Design theory for vibration characterisation experiments on real turbine blades with underplatform damper

Authors

  • Lijian Zou
  • Wenkai Qi

DOI:

https://doi.org/10.54097/hzb1dt09

Keywords:

Aero-engine, blade vibration, vibration reduction, dry friction damping, underplatform damper, structural design, parameter optimization, vibration reduction experiment.

Abstract

One of the main causes of turbine rotor blade failures is high-frequency fatigue caused by blade resonance, and the vibration of turbine blades can be effectively suppressed through the reasonable design of dry friction damping structure. In order to understand the vibration characteristics of the blade-disc system and to check whether the damping effect meets the technical specifications, it is necessary to design and carry out dry friction damping blade vibration characteristics experiment. This paper takes a certain type of underplatform damped turbine blade in production as an example, and briefly describes the design idea and design process of such blade vibration characteristic experiments under the premise of the experiment blade structure, material and other physical parameters.

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References

Sever Ibrahim A.,Petrov Evgeny P.,Ewins David J.. Experimental and Numerical Investigation of Rotating Bladed Disk Forced Response Using Underplatform Friction Dampers[J]. Journal of Engineering for Gas Turbines and Power,2008,130(4).

Laxalde, D. Gibert, C.Thouverez, F. Experimental and numerical investigations of friction rings damping of blisks [M].Proceedings of ASME Turbo Expo 2008.

Li Di,Hong Jie,Lulu Chen.Experimental Study of Dry Friction Damping and Vibration Damping of Crowned Turbine Blades[J].Gas Turbine Experimenting and Research,2008(04):22-27.

Junjie Chen.Study of dry friction damping damping characteristics of crowned leaf discs[D].Nanjing University of Aeronautics and Astronautics,2015.

Xiaoyu Yin.Research on the experiment method of friction damping and vibration damping for group/turned turbine blades [D]. Nanjing University of Aeronautics and Astronautics, 2020. DOI:10.27239/d.cnki.gnhhu.2020.000215.

ZHANG, D., et al., Experimental investigation on dynamic response of flat blades with underplatform dampers[J]. Chinese Journal of Aeronautics, 2019. 32(12):2667-2678.

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Published

14-03-2024