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Using Solid-State Joining in Gas Turbine Engines FREE

[+] Author Affiliations
D. C. Martin

Battelle Memorial Institute, Columbus, OH

F. R. Miller

Air Force Materials Laboratory, Wright-Patterson Air Force Base, Columbus, OH

Paper No. 72-GT-74, pp. V001T01A073; 16 pages
doi:10.1115/72-GT-74
From:
  • ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show
  • ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show
  • San Francisco, California, USA, March 26–30, 1972
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7981-8
  • Copyright © 1972 by ASME

abstract

The ability to fabricate materials and components needed to improve gas-turbine engine performance depends on an ability to achieve reliable joints. Solid-state joining provides this ability. Diffusion bonding of compressor blades, friction welding of engine rotors, and solid-state bonding of turbine shafts by coextrusion of dissimilar metals are discussed as examples of applications of solid-state bonding. Parts made by these techniques have successfully completed engine tests.

Copyright © 1972 by ASME
Topics: Joining , Gas turbines
This article is only available in the PDF format.

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