HIGH TEMPERATURE COMPOSITES

Abstract

Abstract: The purpose of this paper is to review the current state of development of new composite materials for advanced aircraft engines. The advantages and disadvantages of Ti-base.NiAl-base, and MoSi_2-base composites as replacements for today's Ni-base superalloys are discussed from the standpoint of key technical issues. current status, and future directions. Results describing progress in both improved understanding of the mechanisms of deformation and fracture, and improved material performance will be covered.

Key words: composites. Ti alloys, Ti-aluminides, NiAl, MoSi_2-base, jet engines

M. V. Nathal (NASA Lewis Research Center Cleveland OH. USA). HIGH TEMPERATURE COMPOSITES[J]. Acta Metallurgica Sinica (English Letters), 1995, 8(z1): 467-476.

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