• DocumentCode
    691551
  • Title

    Fatigue Life Analysis for Rolling Bearings of a Helicopter Main Reducer

  • Author

    Liao Yashi ; Liu Shaojun ; Jin Yan ; Hu Yun

  • Author_Institution
    Coll. of Mech. & Electr. Eng., Central South Univ., Changsha, China
  • fYear
    2013
  • fDate
    6-7 Nov. 2013
  • Firstpage
    314
  • Lastpage
    317
  • Abstract
    Through a data processing of a helicopter power spectrum, part of a rolling bearing fatigue load spectrum of helicopter transmission system main reducer could be obtained. Based on finite element analysis software ANSYS to establish three-dimensional model for rolling bearing. Through the stress field to get the maximum stress value, combined with the miner cumulative damage theory and S-N curve of a helicopter transmission system the main reduce for rolling bearings to establish life model , and using ROMAX software can predict life .At last, the feasibility of life model is verified.
  • Keywords
    fatigue; finite element analysis; helicopters; mechanical engineering computing; power transmission (mechanical); rolling bearings; stress analysis; ANSYS; ROMAX software; S-N curve; cumulative damage theory; data processing; fatigue life analysis; finite element analysis software; helicopter main reducer; helicopter power spectrum; helicopter transmission system; maximum stress value; rolling bearing; rolling bearing fatigue load spectrum; stress field; three-dimensional model; Fatigue; Finite element analysis; Force; Helicopters; Rolling bearings; Shafts; Stress; Bacterial foraging algorithm; Image enhancement; Intelligent optimization; Particle Swarm Optimization;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Systems Design and Engineering Applications, 2013 Fourth International Conference on
  • Conference_Location
    Zhangjiajie
  • Print_ISBN
    978-1-4799-2791-3
  • Type

    conf

  • DOI
    10.1109/ISDEA.2013.475
  • Filename
    6843452