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航空发动机承力结构系统阻尼减振设计方法

  • Beihang University
  • Collaborative Innovation Center for Advanced Aero-Engine

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

The vibration control method with dry friction damping was put forward for the supporting structure system in high thrust-mass ratio turbofan engine. A dry friction damper with vibration absorption function was designed to enhance the damping characteristic of the supporting structure without loss of stiffness, and achieve vibration response control for the system. Influences of friction contact characteristic and dry friction damper structure characteristic on the damping effect were acquired in theoretical analysis and simulation calculation, and the damping design flow for supporting structure was presented. Results exhibited that vibration response was attenuated with the dry friction damper, and the damping effect could be optimized with reasonable design of friction coefficients and claw's width, which helped attenuate resonance amplitude of bearing house by more than one order in the example.

投稿的翻译标题Damping design technology of aero-engine supporting structure system
源语言繁体中文
页(从-至)2440-2447
页数8
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
卷34
期11
DOI
出版状态已出版 - 1 11月 2019

关键词

  • Dry friction
  • Mechanical impedance
  • Supporting structure
  • Turbofan engine
  • Vibration control

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