ML20080Q455

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Nonproprietary, Response to NRC Question on Waterford-3 Bypass Flowrate
ML20080Q455
Person / Time
Site: Waterford Entergy icon.png
Issue date: 01/16/1984
From:
ABB COMBUSTION ENGINEERING NUCLEAR FUEL (FORMERLY
To:
Shared Package
ML19292C289 List:
References
CEN-275(C)-NP, NUDOCS 8402240065
Download: ML20080Q455 (13)


Text

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COMBUSTION ENGINEERING, INC.

CEN-275(C)-NP s

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- Response to NRC Question on Waterford - 3 Bypass Flowrate

+

January 16, 1984 4

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L LEGAL NOTICE This report was prepared as an account of work sponsored by Combustion Engineering, Inc. Neither Combustion Engineering nor any person acting on its behalf:

A. Makes any warranty or representation, express or implied including the warranties of fitness for a particular purpose or merchantability, with respect to the accuracy, completeness, or usefullness of the information contained in this report, or that the use of any information, apparatus,

. method, or pro ~ cess disclosed in this report may not infringe privately owned rights; or, B. Assumes any liability with respect to the use of, or for damages resulting from the use of, any information, apparatus, method or process disclosed in this report.

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ARD764 Response to NRC Question on Waterford Bypass Flowrate t

Questions:

a) Justify the Waterford-3 design value of 2.6% for the bypass flow and the value of 2.1% for the calculated bypass flow, b) Provide a description of the guide tube designs before and after the reduction in bypass flow.

Responses:

a) Bypass Flow Rate The bypass flow rate for Waterford-3 was recalculated after two minor design changes. This reassessment iustified lowering the design value for the bypass flow, sumarized in the following table:

Previous Now

  • Design bypass flow 3.5% 2.6%

Calculated best estimate bypass flow 2.7% 2.1%

The first design change was the reduction of the overall flow area of inlet flowholes in the guide tubes. The second design change involved adding sleeves in the upper ends of the guide tubes.

Both of these changes increase the hydraulic resistance in the guide tubes and thereby reduce the bypass flow through the guide tubes. Tne bypass flows in the other leakage paths remain the same. This is summarized in the following table:

1 Best Estimate Bypass Flow Rate

  • Bypass flow path Previous Now Outlet nozzle /CSB gap .61 .61 Core shroud /CSB annulus .62 .62 Alignment keys .09 .09 Guide tubes 1.38 .78+

2.70% 2.10%

As a result, the design bypass flow was reduced from the previous 3.5% value to the present 2.6% to take advantage of the lower expected leakage. The present design value of 2.6% contains an additional 0.5% increment over the best estimate value of 2.1% to account for the effects of core crudding, tolerances, etc.

6

  • Figures given in percent of W design of 148.0 x 10 lb/hr.

+See Appendix A for detailed breakdown of bypass flow through guide tubes and the flow networks used to calculate the present guide tube leakage.

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b) Guide Tube Designs A description of the guide tube designs before and after the design changes is given in the following table:

Before - center guide tube flow holes:

flow hole, area = in2 no sleeve, annular area between control rod and guide tube = in2

_c_orner guide tube _ flow holes: .

flow holes, area =L_ ,

no sleeve, annular a'rea between control rod and guide tube =

After - center guide tube flow holes.

flow holes, area =

sleeved guide tube, annular area =__ - __

_ corner guide tube flow holes.

flow holes, area = _

sleeved guide tube, annular area = _ ,

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t APPENDIX A Detailed Description of Bypass Flow Calculations for the Guide Tubes l

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The Waterford 3 reactor contains five different kinds of guide tubes. They are:

1. center guide tubes containing control rods (CEA's)
2. -center guide tubes containing in-core instrumentation
3. center guide tubes containing no control rods
4. corner guide tubes containing control rods
5. corner guide tubes containing no control rods Important values for the different types of guide tubes are summarized below.

Driving AP Flow

  • Type Number PSI lbm/hr  % of Q g Center GT, rodded 87 -

Center GT w/ICI 56 Center GT, unrodded 74 Corner GT, rodded 364 Corner GT, unrodded 504 TOTAL 1085 1,158,900 .78 l Notes concerning flow networks presented on following pages:

1. For convenience, the pressure at the exit of the rodded guide tubes is arbitrarily designated as 0 psi. All other pressures are referenced to this

,,. pressure.

2. The pressure loss coefficients along the branche: are shown in the form K/A2, which can be interpreted as the pressure loss coefficient per unit square area. The K values are based on empirical information from published literature and the design flow rate of 148x106 lbm/hr.

- . - - - , , - - - - , - . . - - , - . _ , , - - . - , - . , - .-, - , - - - , ,en, . .,

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RODCED CENTER GUIDE TUBES

Fue.1 Alignment Plate
[ ] f..

Upper 4N T N N.

End gLN D Fitting g j w

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h i

Lower #+

End

2 Fitting Core } }

Support Plate The numerical solution of the above network yields a GT bypass flow of lbm/hr The total bypass flow for the 87 rodded center guide tubes is lbm/hr e s - ,, , _ . . ~ . - - . - - . , , - , . - - , , . . - - . , - . . . - , .

INSTRIEENTED CENTER GUIDE TUBE ,

) Fuel Alignment

[ } { Plate

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N

  • Upper End r Fitting

..'l_L . ,

i l

k +.

l.. ,

i l l

i y Lower End

/ Fi tting Core Support

} } Plate The numerical solution of the above network yields a GT bypass flow of lbm/hr The total bypass flow for the 56 instrumented center guide tubes is lbm/hr b

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UNRODOED CENTER GUIDE TUBES f Fuel Alignment 3 f. Plate L y_ i Q '

N N Upper End M_ _k Fi tting W.

4 pt h Lower End Fi tting h { Core Support Plate Tiie numerical solution of the above network yields a GT bypass flow of lbm/hr l The total bypass flow for the 74 unrodded center guide tubes is i

_ _lbm/hr i

.+

RODDED CORNER GUIDE TUBES 5

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FUEL ALIGNMENT f }

t .

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UPPER END FITTING D: 3 v

Jb

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s, .

! 4 LOWER END FITTING f 4 CORE SUPPORT PLATE e

.; The numerical solution of the above network yields a GT bypass flow of Ibm /hr The total bypass flow for the 364 rodded corner tubes is lbm/hr

i UNRODDED CORNER GUIDE TUBES 4

Fuel l Alignment

i. Plate n

3 k

D. l Upper End g ,i Fitting a

f A

P Lower End Fitting

$ ) Core Support Plate The numerical solution of the above network yields a GT bypass flow of l

lbm/hr The total bypass flow for the 504 unrodded corner guide tubes is lbm/hr l

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