期刊文献+

非接触式转子叶片振动测试技术应用研究 被引量:9

Investigation and application of non-contact rotor blade vibration measurement technique
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摘要 介绍了旋转叶片整数阶次与非整数阶次的振动理论分析,并利用非接触式叶片振动测量系统进行了模拟试验器和台架压气机试验验证.理论分析和试验结果吻合,表明由非接触式叶片振动测量系统测试振幅的变化特征,可确定整阶次共振与非整阶次叶片振动. This paper briefly describes non-contact rotor blade vibration measurement analysis methods. Theoretical analysis was conducted for both asynchronous and synchronous resonant vibrations. This system has been applied successfully in compressor and engine testing and the theoretical predictions were validated by results from strain gauge measurement.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2008年第1期21-25,共5页 Journal of Aerospace Power
关键词 航空 航天推进系统 叶片共振 整数阶次 非整数阶次 非接触式 aerospace propulsion system blade resonance integer order non-integer order non-contact
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参考文献5

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同被引文献90

  • 1艾延廷,张凤玲.航空发动机转子叶片振动测量技术研究[J].仪器仪表学报,2006,27(z2):1242-1244. 被引量:11
  • 2孙红岩,谢志江,陈平.叶轮机械叶片故障的叶间动态压力诊断法[J].动力工程,2005,25(4):563-566. 被引量:2
  • 3葛永庆,刘江,安连锁.汽轮机叶片振动非接触测量技术综述[J].华北电力大学学报(自然科学版),2006,33(3):54-58. 被引量:11
  • 4王英,沙云东.航空发动机故障诊断技术综述[J].沈阳航空工业学院学报,2007,24(2):11-14. 被引量:16
  • 5陶春虎 钟培道 王仁智 等.航空发动机转动部件的失效与预防[M].北京:国防工业出版社,2000.337.
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  • 10Heath S. A new technique for identifying synchronous resonances using tip-timing [R]. ASME 99-GT-402.

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