Boundary characterization of rub-impact response of a helicopter supercritical transmission shaft with a dry friction damper

被引：0
|
作者：
Jin S. [1 ]
Song L.-Y. [1 ]
Cao P. [2 ]
Li J. [2 ]
You Y.-P. [1 ]
Zhu R.-P. [1 ]
Wang D. [1 ]
机构：
[1] National Key Laboratory of Science and Technology on Helicopter Transmission, Nanjing University of Aeronautics and Astronautics, Nanjing
[2] National Key Laboratory of Science and Technology on Helicopter Transmission, AECC Hunan Aviation Powerplant Research Institute, Zhuzhou
来源：
Zhendong Gongcheng Xuebao/Journal of Vibration Engineering | 2024年 / 37卷 / 05期
关键词：
dry friction damper; response characteristics; rub-impact; stability analysis; supercritical transmission shaft;
D O I：
10.16385/j.cnki.issn.1004-4523.2024.05.004
中图分类号：
学科分类号：
摘要：
In pursuit of the ideal power-to-weight ratio，supercritical transmission shaft systems are increasingly used in the design of helicopter structures，which leads to the generation of violent vibrations driving through its critical speed. To suppress the excessive transcritical vibration，dry friction dampers are usually employed. In this study，a supercritical transmission shaft system with a dry friction damper is investigated. The governing equations are established and the boundary characteristics of various rub-impact responses of the system under eccentric excitation of the transmission shaft are analyzed. Firstly，the nonlinear governing equations of the damper/shaft system are constructed. Secondly，typical response characteristics are determined using frequency sweep，and the boundaries of impact occurrence and stability conditions for the synchronous full annular rub are solved using analytical methods. Finally，the derived response boundaries are verified by the Runge-Kutta method，and the relationship between the response boundaries and the system parameters is further explored. © 2024 Nanjing University of Aeronautics an Astronautics. All rights reserved.
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页码：756 / 769
页数：13
相关论文
共 28 条
  • [1] Zhu H M, Chen W F, Zhu R P，, Et al., Modeling and dynamic analysis of spiral bevel gear coupled system of intermediate and tail gearboxes in a helicopter［J］, Proceedings of the Institution of Mechanical Engineers，Part C：Journal of Mechanical Engineering Science, 235, 22, pp. 5975-5993, (2021)
  • [2] Song L Y，, Chen B, Li B, Et al., Nonlinear vibration response of a helicopter supercritical tail rotor drive shaft equipped with a dry friction damper［J］, Journal of Intelligent Manufacturing and Special Equipment, 3, 2, pp. 173-191, (2022)
  • [3] Wang D, Song L Y, Cao P，, Et al., Nonlinear modelling and parameter influence of supercritical transmission shaft with dry friction damper［J］, International Journal of Mechanics and Materials in Design, 19, pp. 223-240, (2023)
  • [4] Samuel P D, Pines D J., A review of vibration-based techniques for helicopter transmission diagnostics［J］, Journal of Sound and Vibration, 282, 1-2, pp. 475-508, (2005)
  • [5] Wang D, Song L Y，, Zhu R P，, Et al., Nonlinear dynamics and stability analysis of dry friction damper for supercritical transmission shaft ［J］, Nonlinear Dynamics, 110, (2022)
  • [6] Liu S B, Yang B G., Optimal placement of water-lubricated rubber bearings for vibration reduction of flexible multistage rotor systems［J］, Journal of Sound and Vibration, 407, pp. 332-349, (2017)
  • [7] Srivastava A K，, Tiwari M，, Singh A., Identification of rotor-stator rub and dependence of dry whip boundary on rotor parameters［J］, Mechanical Systems and Signal Processing, 159, (2021)
  • [8] Prabith K, Krishna I R P., The numerical modeling of rotor‐stator rubbing in rotating machinery：a comprehensive review［J］, Nonlinear Dynamics, 101, 2, pp. 1317-1363, (2020)
  • [9] Ehrich F., Observations of subcritical superharmonic and chaotic response in rotordynamics［J］, Journal of Vibration and Acoustics, 114, 1, pp. 93-100, (1992)
  • [10] XU Bin, XU Weinan, ZHANG Wen, Study of synchronous full annular rub of Jeffcott rotor and its dynamic stability［J］, Journal of Fudan University（Natural Science）, 45, 2, pp. 148-154, (2006)
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