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ASTM Selected Technical Papers
Fiber-Strengthened Metallic Composites
By
Aerospace Panel of the ASTM-ASME Joint Committee on Effect of Temperature on the Properties of Metals
Aerospace Panel of the ASTM-ASME Joint Committee on Effect of Temperature on the Properties of Metals
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ISBN-10:
0-8031-6179-4
ISBN:
978-0-8031-6179-5
No. of Pages:
185
Publisher:
ASTM International
Publication date:
1967

An investigation of the fibering of oxides by hot deformation in metal matrices was carried out using unalloyed columbium or tantalum as the matrix material and thorium oxide, zirconium oxide, magnesium oxide, or aluminum oxide. Composites were prepared by conventional powder metallurgical techniques and extrusion. The composites were examined for microstructures and fiber length-to-diameter ratio and tested in tension at room temperature and 1100, 2200, 2500, 2750, and 3000 F. Stress-rupture tests were conducted on the composites at 2200 and 2500 F for times up to 1000 hr. It was found that the oxides could be plastically deformed into fibers at temperatures well below their melting points when mechanically worked in a ductile matrix. Composites produced in this way exhibited improved tensile strengths and ratios of tensile strength to density as well as improved stress-rupture strength when compared to additive-free matrix materials and compared favorably with some commercial alloys.

1.
Sutton
,
W. H.
, and
Chorne
,
J.
, “
Development of High-Strength, Heat-Resistant Alloys by Whisker Reinforcement
,”
ASM Metal Engineering Quarterly, American Society for Metals
, Vol.
3
,
1963
, p. 44.
2.
Cratchley
,
D.
, and
Baker
,
A. A.
, “
The Tensile Strength of Silica Fibre Reinforced Aluminum Alloy
,”
Metallurgica
, Vol.
69
,
1964
, p. 153.
3.
Otto
,
W. H.
, “
Properties of Glass Fibers at Elevated Temperatures
,”
Proceedings of the Sixth Sagamore Ordnance Materials Research Conference
, Report No. MET661-601,
Syracuse University Research Inst.
,
1959
.
4.
Gyorgak
,
C. A.
, “
Extrusion at Temperatures Approaching 5000 F
,” NASA TN D-3014,
National Aeronautics and Space Administration
,
1965
.
5.
Hoffman
,
G. A.
, and
Knapp
,
W. J.
, “
On the Linear Relation Between the Softening Temperature and the Melting Point of Ceramics
,” Rand Corp. RM-2263, AD-206554,
1958
.
6.
Wachtman
,
J. B.
, Jr.
, and
Maxwell
,
L. H.
, “
Factors Controlling Resistance to Deformation and Mechanical Failure in Polycrystalline (glass free) Ceramics
,” WADC TR 57-526,
National Bureau of Standards
,
1957
.
7.
Quantinetz
,
M.
,
Weeton
,
J. W.
, and
Herbell
,
T. P.
, “
Studies of Tungsten Composites Containing Fibered or Reacted Additives
,” NASA TN D-2757,
National Aeronautics and Space Administration
,
1965
.
8.
Warrick
,
R. J.
, and
Van Vlack
,
L. H.
, “
Plastic Deformation of Nonmetallic Inclusions Within Ductile Metals
,”
ASM Transactions, American Society for Metals
, Vol.
57
,
1964
, p. 672.
9.
Bruckart
,
W. L.
,
Craighead
,
C. M.
, and
Jaffee
,
R. J.
, “
Investigation of Molybdenum and Molybdenum-Base Alloys Made by Powder-Metallurgy Techniques
,” WADC TR 54-398,
Battelle Memorial Institute
,
1955
.
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