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突加不平衡作用下转子系统的主动降载实验

  • Lizhen Hou
  • , Mingfu Liao
  • , Siji Wang
  • , Wei Huang
  • , Lu Zhao
  • , Linzhi Yang
  • , Dan Wang
  • Northwestern Polytechnical University Xian
  • Aero Engine Corporation of China

科研成果: 期刊稿件文章同行评审

6 引用 (Scopus)

摘要

In order to finish the safety design of rotor system under sudden unbalance, the principle of load reduction by cone wall fused under sudden load was analyzed, the active load reduction experimental system with changing stiffness support was designed and experimental verification was finished. Research shows that the essence of cone wall fuse capable of reducing load is to reduce the stiffness of rotor support, accordingly, reduce the critical speed, the supporting load and amplitude in the deceleration process. The active load reduction structure change the support stiffness adaptively using changing stiffness, and can simulate the load reduction of cone wall fuse completely. Furthermore, it can verify the principle of load reduction by low-cost and highly repetitive experiment, and provide experimental conditions and data support for safety design of sudden unbalance.

投稿的翻译标题Active load reduction experiment of rotor system under sudden unbalance
源语言繁体中文
页(从-至)1225-1236
页数12
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
34
6
DOI
出版状态已出版 - 1 6月 2019

关键词

  • Active load reduction
  • Changing stiffness
  • Experimental verification
  • Safety design
  • Sudden unbalance
  • Vibration control

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