ORNL-1816 - the Molten Salt Energy Technologies Web Site
ORNL-1816 - the Molten Salt Energy Technologies Web Site
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 />
-