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Experimental investigation on dynamic response of flat blades with underplatform dampers

  • Dayi ZHANG
  • , Bin GAO
  • , Jie HONG*
  • , Jianwei FU
  • , Xiangyun GE
  • *Corresponding author for this work
  • Beijing Key Laboratory of Aero-Engine Structure and Strength
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

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.

Original languageEnglish
Pages (from-to)2667-2678
Number of pages12
JournalChinese Journal of Aeronautics
Volume32
Issue number12
DOIs
StatePublished - Dec 2019

Keywords

  • Effective contact area
  • Forced response
  • Friction
  • Test rig
  • Turbo machinery
  • Underplatform dampers

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