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某型航空发动机机匣同轴度测量 被引量:5

Casing Coaxiality Measurement for an Aeroengine
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摘要 为解决由于发动机机匣同轴度不合格引起发动机转、静子碰摩而发生的振动问题,阐述了某型航空发动机机匣同轴度的测量原理和方法,提出了相应的不合格机匣同轴度调整办法和解决措施。多次排故结果表明:车削安装边、选配偏心环等方法对于解决不同轴引起的发动机偏摩问题有重要作用。 To solve the vibration problem caused by rotor-stator rub failures with unqualified casing eoaxiality of an aeroengine, the principle and method of the aeroengine casing coaxiality measurenment were presented. The adjusting methods and measures were proposed. Many troubleshooting results show that the methods of turning flange and selecting eccentric ring are critical to solve rub failures of the aeroengine with unqualified casing coaxiality.
作者 栾艳华
出处 《航空发动机》 2012年第1期44-46,共3页 Aeroengine
关键词 机匣 同轴度 测量 航空发动机 碰摩 振动 casing coaxiality measurement aeroengine rub failures vibration
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参考文献4

  • 1Means W D. Vorticity and non-coaxiality in progressive deformations [J]. Journal of Structural Geology, 1980,2 (3): 371-378.
  • 2Ghosh S K. Measure of non-coaxiality [J]. Journal of Structural Geology, 1987,9( 1 ) : 111-113.
  • 3Sgarra C. Directions of coaxiality between pure strain and stress in linear elasticity [J]. Journal of Elasticity, 1997, 46 (3) : 263-265.
  • 4何俊杰,蔚夺魁,张德平.某型燃气轮机内、外机匣振动传递的动力学分析[J].航空发动机,2009,35(2):34-36. 被引量:5

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