Thermomechanical optimisation of fatigue strength for aircraft engine parts

机译：飞机发动机零件疲劳强度的热机械优化

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The manufacturing process of compressor blades from heat-resistant double-phase titaniun alloy BT8M1 (Ti-5A1-4Mo-1Sn-1Zr) for Motor-Sich JSC turbo-shaft engine has been studied. The objective of study was definition of the manufacturing factors affecting the blades altering of resistance to fatigue and definition of critical points of the manufacturing process.

机译：研究了Motor-Sich JSC涡轮轴发动机用耐热双相钛合金BT8M1（Ti-5A1-4Mo-1Sn-1Zr）制成的压缩机叶片的工艺。研究的目的是确定影响叶片抗疲劳性的制造因素，并确定制造过程的关键点。

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来源
《Surface treatment : Computer methods and experimental measurements》|1997年|p.361-369|共9页
会议地点 Oxford(GB)
作者
P.D.Zhemanyuk; I.E.Kovalev; V.G.Mikhailutsa; S.A.Voitenko; F.P.Banas; A.P.Petrov; A.E.Kovalev;
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正文语种 eng
中图分类金属学与金属工艺;
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Thermomechanical optimisation of fatigue strength for aircraft engine parts

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