跳到主要导航 跳到搜索 跳到主要内容

Experimental investigation on dynamic response of flat blades with underplatform dampers

  • Dayi ZHANG
  • , Bin GAO
  • , Jie HONG*
  • , Jianwei FU
  • , Xiangyun GE
  • *此作品的通讯作者
  • Beijing Key Laboratory of Aero-Engine Structure and Strength
  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

One test rig with three blades and two Under-Platform Dampers (UPDs) is established to better understand the dynamical behavior of blades with UPDs. A pre-loaded spring is used to simulate the centrifugal load acting on the damper, thereby achieving continuous adjustment of the pressing load. UPDs with different forms, sizes and materials are carefully designed as experimental control groups. Noncontact measurement via a laser Doppler velocimeter is employed and contact excitation which is performed by an electromagnetic exciter is adopted to directly obtain the magnitude of the excitation load by a force sensor mounted on the excitation rod. Particular attention is paid to the influence of the contact status of the contact surfaces, e.g. the pressure-sensitive paper is used to measure the effective contact area of the UPDs. The experimental variables are selected as the centrifugal force, the amplitude of the excitation force, the damper mass, the effective contact area, and the damper material. The Frequency Response Function (FRF) of the blade under different experimental parameters is obtained by slow frequency sweep under sinusoidal excitation to study the influence of each parameter on the dynamic characteristics of the blade and the mechanism analysis is carried out combined with the experimental results.

源语言英语
页(从-至)2667-2678
页数12
期刊Chinese Journal of Aeronautics
32
12
DOI
出版状态已出版 - 12月 2019

指纹

探究 'Experimental investigation on dynamic response of flat blades with underplatform dampers' 的科研主题。它们共同构成独一无二的指纹。

引用此