ML18096A623: 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 18: Line 18:
=Text=
=Text=
{{#Wiki_filter:*
{{#Wiki_filter:*
* CDC-92-014 Ref. 1: CDC-91-307 2: PNG-92-005 PEAKING FACTOR LIMIT REPORT EVALUATION FOR SALEM UNIT 2 CYCLE 7 REDESIGN VERIFIER:
* CDC-92-014 Ref. 1: CDC-91-307 2: PNG-92-005 PEAKING FACTOR LIMIT REPORT EVALUATION FOR SALEM UNIT 2 CYCLE 7 REDESIGN L. Green Core Design C                   Date:
L. Green Core Design C (J.O. R.. A. Wiley () Core Design C -----c::--------------,--,, ,r-9204160043 920409 I PDR ADOCK 05000311 p PDR Date: Date:
(J.O. W-~
1 of 3 
VERIFIER:    R.. A. Wiley ( )
*
Core Design C                   Date:    /-/o-'f~
1 of 3
  -----c::- -------------,--,,
,r- 9204160043 920409 I     PDR ADOCK 05000311 p               PDR
 
            *
* RADIAL PEAKING FACTOR LIMIT REPORT This radial Peaking Factor Limit Report is provided in accordance with Paragraph 6.9.l.10 of the Salem Unit 2 Nuclear Plant Technical Specifications.
* RADIAL PEAKING FACTOR LIMIT REPORT This radial Peaking Factor Limit Report is provided in accordance with Paragraph 6.9.l.10 of the Salem Unit 2 Nuclear Plant Technical Specifications.
The Fxy limits for RATED THERMAL POWER within specific core planes for Cycle 7 shall be: 1. For all core planes containing Bank "D" control rods: _RTP r--< 2.26 for all core elevations  
The Fxy limits for RATED THERMAL POWER within specific core planes for Cycle 7 shall be:
',INCORE axial points xy -1 through 61, inclusive).
: 1. For all core planes containing Bank "D" control rods:
: 2. For all unrodded planes: 1-TP < 1.68 for all core elevations (INCORE axial points xy -1 through 61, inclusive).
_RTP r--xy -< 2.26 for all core elevations ',INCORE axial points 1 through 61, inclusive).
These F (z) limits were used to confirm that the heat flux hot xy channel factor FQ(z) will be limited to the Technical Specification values of: F (z) < (2*32] (K( )] f P > 0 5 d Q z . or . an , p FQ(z) (4.64] (K(z)J for P < 0.5 assuming the most limiting axial power distributions expected to result from the insertion and removal of control Banlcs C and D during operation, including the accompanying variations in the axial xenon and power distributions as described in the "Power Distribution Control and Load Following Procedures", WCAP-8385, September, 1974. Therefore, these F limits provide assurance that the initial xy conditions assumed in the I..OCA analysis are met, along the ECCS acceptance criteria of lOCFR.50.46.  
: 2. For all unrodded planes:
*T See Figure 1 for a plot of (FQ PRel] versus Axial. Core Height. 2 of 3
1-TP < 1.68 for all core elevations (INCORE axial points xy -
--------------* * **-'* ' ._,' L I I I r 11 6, 2. 321 i I I ! I ! ' ' -I 1 2 .... I I 1 I ! .........  
1 through 61, inclusive).
.._ 2. 2 I CIC I I r ,, . I\ 10.8,2. 181 I ll '' I I I c : I ' c c c ... .. r"l*C C ape M CJ C CJ I CCC cc *-I ; .... i :I ,., I -2.0 I I I -I I I I I ! i ! --:.1. 8 . I ; I : ! Cl a i I ! \ ' ; I ! ' \ ! i I : I I i I I I I : I I ! 12, 1.5 : I i ! i I 1.4 ' ' ! I I I i c I I I ! I .. i I ' 1.2 i I I .1 ! I I I : 2 4 6 8 10 12 CORE 1&#xa3; I GHT (FEET) FICUU 1 T MAXIMUM (FQ
These F (z) limits were used to confirm that the heat flux hot xy channel factor FQ(z) will be limited to the Technical Specification values of:
32 F (z) < ( 2 * ]     (K( z )]. f or  P > 0 . 5 and ,
Q           p FQ(z) ~ (4.64]     (K(z)J   for P < 0.5 assuming the most limiting axial power distributions expected to result from the insertion and removal of control Banlcs C and D during operation, including the accompanying variations in the axial xenon and power distributions as described in the "Power Distribution Control and Load Following Procedures", WCAP-8385, September, 1974.
Therefore, these F         limits provide assurance that the initial xy conditions assumed in the I..OCA analysis are met, along w~th the ECCS acceptance criteria of lOCFR.50.46.
                                  *T See Figure 1 for a plot of (FQ           PRel] versus Axial. Core Height.
2 of 3
 
                                                                                                  *
- - - - - - - - -- - - - -
  **-'* ' ._,' L
* 2....
I         I I       r             11 6, 2. 321                         i I           I             !
I         !
                                                      '
                                                          '
                                                                                  -                             I                           1 I         I       1                               ~
                                                                                                ......... .._   I                            !
I CIC               I                 I                                 ~
: 2. 2
                                      ~
                                            ~
                                              ,,                                     .                                               r I \ 10.8,2. 181 I
I ll                                                                                           I
                                  ' c I             c c c ...
:
                                                                .. r"l*C C ape CJ I        M   CJ   C   CCC cc
                                                                                                                                  '          I I
2.0        ;
                                                                                      .... ~
i I
                                                                                                                    *-  :I ,.,
                                                                                                                                --           I I                                   I                                       I I
I I             I
                                                                                                                                    ~
                                !                                   i                                       !
I
                                                                      ;                                      I                      :    ~
                  --:.1. 8                                                                                                               Cl
                  ~
                                                                                                              !                                I
                  .         a                                       i                                       !                       '          \
                                ;                                     I                                       !                       '         \
i                                       I
                                                                                                                                                ~'
                                !                                                                                                      :
I                                     I                                       i I
I                                                                             I                       :
I 12, 1.5 I                                                                              I                        !
:                                     I                                       i                       !
1.4
                              '
i                        I I
                              !'                                     I                                       I                       i c I                                     I                                                                 I
                                                                                                                                      !       I ..
1.2 I
                                                                                              ~
i
                              '
i                                                                                                        I I                                                                                                   .1
:
                                !
I                                     I                                       I 2                   4               6                     8             10                           12 CORE 1&#xa3; IGHT (FEET)
FICUU 1 MAXIMUM (FQT
* Pael J VERSUS AXIAL CORE HEIGHT DURING NORMAL OPERATION 3 of 3}}
* Pael J VERSUS AXIAL CORE HEIGHT DURING NORMAL OPERATION 3 of 3}}

Revision as of 11:20, 21 October 2019

Nonproprietary Version of CDC-92-014, Peaking Factor Limit Rept Evaluation for Salem Unit 2 Cycle 7 Redesign.
ML18096A623
Person / Time
Site: Salem PSEG icon.png
Issue date: 01/10/1992
From: Green L, Wiley R
WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP.
To:
Shared Package
ML18096A622 List:
References
CDC-92-014, CDC-92-14, NUDOCS 9204160043
Download: ML18096A623 (3)


Text

  • CDC-92-014 Ref. 1: CDC-91-307 2: PNG-92-005 PEAKING FACTOR LIMIT REPORT EVALUATION FOR SALEM UNIT 2 CYCLE 7 REDESIGN L. Green Core Design C Date:

(J.O. W-~

VERIFIER: R.. A. Wiley ( )

Core Design C Date: /-/o-'f~

1 of 3


c::- -------------,--,,

,r- 9204160043 920409 I PDR ADOCK 05000311 p PDR

  • RADIAL PEAKING FACTOR LIMIT REPORT This radial Peaking Factor Limit Report is provided in accordance with Paragraph 6.9.l.10 of the Salem Unit 2 Nuclear Plant Technical Specifications.

The Fxy limits for RATED THERMAL POWER within specific core planes for Cycle 7 shall be:

1. For all core planes containing Bank "D" control rods:

_RTP r--xy -< 2.26 for all core elevations ',INCORE axial points 1 through 61, inclusive).

2. For all unrodded planes:

1-TP < 1.68 for all core elevations (INCORE axial points xy -

1 through 61, inclusive).

These F (z) limits were used to confirm that the heat flux hot xy channel factor FQ(z) will be limited to the Technical Specification values of:

32 F (z) < ( 2 * ] (K( z )]. f or P > 0 . 5 and ,

Q p FQ(z) ~ (4.64] (K(z)J for P < 0.5 assuming the most limiting axial power distributions expected to result from the insertion and removal of control Banlcs C and D during operation, including the accompanying variations in the axial xenon and power distributions as described in the "Power Distribution Control and Load Following Procedures", WCAP-8385, September, 1974.

Therefore, these F limits provide assurance that the initial xy conditions assumed in the I..OCA analysis are met, along w~th the ECCS acceptance criteria of lOCFR.50.46.

  • T See Figure 1 for a plot of (FQ PRel] versus Axial. Core Height.

2 of 3

- - - - - - - - -- - - - -

    • -'* ' ._,' L
  • 2....

I I I r 11 6, 2. 321 i I I  !

I  !

'

'

- I 1 I I 1 ~

......... .._ I  !

I CIC I I ~

2. 2

~

~

,, . r I \ 10.8,2. 181 I

I ll I

' c I c c c ...

.. r"l*C C ape CJ I M CJ C CCC cc

' I I

2.0  ;

.... ~

i I

  • - :I ,.,

-- I I I I I

I I I

~

! i  !

I

I
~

--:.1. 8 Cl

~

! I

. a i  ! ' \

I  ! ' \

i I

~'

!  :

I I i I

I I  :

I 12, 1.5 I I  !

I i  !

1.4

'

i I I

!' I I i c I I I

! I ..

1.2 I

~

i

'

i I I .1

!

I I I 2 4 6 8 10 12 CORE 1£ IGHT (FEET)

FICUU 1 MAXIMUM (FQT

  • Pael J VERSUS AXIAL CORE HEIGHT DURING NORMAL OPERATION 3 of 3