Dynamic characteristics of rotor system with magnetorheological damper during maneuvering flight

被引：0
|
作者：
Wang, Jun [1 ,2 ]
Liu, Yun-Fei [2 ]
Qin, Zhao-Ye [2 ]
Ma, Liang [3 ]
Hong, Fang-Fang [4 ]
Chu, Fu-Lei [2 ]
机构：
[1] Beijing Key Laboratory of Health Monitoring and Self-Recovery for High-End Machinery Equipment, Beijing University of Chemical Technology, Beijing,100029, China
[2] Department of Mechanical Engineering, Tsinghua University, Beijing,100084, China
[3] College of Aeronautical Engineering, Civil Aviation University of China, Tianjin,300300, China
[4] Tianjin Renai College, Tianjin,301636, China
来源：
Zhendong Gongcheng Xuebao/Journal of Vibration Engineering | / 37卷 / 05期
关键词：
Compilation and indexing terms; Copyright 2025 Elsevier Inc;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Aircraft engines - Damping - Finite element method
引用
收藏
页码：747 / 755
相关论文
共 50 条
  • [1] Dynamic characteristics of a rotor system supported by squeeze film dampers during maneuvering flight: Simulation and experiment
    Zhang, Bo
    Chen, Xi
    Fan, Xiangnan
    Ren, Guangming
    Gan, Xiaohua
    AEROSPACE SCIENCE AND TECHNOLOGY, 2025, 161
  • [2] General dynamic model of aeroengine's rotor system during maneuvering flight
    Zhu, Chang-Sheng
    Chen, Yong-Jun
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2009, 24 (02): : 371 - 377
  • [3] Dynamic performance of a novel integral magnetorheological damper-rotor system
    Wang, Jun
    Liu, Yunfei
    Qin, Zhaoye
    Ma, Liang
    Chu, Fulei
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2022, 172
  • [4] DYNAMIC CHARACTERISTICS OF A SQUEEZE FILM DAMPED ROTOR SYSTEM CONSIDERING INSTANTANEOUS STATIC ECCENTRICITY IN MANEUVERING FLIGHT
    Chen, Xi
    Gan, Xiaohua
    Jiang, Shuyun
    Ren, Guangming
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 10B, 2020,
  • [5] Helicopter rotor dynamic inflow modeling for maneuvering flight
    Krothapalli, KR
    Prasad, JVR
    Peters, DA
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2001, 46 (02) : 129 - 139
  • [6] Design and dynamic characteristics of squeeze film damper for rotor system
    Jia S.
    Zheng L.
    Li S.
    Mei Q.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2020, 35 (12): : 2626 - 2634
  • [7] Effect of squeeze film damper on rotor system with rub-impact fault under maneuvering flight conditions
    State Key Laboratory of Engine, Tianjin University, Tianjin
    300072, China
    不详
    300000, China
    不详
    SO17 1BJ, United Kingdom
    Hsi An Chiao Tung Ta Hsueh, 11 (62-70 and 141):
  • [8] Rotor dynamic wake distortion model for helicopter maneuvering flight
    Zhao, JG
    Prasad, JVR
    Peters, DA
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2004, 49 (04) : 414 - 424
  • [9] Analysis of primary resonance characteristics of dual-rotor system in maneuvering flight environment
    Chen Y.
    Hou L.
    Lin R.
    Yang Y.
    Chen Y.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2022, 43 (01):
  • [10] Influence of uncertainty factors on the dynamic characteristics of magnetorheological damper
    Liang, Zhen
    Yongbao, Feng
    Xiaolin, Wei
    Zhenhua, Zhang
    JOURNAL OF MAGNETISM AND MAGNETIC MATERIALS, 2023, 585
12345