Institute of Metals Division - Heat Treatment and Mechanical Properties of Ti-Fe Alloys

The American Institute of Mining, Metallurgical, and Petroleum Engineers
F. C. Holden H. R. Ogden R. I. Jaffee
Organization:
The American Institute of Mining, Metallurgical, and Petroleum Engineers
Pages:
8
File Size:
1960 KB
Publication Date:
Jan 1, 1957

Abstract

The properties of quenched Ti-Fe alloys have been correlated with their microstruc-tures. For specimens quenched from equilibrium in the a-ß field, the dominant micro-structural variable is the a-ß ratio. A comparison of specimens having equiaxed a-ß structures with those having acicular a-ß structures shows that the equiaxed specimens have better tensile ductility, but lower impact resistance. There is evidence to show that specimens with acicular structures reach equilibrium in the a-ß field more rapidly than specimens with equiaxed structures. Both strength and ductility are lowered by heat treatments below 700°C. IN previous work,1, 2 certain principles of the physical metallurgy of a-ß titanium alloys have been evolved. Most of these principles have been based on data obtained on alloy systems which undergo no eutectoid reaction, or in which the eutec-toid reaction is so sluggish as to be inoperative. The alloy systems previously studied included the Ti-Mn alloys, with and without a-stabilizing additions, and the binary Ti-Mo alloys. The most important of these principles are: I) The compositional factors which affect mechanical properties are solid solution strengthening, the martensite transformation, and instability of
Citation

APA: F. C. Holden H. R. Ogden R. I. Jaffee  (1957)  Institute of Metals Division - Heat Treatment and Mechanical Properties of Ti-Fe Alloys

MLA: F. C. Holden H. R. Ogden R. I. Jaffee Institute of Metals Division - Heat Treatment and Mechanical Properties of Ti-Fe Alloys. The American Institute of Mining, Metallurgical, and Petroleum Engineers, 1957.

Export
Purchase this Article for $25.00

Create a Guest account to purchase this file
- or -
Log in to your existing Guest account