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ORNL-2106 - the Molten Salt Energy Technologies Web Site

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ANP PROJECT PROGRESS REPORT<br />

decrease in ductility observed in ei<strong>the</strong>r alloy.<br />

The ductility of lnconel remained constant between<br />

800 and llOOOF at <strong>the</strong> slower strain rate and<br />

between 800 and 12OOOF at <strong>the</strong> faster strain rate.<br />

At higher temperatures <strong>the</strong> ductility steadily in-<br />

creased. The ductility of Nichrome V decreased<br />

steadily as <strong>the</strong> temperature was increased from<br />

800 to 14OOOF.<br />

Both alloys showed stress fluctuations at both<br />

strain rates, <strong>the</strong> fluctuations being more noticeable<br />

at <strong>the</strong> slower strain rate, but this may have been<br />

<strong>the</strong> result of <strong>the</strong> inadequacy of <strong>the</strong> recording<br />

system at high speeds. In <strong>the</strong> tests on lnconel<br />

<strong>the</strong> stress fluctuations were present at tempera-<br />

tures from 500 to 12OOOF and were largest in<br />

number and amplitude between 600 and 9500F.<br />

The lower temperature limit of <strong>the</strong>se fluctuations<br />

has not yet been determined for Nichrome V, but<br />

<strong>the</strong> upper limit seems to coincide with that of<br />

Inconel.<br />

Specimen2 of Monel, Inconel, and Nichrome V<br />

have been prepared for testing in <strong>the</strong> LlTR (and<br />

later in <strong>the</strong> MTR) to determine <strong>the</strong> effect of irradi-<br />

ation on ductility. Out-of-pile tests will be made<br />

on <strong>the</strong> Hastelloys.<br />

EFFECT OF RADIATION ON STATIC<br />

CORROSION OF STRUCTURAL MATERIALS<br />

BY FUSED-SALT FUELS<br />

W. E. Browning H. L. Hemphill<br />

The study of <strong>the</strong> effect of radiation on <strong>the</strong> corrosion<br />

of lnconel capsules containing static fusedsalt<br />

fuels was ~ontinued.~ Two additional lnconel<br />

capsules containing <strong>the</strong> fuel mixture (No. 30)<br />

NaF-ZrF,-UF, (50-46-4 mole %) were irradiated<br />

in <strong>the</strong> MTR for six weeks each at 15oooF at a<br />

power density of approximately 3.5 ckw/cm3. Two<br />

o<strong>the</strong>r lnconel capsules containing <strong>the</strong> fuel mixture<br />

(No. 44) NaF-ZrF,-UF, (53.5-40-6.5 mole %) are<br />

being irradiated at 15oooF at a power density of<br />

approximately 6 kw/cm3.<br />

Fur<strong>the</strong>r mockup tests were run on Hastelloy B<br />

capsules under simulated MTR conditions. A<br />

method was developed for mounting <strong>the</strong>rmocouples<br />

on <strong>the</strong> capsules without damaging <strong>the</strong> chromiumnickel<br />

plating required to protect <strong>the</strong> capsule from<br />

<strong>the</strong> atmosphere. Hastelloy B capsules are being<br />

prepared for bench tests and for MTR irradiation.<br />

7W. E. Browning and H. L. Hemphill, ANP Quar. Ptog.<br />

Rep. March 10. 19-56, <strong>ORNL</strong>-2061, p 192.<br />

238<br />

They will be filled with an NaF-YF-LiF-UF, fuel hs<br />

mixture containing approximately 25 wt % enriched<br />

uranium and LiF enriched in Li7.<br />

LlTR VERTICAL IN-PILE LOOP<br />

D. E. Guss'<br />

M. F. Osborne<br />

W. E. Browning<br />

H. E. Robertson<br />

R. P. Shields<br />

A vertical in-pile loop, which was essentially<br />

<strong>the</strong> same as <strong>the</strong> one operated previously,' was<br />

installed in <strong>the</strong> LlTR and put into operation; how-<br />

ever, <strong>the</strong> pump stalled when <strong>the</strong> reactor was<br />

started. By reducing <strong>the</strong> pump temperature it was<br />

possible to operate <strong>the</strong> loop with <strong>the</strong> reoctor at<br />

500 kw; but at higher power levels <strong>the</strong> temperature<br />

drop in <strong>the</strong> loop wos great enough to freeze <strong>the</strong><br />

fuel in <strong>the</strong> cold leg. The pump stalled permanently<br />

during an effort to increase <strong>the</strong> pump temperature<br />

gradually so that <strong>the</strong> reactor could be brought to<br />

full power. The specifications for <strong>the</strong> power<br />

characteristics of <strong>the</strong> loop were: toto! power,<br />

11.5 kw; maximum specific power, 577 w/cm3;<br />

dilution factor, 7.64.<br />

While <strong>the</strong> cause of <strong>the</strong> pump failure cannot be<br />

precisely determined until <strong>the</strong> loop has been<br />

examined, it is known, from <strong>the</strong> sounds emanating<br />

from <strong>the</strong> pump and heard through a microphone,<br />

and from variations in electric power demands of<br />

<strong>the</strong> motor, that contact of moving solid parts<br />

overloaded <strong>the</strong> motor.<br />

The parts that had already been fabricated for<br />

three additional loops will be changed to eliminate<br />

most of <strong>the</strong> possible causes of pump failure. The<br />

changes will include a shorter, more rigid impeller<br />

shaft and improved bearings. Also, pump models<br />

are being tested to determine <strong>the</strong> effect of in-<br />

creasing <strong>the</strong> clearance around <strong>the</strong> pump impeller.<br />

When <strong>the</strong>se tests are completed, existing parts<br />

will be modified and assembled for bench and in-<br />

pile tests.<br />

Although failure of <strong>the</strong> pump prevented operation<br />

of <strong>the</strong> loop, <strong>the</strong> experiment provided a test for <strong>the</strong><br />

reliabil ity of o<strong>the</strong>r components. Thermocouples,<br />

heaters, safety circuits, <strong>the</strong> temperature control<br />

system, <strong>the</strong> tachometer, <strong>the</strong> lead wires, and <strong>the</strong><br />

entire instrumentation system performed satis-<br />

factorily. Platinum-platinum-rhodium <strong>the</strong>rmo-<br />

'On assignment from United States Air Force.<br />

'G. W. Keilholtz et al., ANP Quar. Prog. Rep. Sept.<br />

10, 1955, <strong>ORNL</strong>-1947, p 164.

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