Volume 22 Issue 6
Jun.  2007
Turn off MathJax
Article Contents
YANG Jian-qiu, LU Shan. Methods for stress based life and its reliability analyses of discs with medium-long and long life[J]. Journal of Aerospace Power, 2007, 22(6): 991-995.
Citation: YANG Jian-qiu, LU Shan. Methods for stress based life and its reliability analyses of discs with medium-long and long life[J]. Journal of Aerospace Power, 2007, 22(6): 991-995.

Methods for stress based life and its reliability analyses of discs with medium-long and long life

  • Received Date: 2006-05-31
  • Rev Recd Date: 2006-10-24
  • Publish Date: 2007-06-28
  • Considering the difficulty in calculating the stress concentration factor of mortise of a disk and the error of life is big by using the traditional stress-life method,an improved stress-life method is proposed to compute the life of disks.It includes the concept of stress correction coefficient,a new method to determine the stress concentration factor of mortise of a disk and a new method for correcting the stress ratio.When once the stress correction coefficient of the bars was computed,the improved Stress-Life method can be used to calculate disk's life with the experimental data of bars without notch,at the same time,the influence of the stress concentration is also considered.Then a new stress-life probabilistic model is built for the purpose of life reliability analysis.Finally,the fatigue life reliability of a fan disk is analyzed by the method given,and the computational results fit well with experimental ones.

     

  • loading
  • [1]
    陶晓燕,张玉玲,刘晓光.铁路钢桥整体节点双轴疲劳试验研究[J].中国铁道科学,2005,26(2):77-79.TAO Xiaoyan,ZHANG Yuling,LIU Xiaoguang.Biaxial fatigue test research of solid joint in railway steel bridge[J].China Railway Science,2005,26(2):77-79.
    [2]
    姚卫星.结构疲劳寿命分析[M].北京:国防工业出版社,2003.
    [3]
    赵福星,史海秋,耿中行.一种适用于应力疲劳和应变疲劳的通用寿命模型[J].航空动力学报,2003,18(1):140-145.ZHAO Fuxing,SHI Haiqiu,GENG Zhongxing.General life model adapted to both stress fatigue and strain fatigue[J].Journal of Aerospace Power,2003,18(1):140-145.
    [4]
    蔚夺魁,邵丕仁.某型发动机涡轮盘销钉孔边低循环疲劳寿命分析[J].航空发动机,2000,2:37-41.YU Duokui,SHAO Piren.LCF life at edge of pin-hole analysis of some aeroengine turbine disk[J].Aerongine,2000,2:37-41.
    [5]
    Suresh S.材料的疲劳[M].北京:国防工业出版社,1999.
    [6]
    韩希鹏,许超,段作祥,等.高周疲劳曲线的等效应力法[J].航空材料学报,2003,23(3):53-57.HAN Xipeng,XU Chao,DUAN Zuoxiang,et al.Modified equivalent stress model for high cyclic fatigue curves[J].Journal of Aeronauticat Materials,2003,23(3):53-57.
    [7]
    北京航空材料研究所.航空发动机设计用材料数据手册[S].北京:中国航空发动机总公司出版,1990.
    [8]
    陆山.多危险部位轮盘寿命可靠性评估中若干问题探讨[A].第三届航空发动机可靠性学术会议文集[C].湖北宜昌:中国航空学会发动机可靠性专业委员会,2005:208-213.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1711) PDF downloads(537) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return