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新型航空测量耙振动应力测量方案设计

陶冶 田琳 马双员

陶冶, 田琳, 马双员. 新型航空测量耙振动应力测量方案设计[J]. 机械科学与技术, 2017, 36(4): 648-652. doi: 10.13433/j.cnki.1003-8728.2017.0426
引用本文: 陶冶, 田琳, 马双员. 新型航空测量耙振动应力测量方案设计[J]. 机械科学与技术, 2017, 36(4): 648-652. doi: 10.13433/j.cnki.1003-8728.2017.0426
Tao Ye, Tian Lin, Ma Shuangyuan. Conceptual Design for Vibration Stress Survey of a New-type Aero Measuring Rake[J]. Mechanical Science and Technology for Aerospace Engineering, 2017, 36(4): 648-652. doi: 10.13433/j.cnki.1003-8728.2017.0426
Citation: Tao Ye, Tian Lin, Ma Shuangyuan. Conceptual Design for Vibration Stress Survey of a New-type Aero Measuring Rake[J]. Mechanical Science and Technology for Aerospace Engineering, 2017, 36(4): 648-652. doi: 10.13433/j.cnki.1003-8728.2017.0426

新型航空测量耙振动应力测量方案设计

doi: 10.13433/j.cnki.1003-8728.2017.0426
详细信息
    作者简介:

    陶冶(1985-),工程师,硕士研究生,研究方向为动力装置结构特性与强度飞行试验技术,fengyun198575@163.com

Conceptual Design for Vibration Stress Survey of a New-type Aero Measuring Rake

  • 摘要: 研究了配装某型飞机发动机的新型复合结构航空测量耙的组成结构,使用ANSYS软件对其进行了模拟分析。基于有限元分析结果,对新型航空测量耙振动应力测量方案进行了设计,并对方案的有效性进行了评估分析。分析结果表明:方案设计拟定的各振动应力测点的最大拉压应力较对应截面的最大拉压应力的误差不超过2.5%,低于工程可接受的误差要求,说明新型航空测量耙振动应力测量方案设计合理有效。
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出版历程
  • 收稿日期:  2015-11-27
  • 刊出日期:  2017-04-05

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