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首页> 外文期刊>Journal of Failure Analysis and Prevention >Investigation of Fatigue Failures of Titanium Alloy Blades Used in Compressor Modules of Aeroderivative Industrial Gas Turbines
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Investigation of Fatigue Failures of Titanium Alloy Blades Used in Compressor Modules of Aeroderivative Industrial Gas Turbines

机译:航空衍生工业燃气轮机压缩机模块用钛合金叶片的疲劳失效研究

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摘要

Gas turbine axial compressor blades are designed to withstand cyclic stress loading resulting of modal vibrations. However, when surface suffers from foreign object damage, a fatigue crack is likely to initiate. In this paper two failure case-studies of titanium alloy used for aeroderivative gas turbine compressor blades are presented. Both are related to a failure of first stage compressor blades coming from different turbine power ranges. Observed cracks were found at blade spans corresponding to modal vibrations.
机译:燃气轮机轴向压缩机叶片设计用于承受模态振动引起的循环应力载荷。但是,当表面遭受异物损坏时,可能会产生疲劳裂纹。本文介绍了用于航改燃气涡轮压缩机叶片的钛合金的两个失效案例研究。两者都与来自不同涡轮功率范围的一级压缩机叶片的故障有关。在叶片跨距上发现了与模态振动相对应的裂纹。

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