An Investigation of the Protective Action of a Coating Based on Yttrium Aluminosilicate System on Silicon Carbide Material at a Temperature up to 1500°С


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Abstract

A coating based on a precursor of yttrium silicate and yttrium aluminosilicate systems on the ceramic composite material based on silicon carbide was obtained by the Schlicker-firing method and atmospheric plasma spraying. In addition, the regularities of effect of oxidation medium on the heat resistance of this coating at a temperature up to 1500°С inclusive were established.

About the authors

V. A. Voronov

All-Russian Scientific Research Institute of Aviation Materials

Author for correspondence.
Email: voronovvs89@gmail.com
Russian Federation, Moscow, 105005

Yu. E. Lebedeva

All-Russian Scientific Research Institute of Aviation Materials

Email: voronovvs89@gmail.com
Russian Federation, Moscow, 105005

O. Yu. Sorokin

All-Russian Scientific Research Institute of Aviation Materials

Email: voronovvs89@gmail.com
Russian Federation, Moscow, 105005

M. L. Vaganova

All-Russian Scientific Research Institute of Aviation Materials

Email: voronovvs89@gmail.com
Russian Federation, Moscow, 105005

D. V. Grashchenkov

All-Russian Scientific Research Institute of Aviation Materials

Email: voronovvs89@gmail.com
Russian Federation, Moscow, 105005

N. I. Artemenko

All-Russian Scientific Research Institute of Aviation Materials

Email: voronovvs89@gmail.com
Russian Federation, Moscow, 105005

A. V. Zavodov

All-Russian Scientific Research Institute of Aviation Materials

Email: voronovvs89@gmail.com
Russian Federation, Moscow, 105005

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