Increasing the lifetime of gas-turbine engine nozzle blades using a new monocrystalline alloy

S. G. Semenov; L. B. Getsov; A. S. Semenov; N. V. Petrushin; O. G. Ospennikova; A. A. Zhivushkin

doi:10.3103/S1052618816040117

Increasing the lifetime of gas-turbine engine nozzle blades using a new monocrystalline alloy

作者: Semenov S.G.¹, Getsov L.B.², Semenov A.S.¹, Petrushin N.V.³, Ospennikova O.G.³, Zhivushkin A.A.⁴
隶属关系:
1. Peter the Great Polytechnial University
2. Polzunov Scientific-Production Association for Research and Design of Power-Generating Equipment
3. All-Russia Research Institute of Aviation Materials
4. Klimov
期: 卷 45, 编号 4 (2016)
页面: 316-323
栏目: Realibility, Strength, and Wear Resistance of Machines and Structures
URL: https://journal-vniispk.ru/1052-6188/article/view/192874
DOI: https://doi.org/10.3103/S1052618816040117
ID: 192874

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详细

The article presents the results of experiments to study the creep of an intermetallic monocrystalline alloy used to manufacture nozzle blades. The results serve as a basis for calculating the creep-rupture strength and thermal fatigue of gas-turbine engine blades.