Hostname: page-component-586b7cd67f-l7hp2 Total loading time: 0 Render date: 2024-11-29T15:20:13.401Z Has data issue: false hasContentIssue false

Tensile and Creep Behavior of Ordered Orthorhombic Ti2A1Nb-Based Alloys

Published online by Cambridge University Press:  26 February 2011

R.G. Rowe
Affiliation:
Ge Corporate Research and Development, Schenectady, NY 12301
D.G. Konitzer
Affiliation:
Ge Aircraft Engines, Cincinnati, OH 45215
A.P. Woodfield
Affiliation:
Ge Corporate Research and Development, Schenectady, NY 12301
J.C. Chesnutt
Affiliation:
Ge Aircraft Engines, Cincinnati, OH 45215
Get access

Abstract

Titanium aluminide alloys with compositions near Ti-25A1-25Nb at.% were prepared by both rapid solidification and ingot techniques. Their tensile and creep properties were studied after heat treatment to produce various microstructures containing ordered orthorhombic (O) [1], ordered beta (βo), and α2 phases. It was found that these alloys had higher specific strength from room temperature to 760°C than conventional α2 alloys. Ductility and tensile strength of O+βo alloys were strongly dependent upon heat treatment, with the highest strength observed as-heat-treated, and the highest ductility after long term aging. The creep resistance of single phase O and two phase O+βo alloys was strongly dependent upon heat treatment.

Type
Research Article
Copyright
Copyright © Materials Research Society 1991

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

1. Banerjee, D., Acta Met., 36, 871882, (1989).Google Scholar
2. Rowe, R.G., in, High Temperature Aluminides and Intermetallics, Edited by Whang, S. H., Liu, C.T., Pope, D.P. and Stiegler, J.O., TMS, AIME,Warrendale, OH,1990,375401.Google Scholar
3. Rowe, R.G., in, Microstructure/Property Relationships in Titanium Alloys and Titanium Aluminides,Edited by Kim, Y.-W, Hall, J.A. and Boyer, R.R.,TMS, AIME,Warrendale, OH,1990, To be publishedGoogle Scholar
4. Rowe, R.G., To be published.Google Scholar
5. Rowe, R.G. and Amato, R. A., in, Processing of Structural Metals by Rapid Solidification,Edited by Froes, F.H. and Savage, S.J.,ASM International, Materials Park, OH,1987,253260.Google Scholar
6. Rowe, R.G., U.S. Patent No. 4,654,858, (1987)Google Scholar
7. Larsen, J.M., Williams, K. A., Balsone, S. J. and Stucke, M. A., High Temperature Aluminides and Intermetallics, Edited by Whang, S.H., Liu, C.T., Pope, D.P. and Stiegler, J.O., TMS-AIME, Warrendale, PA, 1989, 521556.Google Scholar
8. Blackburn, M.J. and Smith, M.P., Report # WRDC-TR-89–4095, Final report, Contract # F33615-85-C-5030, U.S. Air Force, WRDC, Wright-Patterson AFB, OH, 1990Google Scholar
9. Rowe, R.G., Scripta Met., 24, 12091214, (1990).Google Scholar
10. Marquardt, B.J., Scarr, G.K., Chesnutt, J.C., Rhodes, C.G. and Fraser, H.L., Report # WRDC-TR-89–4133, Final report, Contract # F33615-85-C-5167, U.S. Air Force, WRDC, Wright-Patterson AFB, OH, 1990Google Scholar