Summary
This paper discusses the development of high-temperature titanium alloys for use in gas turbine engines, airframes, and other applications. The high strength-to-density ratio of titanium makes it a very attractive design choice in energy-efficient high thrust-to-weight engines. Consideration is given to both alloy chemistry effects and the role of microstructure in determining mechanical properties. Future developments in alloy modifications and coating advances should result in increased use of titanium in demanding high-temperature applications.
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Eylon, D., Fujishiro, S., Postans, P.J. et al. High-Temperature Titanium Alloys—A Review. JOM 36, 55–62 (1984). https://doi.org/10.1007/BF03338617
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DOI: https://doi.org/10.1007/BF03338617