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ORNL-2106 - the Molten Salt Energy Technologies Web Site

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ANP PROlECT PROGRESS REPORT<br />

<strong>the</strong> extrusion conditions for <strong>the</strong> special compositions.<br />

Two billets, T-23012 and T-23014, were<br />

extruded slowly at 2200°F with a 3/-in.-dia<br />

mandrel at an extrusion ratio of 5.41. Bo d alloys<br />

responded satisfactori ly, but <strong>the</strong> mandrel broke<br />

within <strong>the</strong> tube blank in each case. With a decreased<br />

rate of extrusion <strong>the</strong> billet remained in<br />

contact with <strong>the</strong> mandrel for an excessive length<br />

of time, and <strong>the</strong> resultant overheating of <strong>the</strong> tool<br />

caused a subsequent decrease in its ultimate<br />

strength. The utilization of a 1-in.-dia mandrel<br />

alleviated this problem. The final results of slow<br />

extrusion of <strong>the</strong>se alloys at 22OOOF are presented<br />

in Table 3.3.5. Extrusions 1 through 5, shown<br />

in Fig. 3.3.4, are representative of <strong>the</strong> good tube<br />

blanks obtained from <strong>the</strong>se special compositions.<br />

The tube blanks have been sent to <strong>the</strong> Superior<br />

Tu be Company for redrawing to 0.500-in.-OD,<br />

0.035-in.-wall tubing.<br />

TABLE 3.3.5. RESULTS OF THE FINAL EXTRUSIONS<br />

OF SPECIAL ALLOYS PREPARED BY THE<br />

INTERNATIONAL NICKEL COMPANY<br />

Mandrel size: 1 in. dio<br />

Nunber of<br />

Alloy Extrusion Extruded ~ccessful<br />

No. Ratio Shape Ex ir us ions<br />

T-230 11 21 Tube blank 2<br />

T-23012 7:l Tube blank 1<br />

T-23013 21 Tube blank 2<br />

T-23014 7:l Tube blank 1<br />

T-23015 7:l Tube blank 2<br />

T-230 11 6.25: 1 Rod 1<br />

T-23012 6.25: 1 Rod 1<br />

T-23013 6.25: 1 Rod 1<br />

T-23014 6.25: 1 Rod 1<br />

T-23015 6.25~1 Rod 1<br />

Hot rolling of <strong>the</strong> extruded rods was only moder-<br />

ately successful. The rolling temperature was<br />

varied between 1925 and 2100°F, and <strong>the</strong><br />

scheduled reduction was approximately 10% per<br />

pass. In general, <strong>the</strong> lower temperature proved<br />

to be more satisfactory for minimizing edge<br />

cracking. Each alloy was hot rolled to 0.250-in.<br />

strip, pickled, annealed at 205OoF for 1 hr, and<br />

1 64<br />

cold finished to 0.065-in. strip with an intermediate<br />

anneal at 2050°F for 4 hr. Final an- s<br />

nealing of each alloy was scheduled to yield a<br />

grain size of ASTM 6-7. Alloy T-23015 edge-<br />

cracked severely during hot rolling. The o<strong>the</strong>r<br />

alloys for which edge cracking did not interfere<br />

with <strong>the</strong> machining of sound test specimens will<br />

be evaluated for strength.<br />

Battelle Memorial Institute Compositions. - In<br />

cooperation with Battelle Memorial Institute in <strong>the</strong><br />

development of nickel-molybdenum-base alloys for<br />

h igh-temperature use, extrusion experiments were<br />

conducted on three promising compositions with<br />

<strong>the</strong> intention of producing seamless tubing for<br />

corrosion testing. A total of 10 forged billets<br />

representing portions of 220-lb air-melted heats<br />

was fabricated. The results of <strong>the</strong> experiments<br />

are presented in Table 3.3.6.<br />

Although fast extrusion at a ratio of 5.4:1 re-<br />

sulted in cracking on <strong>the</strong> inside, all <strong>the</strong>se tube<br />

blanks are being salvaged at <strong>the</strong> Superior Tube<br />

Company by drilling <strong>the</strong> as-extruded tube blank<br />

and thus increasing <strong>the</strong> inside diameter from to<br />

1 in. before tubing reducing. Tube No. 6, shown<br />

in Fig. 3.3.4, is representative of a good extrusion<br />

obtained from <strong>the</strong>se alloys. As is typical of most<br />

of <strong>the</strong>se h igh-strength n ic kel-molybdenum-base<br />

alloy extrusions, a certain amount of surface<br />

roughening was found on <strong>the</strong> inside, but it was<br />

not so severe as it appears to be in Fig. 3.3.4.<br />

Slight conditioning of <strong>the</strong> blanks before redrawing<br />

will eliminate <strong>the</strong>se defects. The cause of this<br />

roughening is not completely understood at this<br />

time, but it may be related to <strong>the</strong> surface condition<br />

of <strong>the</strong> billet before extrusion or to lubrication<br />

practice during extrusion. All <strong>the</strong> blanks are<br />

being fabricated to 0.500-in.-OD, 0.035-in.-waII<br />

tubing.<br />

<strong>ORNL</strong> Compositions. - The basic nickel-<br />

molybdenum alloy containing 15 to 20% mo-<br />

lybdenum possesses corrosion resistance on a par<br />

with that of Hastelloy B, better ductility and<br />

fabricability, but poorer strength properties. Con-<br />

sequently, alloy additions to <strong>the</strong> basic composition<br />

are required for improving <strong>the</strong> strength properties.<br />

The elements being investigated as streng<strong>the</strong>ners<br />

are Ti, AI, W, Nb, Cr, Fe, V, and C. In order to<br />

determine <strong>the</strong> effect of <strong>the</strong>se elements individually<br />

on corrosion resistance and to establish <strong>the</strong><br />

maximum quantity of each element that can he<br />

a<br />

*

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