 SE        -
0.1        + 1.7 0                    3        SW        + 7.4        + 5.8 NE        - 7.6        - 5.2 NW        - 0.4        -
0.1        + 1.7 0                    3        SW        + 7.4        + 5.8 NE        - 7.6        - 5.2 NW        - 0.4        -
Line 201: Line 134:
2.3      - 1.7 NW        - 0.5        -
2.3      - 1.7 NW        - 0.5        -
0.8 SE        + 0.3        + 0.5 200 hrs            50        SW        + 2.1        +  1.6 NE        - 1.9        -  1.4 NW        -
0.8 SE        + 0.3        + 0.5 200 hrs            50        SW        + 2.1        +  1.6 NE        - 1.9        -  1.4 NW        -
0.3      -  0.7 SE        + 0.1        +  0.4
0.3      -  0.7 SE        + 0.1        +  0.4 250 hrs            50        SW                    + 1.4 NE                    - 1.2 MW                    - 0.6 SE                    + ,0 . 4 300 hrs            100        SW        + 0.9        + 0.9 NE        - 0.7        -
                                                  '
250 hrs            50        SW                    + 1.4
                -
NE                    - 1.2 MW                    - 0.6 SE                    + ,0 . 4 300 hrs            100        SW        + 0.9        + 0.9 NE        - 0.7        -
0.4 MW        - 0.2        - 0.8 SE        -
0.4 MW        - 0.2        - 0.8 SE        -
0.1      + 0.3
0.1      + 0.3


.  .
.
.                                    TABLE 3 CALCULATED  QUADRANT POWER TILT DEPLETION THROUGH CYCLE 2 NORTH ANNA UNIT NO. 1, CYCLE 2 Core Average                                  il  I I Burnup(MMD/MTU) Power    2uadrant            Imb  an ce r) 1000            100        SW                + 0.1 NE                - 0.1 MM                - 0.1 SE                + 0.1 2000            100        SW                + 0.5 NE                - 0.5 NW                - 0.2 SE                + 0.2 4000            100        SW                - 0.5 NE                + 0.4 MW                + 0.2 SE                - 0.1 6000            100        SW                -
.                                    TABLE 3 CALCULATED  QUADRANT POWER TILT DEPLETION THROUGH CYCLE 2 NORTH ANNA UNIT NO. 1, CYCLE 2 Core Average                                  il  I I Burnup(MMD/MTU) Power    2uadrant            Imb  an ce r) 1000            100        SW                + 0.1 NE                - 0.1 MM                - 0.1 SE                + 0.1 2000            100        SW                + 0.5 NE                - 0.5 NW                - 0.2 SE                + 0.2 4000            100        SW                - 0.5 NE                + 0.4 MW                + 0.2 SE                - 0.1 6000            100        SW                -
0.1 NE                + 0.1 MW                + 0.1 SF                + 0.0 8000            100        SW                - 0.8 NE                + 0.6 NW                + 0.3 SE                - 0.1 8900            100        SW                - 0.4 NE                + 0.2 NW                + 0.2 SE                - 0.1 9400            100        SW                - 0.8 NE                + 0.6 NW                + 0.3 SE                - 0.1
0.1 NE                + 0.1 MW                + 0.1 SF                + 0.0 8000            100        SW                - 0.8 NE                + 0.6 NW                + 0.3 SE                - 0.1 8900            100        SW                - 0.4 NE                + 0.2 NW                + 0.2 SE                - 0.1 9400            100        SW                - 0.8 NE                + 0.6 NW                + 0.3 SE                - 0.1
                                            .


.
.                            TABLE 3 (Continued)
.                            TABLE 3 (Continued)
Tilt (%)
Tilt (%)
Line 221: Line 146:
0.1 MW                  + 0.0 SE                  - 0.0 10400              0      SW                  +  7.0 NE                  -  6.2 HW                  -  2.4 SE                  +  1.6
0.1 MW                  + 0.0 SE                  - 0.0 10400              0      SW                  +  7.0 NE                  -  6.2 HW                  -  2.4 SE                  +  1.6


    ,
.
.
TABLE 4 CALCULATED WITH NO TEMPERATURE IMBALANCE IN CYCLE 2 AND MEASURED QUADRANT POWER TILT NORTH ANNA UNIT NO. 1, CYCLE 2 Calculated Core Average                            Measured  Calculated BurnuP              Power    2uadrant  Tilt (%)  Tilt (%)
TABLE 4 CALCULATED WITH NO TEMPERATURE IMBALANCE IN CYCLE 2 AND MEASURED QUADRANT POWER TILT NORTH ANNA UNIT NO. 1, CYCLE 2 Calculated Core Average                            Measured  Calculated BurnuP              Power    2uadrant  Tilt (%)  Tilt (%)
0                    3          SW      + 7.4      + 5.P NE      - 7.6      - 5.2 NW      - 0.4      - 2.2 SE      + 0.6      + 1.7 30 hrs              30          SW                  + 3.7 NE                  -
0                    3          SW      + 7.4      + 5.P NE      - 7.6      - 5.2 NW      - 0.4      - 2.2 SE      + 0.6      + 1.7 30 hrs              30          SW                  + 3.7 NE                  -

Revision as of 15:09, 1 February 2020

Proposed Tech Specs Change 28 Consisting of Page 1-26 Re Rod Group Insertion Limits Vs Thermal Power.Safety Evaluation & Related Data Encl
ML19290E583
Person / Time
Site: North Anna Dominion icon.png
Issue date: 03/11/1980
From:
VIRGINIA POWER (VIRGINIA ELECTRIC & POWER CO.)
To:
Shared Package
ML19290E579 List:
References
NUDOCS 8003140236
Download: ML19290E583 (20)


Text

. .

Attachment 1 Safety Evaluation for Preposed Technical Specifications Chance : o. 28 North Anna Power Station Unit No. 1 suos e 2 3 6

SAFETY lliALYSIS FOR REVISED CONTROL ROD INSERTION LIMITS FOR NORTil ANNA CMIT 1 1.0 Introduction and Summary A quadrant power tilt ana localized power distribution asymmetry was observed during the later portions of North Anna Unit 1, Cycle 1 operation. A safety assessment was made and no adverse impact on continued operations was predicted. The characterization of this quadrant power tilt and potential mechanisms causing the tilt were discussed with Nuclear Regulatory Commission Staf f personnel on August 21, 1979. During the refueling for Cycle 2, the fuel, burnable poison, and control rods were inspected and no anomalies were observed. In addition, analytical investigations were undertaken to better understand and represent the observed end of Cycle 1 tilt and to assess any impact on Cycle 2. The result of these investigations was that no significant impact was pre-dicted for Cycle 2.

However, during the low power physics testing of North Anna 1, Cycle 2, che local power distribution and reactivity in the southwest quadrant were determined to be significantly greater than those of the other quadrants in the core. Further, measurements of radial peaking f actors at very low core power levels indicated that adjustments to the control rod insertion limits were needed in order to maintain F aH "

the limits required by the Technical Specifications.

Additional analytical simulation of the tilted condition in Cycle 2 was performed in order to a) provide a basis for revising the control rod insertion limits and b) generate core physics input re-quired to support a safety evaluation of the impact of the power tilt on the postulated accidents presented in Chapter 15 of the FSAR. Based on this analytical simulation, a new and very conservative set of control

rod insertion limits was developed and administratively imposed. These new limits were verified by measurement at several power levels during the unit startup physics testing program. In addition, these newly in-posed limits were developed consistent with the commitment made in Reference 1.

The remaining sections present a summary of both the results of the analytical Cycle 2 flux tilt simulation, and the evaluation per-formed to assess the impact of the core tilt and the proposed control rod insertion limits on the conclusions stated in the FSAR regarding core safety. It has been concluded, based on this safety assessment, that the presence of the observed and predicted core tilt in Cycle 2 does not invalidate the conclusions presented in the FSAR. In addition, a company task force has been established to continue to investigate the basic underlying causes for the observed tilt.

2. 0 Analytical Simulation of the North Anna Tilt Analytical simulation of the quadrant burnup asymmetry which existed at the end of North Anna Unit 1, Cycle 1, indicates that this burnup asymmetry is the basic caure of the tilt observed in Cycle 2.

This has been established by Cycle 2 full core calculations which are based on the actual TOTE measured burnups at the end of Cycle 1 and which show a quadrant tilt in Cycle 2 similar to the measured quadrant tilt.

This end of Cycle 1 burnup asymmetry can be accurately simulated by a full core depletion through Cycle 1 with a thermal imbalance between the reactor coolant loops (i.e., higher moderator temperature in Loop "A") represented in the depletion models. Table 1 compares the burnup tilt produced with an analytical simulation of a 6 F thermal imbalance with the measured burnup asymmetry at the end of Cycle 1 (This analytical simulation also produces a quadrant power tilt). A thermal imbalance produces a quadrant reactivity and power imbalance which increases in magnitude with burnup due to the isothermal temperature coef ficient becoming more negative. This type of phenomenon was generally observed in Cycle 1.

To represent the effect of the end of Cycle 1 burnup asymmetry on Cycle 2, a full core shuffle was made. Then, full core Cycle 2 calcu-lations at various power and burnup conditions were made assuming that the thermal imbalance still existed. The quadrant power tilts calculated with this model are compared to tne measured tilts during the Cycle 2 power ascension in Table 2. (Note that all of the values in Table 2 are average quadrant tilts. The maximum measured tilt values, which are compared to the Technical Specifications limits, are based on octants where the core is represented in radial quadrants and divided into octants by the core midplane).

The calculated quadrant power tilts during the Cycle 2 deple-tion at full power are presented in Table 3. As shown in this table, the full power tilts are less than 1% during the depletion through Cycle 2.

Th is table also includes tilt values calculated during a power coastdown of Cycle 2 which is allowed for in the Cycle 2 reload safety evaluation (Reference 2).

As was discussed previously, a temperature imbalance was assumed for the calculations presented in Tables 1, 2 and 3. Calculations of the Cycle 2 tilt based on the Cycle 1 burnup asymmetry with no thermal imbalance are presented in Table 4. These results give a power tilt which was slightly larger at the beginning of Cycle 2 (1. 7% at full power compared to 0.9% with the thermal imbalance), but which drops of f rapidly in magnitude with depletion through Cycle 2.

The cniculations presented in this section were performed with the Vepco one zone dif fusion theory model (Reference 3). Independent calculations were also performed by Westinghouse and their analytical results were comparable to the Vepco model results. The methodolcgy used in the Westinghouse calculation was to determine the impact of the tilt with a full core nodal model and then apply the impact to the discrete symmetric diffusion theory analysis originally used to develop Reference

2. The major dif ference between the results generated with the Westinghouse and Vepco models was a larger tilt projected by Westinghouse at hot zero power, end of Cycle 2. The Westinghouse analytical model, which included the impact of this larger tilt, was used to evaluate the impact of the observed and projected tilt on the safety analysis parameters as discussed in the following sections. Westinghouse concluded, based on their review, that the use of their analytical representation of the tilt for the safety evaluation would bound the inpact of results obtained with the Vepco model.

3.0 Imoact on Core Safety An explicit assessment of the impact of the observed (beginning of life) and analytically predicted (end of life) Cycle 2 core power tilt on all of the accidents postulated in Chapter 15 of the FSAR (Reference 4) has been made. This assessment assumes operation within the revised control rod insertion limits shown in Figure 1. In addition, the impact of a postulated coolant flow and temperature imbalance (a potential cause of the tilt) was determined.

3.1 Impact of Core Power Tilt Core physics analyses have demonstrated that the observed and predicted flux asymmetry will have negligible impact on core average reactivity parameters (e.g., temperature coefficients and control rod bank worths). These conclusions have been confirmed by startup physics test results. Calculations have also indicated that core peaking factors associated with routine steady state operation over the power range will remain within appropriate design limits. This conclusion has been supported by all core power distribution measurements performed to date.

Since F H w e ma n a ne wt n e ec n cal Specifications limits with the proposed control rod insertion limits, the basis assumed in the safety analysis for transients sensitive to F (e.g., rod with-g drawal and loss of flow) remains valid. The remaining potential core physics related impact of the tilt concerns the reactivity worth cf postulated stuck, misaligned, dropped and ejected rods and their associated peaking factors. These parameters have a potential impact on core shutdown margin and the following accidents: all cases of the Rod Ejection Accident (i.e., from HZP and from HFP at BOL and EOL), Rod Misalignment, Dropped Rod, and the Main Steam Line Break Accident.

The stuck and ejected rod worths and their corresponding local peaking f actors have been examined over the Cycle 2 range of power and core burnup. It has been concluded that even if the current rod insertion limits were used, the observed and predicted flux tilt will have negligible impact on the stuck and ejected rod worths and peaking factors in most cases. This results from the f act that the orientation of the flux tilt (which is along the S.W./N.E. core diagonal) is such that the limiting locations for stuck and ejected rods for this cycle (i.e. ,

on the major core axes) are not significantly af fected. While a potentially significant impact on the HZP, EOL ejected rod worth and peaking factors was identified with use of the current rod insertion limits, the revised rod insertion limits substantially reduce the magnitudes of both parameters for all cases. As a result, the currently applicable analyses of the Rod Ejection Accident remain limiting.

In a similar manner, it has been shown that the radial peaking factors associated with statically misaligned rods are negligibly impacted by the observed Cycle 2 flux tilt. Thus, the safety conclusions of the FSAR regarding this accident remain valid. In addition, an evaluation has been performed which determined that the Westinghouse interim generic position on the Dropped Rod Accident (Reference 5) remains valid.

The Main Steam Line break is potentially impacted by increased local peaking factors in the vicinity of the assumed stuck rod and by any decrease in the core shutdown margin. The orientation of the observed flux imbalance is such that the stuck rod worth and local peaking factors in the core location which are most limiting for the Main Steam Line Break accident are not significantly impacted. The Technical Specifications shutdown margin requirement has been confirmed for Cycle 2. Thus, all of the original core physics assumptions made and values of parameters used

in the safety analysis for this accident remain valid.

3.2 Impact of a Postulated Core Thermal / Hydraulic Imbalance While a detailed review of plant performance data is underway, preliminary results indicate only a small loop thermal-hydraulic imbalance.

However, the impact of a significant flow imbalance (% 6%) and the associated temperature imbalance on the thermal-hydraulic bases of the safety analysis has also been evaluated. Thermal hydraulic imbalances have a potential i= pact on postulated transients which result from changes in primary coolant system flow rate (such as a Complete Loss of Flow, or Locked Rotor and the loss of offsite power Main Steam Line Break (MSLB) t rans ient cases). The mixing assumptions for the MSLB are also potentially affected. In addition, the core thermal limit curves, which form the basis for some reactor protection system setpoints (: 1 particular, the overpower and overtemperature LT trips), are potentially impacted by a thermal-hydraulic imbalance.

Studies of the Loss of Flow transients have shown that flow imbalances of s 6% will result in no DNBR penalty relative to the limiting case, assuming the lowest loor flow is ca less than the thermal design flow. The measured loop and total core flows at North Anna substantially exceed the thermal design value. In addition, the impact of an initial flow imbalance on the Lccked Rotor transient has been investigated and determined to be negligible. In a similar fashion, the impact of a loop flow imbalance on the current core thermal limit curves has been assessed.

It has been concluded that the thermal limits remain adequate and that the overtemperature and overpower AT trip setpoint calibration procedures remain valid.

The Main Steam Line Break transient could potentially be impacted by an initial flow imbalance due to changed flow coastdown characteristics and flow mixing assumptions. Both potential impacts have been assessed and

found to be negligible and therefore, the current Main Steam Line Break analyses remain conservative.

These evaluations have demonstrated that the impact of a potential loop flow and temperature imbalance for North Anna Unit ' does not invalidate the conclusions of the FS AR, provided the flow in all loops is equal to the thermal design flow or greater. As discussed previously, measurements indicate substantial cargins to the thermal design flow rate in all loops.

4.0 Conclusions It has been concluded tnat the presence of the observed and predicted core tilt in North Anna Unit 1, Cycle 2 does not invalidate the conclusions of the FS AR regarding core safety from either a physics or thermal-hydraulics s tandpoint . These conclusions have been based on the assumption that the actual tilt will not significantly exceed those measured to date or predicted to occur under various plant conditions with currently available models. The tilt will be monitored throughout Cycle 2 in order to confirm that the bases of this evaluation remain valid.

Si gnif ic an t changes in the value of tilt will be detectable by the EXCORE and INCORE monitoring sys tems.

".0 References

1. Letter from C. M. Stallings (Vepco) to H. R. Denton (NRC),

Serial No. 973. Docket Nos. 50-338 and 50-339, December 17, 1979.

2. Letter from C. M. Stallings (Vepco) to H. R. Denton (NRC), Serial No. 867, Docket No. 50-338, November 2, 1979.
3. Letter from W. N. Thomas (Vepco) to B. C. Rusche (NRC), Serial No.

Oll, January 25,1977, (VEP-FRD-20, "The PDQ07 One Zone Model, Virginia Electric and Power Company").

4 North Anna Power Station Units 1 and 2, Final Safety Analysis Report, Docket Nos. 50-338 and 50-339, dated January 3, 1973, as amended.

5. Letter from T. M. Anderson (Westinghouse) to A. T. Schwencer (NRC),

NS-TMA-2167, November 28, 1979.

Figure 1 FULLY WITEDPEG 228 ,' - - - - - -

_-__n g _g= =

220 ; -

5

,

.=. ..

p 200 (1.194)k -

t r -----

180 ;

0

.- .-f

/

5 y  :

), '

160 /

l

/ - ---

-- 140 --

5 t

n -

f' BANS D ,

H s'

~ / -

" 120 6

9

e c 1 '

p h 100 ' '

G

  • _ C' (0, 100)

n s

= >

5 SO r . -_ ___ _ _. .

c ) - _

9 r .

60 ;

i t _

, ==

40 r -

s, -.-

t -

  • t P

90

r .-_.

a _

0 .1 .2 .3 4 .5 .6 .7 .3 .9 1.0 FULLY INSERTED FRACTION OF RATED THEFF.AL POWER Fi;ura 3.1-1 Rod Group Insertion Limits Versus Thermal Po<ier NORTH AN':A-UNIT 1 3/4 1-26

TABLE 1 CALCULATED AND MEASURED SUADRANT BURNUP TILT NORTN ANNA. UNIT NO. 1. CYCLE 1 Calculated Tilt (%)

Core Average Measured (Temperature Burnup Sundrant Tilt (%) Imbalance 6 F) 15900 SW -

0.7 -

0.7 NE + 0.8 + 0.5 NW + 0.1 + 0.3 SE -

0.1 -

0.1

. TABLE 2 CALCULATED AND MEASURED QUADRANT POWER TILT RAMP UP TO POWER NORTH ANNA UNIT NO. 1, CYCLE 2 Calculated Calculated Tilt (%) -

Core Average Measured (Temperature Burnup Power Quadrant Tilt (%) Imbalanc 6 P) 0 0 SW + 8.1 + 6.0 NE - 8.6 - 5.4 MW + 0.6 - 2.3 SE -

0.1 + 1.7 0 3 SW + 7.4 + 5.8 NE - 7.6 - 5.2 NW - 0.4 -

2.2 SE + 0.6 + 1.7 10 hrs 3 SW + 5.2 NE - 4.6 NW -

2.1 SE + 1.5 30 hrs 30 SW + 3.4 NE - 3.0 NW -

1.4 SE + 0.9 160 hrs 30 SW 4 2.5 + 2.0 NE -

2.3 - 1.7 NW - 0.5 -

0.8 SE + 0.3 + 0.5 200 hrs 50 SW + 2.1 + 1.6 NE - 1.9 - 1.4 NW -

0.3 - 0.7 SE + 0.1 + 0.4 250 hrs 50 SW + 1.4 NE - 1.2 MW - 0.6 SE + ,0 . 4 300 hrs 100 SW + 0.9 + 0.9 NE - 0.7 -

0.4 MW - 0.2 - 0.8 SE -

0.1 + 0.3

. TABLE 3 CALCULATED QUADRANT POWER TILT DEPLETION THROUGH CYCLE 2 NORTH ANNA UNIT NO. 1, CYCLE 2 Core Average il I I Burnup(MMD/MTU) Power 2uadrant Imb an ce r) 1000 100 SW + 0.1 NE - 0.1 MM - 0.1 SE + 0.1 2000 100 SW + 0.5 NE - 0.5 NW - 0.2 SE + 0.2 4000 100 SW - 0.5 NE + 0.4 MW + 0.2 SE - 0.1 6000 100 SW -

0.1 NE + 0.1 MW + 0.1 SF + 0.0 8000 100 SW - 0.8 NE + 0.6 NW + 0.3 SE - 0.1 8900 100 SW - 0.4 NE + 0.2 NW + 0.2 SE - 0.1 9400 100 SW - 0.8 NE + 0.6 NW + 0.3 SE - 0.1

. TABLE 3 (Continued)

Tilt (%)

Core Average (Temperature Burnup(MWD /MTU) Pouer 2uadrant Imbalannce 6 F) 9600 96 SW - 0.6 NE + 0.4 HW + 0.3 SE - 0.1 9800 87 SW - 0.4 NE + 0.3 NW + 0.2 SE - 0.1 10000 81 SW - 0.2 NE + 0.1 NW + 0.1 SE - 0.0 10200 75 SW - 0.1 NE + 0.0 MW + 0.1 SE - 0.0 10400 70 SW - 0.0 NE -

0.1 MW + 0.0 SE - 0.0 10400 0 SW + 7.0 NE - 6.2 HW - 2.4 SE + 1.6

TABLE 4 CALCULATED WITH NO TEMPERATURE IMBALANCE IN CYCLE 2 AND MEASURED QUADRANT POWER TILT NORTH ANNA UNIT NO. 1, CYCLE 2 Calculated Core Average Measured Calculated BurnuP Power 2uadrant Tilt (%) Tilt (%)

0 3 SW + 7.4 + 5.P NE - 7.6 - 5.2 NW - 0.4 - 2.2 SE + 0.6 + 1.7 30 hrs 30 SW + 3.7 NE -

3.2 NW - 1.4 SE + 1.0 200 hrs 50 SW + 2.1 + 2.1 NE - 1.9 - 1.7 NW - 0.3 - 0.8 SE + 0.1 + 0.5 300 hrs .

100 SW + 0.9 + 1.7 NE - 0.7 - 1.4 MW - 0.2 - 0.7 SE - 0.1 - 0.4 4000 mud /mtu 100 SW + 0.3 NE - 0.2 NW - 0.2 SE - 0.1 10400 mud /mtu 100 SW + 0.4 NE - 0.4 MW - 0.2 SE + 0.1

.