ML20237J085

From kanterella
Jump to navigation Jump to search

Proposed Tech Specs,Providing Temporary Restrictions to Support Coastdown Operations
ML20237J085
Person / Time
Site: Millstone Dominion icon.png
Issue date: 08/31/1987
From:
NORTHEAST NUCLEAR ENERGY CO.
To:
Shared Package
ML20237J013 List:
References
TAC-66056, NUDOCS 8709030486
Download: ML20237J085 (8)


Text

.

Dec!:et No. 50-336 B12652 l

Millstone Nuclear Power Station, Unit No. 2 Proposed Changes to Technical Specifications l

l l

l l

1 8709030486 870828 PDR ADOCK 05000336 P

PDR August 1987 l

..g s.

l

{.

o i

I W

G U

~a w

Q>c C

nco 5lm C

0

~

4o g

i

{

5 3

=

o

=

E 'O E.

L 4

E M

C E

<c s

-n w

.a

.J ap a.

s pp w

0 m

wn

=e w

0%

e

.e cr a 4

m o'.e g

p.

W a.

w c: c 0

U I.

3 m

em 5

t ai l

T Um N

s

=. c.

D l

.3-c

]

u o

- en 1

.a n l

A %

~o i

l

$o i

=-

o o,

g n'

o g

e (WO1VB3OOW + OY13 + 7304) id/MM ~31VW IV3M WV3 Nil XV3d 318vM011V t

l l

MILLSTONE - UNIT 2 3/4 2-3 i

i i

I

l l

POWER DISTRIBUTION LIMITS TOTAL PLANAR RADIAL PEAKING FACTOR - Fly LIMITING CONDITION FOR OPERATION 3.2.2 Meet either of 3.2.2.1 or 3.2.2.2.

3.2.2.1 The calculated value of F1 defined as Fly * * = Fxy (1+Tq), shall be l

limited to.61.62 with the AX1AL Sb, APE INDEX alarm setpoints adjusted i

consistent with the limits shown on Figure 3.2-2a, or 3.2.2.2 The calculated value of F{ defined as F1 * * = Fxy (1+Tq), shall be l

limited to 61.719 with the AXIAL b,HAPE INDEX [larm setpoints adjusted consistent with the limits shown on Figure 3.2-2b.

APPLICABILITY: MODE 1.*

ACTION:

With Fly > 1.62 and the AXIAL SHAPE INDEX alarm setpoints adjusted a.

consistent with the limits shown on Figure 3.2-2a, within 6 hours6.944444e-5 days <br />0.00167 hours <br />9.920635e-6 weeks <br />2.283e-6 months <br /> either:

1)

Reduce THERMAL POWER to bring the combination of I

THERMAL POWER and Fly to within the limits of Figure 3.2-3a and withdraw the fulllength CEAs to or beyond the Long i

Term Steady State Insertion Limit of Specification 3.1.3.6, or i

2)

Apply the limits of Specification 3.2.2.2 and Figure 3.2-3b and within 72 hours8.333333e-4 days <br />0.02 hours <br />1.190476e-4 weeks <br />2.7396e-5 months <br /> adjust the AX1AL SHAPE INDEX alarm setpoints consistent with the limits shown on Figure 3.2-2b, or 3)

Be in at least HOT STANDBY.

With F[y > 1.719 and the AXIAL SHAPE INDEX alarm setpoints adjusted I

b.

consistent with the limits shown on Figure 3.2-2b, within 6 hours6.944444e-5 days <br />0.00167 hours <br />9.920635e-6 weeks <br />2.283e-6 months <br /> either:

1)

Reduce THERMAL POWER to bring the combination of THERMAL POWER and Fly to within the limits of Figure 3.2-3b and withdraw the full length CEAs to or beyond the Long Term Steady State Insertion Limit of Specification 3.1.3.6, or 2)

Be in at least HOT STANDBY.

See Special Test Exception 3.10.2 l

  • For Cycle 8 only, whenever the core average burn-up ish 9500 MWD /MTU, an additional multiplier of 1.115 shall be used in the calculation. Therefore, for these conditions, Fly = 1.115 Fxy (1+T ),

q MILLSTONE - UNIT 2 3/4 2-5

1 f

POWER DISTRIBUTION LIMITS SURVEILLANCE REQUIREMENTS 4.2.2.1 The provisions of Specification 4.0.4 are not applicable.

4.2.2.2 Fl shall be calculated by the expression FI[he following intervals: y

  • = Fxy (1+Tq) and Fl shall be determined to be within its limit at a.

Prior to operation above 70 percent of RATED THERMAL POWER af ter each fuel loading, b.

At least once per 31 days of accumulated operation in MODE 1, and Within four hours if the AZIMUTHAL POWER TILT (T )is _0.02.

c.

q 4.2.2.3 Fxy shall be determined each time a calculation of Fly is required by using the incore detectors to obtain a power distribution map wi'th all full

)

length CEAs at or above the Long Term Steady State Insertion Limit for the J

existing Reactor Coolant Pump combination. This determination shall be limited I

to core planes between 15% and 35% of full core height inclusive and shall exclude regions influenced by grid effects.

l 4.2.2.4 T shall be determined each time a calculation of Fly is required and q

the value of Tq used to determine Fly shall be measured value of T.

q l

For Cycle 8 only, whenever the core average burn-up is 9500 MWD /MTU, an additional multiplier of 1.115 shall be used in the calculation. Therefore, for these conditions, FxyT = 1.115 Fxy (1 + T ).

q MILLSTONE - UNIT 2 3/42-6

P

]

' ~

~

1

~

L N

I fi I 6 I

I i ! 16 I

I

,I l

A O

)s M

G t

E c

R I i l

e.

I E

I i L

i R c

N H

l L

i T

IiiI4 IO 1i t

I 1 iy; l

' i 1

T 2

D A

8 A

)s P

~ N=oI I I 8

E 1

I I

' R '

8 (

E e

1 TA I

'i O I t N1 R

I I l e

E

)

L a

s f

r a.

I !e r

t I 1 1

o B

I I l

!6 A

1 T

o.

(

ro o

P

" i i i

!!4 t

I I6 F

C e

/

E

/

V 6

c C

4 R

7 a

i I i I l

!I !

C' L !/ j U '

r 7

A l

I4 j

F 1

N 1

C U

(

/

i l

/T i

e I

l M

b

)

I a

L i ll '

0

?i

)

ii1 I f w

1 s

o r

l

! 1 i8 o.

p F

i i l l

o.a A

)s o

t 0

r.

r 1i i l 1

i o. i i i ' sp 1

7 s

(

r 1

v o

o.

r I i i

! i i l 6 6

0 t iii t y

1 I ii o

(

1 t

?

i i i i i t

8 1

t

{ i 1-],

I I 1 1 1 I l

c 7

" 1 11 I 4 a

(

)s F

s I i 1 I i

I N

g N' e.

iI !

I i i i

I

' 7 y

o tO T

m n

)

4 o

i O

8 F

k a.

1 Ii iIi i

E i

1 Ii 1 1 i t 0

n o

1 2

R e

P s

I I'i I

1 I N

T r

I l

t I

f 1 I i e

O I

F l

e. -s.N

(,

1 I I 1 1 I A

id a

T t

i i I

I i 1 I i e )

i

(

e R

a E

E P

R l i i 1

i of t

il 1'

I i i I O

V

\\! i (y i' C ' 1 i ii L 5

o l

/

R 8

a s

U E

t e

i f i I

i I f

4 s. f

/

B 1

' T A _

T '

1

!1 i,

I

' 1 Ii I T._

(

M P

i

  • l

!i

)

. a N

'1 l

1 f'1.

A 0

I E

b L

C 3

1

.iN(

I C

! i i Ii i.

7 F

, i a i

i i i I l i'1 I

i I L1 2

\\

3 1

1 1

I I i 8 3

1 2

E

(

I I

l Y

5 R

1 U

4 2

0 4

2 0

G 1

1 1

0 0

0 I

F o ;.a <

$sO" j2$x> oW <" LO oiO CwWd<

EF[Hh A ' g-w) Yw8

3/4.2 POWER DISTRIBUTION LIMITS I

BASES l

3/4.2.1 LINEAR HEAT RATE i

The limitation on linear heat rate ensures that n the event of a LOCA, the peak temperature of the fuel cladding will not exceed 22000F.

Either of the two core power distribution monitoring systems, the Excore Detector Monitoring System and the Incore Detector Monitoring System, provide adequate monitoring of the core power distribution and are capable of verifying I

that the linear heat rate does not exceed its limits.

The Excore Detector Monitoring System performs this function by continuously monitoring the AXIAL SHAPE INDEX with two OPERABLE excore neutron flux detectors and verifying that the AXIAL SHAPE INDEX is maintained within the allowable limits of Figure 3.2-2. In conjunction with the use of the excore monitoring system and in establishing the AXIAL SHAPE INDEX limits, the following assumptions are made: 1) the CEA insertion limits of Specifications 3.1.3.2, 3.1.3.5 and 3.1.3.6 are satisfied, 2) the flux peaking augmentation factors are as shown in l

Figure 4.2-1,3) the AZIMUTHAL POWER TILT restrictions of Specification 3.2.4 l

are satisfied, and 4) the TOTAL PLANAR RADIAL PEAKING FACTOR does not exceed the limits of Specification 3.2.2.

The Incore Detector Monitoring System continuously provides a direct measure of the peaking factors and the alarms which have been established for the individual incore detector segments ensure that the peak linear heat rates will be maintained within the allowable limits of Figure 3.2-1. The setpoints for these alarms include allowances, set in the conservative directions, for 1) flux peaking augmentation factors as shown in Figure 4.2-1, 2) a measurement-calculational uncertainty factor of 1.07, 3) an engineering uncertainty factor of 1.03, 4) an allowance of 1.01 for axial fuel densification and thermal expansion, and 5) a THERMAL POTER measurement uncertainty factor of 1.02.

1 A reduced linear heat rate limit of 14.0 kW/f t for Cycle 8 operation beyond l

a core average burn-up cf 9500 MWD /MTU ensures that the 22000F peak fuel cladding temperature limit will not be exceeded in the event of a LOCA. The value of 9500 MWD /MTU is the predicted end-of-cycle for Cycle 8.

Operation beyond the predicted end-of-cycle may require reductions in the reactor coolant temperatures which can increase the calculated peak clad temperatures. The reduction in the linear heat rate limit will more than compensate for the effect of the reduction in the reactor coolant temperatures on the LOCA analysis.

3/4.2.2, 3/4.2.3 and 3/4.2.4 TOTAL PLANAR AND INTEGRATED RADIAL PEAKING FACTORS - Fl AND Fi AND AZIMUTHAL POWER TILT - T xy r

q The limitations on FT and T are provided to ensure that the assumptions xy q

used in the analysis for establishing the Linear Heat Rate and Local power Density - High LCOs and LSSS setpoints remain valid during operation at the

~

various allowable CEA group insertion limits.

l MILLSTONE - UNIT 2 B 3/4 2-1 l

POWER DISTRIBUTION LIMITS BASES The limitations on Ft and T are provided to ensure that the assumptions r

q used in the analysis establishing the DNB Margin LCO, and Thermal Margin / Low Pressure LSSS setpoints remain valid during o eration at the various T or T exceed their basic j

allowable CEA group insertion limits. If F x,F limitations, operation may continue under the additional restrictions imposed by r

the ACTION statements since these additional restrictions provide adequate provisions to assure that the assumptions used in establishing the Linear Heat

{

Rate, Thermal Margin / Low Pressure and Local Power Density - High LCOs and LSSS setpoints remain valid.

An AZIMUTHAL POWER TILT > 0.10 is not expected and if it should occur, subsequent operation would be restricted to only those operations required to identify the cause of this unexpected tilt.

The value of T T

T = Fr (1 + T )is the measured tilt.that must be used in the equation F xy = Fxy (1 + T ) a q

F r q

The surveillance requirements for verifying that FT FT and T are x

r q

within their limits provide assurance that the actual values of,FT FT and T x

r x and F r afke,r each fuei do not exceed the assumed values. Verifying FT T

loading prior to exceeding 75% of RATED THERMAL f)OWER provides additional assurance that the core was properly loaded.

For Cycle 8 operation beyond a core average burn-up of 9500 MWD /MTU, an additional multiplier of 1.115 is used in the calculation of Fxy. This value is T

proportional to the reduction in the maximum linear heat rate. The value of 9500 MWD /MTU is the predicted end-of-cycle for Cycle 8.

3/4.2.6 DNB MARGIN The limitations provided in this specification ensure that the assumed margins to DNB are maintained. The limiting values of the parameters in this specification are those assumed as the initial conditions in the accident and transient analyses; therefore, operation must be maintained within the specified limits for the accident and transient analyses to remain valid.

i l'

MILLSTONE - UNIT 2 B 3/4 2-2 L--

g-s.

92 6 V E-d3S LBbl SG-3ENSO

- _ _ _