On the issue of research of the properties of the heat-resistant nickel single-crystal superalloys

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Abstract

The work studies issues to provide the guaranteed construction strength of the single-crystal rotor blades of the aviation gas turbine engines taking into account the anisotropic properties conditioned by their crystallographic orientation. Special attention is paid to research of the thermo-fatigue properties of the samples taken from the single-crystal superalloys. Influence of the thermo-cycling intervals on the durability of the samples with given orientation has been shown taking as an example ЖС36ВИ alloy.

About the authors

E. A. Tikhomirova

Klimov JSC

Author for correspondence.
Email: klimov@klimov.ru

Engineer

Russian Federation

A. A. Zhivushkin

Klimov JSC

Email: klimov@klimov.ru

Leading specialist

Russian Federation

L. B. Getsov

NPO CKTI JSC

Email: metall126@mail.ru

doctor of technical sciences
scientist

Russian Federation

A. I. Rybnikov

NPO CKTI JSC

Email: metall126@mail.ru

doctor of technical sciences
leader of department

Russian Federation

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