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ORNL-2106 - the Molten Salt Energy Technologies Web Site

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FABRICATION OF JOINTS BETWEEN PUMP<br />

BARRELS AND THE PRESSURE SHELL<br />

OF THE ART<br />

P. Patriarca<br />

The ability to weld an accurately machined and<br />

properly stress-relieved pump barret to a thick-<br />

walled pressure shell without <strong>the</strong> need for finish<br />

machining or subsequent stress relieving would<br />

simplify considerably <strong>the</strong> assembly of <strong>the</strong> “north<br />

head” of <strong>the</strong> ART. A design was suggested to<br />

permit such a procedure, and a test was conducted<br />

to evaluate <strong>the</strong> feasibility of <strong>the</strong> design.<br />

The component parts of <strong>the</strong> joint used for <strong>the</strong><br />

test are shown in Fig. 3.4.7. The liner flange<br />

is shown attached to <strong>the</strong> pump barrel sleeve,<br />

which in turn was welded to <strong>the</strong> pump barrel. The<br />

liner flange is also shown attached to a carbonsteel<br />

pipe, .. which was in turn welded to a 2k-in.-<br />

~<br />

thick carbon-steel base plate. This auxfliary<br />

weldment was intended to provide a degree of<br />

restraint comparable to that to be expected from<br />

<strong>the</strong> northhead expansion tank.<br />

PERfOD ENDING JUNE 10, 1956<br />

It is interesting to note that at least partial<br />

relief of residual stresses was accomplished by<br />

cutting <strong>the</strong> barrel assembly from <strong>the</strong> restraints<br />

und soaking at 1SWF. This procedure resulted<br />

in additional diametrical changes, which indicate<br />

that some distortion will occur in <strong>the</strong> north head<br />

in service that may be unacceptable.<br />

Axial changes were also determined by mi-<br />

crometer measurements at <strong>the</strong> positions described<br />

in Fig. 3.4.12. The results of <strong>the</strong> measurements<br />

are summarized in Table 3.4.4. It may be noted<br />

that an axial shift occurred that was significant<br />

in magnitude but remarkably small for <strong>the</strong> amount<br />

of welding involved. These results indicate that<br />

some distortion is inevitable and must be ei<strong>the</strong>r<br />

accepted or removed by subsequent machining and<br />

that a stress relief anneal will be necessary to<br />

remove effects of residual stresses during oper-<br />

ation.<br />

TABLE 3.4.4. RESULTS OF MICROMETER<br />

MEASUREMENTSONAXISOF PUMPBARREL<br />

Dimensions (in.)<br />

It may be noted that <strong>the</strong> shell flange is quite Posit ion Before After<br />

large, <strong>the</strong> intent being to minimize distortion of Welding Welding<br />

Change<br />

<strong>the</strong> flange and <strong>the</strong>reby require a realistic proportion<br />

of <strong>the</strong> distortion during welding to occur A1 2.459 2.447 -0.01 2<br />

in <strong>the</strong> barrel sleeve and hence in <strong>the</strong> barrel itself.<br />

The restraint provided by <strong>the</strong> auxiliary weldment<br />

2<br />

3<br />

2.459<br />

2.444<br />

2.468<br />

2.468<br />

+0.009<br />

+ 0.024<br />

shown in Fig. 3.4.8 was intended to supplement 4 2.437 2.431 -0.006<br />

<strong>the</strong> afore-mentioned condition and, hence, to more<br />

nearly simulate <strong>the</strong> northhead pressure shell.<br />

B1<br />

2<br />

2.492<br />

2.466<br />

2.480<br />

2.470<br />

-0.012<br />

+ 0.004<br />

2.433 +0.017<br />

s welded into <strong>the</strong> p 2.429 -0.008<br />

welding procedure<br />

2.516 -0.008<br />

determined by micrometer me<br />

2.474<br />

2.394<br />

2.431<br />

+0.001<br />

+ 0.01 4<br />

-0.006<br />

2.56T -0.002<br />

2.573 -0.002<br />

2.361 +0.010<br />

2.437 -0.003<br />

2.594 0<br />

summarized In Table<br />

d that <strong>the</strong> maximum changes<br />

considering <strong>the</strong> extent of<br />

2.478<br />

2.321<br />

2.438<br />

-0.006<br />

+0.003<br />

- 0.004<br />

181

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