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直升机行星架疲劳裂纹扩展寿命预测

范磊 王少萍 张超 孔德贺 毛阳

范磊, 王少萍, 张超, 等 . 直升机行星架疲劳裂纹扩展寿命预测[J]. 北京航空航天大学学报, 2016, 42(9): 1927-1935. doi: 10.13700/j.bh.1001-5965.2015.0586
引用本文: 范磊, 王少萍, 张超, 等 . 直升机行星架疲劳裂纹扩展寿命预测[J]. 北京航空航天大学学报, 2016, 42(9): 1927-1935. doi: 10.13700/j.bh.1001-5965.2015.0586
FAN Lei, WANG Shaoping, ZHANG Chao, et al. Life prediction of helicopter planetary carrier plate fatigue crack propagation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(9): 1927-1935. doi: 10.13700/j.bh.1001-5965.2015.0586(in Chinese)
Citation: FAN Lei, WANG Shaoping, ZHANG Chao, et al. Life prediction of helicopter planetary carrier plate fatigue crack propagation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(9): 1927-1935. doi: 10.13700/j.bh.1001-5965.2015.0586(in Chinese)

直升机行星架疲劳裂纹扩展寿命预测

doi: 10.13700/j.bh.1001-5965.2015.0586
基金项目: 国家“973”计划(2014CB046402);国家自然科学基金(51175014)
详细信息
    作者简介:

    范磊,男,博士研究生。主要研究方向:机电系统可靠性、故障诊断及寿命预测。Tel.:010-82338917,E-mail:leifan@buaa.edu.cn;王少萍,女,博士,教授,博士生导师。主要研究方向:机电系统故障诊断、容错与可靠性、加速寿命试验、机电系统控制与仿真。Tel.:010-82338933,E-mail:shaopingwang@vip.sina.com

    通讯作者:

    王少萍,Tel.:010-82338933,E-mail:shaopingwang@vip.sina.com

  • 中图分类号: V275+.1;TB31

Life prediction of helicopter planetary carrier plate fatigue crack propagation

Funds: National Basic Research Program of China (2014CB046402); National Natural Science Foundation of China (51175014)
  • 摘要: 直升机行星齿轮保持架(简称行星架)是传动系统的重要部件,其可靠性对于直升机的飞行安全至关重要。行星架疲劳裂纹故障的发生、发展受多种因素影响,其故障诊断和寿命预测都有难度。为准确预测行星架疲劳裂纹寿命,研究了其裂纹故障发生、发展规律,提出了基于对数线性的方法,将裂纹扩展过程离散化处理,采用Paris公式,定量描述裂纹扩展速率,结合Miner准则,累积其疲劳损伤过程,最终得到随裂纹长度变化的行星架剩余使用寿命数值。利用有限元软件ANSYS Workbench的疲劳寿命模块对计算得到的数值结果进行了仿真对比,验证了方法的精确性和有效性。

     

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出版历程
  • 收稿日期:  2015-09-09
  • 刊出日期:  2016-09-20

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