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ORNL-2106 - the Molten Salt Energy Technologies Web Site

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EFFECTOF ENVIRONMENTONCREEP-<br />

RUPTURE PROPERTIES<br />

OF HASTELLOY 6<br />

C. R. Kennedy'<br />

Revised design data obtained from creep tests<br />

of solution-annealed Hastelloy B sheet stock in<br />

various environments at 1300, 1500, and 1650°F<br />

ore summarized in Figs, 3.5.1, 3.5.2, and 3.5.3.<br />

The times to 0.5, 1, 2, 5, and 10% total strain at<br />

each temperature in <strong>the</strong> various environments are<br />

<strong>the</strong> same, and for stresses for which <strong>the</strong> rupture<br />

life is more than 300 hr <strong>the</strong> effect of environment<br />

is shown to be negligible. The creep curves<br />

obtained at 1500OF in air and in argon, shown in<br />

Fig, 3.5.4, appear to indicate that <strong>the</strong> better<br />

performance in air than in <strong>the</strong> o<strong>the</strong>r environments<br />

at stresses for which <strong>the</strong> rupture life is less than<br />

'On assignment from Pratt 8, Whitney Aircraft.<br />

3.5. MECHANICAL PROPERTIES STUDIES<br />

D. A. Douglas<br />

(0 20 50 400 200<br />

TIME (hr)<br />

PERIOD ENDING JUNE 16, 1956<br />

300 hr is caused by <strong>the</strong> ability of air to streng<strong>the</strong>n<br />

Hastelloy B during third-stage creep. For rupture<br />

lives longer than 300 hr <strong>the</strong>re is considerably<br />

less third-stage creep because of <strong>the</strong> aging<br />

characteristics of <strong>the</strong> alloy, and, as seen in<br />

Figs. 3.5.1, 35.2, and 3.5.3, <strong>the</strong> effect of environ-<br />

ment diminishes. Design curves produced from<br />

limited data for solution-annealed Hastelloy B<br />

sheet tested at 1800OF in argon and in <strong>the</strong> fuel<br />

mixture (No. 30) NaF-ZrF,-UF, (50-46-4 mole %)<br />

are shown in Fig. 3.5.5. At 180OOF Hastelloy B<br />

does not age perceptibly and <strong>the</strong> amount of third-<br />

stage creep is great in tests at all stress levels.<br />

Thus <strong>the</strong> fuel dxture streng<strong>the</strong>ns <strong>the</strong> alloy at all<br />

stress levels, Of <strong>the</strong> environments tested, only<br />

those which are "surface active" (produce a<br />

thin, tightly adherent film on <strong>the</strong> surface of <strong>the</strong><br />

metal) affect <strong>the</strong> creep properties of <strong>the</strong> metal.<br />

It can be seen from Figs. 3.5.1, 3.5.2, 3.5.3,<br />

and 3.5.5 that, of <strong>the</strong> environments tested, only<br />

500 tow 2<br />

5FeRu<br />

<strong>ORNL</strong>-LR-DWG 14729<br />

D 5000 10,Ooo<br />

Fig. 3.5.1. Design Curves for Hastelloy B Sheet Solution Annealed at 210OOF for 2 hr and Tested<br />

in Argon and in <strong>the</strong> Fuel Mixture (No. 30) NaF-ZrF,-UF, (50-46-4 mole 56) at 1300OF.<br />

2 01

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