Study on the vibration control method of a turboshaft engine rotor based on piezoelectric squeeze film damper oil film clearance
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Published:2023-05-17
Issue:1
Volume:14
Page:237-246
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ISSN:2191-916X
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Container-title:Mechanical Sciences
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language:en
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Short-container-title:Mech. Sci.
Author:
Lu Qingxiong,Li Chao,Zhang Yangyan,Fang Hao,Bin Guangfu
Abstract
Abstract. In the complex environment of the battlefield and dust weather, hard objects including birds, bullets, sand and others will
inevitably cause impact damage to the compressor blades of turboshaft
engines. The damage will further result in fatigue vibration of the gas
generator rotor and catastrophic accidents such as excessive engine
vibration and even crash. The relation between oil film clearance of dampers and damping of rotor systems as well as the damping and vibration amplitude of
a rotor system are analyzed. The functional relation between oil film
clearance and vibration amplitude is derived. Taking the gas generator rotor
of a certain turboshaft engine as an example, the rotor dynamic model of a gas generator rotor with oil film bearing clearance is constructed, and the
vibration response of the rotor system under different oil film clearances
is analyzed. A new type of squeeze film damper (SFD) structure with
piezoelectric-driven split pads is innovatively designed, and the vibration control system of the gas generator rotor is built. In addition, experimental research on rotor fault vibration control under different oil
film clearances is carried out. The results show that, within a certain range, when oil film clearance decreases, amplitude will decrease. Under the
experimental conditions, when the driving voltage of the piezoelectric
actuator is adjusted from 0 to 70 V, the oil film clearance decreases from
156 to 118 µm. Then, the vibration amplitude decreases and
gradually reaches stability after 0.036 s, and the vibration amplitude of
the rotor system decreases by 12 %. When the driving voltage of the
piezoelectric actuator is adjusted to 150 V, the oil film clearance
decreases to 76 µm, and the vibration amplitude of the rotor system
decreases by 28 %. When the new SFD adopts a piezoelectric-driven split-pad structure, the structure can adjust quickly the oil film clearance
online so as to control the vibration of the rotor system. The research results can provide a technical reference for the vibration control of turboshaft
engine rotor systems.
Funder
National Natural Science Foundation of China
Publisher
Copernicus GmbH
Subject
Industrial and Manufacturing Engineering,Fluid Flow and Transfer Processes,Mechanical Engineering,Mechanics of Materials,Civil and Structural Engineering,Control and Systems Engineering
Reference55 articles.
1. Bin, G., Huang, Y., Guo, S., Li, X., and Wang, G.: Investigation of Induced
Unbalance Magnitude on Dynamic Characteristics of High-speed Turbocharger
with Floating Ring Bearings, Chin. J. Mech. Eng.,
31, 88, https://doi.org/10.1186/s10033-018-0287-5, 2018a. 2. Bin, G., Li, X., Shen, Y., and Wang, W.: Development of whole-machine high speed
balance approach for turbomachinery shaft system with N+1 supports,
Measurement, 122, 368–379,
https://doi.org/10.1016/j.measurement.2018.02.035, 2018b. 3. Bin, G., Zhang, L., Yang, F., Chen, A.: The Influence of Ring-Speed Ratio
Dynamic Change on Nonlinear Vibration Response of High-Speed Turbocharger
Rotor System, Shock Vib., 2021, 9649232, https://doi.org/10.1155/2021/9649232,
2021. 4. Bin, G., Li, C., Li, J., and Chen, A.: Erosion-damage-induced vibration response
of aero-gas generator rotor system, Mech. Syst. Signal
Pr., 195, 110298, 0888–3270,
https://doi.org/10.1016/j.ymssp.2023.110298, 2023. 5. Chasalevris, A. and Dohnal, F.: Vibration quenching in a large scale
rotor-bearing system using journal bearings with variable geometry, J. Sound Vib., 333, 2087–2099,
https://doi.org/10.1016/j.jsv.2013.11.034, 2014.
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