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| number = ML18096A664 | | number = ML18096A664 | ||
| issue date = 03/18/1992 | | issue date = 03/18/1992 | ||
| title = Cycle 11 Peaking Factor Limit Rept | | title = Cycle 11 Peaking Factor Limit Rept | ||
| author name = Schmidt J, Wiley R | | author name = Schmidt J, Wiley R | ||
| author affiliation = WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP. | | author affiliation = WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP. | ||
| Line 17: | Line 17: | ||
=Text= | =Text= | ||
{{#Wiki_filter:* CDC-92-076 Ref.: PSK-92-011-0 SALEM UNIT 1 CYCLE 11 PEAKING FACTOR LIMIT REPORT J 1Jffi VERIFIED BY: J. S. Schmidt Core Design C 02-. a . | {{#Wiki_filter:* | ||
R. A. Wiley () Core Design C 9205040299 920424 PDR ADOCK 05000272 P PDR Date: Date: 1 of 3 | CDC-92-076 Ref.: PSK-92-011-0 SALEM UNIT 1 CYCLE 11 PEAKING FACTOR LIMIT REPORT J 1Jffi VERIFIED BY: | ||
J. S. Schmidt Core Design C 02-. a. c;,r~ | |||
The F limits for RATED THERMAL POWER within specific core planes for xy Cycle 11 shall be: 1. For all core planes containing Bank "D" control rods: < 2.28 for all core elevations (INCORE axial points xy -1 through 61, inclusive). | R. A. Wiley | ||
: 2. For all unrodded planes: < 1.67 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: F ( ) < [2. 32] Q z p [K(z)] for P > 0.5 and, [K(z)] for P < 0.5 assuming the most limiting axial power distributions expected to result from the insertion and removal of control Banks 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 LOCA analysis are met, along with the ECCS acceptance criteria of | Core Design C 9205040299 920424 | ||
See Figure 1 for a plot of [FQT . PRel] versus Axial Core Height. 2 of 3 | ~ | ||
PDR ADOCK 05000272 P | |||
PDR Date: | |||
Date: | |||
1 of 3 | |||
RADIAL PEAKING FACTOR LIMIT REPORT This radial Peaking Factor Limit Report is provided in accordance with Paragraph 6.9.1.9 of the Salem Unit 1 Nuclear Plant Technical Specifications. | |||
The F limits for RATED THERMAL POWER within specific core planes for xy Cycle 11 shall be: | |||
: 1. | |||
For all core planes containing Bank "D" control rods: | |||
~TP < 2.28 for all core elevations (INCORE axial points xy - | |||
1 through 61, inclusive). | |||
: 2. | |||
For all unrodded planes: | |||
~TP < 1.67 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: | |||
F ( ) < [2. 32] | |||
Q z p | |||
[K(z)] | |||
for P > 0.5 and, | |||
[K(z)] | |||
for P < 0.5 assuming the most limiting axial power distributions expected to result from the insertion and removal of control Banks 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 LOCA analysis are met, along with the ECCS acceptance criteria of 10CFRS0.46. | |||
See Figure 1 for a plot of [FQT. PRel] versus Axial Core Height. | |||
2 of 3 | |||
'.i 2.4 LI 0.2.32 I I 6.2.32 I r-......... | |||
Cc | |||
-i--.. - | |||
10.82.181 I | |||
-n 2.2 c | |||
~ | |||
UC I" r a ll... | |||
... [ | |||
OL.J | |||
.., '- n c* - | |||
2.0 Cl n | |||
-.;;[ | |||
- \\ | |||
ID | |||
\\ | |||
[ \\ | |||
\\ | |||
Lj 1.8 | |||
... 1 | |||
,E-. | |||
\\ | |||
~ - | |||
~ 1.6 | |||
::II c | |||
\\ | |||
\\ | |||
... \\ | |||
12.1.5 I 1.4 | |||
[] | |||
Cl 1.2 2 | |||
4 6 | |||
8 10 12 CORE HEIGHT (FEET) | |||
FIGURE 1 MAXIMUM CFaT*PRELJ VS AXIAL CORE HEIGHT DURING NORMAL OPERATION 3 of 3}} | |||
Latest revision as of 02:28, 6 January 2025
| ML18096A664 | |
| Person / Time | |
|---|---|
| Site: | Salem |
| Issue date: | 03/18/1992 |
| From: | Jeffrey Schmidt, Wiley R WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP. |
| To: | |
| Shared Package | |
| ML18096A663 | List: |
| References | |
| CDC-92-076, CDC-92-76, PSK-92-011-0, PSK-92-11, NUDOCS 9205040299 | |
| Download: ML18096A664 (3) | |
Text
CDC-92-076 Ref.: PSK-92-011-0 SALEM UNIT 1 CYCLE 11 PEAKING FACTOR LIMIT REPORT J 1Jffi VERIFIED BY:
J. S. Schmidt Core Design C 02-. a. c;,r~
R. A. Wiley
()
Core Design C 9205040299 920424
~
PDR ADOCK 05000272 P
PDR Date:
Date:
1 of 3
RADIAL PEAKING FACTOR LIMIT REPORT This radial Peaking Factor Limit Report is provided in accordance with Paragraph 6.9.1.9 of the Salem Unit 1 Nuclear Plant Technical Specifications.
The F limits for RATED THERMAL POWER within specific core planes for xy Cycle 11 shall be:
- 1.
For all core planes containing Bank "D" control rods:
~TP < 2.28 for all core elevations (INCORE axial points xy -
1 through 61, inclusive).
- 2.
For all unrodded planes:
~TP < 1.67 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:
F ( ) < [2. 32]
Q z p
[K(z)]
for P > 0.5 and,
[K(z)]
for P < 0.5 assuming the most limiting axial power distributions expected to result from the insertion and removal of control Banks 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 LOCA analysis are met, along with the ECCS acceptance criteria of 10CFRS0.46.
See Figure 1 for a plot of [FQT. PRel] versus Axial Core Height.
2 of 3
'.i 2.4 LI 0.2.32 I I 6.2.32 I r-.........
Cc
-i--.. -
10.82.181 I
-n 2.2 c
~
UC I" r a ll...
... [
OL.J
.., '- n c* -
2.0 Cl n
-.;;[
- \\
ID
\\
[ \\
\\
Lj 1.8
... 1
,E-.
\\
~ -
~ 1.6
- II c
\\
\\
... \\
12.1.5 I 1.4
[]
Cl 1.2 2
4 6
8 10 12 CORE HEIGHT (FEET)
FIGURE 1 MAXIMUM CFaT*PRELJ VS AXIAL CORE HEIGHT DURING NORMAL OPERATION 3 of 3