Volume 21 Issue 5
Oct.  2006
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2006  >  21(5): 862-866
WANG Wei-guo, GU Yuan-xing, QING Hua, TENG Guang-rong. Investigation of disk LCF life prediction and its experimental verification[J]. Journal of Aerospace Power, 2006, 21(5): 862-866.
Citation: WANG Wei-guo, GU Yuan-xing, QING Hua, TENG Guang-rong. Investigation of disk LCF life prediction and its experimental verification[J]. Journal of Aerospace Power, 2006, 21(5): 862-866.
shu

Investigation of disk LCF life prediction and its experimental verification

  • 1.

    College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

  • 2.

    Gas Turbine Establishment, Chengdu 610500, China

  • Received Date: 2005-08-17
  • Rev Recd Date: 2005-11-15
  • Publish Date: 2006-10-28
    Abstract
  • A simplified Walker strain model was presented to predict the disk Low Cycle Fatigue(LCF) life for unsymmetrical loads and the main life regions.The effect of number of life critical regions in each disk was taken into account in the life prediction.A series of axial strain-controlled LCF tests of GH4133 bar specimens were conducted.An experimental turbine disk was designed,and the high temperature LCF test of the rotor was carried out on the spin test rig.The result indicates that the disk LCF life prediction method is effective,and the accuracy of the life prediction is within the targeted scatter band of two compared to the turbine disk LCF test data.

     

    • FullText(HTML)
  • loading
    • References(7)
  • [1]
    Jaske C E,Feddersen C E,Davis K B,et al.Analysis of fatigue,fatigue crack propagation,and fracture Data[R].NASA CR--132332,1973:49-54.
    [2]
    Shepherd D P.The prediction of fatigue life for arbitrary geometries from the statistical analysis of plain specimen data[R].NASA/CP-2002-211682,Fifth Annual Workshop on the Application of Probabilistic Methods for Gas Turbine Engines,Editors:Victoria Briscoe,2002:511-538.
    [3]
    姚卫星.结构疲劳寿命分析[M]北京:国防工业出版社,2003.
    [4]
    中国航空材料手册:第2卷[Z].第2版:北京:中国标准出版社,2002.
    [5]
    龚梦贤,黄庆东,肖玉祥,等.某型发动机第Ⅰ级涡轮盘低循环疲劳试验研究[J].燃气涡轮试验与研究,1998,11(3):40-45.Gong Mengxian,Huang Qingdong,Xiao Yuxiang,et al.An experimental study on low cycle fatigue life of 1st turbine disk in aeroengine[J].Gas Turbine Experiment and Research,1998,11 (3):40-45.
    [6]
    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):37-51.Yu Duokui,Shao Piren.LCF life prediction of turbine disk pin holes in aeroengine[J].Aeroengine,2000,(2):37-51.
    [7]
    Melis M E,Zaretsky E V,August R.Probabilistic analysis of aircraft gas turbine disk life and reliability[R].NASA/TM 1999-107436.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 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
    Get Citation
    PDF(1522.0KB)
    XML

    Article Metrics

    Article views (2189) PDF downloads(571) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return