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NASA NTRS · 19950013260

New Trends in Coatings Developments for Turbine Blades: Materials Processing and Repair

S Alpérine·R Martinou·R Mévrel·J P Huchin
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Abstract

Turbine engines for aeronautic applications now have to face strenuous requirements concerning not only operating performances but also reliability and repairability. This evolution of the specifications induces important consequences regarding the choice and the design of turbine blade protective coatings. This paper presents several key features concerning the deposition techniques and the real-life behavior of such coatings: (1) complex aluminides well suited to the protection against high temperature oxidation and hot corrosion of directionally solidified nickel-base superalloy turbine blades; (2) ceramic coatings used as thermal barriers - they have to exhibit both high resistance to thermomechanical fatigue and adequate smoothness; (3) processing techniques for thermal barriers, including plasma spraying, electron beam physical vapor deposition and plasma enhanced chemical vapor deposition; and (4) blades and coatings repair techniques.

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S Alpérine, R Martinou, R Mévrel, J P Huchin. 1994-11-01. New Trends in Coatings Developments for Turbine Blades: Materials Processing and Repair. https://ntrs.nasa.gov/citations/19950013260

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