Development of thermal barrier coatings for rotor and nozzle turbine blades made of nickel-base super- and intermetallic alloys

Budinovskiy S.A., Smirnov A.A., Matveev P.V., Chubarov D.A.
UDC
629.7.023.224:629.7.03-226.2
DOI
10.18577/2307-6046-2015-0-4-5-5
Article PDF (Russian) (801.73 KB)
How to cite
Budinovskiy S.A., Smirnov A.A., Matveev P.V., Chubarov D.A. Development of thermal barrier coatings for rotor and nozzle turbine blades made of nickel-base super- and intermetallic alloys // Proceedings of VIAM. 2015. No. 4. DOI: 10.18577/2307-6046-2015-0-4-5-5. URL: https://test.viam.ru/en/journal/2015/4/5
Abstract

The complex thermal barrier coating (TBC) for rotor blades of jet prop engines made of nickel-base superalloy VZHM4 working at temperatures up to 1200°С is represented, and also application of high-temperature heat resistant coatings for intermetallic nickel-base alloys as a bond coatings for turbine nozzle blades working at temperatures up to 1250°С is considered. Results of high-temperature tests of VZhM4 and VKNA-25 alloys with applied TBC are represented. It is shown that [Ni–Cr–Al–Ta–Re–Y–Hf+Al–Ni–Y]+(Zr–Y–Gd)O TBC protects VZhM4 alloy at temperatures up to 1200°С and [Ni–Cr–Al–Hf+Al–Ni–Hf]+(Zr–Y–Gd)O HPC protects VKNA-25 alloy at temperatures up to 1250°С. Research of thermal conductivity of ceramic (Zr–Y–Gd)O material is made.

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