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高压涡轮叶尖径向运行间隙概率设计

费成巍 白广忱 赵合阳 韩彦彬

费成巍, 白广忱, 赵合阳, 等 . 高压涡轮叶尖径向运行间隙概率设计[J]. 北京航空航天大学学报, 2013, 39(3): 305-309.
引用本文: 费成巍, 白广忱, 赵合阳, 等 . 高压涡轮叶尖径向运行间隙概率设计[J]. 北京航空航天大学学报, 2013, 39(3): 305-309.
Fei Chengwei, Bai Guangchen, Zhao Heyang, et al. Probabilistic design for blade-tip radial running clearance of HPT[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(3): 305-309. (in Chinese)
Citation: Fei Chengwei, Bai Guangchen, Zhao Heyang, et al. Probabilistic design for blade-tip radial running clearance of HPT[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(3): 305-309. (in Chinese)

高压涡轮叶尖径向运行间隙概率设计

基金项目: 国家自然科学基金资助项目(51175017,51275024);高等学校博士学科点专项科研基金资助课题;北京航空航天大学博士生创新基金资助项目(YWF-12-RBYJ-008)
详细信息
    作者简介:

    费成巍(1983-),男,河南开封人,博士生,Feicw544@163.com.

  • 中图分类号: V231.95

Probabilistic design for blade-tip radial running clearance of HPT

  • 摘要: 为了改善高压涡轮叶尖径向运行间隙(BTRRC,Blade-Tip Radial Running Clearance)设计和控制合理性,考虑典型载荷下的热载荷和机械载荷和合理选取随机变量,在确定性分析基础上对BTRRC进行了概率设计.通过确定性分析,得出涡轮盘、叶片和机匣的径向变形以及BTRRC随时间变化规律,并找出危险点(t=180 s)作为概率设计的计算点.通过概率分析,不但得到了各部件径向变形的概率分布特征及不同稳态叶尖间隙δ下的失效数、失效概率和可靠度,还找到了影响它们径向变形和BTRRC的主要因素.综合考虑航空发动机可靠性和效率,将δ设定为1.95 mm为宜,满足设计和工程要求,为BTRRC的控制和设计提供了依据.

     

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出版历程
  • 收稿日期:  2012-02-21
  • 网络出版日期:  2013-03-31

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