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    HU Chun-yan, ZHAO Xu, LIU Xin-ling. Failure Analysis of Flexible Shaft of Starter-Generator for A Plane[J]. Materials and Mechanical Engineering, 2011, 35(3): 92-94.
    Citation: HU Chun-yan, ZHAO Xu, LIU Xin-ling. Failure Analysis of Flexible Shaft of Starter-Generator for A Plane[J]. Materials and Mechanical Engineering, 2011, 35(3): 92-94.

    Failure Analysis of Flexible Shaft of Starter-Generator for A Plane

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    • Received Date: December 15, 2010
    • Flexible shaft of the starter-generator for a plane fractured early after serving for 160 h. In order to find out the fracture cause, fracture observation, wear trace analysis, hardness test and microstructure analysis were carried out. The results show that the fracture mode of the flexible shaft was low cycle fatigue failure under high stress. The main reason for the flexible shaft fracture was that the abnormal bending stress was caused by the dislocation of the flexible shaft of engine and generator as link dislocation of end cap and ring flange. The stress superposition of the mormal distorting and abnormal bending stress which exceeded the fatigue strength of the shaft. The fracture of the flexible shaft could be effectively prevent by improving the height of the dowels.
    • [1]
      《中国航空材料手册》编辑委员会.航空材料手册[M].北京: 中国标准出版社, 2002.
      [2]
      冯冬维, 苏德达.超高强度50CrVA弹簧钢丝扭转疲劳性能及其断口分析[J].弹簧工程, 1991(1):32-39.
      [3]
      陶春虎, 习年生, 钟培道,等.航空装备失效典型案例分析[M].北京: 国防工业出版社, 1998.
      [4]
      路兰英.启动发电机软轴断裂分析[J].材料工程, 2003(增刊): 100-102.
      [5]
      张栋, 钟培道, 陶春虎, 等.失效分析[M].北京: 国防工业出版社, 2004.

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