Volume 45 Issue 9
Sep.  2019
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Article Contents
ZHANG Jian, ZHANG Dayi, WANG Yongfeng, et al. Coupling vibration characteristics analysis of shared support-rotors system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(9): 1902-1910. doi: 10.13700/j.bh.1001-5965.2019.0002(in Chinese)
Citation: ZHANG Jian, ZHANG Dayi, WANG Yongfeng, et al. Coupling vibration characteristics analysis of shared support-rotors system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(9): 1902-1910. doi: 10.13700/j.bh.1001-5965.2019.0002(in Chinese)

Coupling vibration characteristics analysis of shared support-rotors system

doi: 10.13700/j.bh.1001-5965.2019.0002
Funds:

National Natural Science Foundation of China 51575022

National Natural Science Foundation of China 11672017

More Information
  • Corresponding author: HONG Jie, E-mail: hongjie@buaa.edu.cn
  • Received Date: 07 Jan 2019
  • Accepted Date: 05 Apr 2019
  • Publish Date: 20 Sep 2019
  • The rotor system with turbine mid frame is researched as an objected, and the dynamic model with coupling vibration in transverse and angular degree was employed to reveal the vibration coupling mechanism and influence in shared support-rotors system. It is pointed that support response of one rotor can influence the bearing dynamic stiffness and rotor dynamic characteristic of another, and the calculation error of traditional rotor dynamic modeling exceed 10%, so the vibration coupling should be considered when analyzing critical speed and dynamic response in the rotor system with mid frame. The finite element calculation results for the shared support-rotors system in turbo-shaft engine exhibit that the coupling modes will arise, and the speed of one rotor can affect the critical resonant speed excited by another. The vibration isolation characteristics of mid turbine can also be affected due to the coupling vibration, and compared with non-coupling system, the dynamic response and load-transferring coefficient both remarkably increase.

     

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