Comparative Evaluation of Forged Ti-6A1-4V Bar Made from Shot Produced by Rep and CSC Processes

  • R. F. Vaughan
  • P. A. Blenkinsop
  • P. H. Morton

Abstract

Like other studies(1,2) of titanium alloy powder, the present evaluation was targetted towards potential aerospace applications of consolidated material, in particular use in rotating aero-engine components.

Keywords

Consolidate Material Internal Origin Fracture Toughness Property Heat Treated Material Titanium Alloy Powder 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. 1.
    Friedman, G., Int. J. of Powder Met. 6 (2), 1970, 43.Google Scholar
  2. 2.
    Abkowitz, S., Titanium Science and Technology Vol 1, New York Plenum Press, 1973, 501.Google Scholar
  3. 3.
    Friedman, G., Metal Prog. 107, 1975, 81.Google Scholar
  4. 4.
    Hodkin, D. J., Sutcliffe, P. W., Marden, P. A. and Russell, R.E., Powder Met. 16, 1973, 277.Google Scholar
  5. 5.
    Geisendorfer, R. F., Saidak, R. J. and Harth, G. H., Titanium Science and Technology, Vol. 1, New York Plenum Press, 1973, 399.Google Scholar

Copyright information

© Springer Science+Business Media New York 1982

Authors and Affiliations

  • R. F. Vaughan
    • 1
  • P. A. Blenkinsop
    • 1
  • P. H. Morton
    • 1
  1. 1.New Metals DivisionImperial Metal Industries (Kynoch) Ltd., WittonBirminghamUK

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