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ORNL-2106 - the Molten Salt Energy Technologies Web Site

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ANP PROJECT PROGRESS REPORT<br />

<strong>the</strong> shrinkage data described herein should be<br />

determined by conducting ano<strong>the</strong>r test prior to<br />

attempting fabrication of a pump with a complex<br />

volute.<br />

Since <strong>the</strong> shrinkage at position 3 was less than<br />

expected, it was not possible to use <strong>the</strong> spacers,<br />

as machined, to prevent fur<strong>the</strong>r shrinkage during<br />

annealing. The pump casing was annealed at<br />

185OOF for 4 hr in order to determine <strong>the</strong> necessity<br />

for this operation. The additional shrinkage of<br />

0.002 to 0.004 in. observed indicates that <strong>the</strong> role<br />

of residual stresses is significant. Properly<br />

machined spacers should be used to prevent fur<strong>the</strong>r<br />

shrinkage during annealing, as was accomplished<br />

in <strong>the</strong> previous investigation.'<br />

Brazing Studies<br />

Tests have also been performed to study <strong>the</strong><br />

feasibility of a brazed NaK (PK-2) pump volute.<br />

The component parts for <strong>the</strong> test are shown in<br />

Fig. 3.4.4. The bottom volute is shown with eight<br />

0.187-in.-diaI 1-in.-long lnconel shear pins inserted<br />

into 0.197-in.dia holes drilled to a depth<br />

of ?$ in. These pins were intended to provide<br />

approximately 5 in.2 of shear area to supplement<br />

<strong>the</strong> 18 in.2 of area that constitutes <strong>the</strong> faying<br />

surfaces of <strong>the</strong> upper and lower volutes in <strong>the</strong><br />

brazed assembly. The top volute is shown with<br />

0.200-in.-ID tubes welded over <strong>the</strong> shear pin holes<br />

to act as reservoirs for <strong>the</strong> Coast Metals No. 52<br />

brazing alloy. The alloy was applied in <strong>the</strong> form<br />

of 3.16-in.-dia slugs, which ranged from 3.8 to<br />

4 in. in length and were fabricated by casting<br />

in graphite molds. Several of <strong>the</strong>se slugs are<br />

shown in <strong>the</strong> center of Fig. 3.4.4. A total of<br />

30.8 g of Coast Metals No. 52 alloy was used.<br />

This amount was calculated to supply approximately<br />

0.19 in? of alloy, of which 0.048 in.3<br />

would fill <strong>the</strong> space between <strong>the</strong> shear pins and<br />

<strong>the</strong> shear pin holes and approximately 0.054 in.<br />

3<br />

would comprise a 0.0003-in.-thick brazing alloy<br />

layer between <strong>the</strong> faying surfaces of <strong>the</strong> volutes.<br />

It was expected that a surplus of brazing alloy<br />

would be desirable to ensure complete brazing.<br />

The excess alloy was to remain in <strong>the</strong> reservoirs.<br />

A 0.003-in. separation between <strong>the</strong> parts of <strong>the</strong><br />

volutes was achieved by using 0.003-in.dia nickel<br />

wire as a spacer.<br />

Micrometer measurements were made before and<br />

after brazing at <strong>the</strong> positions described in Fig.<br />

3.4.5. The assembly was braze$ at 1050°C in<br />

dry hydrogen. The heating and cooling rate of<br />

<strong>the</strong> brazing cycle was approximately 35O0C/hr,<br />

178<br />

and a hold time of 3 hr at 1050°C was used. A<br />

photograph of <strong>the</strong> completed assembly is shown<br />

in Fig. 3.4.6. As may be seen, excess brazing<br />

alloy flowed out of <strong>the</strong> capillary and down <strong>the</strong><br />

side of <strong>the</strong> casing. A similar condition was<br />

evident on <strong>the</strong> inside of <strong>the</strong> volute; <strong>the</strong>re wps a<br />

fillet of brazing alloy thinly distributed around<br />

<strong>the</strong> bottom volute.<br />

The failure of <strong>the</strong> reservoirs to retain <strong>the</strong> excess<br />

brazing alloy is attributed to <strong>the</strong> relatively large<br />

clearance between <strong>the</strong> lnconel shear pins and <strong>the</strong><br />

shear pin holes. It is expected that a clearance<br />

of 0.001 to 0.002 in., coupled with a supplementary<br />

capillary on <strong>the</strong> periphery of <strong>the</strong> casing, which<br />

could be removed later, would remedy this dif-<br />

ficulty.<br />

The braze joint was subjected to dye-penetrant<br />

and radiographic inspections and was considered<br />

to be sound. The degree of correlation between<br />

<strong>the</strong> radiographic interpretation and <strong>the</strong> joint sound-<br />

ness should be determined by metallographic<br />

exam i no t i on.<br />

The results of <strong>the</strong> micrometer measurements are<br />

summarized in Table 3.4.2. As may be noted,<br />

most of <strong>the</strong> dimensional changes found are within<br />

<strong>the</strong> limit of error of <strong>the</strong> measurements. As was<br />

expected, <strong>the</strong> data indicate that <strong>the</strong> brazed con-<br />

struction affords a high degree of dimensional<br />

control and should be given consideration as a<br />

fabrication method.<br />

TABLE 3.4.2. RESULTS OF MICROMETER<br />

MEASUREMENTS BEFORE AND AFTER BRAZING<br />

OF NaK (PK-2) PUMP VOLUTE<br />

Position<br />

Dimensions* (in.)<br />

As Assembled After Brazing Change<br />

A-1 3.815 3.813 -0.002<br />

2 3.818 3.817 -0.001<br />

3 0.629 0.628 -0.001<br />

B-1 3.817 3.817 0<br />

2 3.816 3.816 0<br />

3 0.629 0.627 -0.002<br />

c- 1 3.81 9 3.820 +0.001<br />

2 3.81 8 3.81 8 0<br />

3 0.629 0.628 -0.001<br />

D-1 3.818 3.817 -0.001<br />

2 3.816 3.815 -0.001<br />

3 0.629 0.628 -0.001<br />

*Estimated accuracy of measurement *0.001 in.<br />

6<br />

t<br />

c<br />

3<br />

C<br />

A<br />

*'<br />

L

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