Latest revision as of 19:58, 3 February 2020

Text

Cycle 6 COLR, Rev 1
	ML18011A457
Person / Time
Site:	Harris
Issue date:	04/15/1994
From:	Wells L; CAROLINA POWER & LIGHT CO.
To:	;
Shared Package
ML18011A455	List: ML18011A454; ML18011A457;
References
	NUDOCS 9405260054
	Download: ML18011A457 (26)
	v • d • e

~ ~

Harris Unit 1 Cycle 6 Core Operating Limits Report - Rev, 1 NFMRSA File: 2494-0027 Prepared By: Lewis E. Wells Approved By:

Date:

1 of 13 (Rev. 1l 940528>00>4.

PDR ADOCk'5000400

.. ".PDR

Harris Unit 1 Cycle 6 Core Operating Limits Report - Rev. 1 1.0 CORE OPERATING LIMITS REPORT This Core Operating Limits Report (COLR) for Shearon Harris Unit 1 Cycle 6 has been prepared in accordance with the requirements of Technical Specification 6.9.1.6.

The Technical Specifications affected by this report are listed below:

3/4.1.1.3 Moderator Temperature Coefficient 3/4.1.3.5 Shutdown Rod Insertion Limit 3/4.1.3.6 Control Rod Insertion Limits 3/4.2.1 Axial Flux Difference 3/4.2.2 Heat Flux Hot Channel Factor - Fe(Z) 3/4.2.3 Nuclear Enthalpy Rise Hot Channel Factor - F<<

3/4.9.1.a Boron Concentration During Refueling Operations 2 of 13 (Rev. 1)

Shearon Harris Unit 1 Cycle 6 Core Operating Limits Report - Rev. 1 2.0 OPERATING LIMITS The cycle-specific parameter limits for the specifications listed in Section 1.0 are presented in the following subsections. These limits have been developed using NRC-approved methodologies specified in Technical Specification 6.9.1.6 and given in Section 3.0.

2.1 Moderator Tem erature Coefficient (Specification 3/4,1,1.3)

The Moderator Temperature Coefficient (MTC).limits are:

The Positive MTC Limit (ARO/HZP) shall be less positive than

+5.0 pcm/'F for power levels up to 70% RTP with a linear ramp to 0 p"m/ F at 100% RTP.

The Negative MTC Limit (ARO/RTP) shall be less negative than

-45 pcm/~F.

2. The MTC Surveillance limit is; The 300 ppm/ARO/RTP-MTC should be less negative than or equal to

-37.4 pcm/~F.

where: ARO stands for All Rods Out HZP stands for Hot Zero THERMAL POWER RTP stands for RATED THERMAL POWER 2,2 Shutdown Rod Insertion Limit (Specification 3/4.1,3.5)

'Fully withdrawn for all shutdown rods shall be 231 steps.

2.3 Control Rod Insertion Limit (Specification 3/4.1.3.6)

The control rod banks shall be limited in physical insertion as specified in Figure 1.

Fully withdrawn for all control rods shali be 231 steps.

2.4 Axial Flux Difference (Specification 3/4.2.1)

The AXIALFLUX DIFFERENCE (AFD) target band is specified in Figure 2.

3 of 13 (Rev. 1)

Shearon Harris Unit 1 Cycle 6 Core Operating Limits Report - Rev. 1 2.5 Heat Flux Hot Channel Factor - F~(Z) (Specification 3/4.2.2)

F~(Z) < F~" 'lZ)/P for P ) 0.5 F~(Z) < F~"" " K(Z)/0.5 for P < 0.5 where: P = THERMAL POWER/RATED THERMAL POWER

a. F~"" = 2.45 for LOPAR and VANTAGE 5 fuel

b. F "" = 2.52 for SPC fuel

c. K(Z) is specified in Figure 3.

V(Z) Curve for PDC-3 Operation is specified in Figure 4. The V(z) curve is sufficient to determine the PDC-3 V(z) versus core height for Cycle 6 burnups through the end of full power reactivity plus a coastdown for a maximum cycle energy of 461 EFPDs.

t 2.6 Nuclear Enthal Rise Hot Channel Factor - F<<(Specification 3/4.2.3)

F< F" '(1 + PF(1-P))

where: P = THERMAL POWER/RATED THERMAL POWER a0 F<<"~ = 1.62 for LOPAR fuel

b. F, "" = 1.65 for VANTAGE 5 fuel C. F<<"" 1.73 for SPC fuel

d. PF<< = 0.3 for LOPAR fuel

e. PF<< = 0.35 for VANTAGE 5 and SPC fuel 2.7 Boron Concentration for Refuelin 0 erations (Specification 3/4.9.1.a)

Through the end of Cycle 6, the boron concentration required to maintain K, less than or equal to,95 is less restrictive than the 2000 ppm boron requirement.

Boron concentration must be maintained greater than or equal to 2000 ppm during refueling operations.

4 of 13 (Rev. 1)

Shearon Harris Unit 1 Cycle 6 Core Operating Limits Report - Rev. 1 3.0 METHODOLOGY REFERENCES XN-75-27(A), and Supplements 1, 2, 3, 4, and 5, "Exxon Nuclear Neutronics Design Methods for Pressurized Water Reactors," Exxon Nuclear Company, Richland, WA 99352.

(Methodology for Specification 3.1.1.3 - Moderator Temperature Coefficient, 3.1.3.5 - Shutdown Bank Insertion Limits, 3.1.3.6 - Control Bank Insertion Limits, 3.2.1 - Axial Flux Difference, 3.2.2 - Heat Flux Hot Channel Factor, 3.2.3 - Nuclear Enthalpy Rise Hot Channel Factor, and 3.9.1 - Boron Concentration).

2. ANF-89-151(A}, and Correspondence, "ANF-RELAP Methodology for Pressurized Water Reactors: Analysis of Non-LOCA Chapter 15 Events,"

Advanced Nuclear Fuels Corporation, Richland, WA 99352.

(Methodology for Specification 3.1.1.3 - Moderator Temperature Coefficient, 3.1.3.5 - Shutdown Bank Insertion Limits, 3.1.3.6 - Control Bank Insertion Limits, 3.2.1 - Axial Flux Difference, 3,2.2 - Heat Flux Hot Channel Factor, and 3.2.3 - Nuclear Enthalpy Rise Hot Channel Factor).

3. XN-NF-82-21(A), Revision 1, "Application of Exxon Nuclear Company PWR Thermal Margin Methodology to Mixed Core Configurations," Exxon Nuclear Company, Richland, WA 99352.

(Methodology for Specification 3.2.3 - Nuclear Enthalpy Rise Hot Channel Factor),

XN-75-32(A), Supplements 1, 2, 3, and 4, "Computational Procedure for Evaluating Fuel Rod Bowing," Exxon Nuclear Company, Richland, WA 99352.

(Methodology for Specification 3.2.2 - Heat Flux Hot Channel Factor, and 3.2.3 - Nuclear Enthalpy Rise Hot Channel Factor).

5. XN-NF-84-93(A), and Supplement 1, "Steamline Break Methodology for PWRs," Exxon Nuclear Company, Richland, WA 99352.

(Methodology for Specification 3.1.1.3 - Moderato'r Temperature Coefficient, 3.1.3.5 - Shutdown Bank Insertion Limits, 3.1.3.6 - Control Bank Insertion Limits, and 3,2.3 - Nuclear Enthalpy Rise Hot Channel Factor) ~

5 of 13 (Rev. 1)

Shearon Harris Unit 1 Cycle 6 Core Operating Limits Report - Rev. 1 3.0 METHODOLOGY REFERENCES (Continued)

6. EXEM PWR Large Break LOCA Evaluation Model as defined by:

XN-NF-82-20(A), Revision 1 and Supplements 1, 2, 3, and 4, "Exxon Nuclear Company Evaluation Model EXEM/PWR ECCS Model Updates,"

Exxon Nuclear Company, Richland, WA 99352.

XN-NF-82-07(A), Revision 1, "Exxon Nuclear Company ECCS Cladding Swelling and Rupture Model," Exxon Nuclear Company, Richland, WA 99352.

XN-NF-81-58(A>, Revision 2 and Supplements 1, 2, 3, and 4, "RODEX2 Fuel Rod Thermal Response Evaluation Model," Exxon Nuclear Company, Richland, WA 99352.

XN-NF-85-16(A), Volume 1 and Supplements 1, 2, and 3, Volume 2, Revision 1 and Supplement 1, "PWR 17x17 Fuel Cooling Test Program,"

Exxon Nuclear Comp'any, Richland, WA 99352.

XN-NF-85-105(A), and Supplement 1, "Scaling of FCTF Based Ref lood Heat Transfer Correlation for Other Bundle Designs," Exxon Nuclear Company, Richland, WA 99352.

(Methodology for Specification 3.2.1 - Axial Flux Difference, 3.2.2 - Heat Flux Hot Channel Factor, and 3.2.3 - Nuclear Enthalpy Rise Hot Channel Factor).

7, XN-NF-78-44(A), "A Generic Analysis of the Control Rod Ejection Transient for Pressurized Water Reactors," Exxon Nuclear Company, Richland, WA 99352.

(Methodology for Specification 3.1.3.5 - Shutdown Bank Insertion Limits, 3.1.3.6 - Control Bank Insertion Limits, and 3.2.2 - Heat Flux Hot Channel Factor).

6 of 13 (Rev. 1)

'* ~

Shearon Harris Unit 1 C 6 Core Operating Limits Report - Rev. 1 3.0 METHODOLOGY REFERENCES (Continued)

8. ANF-88-054(A), "PDC-3: Advanced Nuclear Fuels Corporation Power Distribution Control for Pressurized Water Reactors and Application of PDC-3 to H. B. Robinson Unit 2," Advanced Nuclear Fuels Corporation, Richland, WA 99352.

(Methodology for Specification 3.2.1 - Axial Flux Difference, and 3.2.2-Heat Flux Hot Channel Factor).

9. WCAP-9272-P-A, "WESTINGHOUSE RELOAD SAFETY EVALUATION METHODOLOGY", July 1985 (W Proprietary).

(Methodology for Specification 3.2.2 - Heat Flux Hot Channel Factor and 3.2.3 - Nuclear Enthalpy Rise Hot Channel Factor).

10. WCAP-10266-P-A, Rev. 2, "The 1981 Version of the WESTINGHOUSE ECCS EVALUATION MODEL USING THE BASH CODE", March 1987 (W Proprietary).

(Methodology for Specification 3.2.2 - Heat Flux Hot Channel Factor).

WCAP-11837-P-A, "EXTENSION OF METHODOLOGY FOR CALCULATING TRANSITION CORE DNBR PENALTIES", January 1990 (W Proprietary).

(Methodology for Specification 3.2.3 - Nuclear Enthalpy Rise Hot Channel Factor).

12. EMF-92-081(A), and Supplement 1, "Statistical Setpoint/Transient Methodology for Westinghouse Type Reactors," Siemens Power Corporation, Richland, WA 99352.

(Methodology for Specification 3.1.1,3 - Moderator Temperature Coefficient, 3.1.3.5 - Shutdown Bank Insertion Limits, 3.1.3.6 - Control Bank Insertion Limits, 3.2.1 - Axial Flux, Difference, 3.2.2 - Heat Flux Hot Channel Factor, and 3.2.3 - Nuclear Enthalpy Rise Hot Channel Factor).

13. EMF-92-153(A), and Supplement 1, "HTP; Departure from Nucleate Boiling Correlation for High Thermal Performance Fuel," Siemens Nuclear Power Corporation, Richland, WA 99352.

(Methodology for Specification 3.2.3 - Nuclear Enthalpy Rise Hot Channel Factor).

7 of 13 (Rev. 1)

~ ~

0 Shearon Harris Unit 1 Cycle 6 Core Operating Limits Report - Rev. 1 3.0 METHODOLOGY REFERENCES (Continued)

14. XN-NF-82-49(A), Revision 1, and XN-NF-82-49(P), Revision 1, Supplement 1, "Exxon Nuclear Company Evaluation Model EXEM PWR Small Break Model," Exxon Nuclear Company, Richland, WA 99352.

(Methodology for Specification 3.2.1 - Axial Flux Difference, 3.2.2 - Heat Flux Hot Channel Factor, and 3.2.3 - Nuclear Enthalpy Rise Hot Channel Factor).

8 of 13 (Rev. 1)

e Shearon Harris Unit 1 Cycle 6 FlGURE 1 ROD GROUP INSERllON LlMITS VERSUS THERMAL POWER (THREE-LOOP OPERATlON)

I

~ ~ 0~0~ \~ 0~0 0000 ~ ~1 ~ ~ ~ 001 ~ 00 ~ 0 ~ 0 ~ 0 ~ 0001 1 ~ 1 ~ 0 ~ OOOO ~ ~ 0 ~ 00 ~ ~ 00000000

~ 0 ~ 1000000 tSS4,231)

~ 00 ~ ~ 0 ~ 010 001 01 1\1 1~ ~ ~ 0 ~ 0 ~ 0 ~ 11 ~ ~ \ ~ 000 ~ 0000 ~ ~ 0 ~ 0 ~ 0 ~ 0000011000

~ ~

200 ~ ~1~0 ~ \F1' 0~0~0~~ 11 F0 ' ~ 040 0

~ 01100 ~ 0 ~ 0 ~ ~0~0 ~0 ~0 1~ ~1~ 001 ~ 1001 SAN}< C C 18D ~ ~~ ~ 01 ~ ~ 0 ~ 0 ~ 100010W ~ ~0~ ~ ~ ~ ~0 ~ 000 ~ OOOO ~ 0 ~ 0 ~ 0 ~ 000 ~ ~ 01 ~ ~ 1 ~ ~ 0 ~ 0 ~ 0 ~ 00000

~ ~ ~ 1100 ~ 0 ~ 0 ~ ~ 0010 ~ ON1000000 ~ ~ 0 ~ ~ 0 ~ 00000000 1dO F 004 ~ 00 ~ 1 ~ 0 ~ 0 ~ 00 ~ F 00 ' ~ 1 ~ 01NOO ~ 1010400 ~ ~ 00 ~ 000000000

~ ~

4000 ~ 0 ~ ~ 1 ~ 0 ~

~

~ OOOO

~

000010 ~ 01 ~1~

(1 1B81 F 00 'N

~0 00 F 000 ' 0 ~0 ~ 010000 ~ ~ ~ ~ 0 ~ 0 ~ 00001001010 ~ \ \ \ 0000 0

~00 0 0 ~ ~ 0 ~ 0 ~ 0 00 140 ~0 ~0~ 0 ~ ~ ~ ~ ~ ~ 0001 ~ 0 ~ 000 ~ ~ 1 ~ ~ ~0 000 ~ 1000 ~ 00 ~ 00 ~ ~ 010 \

~ 0000 ~ 01 0 0 1 ~ 0 ~ 1 ~ 0 ~ 1 1 0 0 000 ~ ~ ~0 (O,.:'12' 0 ~ 0 ~ OW10110 ~ ~ 0000 ~ ~0~1~0 ~0 ~1 1010 10 ~ 000000 ~ 0 ~ ~ N000000400000 ~ 0 ~ 0 ~ 0 ~ ~ 0 ~ OOONOO 12D' OOOO ~ 10 F 0 ' F 01 '1100010 ~ ~0~0~0~0 ~ W 0000000 ~ 0010 ~ ~ OWO ~ 000000W ~ \ ~ 0 ~ 0 ~ 0001 ~0 ~1 ~

O

~ 0000 0 00 F 0 ' ~1~0~1 ~ 000001010 ~ 00110 ~0~1 ~ ~ ~ ~ 00 ~ 1 ~ 000001 ~ 00 OOOO ~ ~ 0 ~ 0 ~ 0 ~ 00000 ~ 0 ~ 0000000 ~ 0 ~ 0 ~ 0 ~ ~ 00 ~ 0 ~ ~ 0000

~ ~

10D ~ 00101 ~ 0 ~ 10 ~ 0 ~ 1000000010000000 ~ 011 000000000000 ~0~ ~ 10NW10 ~ 0 ~ ~ ~ ~ ~ ~ 000 00

~ 00000000000 ~ ~ 0 ~ 00 ~ 0 ~ 0000 ~ 00 ~0 ~ *~ 0 ~ 0 ~ 0 ~ 0 ~ 00 ~ oeoo 80 ~ 000 ~ 0 ~ 0 ~ ~ 0 ~ 0 ~ 0 ~ N000011 '

~ 0100 ~ 0 ~ 00 F 0 ~ 0011110 ~0 ~0 ~ 010 ~ 001\ ~ 0 ~ ~ 00 ~ 0 ~ 1

~

~ Wooo ~ ~ 0 ~ 0 ~ ~ 0 ~ 0 ~ 0 ~ 000 0 ~

~

' ONOOONOO ~ 0 ~ 0 4 ~ 00000 ~ 00 ~ 0 ~ ~ F 00 0

~ 0 ~ 0 ~ 0 ~ 0 ~ 0 10000 ~ 00 ~ 00 ~ 0 ~ 0 ~ 1000 ~ 0 ~

0~0 ~0 F 000 ~ ~

dO ~0~0 Q

~ 110 00 \

~ 00 ~ ~ 0 ~ ~ 00 ~ 000000100 ~1~ ~ ~0~ ~ 0 ~0 ~ F 00 Wo ~ 0 ~ \1 ~ 0 ~ ~ 00 F 0 ' F1 ' \~ 0 00 ~ 1 ~ 0~0~0~ 0~0 \

~ 000000 ~ ~ ~ 0 ~ 0 ~ 0 0 ~ 0 ~ 10000000

~ OWO ~ 0 ~ 00 ~ 00 ~ 0 ~ ~ ~ ~ 0 ~ 1 ~ 0 ~ 0 ~ 0 ~ 0000000010000 ~ 0000 ~ 0 ~ 00 000 ~ ONO ~ 0 ~ 0 F 00 0

~ ~

20 ~ 0000000 ~ ~ 0 ~ 0 ~ ~ 00 OOW ~ ~ 000 ~ 0 ~ 0 ~ ~ 00 ~ 100 ~ 0 ~ 0 ~ 0 ~ 00010100 F 00 010 ~ 0 ~ 0 ~ 0 ~ 00010000

~ \0 0~ \ ~

(O, O) ~0 ~ 0 ~ 000000100 0.1 04 . O.B 0.4 0J5 O.d 0.7 O.d 0.9 1 FRACTiON OF RATED THERMAL POSER (F'ully withdrawn shall bb 231 steps)

Nots: Contral Banks A and B Must bb Withdrawn From Thb Cars Prior ta Powbl'pbratian 9 of 13 (Rev. 1)

~ 4 Shearon Harris Unit 1 Cycle 6 FIGURE 2 AXIALFLUX DIFFERENCE LIMITS AS A FUNCTION OF RATED THERMAL POWER 120

~ ~~ I ~ \ ~ 0 ~ 0 ~ 0 ~ I ~ \ ~ ~ I ~ ~ I ~ ~ ~ ~ ~ I ~ ~ I ~ 00 ~ I ~ I~ I ~ ~ I ~ I ~ ~ ~~~ ~ I ~ I~

~ F 10 ' 0 F0 '

110 100 ~ tt I ~

~ ~ ~ I ~ I~

I~ ~ II~

(-1Q,

~0 ~ \~

1do),',

~ ~ ~ I~ F 001 I ~ 010101

~ 10 ~

000 ~

\~ ~

~

>so)

~

I I I~

~~ I~ ~ I ~ I

~ 00 ~ ~ ~ 00

~

II

~ ~ ~ 010 ~ 1011

~

IIII

~ ~ ~ ~

~ ~

I~

PNACC~ABLg \

+AQCEPTAPLE 80 ~ ~ 10001 ~ ~ ~ ~0~0~ ~ ~

\

~ I ~ I ~ 100 ~ I ~ I ~ ~~ I~ I~ ~ ~ I~ I ~ I~ I~ 4 ~ I ~ 000 ~ ~ ~ I ~ ~ ~

I

~ ~ ~~ ~ 00 ~ 10000 ~ ~ ~ ~ III 01 ~ I ~ 0000 ~ 000 ~ 00000 O

ao I I F 00

~ ~~ ' I~ ~ ~ ~ 00000 ~ I ~ I ~ I ~ F 00 '

I

~ 0010010 4~ ~ ~ 00 ~~4~ ~ I~ I I

~ 00 ~ 0100 ~ ~ ~ ~ ~ ~

I I I ~I

~ ~ ~ ~4~ ~ ~ ~ 0 ~ 0000100 ~ ~ 0 ~ I I\I~ 00000 ~ 0000 ~ 00000 ~ 0001 ~~0 ~ I~ 000000 ~ I ~ I~ 001 I ~ ~ I ~ I ~ 0 ~ It10000000 70 I I

~ 00 ~ ~ 000 ~ ~ 00000 ~ 01 I

~ ~ 0101 '

F 111 ~ 00 ~ 00000 ~ 0000 ~ IOt 0001tO ~ I ~ I~ I ~ I I I

~ ~~ 00t ~ I ~ I~ I F 000 ' ~ 00 ~ ~ ~ 00 ~ ~ ~ 00001 ~ I ~0 I~ I ~~ I ~ 000 ~ I ACCEPTABLE F 00 ' ~~ ~ ~ 01010000 F ~ ~ ~

60 I

~ ~ ~ ~ 00010 ~ ~ I 10 ~ 0000 ~ ~ t010 ~ 10 ~ I ~ OtO ~ 000 ~ 100 00 ~ 0001 ~ 1000 00000 ~ ~ 0011 ~ ~ 00tO ~ F 00 I 000000 ~ I II

~ ~

~ \0000 ~ 00000 ~ ~ I ~~ \ ~0 ~ I~ ~ I ~ 00 ~ I ~ ~ ~ 10000 ~ OOOO ~ ~ I 000 ~ OOOO ~ I~ 00001 ~ I~ ~ 00000 F 00 ' ~ I 0010tt100 50-(-~~.oo):

~ 00 ~ ~ 01011 ~ ~ \ I 10 ~ 0100 ~ ~ 0000 ~ ~ Ot000 ~ 00 ~ 000 001 ~ I I

~ 0001100 ~ ~ ~ 00000 ~ 00000 ~ ~ t00 ~ ~ It t28,::5O) 1100tO ~ I~ I 010100 ~

I 0 \

~ ~ ~ ~ ~ I000 ~ I ~ I ~ ~ I ~ ~ 00 ~ 0000 ~ ~ I ~ ~ ~

I 000000 ~~ ~\ I ~ ~ ~ ~ ~ Ot00 I

~ ~ Ot001 I ~ I ~ I ~ I~ I ~ II

~ ~ ~ 00 ~ II I

~ 001 ~ ~ ~ ~ 000 ~ ~ ~ t10010 ~ ~ ~ ~ ~ I I I t00 ~ I~ 000 a 30 I I ~ 10

~ ~ ~ I I~ ~ ~ ~

~ 01 ~ ~ 00010 ~ I

~ ~ ~ I ~ ~ 000 ~ I ~ 00 ~ 00 ~ I 20 ~ ~ ~ 00tO ~ ~

~ 10 ~ I~ 11 Ot10 F 110 ~ ~ F 000 ' ~ ~ ~ I ~ ~ ~ ~

~ ~

~

10 ~ ~

~

~ ~ I I \

~~ ~~ ~ 000 I ~ 0 ~ I I~ I ~ I ~ I~ IF 00 0 '1\10 ~ 0 I ~ 0 ~ \

~ 0110000010 ~ ~ 0000 ~ 10100 ~ ~

~

I ~

~

Ott00 ~ 000000000 ~ I~ ~ 010 ~ ~ 0' I

~ ~ 000000 ~ 0000 ~ 000 ~ 00000

-50 ~ -30 -20 -10 AXIALFLLIX DIFFERENCE {X DELTA-I) 0 10 20 30 50 (DEYIATION FROM TARGET AFD) 10 of 13 (Rev. 1)

i 0

Shearan Harris Unit 1 Cycle 6 FIGURE 3 K(Z) LX)GAL AXlALPENALTY FUNCITON FOR FQ(Z) 0

~ ~ ~ ~ ~ ~

~ ~

otto ~ ~ OOOO ~ 1 ~ ~ ~0 ~0~ ~0~0 ~0 ~0 ~~0 0~

~ ~

~0 ~ F0 '000 ~ 0 ~ ~ ~0 ~0~ ~

~

~ ~ ~

~

~ ~

~ ~ ~ ~ ~ ~

~

~ 00 ~

~

~1

~

~0 ~ 011 ~ ~ 004t ~ t01 ~ ~ 001 ~

~

\ ~

~0~0~ ~ ~ 000 ~ 0000 ~ 0 ~ 0 ~0~ ~ ~ 00 ~ ~ 0 ~ 0 ~ 0 ~ 0 ~ 0 ~ Otott ~ 0

~ ~ ~ ~ 0 ~ ~ ~

~ ~ ~ ~ ~ ~ ~ ~

~ ~ ~

~ 0111 ~ 00 ~ 1 ~ 00 ~ ~ 0

~ ~

Ott~ ~ 0 ~ 01 ~ ~ 00 ~ 0 ' ~~ \ ~0 ~1 ~1~~ ~0~1 ~0 ~

~

~ ~0~4 ~0 0 ~ ~ ~~

~

~ ~

~

~ ~ 0 ~ 0 ~ ~ 001 (q,o ~ ~ 1 ~ 0 ~ ~ 0 ~ 0 ~ ~ 0 ~ ~ 0 ~ 0 ~ ~ 0000 ~ 0 ~ 0 ~

~ ~

Oottt ~ 0 ~ 0 ~ 1 ~ Ottt ~ 0000 ~ 0

~

~ ~ ~ 0, %925)

~

~ OH 0 ~ 1010 ~ 11 ~ 1 ~ 1110

~ ~

~

~ ~

~ 00 ~ 0 ~ 0 ~ 1 ~ ~0~

~ ~ ~

~ 0 ~ 110100000000 ~

~ ~ ~ ~

Ottt ~~~ 0000 ~ ~ 0

~

0~ ottt ~ Otott ~

~ ~

~ ~ 00 ~

~ ~ ~ ~

~ ~

~ ~ ~ ~ ~ ~

0.9 \

~ ~ ~ Ott1 ~ 000 ~ ~ 00 ~ 0 ~ 1 ~ 0 ~0 ~0 ~ ~ 0 ~ 0 ~ 0~ ~ 00010 ~ 0000 ~ 000 ~ OOH ~ 0 ~

~ ~

~ ~ ~0 ~ ~ 000 ~

~ ~ ~ ~

~ ~

~ oooe ~ 00 ~ 000 ~ ~ OOOO ~ 00 ~ 0 ~ 000 ~ ~ ~ ~ ~ 0 ~~ ~ ~

~

~ ~ ~ \ ~ 0 ~ 0 ~ 00 ~ 4 ~ \ ' \

0 ~ F 000 ~ 1 ~ ~ ~ 0010 ~ 0 0 0 0 0 HO

~ ~ ~ ~

~ ~

0.5 001 ~ 00 ~

~ ~

~ 04 ~ 00 ~ 0 ~ 0 ~ ~ ~ 000 ~ ON00000 ~ tttt ~ ~ 000 ~ 0 ~ ~ ~ OH 0 ~ H ~~0 ~ 0 0 ~ ~ 10 ~ 000 ~ 000000

~ ~

Z ~ 0000 ~0 ~ ~ ~ ~ ~ ~

~

1 ~ 10110100

~

~ ~ 0

~

~ ~0~ ~ 0 ~ 0 ~ Otto ~ 0 ~ 0 ~ ~ 0 ~ 0 ~ ~ 0 ~ 0 ~ HOOO ~ OtOONO hC ~

~

~ ~ ~ ~ ~

~ ~ ~

Ottt ~ 0010 ~ 00000WOOHO ~ Ottt ~ et 0.7 ~ ~ ~ 00100 ~ 0 ~ Oett ~ 0 ~ 0111 ~ 01 ~ 0 ~ 0 ~ 0 ~ F 00 ~ ~

~

~ ~ ~ ~

~

N ' 00 ' Nttt

~

Cl ~ 0101 ~ F 000 F 0000 ~ 0000 ~ HO ~ ~ 0010 ~ 0 ~ ~ ~ 0 ~~ 0 ~ ~ 00 00 ~ OOOO ~ ~1~ ~~

~

~ 00000000tt

~

hl ~ ~ ~

N

~ ~ ~

~ ~

~ ~ ~

0.8 000 ~ 0 10 ~ 0000 ~ 0 ~ ~ OH1 NO F 000 ' ~ ~ ~

~ ~

~ OOOO ~ Ot ~ ~ ~ ~ 0 ~ ~ ~0 ~ ~ \ ~

~

~ ~ 0000 ~ 1000 ~ 0 ~

\~ ~

O ~

~

~ ~

~

Z

~

~ ~ ~ ~ ~

0.5 ~ 100 ~ 0 ~ 10 ~ 1 ~ 1 ~ 1

~

~~1

~

~0 ~ ~ 0 ~ 0 ~ 00 ~ ~ 00 ~ ~ 01HOO ~ ~0 1~1 ~ 01 ~ ~0~0~~0~~ ~ 0 ~ 0 ~ ~ 0 ~ ~ ~ ~ ~ ~ 0010 ~ 0 0

~ ~

~ ~ ~ ~

~ Ottt ~ 0 ~

~

F0 ' ~

~

Ottt

~ ~ ~

~1~

~

~~0~~0~

~

0~~

~

~ ~ 1 100 ~ 000000

~ I

~ ~ ~ ~ ~ ~

~ ~ ~ ~ ~ ~ ~ ~

~ ~

O.f ~0 ~ 0 ~

~

~ ~ 1 10 ~ ON000011 ~0~0 ~0 ~ 0~

~

~0

~ ~ ~ ~ ~ ~ ~ ~

~ ~ ~ ~ ~ ~ ~ ~ ~ ~

~ HO ~ 010000000 ~ OH11000 ~ 0101 ~ Ott ~ 000 00000 ~ 00000 ~ OOOO ~

~ ~

Otttttttt~ 00000 ~ 00

~

~ ~

~ 0 ~ 0 ~ 0 ~ 000

~

~ ~0~ ~0

~ ~ ~ ~ ~ ~ ~

~ ~ ~ ~

~ 0 ~ ~ ~

~ 10 ~ ~ ~ 0 ~ ~ \01 ~ ~ 0 ~ 0 ~ ~ 0 ~ 0 ~ ~ 000 ~ tttt ~

~ 0 ~ 1 ~ ~ 00001

~

WOO 014 ~ 0001 ~ 000 ~ 00001 ~ 00 ~ 0 ~ \

~

~ ~

~0 ~0~0 ~~0~ ~ ~0 ~ ~0 \ ~ ~ 0 ~ 1 ~ ~ oe 00 ~

~ ~

~ ~ ~ ~

~ H10 ~ 0 ~ 0 ~ F 000 ' 1001

~ 0 ~ 0 ~ 0 ~ 0 ~ 010

~ ~

~ 0000 ~ 000000000 ~ t10000010 ~

~

~ 000

~

~ F 01 ~ 0 ~ 0 ~ ~ 0 ~ OOOH0

~ ~ ~ ~ ~ ~

~ ~

OZ, 0 4 5 d' 0 10 11 Q CORE HEIGHT O.eet) 11 of 13 IRev. 1)

Shearon Harris Unit 1 Cycle 6 FIGURE 4 V(Z) VERSUS CORE HEIGHT 1MO I I

~ ~ ~ ~ ~ ~ ~ ~

~

~ ~

~ ~ ~ I~ ~ ~ ~ ~ ~ ~ ~

~ ~

~

II ~

~ ~ ~ 1000 I I

~ ~

~ 00110 ~ 10 ~ ~ ~ 00000 ~ ~ ~

~ ~

~

I

~ ~ ~ 00 Noo ~ \ ~ I ~ I ~ 0 ~ 0 ~ I ~ I

~ ~ ~

~ ~ I

~~ ~ ~ 0000 ~ I ~ ~ I ~ I ~ I ~ BIFID ~ ~ ~ II

~ ~ ~ OOIOHO ~ ~ 0000 ~

~

I

~ ~

00tt ~ I ~ I~ ~ 01000 ~

~

~ 0~~~ ~ I I ~ I ~ I~ I~ F 000

~

' ~

~

~ ~ ~ ~

~ ~ ~ ~ ~ ~

~ ~

to ~ I ~ ~

~ ~I ~

0000000

~

II II ~

~ ~ ~ ~ ~ ~ ~ 0000 ~ \ BIFID BIFID ~ I~ Oto Oot001

~ ~

~ I ~ I~ ~

~

~ ~ ~ t ~ I ~ IF 0000010000

~

~ I ~ I~~ I 1.183, ~

~

~ ~ ~ ~ ~ ~ ~ ~

I ~ I~ ~ 00 ~ I~ BIFID ~ 000 ~ \ ~ 0 ~ 0 ~ I ~ I~ I~ 00000000 ~ I~ I ~ I ~ I ~ ~ 00000 ~ I~ I I~ I ~ 1 ~ I ~ I ~ I

~ ~ ~ ~ ~ ~ ~ ~ ~

~

I toooooo

~

~ ~ ~

~ ~ ~ ~ ~ ~ ~ ~

~

I ~ ~ (h.875, 5.165) ~

~

I ~ \ ~ I~ I~ I~ ~ OOOO F 00 ~ 00 ~ I~ ~ \ ~ 0 ~ OotoIWO ~ ~ I~ I~ I ~ OIHO 000001 ~ I ~ ~ ~ I ~ Iott

~ ~

'4175 ~

~ ~

~

~ ~ ~ ~

~ ~ ~

~ ~ ~ ~

~

I

~

~ 0001 ~ ~ 00 ~ 00 ~ ~ 0100 ~ Itt I ~ ~ I ~ ~

~

~ ~

I I ~ I~ I~ ~ I ~

~

~ 000 0100 ~ I~ I~ ~ I ~ I ~ I ~ I~ ~ ~

(15'.mn)

I ttt ~0 ~ ~

I

~ ~

I ~ ~

~ ~

1.150- II

~ ~ ~ t ~ ~ ~ ~ ~ I F 000 'IFID ~ Ooto ~ to\I~ I~ I ~ 0 ~ \ ~ ~ I~

~ ~ ~ ~

F 00 ~ 000000 ~

~ ~

I (2.575; 1.185)i i(8 h75I, 115O) ~

~

~ Ho ~ ~ 00 ~ 0 ~ 000 ~ ON0000100 ~ III

~ ~ ~ ~ ~ ~ ~ ~ ~ I~ I I

~ ~ ~ H OOON

~ ~ ~

80 1.125 ~ I~ ~~ Ot00100 ~ I BIFID ~ I~ ~ I~ 011

~

~ 000

~

I~ I~ ~ OOOO

~ ~

F 00 'IFID~ I~ 00 ~ F 000 ~ ' I~ I~~ I~ I~ IF 000 ' ~ oooo

~

00 ~ ~~ I BIFID RH0 010000000 ~ 00 ~ I ~ 0000 OW0 00 ~ I~ I F 00 ' ~

~

00tO ~ OttotHO

~

~ ~

~ ~ ~ ~

1.100 IIII

~

~ ~ ~ ~ ~ 00 ~ ~ ~

~

I I

~

10 ~ 000 ~

~

I 00 ~ I~ I~ I ~ ~ I~ 000

~

~ ~ ~

~

I ~ I~ I ~ ~ ~ I II ~

~ 100 ~ ~ ~ 00 ~ 0 ~ ~

~

\ I

~

~ ~ 00001

~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~

~ ~

~ 00010000 ~ 0010 F 000

~ ~ ~

~ 0000 F 00

~

'00000 ~ ~ ~ ~ ~

~ OOIOHHOIOOOOOHO ~ 1001000000000000 ~ ~ ~ 0000 F 00

~ ~ ~ ~ ~

~

II~ ~

~ ~ ~ ~ ~ ~ ~ ~ ~

~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~

~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~

I II ~ ~

~ 00 ~ ~ ~ 0000 ~ 000 ~ ~

~

\ 00 ~ 01 ~ I 000

~ ~ ~

~ OOOONOO ~ Ot ~ ~ 00 ~ ~ 00000 ~ OOOO

~ ~

~

I ~

I 10 ~ ~ I ~ ~

~

I I~ I~ OOOO ~ W

~

00000

~

~0~ \ ~~ ~ I I~

~ ~

~ I~ I~ ~ I ~~ I~ I~ ~ 000 ~ I

~ ~ ~ ~ I ~ ~ I~ I ~ ~ Oto ~~ I~ I ~

~~ I I~ ~ I ~

~ ~

~ ~ 101 II

~ ~ ~ tttt ~ 0000 H010000

~ ~ ~ ~ ~ ~

~ ~ ~ ~

1.050 ~ ~ ~ ~ ~ ~ ~ ~ ~

~ I~ I~ 00101001

~ ~ ~ ~ ,

~ ~ ~ ~ ~ ~ ~ ~ ~

~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~

~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~

~ ~ I

~ ~1

~

Otoo ORO

~

~ I I~

~

tte ~ \

~

~ OR OHO

~

IIII ~

~ ~ ~ ~ ~ HO ~ ~ ~ I I I I~ I\ ~ OOOO

~~ ~ ~ ~ I OOW

~ ~ ~ ~

~ ~ ~ ~ ~ ~ ~ ~

~ ~ ~ ~ ~ ~

1.025 I I~ I~ F 000

~ ~ ~ 000 ~ 0000 ~ II ~ ~

~ ~ ot00 ~ 00000000 ~ ~

~ \ I ~ F 000 ' ~ 0000 ~ Ho ~ ~ tottoo ~ I I

~ ~

~

~ I~ INI I I I I

~ ~

~

~ ~ ~

~

~~ ~ ~ ~ 00

~ ~ ~ ~

~ ~ ~ ~ ~ ~ ~

~ ~ ~ ~ ~

~ 01 ~ 0 ~ 0000 ~ 01 ~ I~ lo I I I ~ I ~ 0000000 ~ I

~ ~ ~ ~ ~ ~ ~ I~ ~ ~ I~ I I I ~

II ~

II

~ 00 ~ ~ ~ ~ 0000 F 1000 ~ ~ ~ 0 ~ ~ ~ 00 ~ 00001000000

~ ~ ~

~ ~

2 3 4 5 8 7 8 9 10 11 12 CORE HEIGHT 0=act)

Mote: Top and 8ottom 15K excluded as per Technical Specification 4~4 12 of 13 (Rev. 1)

V E

P Harris Unit 1 Cycle 6 Core Operating Limits Report - Rev. 1 Distribution List:

Harris Plant R. J. Duncan, Manager NSSS J. F. Nevill, Manager - Technical Support D. C. McCarthy, Manager - Regulatory Affairs NFMRSA Section File: NF-2494-0027 Distribution list Approved: //f~Y 13 of 13 (Rev. 1)

h e

ML18011A457: Difference between revisions

Latest revision as of 19:58, 3 February 2020

Text

Navigation menu

ML18011A457: Difference between revisions

Latest revision as of 19:58, 3 February 2020

Text

Navigation menu

Search