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JOM

, Volume 19, Issue 6, pp 8–10 | Cite as

Progress in superalloys for SST jet engines

  • W. J. Boesch
  • R. S. Cremisio
  • F. M. Richmond
News Feature
  • 6 Downloads

Abstract

The IMD High Temperature Alloy Committee sponsored a two-session program on the SST jet engine on February 20th at the 1967 AIME Annual Meeting in Los Angeles. At the two sessions, 14 technical papers presented a broad picture of the performance requirements and superalloy research necessary for the development of the SST engine.

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References

  1. 1.
    G. J. Wile, Polymet Corp., Cincinnati, Ohio: “Superalloys in SST Jet Engines—Opportunities and Hazards.”Google Scholar
  2. 2.
    E. J. Briggs, Jr., Flight Standards Service, FAA, Washington, D. C: “FAA Engine Certification for SST Engines.”Google Scholar
  3. 3.
    W. J. Glover, General Electric Co., F.P.D., Cincinnati, Ohio: “The Effect of Hold Time on Low Cycle Fatigue in Inconel 718.”Google Scholar
  4. 4.
    J. P. Stroup and L. A. Pugliese, Latrobe Steel Co., Latrobe, Pa.: “Influence of Very Low Carbon Contents on the Properties and Structures of Nickel and Nickel-Iron Base Superalloys.”Google Scholar
  5. 5.
    V. Mehra and J. F. Slepitis, Wright Aeronautical Div., Curtiss-Wright Corp., Wood-Ridge, N. J.: “Thermo-Mechanical Treatment of Age-Hardenable Alloys.”Google Scholar
  6. 6.
    H. J. Murphy, C. T. Sims and G. R. Heckman, General Electric Company, Schenectady, N. Y.: “Long-Time Structures and Properties of Three High-Strength Nickel-Base Alloys.”Google Scholar
  7. 7.
    J. R. Mihalisin, C. G. Bieber, INCO, Sterling Forest, N. Y., and R. T. Grant, INCO, New York, N. Y.: “Sigma—Its Occurrence, Effect, and Control in Nickel Base Super-alloys,”Google Scholar
  8. 8.
    M. L. Shepard, W. P. Danesi and M. J. Donachie, Jr, Pratt and Whitney Aircraft, E. Hartford, Conn.: “Hot Corrosion Resistance Related to Microstructural Stability of Several Nickel-Base Superalloys,”Google Scholar
  9. 9.
    J. B. Moore, Pratt and Whitney Aircraft, W. Palm Beach, Fla.: “Development of Astroloy Disks for Advance Jet Engine Application.”Google Scholar
  10. 10.
    R. Brunetaud, SNECMA, Paris, France: “Application of a Cracking Test Under Biaxial Stresses to Study the Weldability of Refractory Alloys.”Google Scholar
  11. 11.
    E. G. Thompson, Rocketdyne, Canoga Park, Calif.: “Hot Cracking Studies of Inconel 718 Weld Heat Affected Zones.”Google Scholar
  12. 12.
    T. K. Redden, General Electric Co., Cincinnati, Ohio: “Coating-Base Metal Interactions in Nickel Superalloys.”Google Scholar
  13. 13.
    J. C. Freche, R. L. Dreshfield and G. D. Sandrock, NASA, Lewis Research Center, Cleveland, Ohio: “Investigation of Cobalt-Tungsten Alloys for Advanced Gas Turbines.”Google Scholar
  14. 14.
    R. G. Barrows and J. B. Newkirk, University of Denver, Dept. of Metallurgy, Denver, Colo.: “A Study of Two Criteria for the Design of High Temperature Alloys,”Google Scholar

Copyright information

© The Minerals, Metals & Materials Society 1967

Authors and Affiliations

  • W. J. Boesch
    • 1
  • R. S. Cremisio
    • 1
  • F. M. Richmond
    • 2
  1. 1.Special Metals CorporationNew HartfordUSA
  2. 2.Universal-Cyclops Specialty Steel Div.Cyclops CorporationBridgevilleUSA

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