Improving the quality of titanium alloy parts used in the space industry

The influence of surface plastic deformation on the surface layer roughness and fatigue strength of titanium alloy parts is considered. Statistical analysis of experimental data is carried out. The dependence of roughness change on the value of load on the treated surface, fatigue crack propagation in titanium alloys on the state of the surface layer is established. Comparative analysis of the carrying capacity of gas turbine engine blades made of BT-3, BT-6 alloys with the use of Autodesk Fusion 360 software product is carried out. © 2021, Univelt Inc. All rights reserved.

Authors
Asoyan A. 1, 2 , Gorshkov A. 2 , Danilov I. 2 , Marusin A. 2
Conference proceedings
Advances in the Astronautical Sciences
Publisher
Univelt Inc.
Language
English
Pages
621-629
Status
Published
Volume
174
Year
2021
Organizations
  • 1 Moscow Automobile and Road Construction State Technical University (MADI), 64 Leningradsky prospect Str., Moscow, 125319, Russian Federation
  • 2 Department of Mechanical Engineering and Instrumentation, RUDN University, 6 Miklukho-Maklaya Str., Moscow, 117198, Russian Federation
Keywords
Aerospace industry; Fatigue crack propagation; Plastic deformation; Space applications; Space flight; Space platforms; Surface roughness; Titanium alloys; Autodesk; Comparative analysis; Fatigue strength; Roughness change; Software products; Space industry; Surface layers; Surface plastic deformation; Fatigue of materials
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