Skip to main content
Log in

Effect of Long-Term 1093 K Exposure to Air or Vacuum on the Structure of Several Wrought Superalloys

  • Published:
Journal of Materials Engineering and Performance Aims and scope Submit manuscript

Abstract

Long-term 1093 K heat treatments of three commercial superalloy sheet materials were undertaken in air and vacuum. With either exposure, significant precipitation of second phases occurred in the Co-base Haynes® Alloy 188 (HA 188) and the Ni-base Haynes® Alloy 230 (HA 230); however, much less precipitation was found in the exposed Ni-base alloy Inconel® 617 (IN 617). Although some grain growth occurred in HA 188, no changes in the grain size of either HA 230 or IN 617 were observed after 22,500 h at temperature. Oxidation during air heat treatments led to weight gain due to the formation of chromia + spinel scales and surface-connected grain boundary pits/oxides in all three superalloys. Both the weight gain and depth of intergranular attack were dependent on the square root of time, which is indicative of diffusion-controlled phenomena. Because many alloy samples had neighbors in close proximity, dmost vacuum heat treated specimens did not suffer significant loss of volatile elements. However, some exposed samples were subjected to unrestricted vacuum heat treatments, allowing estimates of volatilization to be made. Based on the data for HA 188, the weight loss during 1093 K vacuum exposure was diffusion controlled once the inhibiting effects of surface films on the as-received alloys were broken down.

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.

Similar content being viewed by others

References

  1. T.L. Labus, R.R. Secunde, and R.G. Lovely, Solar Dynamic Power Module Design, Paper No. 899277,IECEC ’89, Vol 1,IEEE, 1989, p 299–307

    Google Scholar 

  2. H.J. Strumpf, R.P. Rubley, and M.G. Coombs, Material Compatibility and Simulation Testing for the Brayton Engine Solar Receiver for the NASA Space Station Freedom Solar Dynamic Option,Paper No. 899076,IECEC ’89, Vol 2, IEEE, 1989, p 895–903

    Google Scholar 

  3. R.C. Schulze, NASA CR-54781, 1965

  4. D.T. Bourgette and H.E. McCoy,Trans. ASM, Vol 59, 1966, p 324–339

    CAS  Google Scholar 

  5. J.D. Whittenberger,J. Mater. Eng., Vol 12, 1990, p 211–226

    CAS  Google Scholar 

  6. J.D. Whittenberger,J. Mater. Eng. Perf., Vol 1, 1992, p 469–482

    CAS  Google Scholar 

  7. J.D. Cotton and L.M. Sedgwick, Compatibility of Selected Superalloys with Molten LiF-CaF2 Salt, Paper No. 899235,IECEC ’89, Vol 2, IEEE, 1989, p 917–921

  8. M. Rothman, Haynes International, personal communication

  9. W.L. Mankins, J.C. Hosier, and T.H. Bassford,Metall. Trans.,Vol 5, 1974, p 2579–2590

    Article  CAS  Google Scholar 

  10. C.A. Barrett,Environmental Degradation of Engineering Materials,Virginia Polytechnical University, 1977, p 319–327

  11. J.R. Stephens and C.A. Barrett, NASA TM-83609, 1984

  12. P. Ganesan and G.D. Smith,J. Mater. Eng., Vol 9, 1988, p 337–343

    CAS  Google Scholar 

  13. D.T. Bourgette, ORNL-TM-13677, 1964

  14. L.A. Chariot and R.E. Westerman,Corrosion, Vol 23, 1967, p 50–56

    Google Scholar 

  15. D.T. Bourgette, ORNL-TM-1786, 1967

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Whittenberger, J.D. Effect of Long-Term 1093 K Exposure to Air or Vacuum on the Structure of Several Wrought Superalloys. JMEP 2, 745–758 (1993). https://doi.org/10.1007/BF02650066

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02650066

Keywords

Navigation