Skip to main content
Log in

Progress in superalloys for SST jet engines

  • News Feature
  • Published:
JOM Aims and scope Submit manuscript

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.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Similar content being viewed by others

References

  1. G. J. Wile, Polymet Corp., Cincinnati, Ohio: “Superalloys in SST Jet Engines—Opportunities and Hazards.”

  2. E. J. Briggs, Jr., Flight Standards Service, FAA, Washington, D. C: “FAA Engine Certification for SST Engines.”

  3. W. J. Glover, General Electric Co., F.P.D., Cincinnati, Ohio: “The Effect of Hold Time on Low Cycle Fatigue in Inconel 718.”

  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.”

  5. V. Mehra and J. F. Slepitis, Wright Aeronautical Div., Curtiss-Wright Corp., Wood-Ridge, N. J.: “Thermo-Mechanical Treatment of Age-Hardenable Alloys.”

  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.”

  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,”

  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,”

  9. J. B. Moore, Pratt and Whitney Aircraft, W. Palm Beach, Fla.: “Development of Astroloy Disks for Advance Jet Engine Application.”

  10. R. Brunetaud, SNECMA, Paris, France: “Application of a Cracking Test Under Biaxial Stresses to Study the Weldability of Refractory Alloys.”

  11. E. G. Thompson, Rocketdyne, Canoga Park, Calif.: “Hot Cracking Studies of Inconel 718 Weld Heat Affected Zones.”

  12. T. K. Redden, General Electric Co., Cincinnati, Ohio: “Coating-Base Metal Interactions in Nickel Superalloys.”

  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.”

  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,”

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Boesch, W.J., Cremisio, R.S. & Richmond, F.M. Progress in superalloys for SST jet engines. JOM 19, 8–10 (1967). https://doi.org/10.1007/BF03378579

Download citation

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF03378579

Navigation