ML20100P705

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Applicant Exhibit A-P-17,consisting of Undated Table, Cyclic Stresses in Ae Piston Skirts Under Isothermal & Steady-State Conditions
ML20100P705
Person / Time
Site: Shoreham File:Long Island Lighting Company icon.png
Issue date: 09/10/1984
From:
AFFILIATION NOT ASSIGNED
To:
References
OL-A-P-017, OL-A-P-17, NUDOCS 8412140396
Download: ML20100P705 (2)


Text

..

./

e

o l

1,. !

2 p.

Q\\

(bf

~

t.-

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o (.

< r+

L36 Hg

'l*M ~

g

.J e

CYCLIC STRESSES IN AE PISTON SKIRTS UWER E

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IS0 THERMAL AW STEADY-STATE COWITIONS

'A d

op'

- h

/

AE j

Notes F.E.

nominal min max

%in 1

<------------ -68.1- ----------->

%ax 1ift-off 1

7.32 ----------->

no 11ft-off 1

1. 77 -------- -- >

kj 2

96.9 83.7 45.7 121 kf 2

118 24.0 7.95 283 90 o

3 7

1.999 1.403 0

2.140 g

9

0. 157 0

0 0.285 11 0

0 0

0 O

isoEhermal.

9

-62.1

-62.9

-62.0

-63.4 gi,

4 7-

-57.5-

-59.7

-60.3

-58.4 11

-66.7

-66.2

-63.8

-68.1 Sin,

4 7

-33.0

-42.7

-50.9

-31.5 steady-state 9

-37.6

-45.9

-52.7

-36.6 11

-42.2

-49.1

-54.4

-41.6

%ax,

5 7

7.91 7.74 1.77 7.96 steady-state 9

7.37 1.77 1.77 7.40 11 1.77 1.77 1.77 1.77 all suresses.in kst, go and ( In mils Notes:

1. From isothermal finite element calculations of skirt with crown, no gap closure.
2. From finite Clement calculations and estimates based on experiments.
3. Maximum crown / skirt lift-off distance in mils based on crown / skirt model.
4. From crown / skirt interaction model.
5.. Equals %ax with no lift-off if a = 0, adjusted from finite element %ax t

with lift-off if at > 0 by use of crown / skirt interaction model.

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8412140396 840910 4

PDR ADOCK 05000 o

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