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ORNL-1816 - the Molten Salt Energy Technologies Web Site

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ANP QUARTERLY PROGRESS REPORT<br />

7. METALLURGY AND CERAMICS<br />

W. D. Manly<br />

Metal I urgy<br />

el-molybdenum base alloys are being<br />

studied extensively as possible reactor structural<br />

materials with qualities superior to those of<br />

Inconel. Efforts are under way to evaluate and<br />

improve <strong>the</strong> existing alloys and to develop better<br />

ones, Radiator test assemblies have been fabri-<br />

cated, and weld stability and mechanical properties<br />

are being studied. Work has continued on <strong>the</strong><br />

preparation of duplex tubing, boron carbide shield-<br />

ing, tubular fuel elements, and o<strong>the</strong>r special<br />

materials. The results of oxidation resistance<br />

tests of brazing alloys are presented. In addition,<br />

<strong>the</strong> first production of beryllium oxide ceramics by<br />

casting from a slip which is basic is described.<br />

DEVELOPMENT OF NICKEL-MOLYBDENUM<br />

BASE ALLOYS<br />

The investigations under way for <strong>the</strong> evaluation<br />

of nickel-molybdenum base alloys as structural<br />

materials for circulating-fuel reactors include<br />

attempts to improve <strong>the</strong> ductility and <strong>the</strong> fabrica-<br />

bility of commercially available Hastelloy B through<br />

purification, and efforts to find ano<strong>the</strong>r suitable<br />

and improved nickel-molybdenum base alloy that<br />

has <strong>the</strong> strength and corrosion resistance of<br />

Hastelloy B. Fabrication experiments are being<br />

used to determine <strong>the</strong> effects of various treatments<br />

on <strong>the</strong> materials developed.<br />

Fabrication Experiments<br />

H. lnouye J. H. Coobs<br />

Meta I I urgy Division<br />

One of <strong>the</strong> difficulties experienced in <strong>the</strong> fabri-<br />

cation of Hastelloy B is due to <strong>the</strong> narrow range<br />

of forgeability of <strong>the</strong> alloy - between 1950 and<br />

21OOOF. The upper limit of forgeability is due to<br />

impurities which cause gra i n-boundary me1 ti ng .<br />

The low ductility at temperatures between 900 and<br />

180OOF is less understood, but it is believed to be<br />

due to aging and impurity precipitation in grain<br />

boundaries. Therefore efforts are being made<br />

to eliminate trace (tramp) elements by vacuum<br />

elting and <strong>the</strong> addition of elements to neutralize<br />

One of <strong>the</strong> most critical components of a circu-<br />

lating-fuel reactor will be <strong>the</strong> fluoride-to-NaK<br />

J. M. Warde<br />

Division<br />

heat exchanger, for which, because of its com-<br />

plexity and fragility, it will be highly desirable to<br />

have seamless tubing. Commercially available<br />

Hastelloy B tubing, which is now made by welding<br />

strip, is not satisfactory because of cracks in <strong>the</strong><br />

weld, checks on <strong>the</strong> surface, and, in <strong>the</strong> absence<br />

of severe working of <strong>the</strong> weld, nonuniform proper-<br />

ties. Therefore several extrusion experiments have<br />

been performed in an effort to produce seamless<br />

tubing.<br />

The initial extrusion experiments were attempts<br />

to produce rod from air melts of Hastelloys B and<br />

C. When extrusion temperatures above 21OO0F<br />

and up to 235OOF were used, <strong>the</strong> alloys fractured<br />

severely in all instances. For <strong>the</strong> subsequent<br />

experiments, <strong>the</strong> extrusion temperature was lowered<br />

to 21OO0F, and a reduction ratio of 6.3:l was<br />

established. The results obtained for <strong>the</strong> various -<br />

.<br />

t<br />

/<br />

c<br />

materials are summarized in <strong>the</strong> following.<br />

-<br />

Vacuum-Melted, As-Cost Hastelloy B. The 6’<br />

ingot that was extruded had been homogeneized<br />

at 21OOOF for 48 hr. The front of <strong>the</strong> extrusion<br />

fractured severely, but some improvement was<br />

noted in comparison with <strong>the</strong> air melts previously<br />

extruded.<br />

Air-Melted, As-Cast Hastelloy B PluyO.2% Ti<br />

as Ti-Mn-AI-Ni Master Alloy. The ingot was<br />

homogeneized 48 hr at 2 100°F before extrusion.<br />

The extrusion fractured severely, and no improvement<br />

in comparison with <strong>the</strong> vacuum melt was<br />

noted.<br />

Air-Melted, Commercial, Wrought Hastelloy B .<br />

The extrusion fractured severely and thus indicated<br />

that <strong>the</strong> cast structure was not responsible for<br />

<strong>the</strong> poor hot forgeability of <strong>the</strong> alloy.<br />

Air-Melted, Commercial, As-Cast Hastelloy C.<br />

The extrusion was made through a cascade die<br />

(cone plus shear) to determine <strong>the</strong> effect of die<br />

design. Thus far, <strong>the</strong> alloy has been extruded<br />

through cone dies varying from 45 to 25 deg and<br />

through a shear die. In all extrusions, <strong>the</strong> rod<br />

-.<br />

-<br />

;-<br />

fractured severely. An extrusion was also made 3 ,<br />

by containing <strong>the</strong> billet in an lnconel can 0.063 - 1<br />

in. thick on <strong>the</strong> outside diameter and with a %-in.-<br />

thick disk at <strong>the</strong> nose of <strong>the</strong> billet. The lnconel<br />

nose separated from <strong>the</strong> Hastelloy, but <strong>the</strong> Hastelloy * I<br />

. I<br />

c<br />

i<br />

-<br />

-

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