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Metal Matrix Composite Fabrication Procedures for Gas Turbine Engine Blades FREE

[+] Author Affiliations
J. A. Alexander, E. G. Parks, Jr., P. Melnyk

TRW Inc., Cleveland, OH

Paper No. 71-GT-46, pp. V001T01A046; 7 pages
doi:10.1115/71-GT-46
From:
  • ASME 1971 International Gas Turbine Conference and Products Show
  • ASME 1971 International Gas Turbine Conference and Products Show
  • Houston, Texas, USA, March 28–April 1, 1971
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7982-5
  • Copyright © 1971 by ASME

abstract

Metal matrix composites constitute an attractive class of materials which must be considered as serious candidates for application in advanced gas turbine engines. Materials development programs have been successful in fabricating and characterizing metallic composite materials. Demonstration programs have shown that aerospace structural components can be fabricated from them. This paper deals with the application of the diffusion bonding process to the formation of a complex shape such as a gas turbine engine fan blade from titanium or aluminum matrix composites. It deals with the route to volume producibility rather than with the documentation of progress to date.

Copyright © 1971 by ASME
This article is only available in the PDF format.

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