Fatigue Safe Life Evaluation of Rotating Swashplate of Helicopter Main Rotor Control System

被引：0
|
作者：
Kim, Dong Chul [1 ]
Lee, Pan Ho [1 ]
Kang, Shin Hyun [1 ]
Choi, Young Don [2 ]
Kim, Tae Joo [3 ]
机构：
[1] HYUNDAI WIA Corp, Seoul, South Korea
[2] Korea Univ, Dept Mech Engn, Seoul, South Korea
[3] Korea Aerosp Res Inst, Seoul, South Korea
来源：
TRANSACTIONS OF THE KOREAN SOCIETY OF MECHANICAL ENGINEERS A | 2012年 / 36卷 / 02期
关键词：
Fatigue Safe Life; Fatigue Test; Main Rotor Control; Pitch Rod Assy; Rotating Swashplate;
D O I：
10.3795/KSME-A.2012.36.2.203
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
The main rotor control system is an important structural part of a helicopter that manages the thrust and control force of the helicopter. The main rotor control system consists of a swashplate assembly, scissor assembly, pitch rod assembly, guide, etc. The main rotor control system must endure various loads, such as the thrust and control force, and must meet the optimized fatigue safety life. The rotating swashplate is an important structure influenced by the pitch rod load and rotating scissor load. In this paper, the accuracy of a result about the rotating swashplate part of the main rotor control system is proven through comparison between fatigue test and FEM results. Based on this result, we estimate the lifetime and deduce the fatigue safe lifetime.
引用
收藏
页码：203 / 210
页数：8
相关论文
共 50 条
  • [1] PERFORMANCE EVALUATION OF A HELICOPTER MAIN ROTOR HYDRAULIC CONTROL SYSTEM USING ROTOR EQUIVALENT DYNAMIC PARAMETERS
    Duzagac, Hasan Ali
    Caliskan, Hakan
    Balkan, Raif Tuna
    PROCEEDINGS OF ASME 2022 INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, IMECE2022, VOL 5, 2022,
  • [2] Fatigue life evaluation in composite rotor blade of multipurpose helicopter
    Kwon, JH
    Hwang, KJ
    Kim, SS
    Kim, PJ
    Kim, CS
    KORUS-2002: 6TH RUSSIAN-KOREAN INTERNATIONAL SYMPOSIUM ON SCIENCE AND TECHNOLOGY, PROCEEDINGS, 2002, : 15 - 20
  • [3] Damage tolerance and classic fatigue life prediction of a helicopter main rotor blade
    A. R. Shahani
    S. Mohammadi
    Meccanica, 2016, 51 : 1869 - 1886
  • [4] Damage tolerance and classic fatigue life prediction of a helicopter main rotor blade
    Shahani, A. R.
    Mohammadi, S.
    MECCANICA, 2016, 51 (08) : 1869 - 1886
  • [5] Hybrid Control of Helicopter Main Rotor Concordant Load System
    Zhang, Wei
    Yuan, Chaohui
    Zhang, Weiguo
    Hou, Chen-guang
    7TH INTERNATIONAL CONFERENCE ON SYSTEM SIMULATION AND SCIENTIFIC COMPUTING ASIA SIMULATION CONFERENCE 2008, VOLS 1-3, 2008, : 64 - +
  • [6] Helicopter Safe Landing Trajectory after Main Rotor Actuator Failures
    Wang, Yunjie
    Jiang, Chen
    Zhang, Yuwen
    Wang, Haowen
    APPLIED SCIENCES-BASEL, 2020, 10 (08):
  • [7] Helicopter dynamic components fatigue safe life prediction
    Mu Zhitao
    Liu Wenlin
    Jin Ping
    PROGRESS IN SAFETY SCIENCE AND TECHNOLOGY, VOL 6, PTS A AND B, 2006, 6 : 2397 - 2401
  • [8] Forced aeroelastic oscillations of a rotating anisotropic helicopter main rotor blade at hovering
    Grishanina T.V.
    Shklyarchuk F.N.
    Russian Aeronautics, 2013, 56 (03): : 303 - 313
  • [9] The Motion Reliability Simulation and Analysis of Main Rotor Head of Helicopter Rotor System
    Chen, Fang
    Zhang, Jianguo
    Gong, Qi
    Song, Yonglei
    Su, Duo
    PROCEEDINGS OF 2009 8TH INTERNATIONAL CONFERENCE ON RELIABILITY, MAINTAINABILITY AND SAFETY, VOLS I AND II: HIGHLY RELIABLE, EASY TO MAINTAIN AND READY TO SUPPORT, 2009, : 1008 - +
  • [10] Reliability assessment to helicopter dynamic components fatigue safe life
    Mu, ZT
    Liu, WL
    Yang, XH
    Sun, ML
    PROGRESS IN SAFETY SCIENCE AND TECHNOLOGY, VOL V, PTS A AND B, 2005, 5 : 1550 - 1556
12345