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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.

     

  • [1] Hennecke D K,Trappmann K.Turbine tip clearance control in gas turbine engines[R].NASA,N83-29254,1983 [2] Annette E N,Christoph W M,Stehan S.Modeling and validation of the thermal effects on gas turbine transients [J].Journal of Engineering for Gas Turbines and Power,2005,127(3):564-572 [3] Pilidis P,Maccallum N R L.Models for predicting tip clearance changes in gas turbines[R].NASA,N83-29258,1983 [4] Lattime S B,Steinetz B M.Turbine engine clearance control systems:current practices and future directions [J].Journal of Propulsion and Power,2004,20(2):302-311 [5] Jia Binghui,Zhang Xiaodong.Study on effect of rotor vibration on tip clearance variation and fast active control of tip clearance[J].Advanced Material Research,2010,139-141(1):2469-2472 [6] Kypuros J A,Melcher K J.A reduced model for prediction of thermal and rotational effects on turbine tip clearance[R].NASA/TM-2003-212226,2003 [7] Lattime S B,Steinetz B M.Robbie M G.Test rig for evaluating active turbine blade tip clearance control concepts [J].Journal of Propulsion and Power,2005,21(3):552-563 [8] Forssell L S.Flight clearance analysis using global nonlinear optimisation-based search algorithms[C]//AIAA Guidance,Navigation,and Control Conference and Exhibit.Austin,Texas:AIAA,2003:1-8 [9] Kartal M E,Basaga H B,Bayraktar A.Probabilistic nonlinear analysis of CFR dams by MCS using response surface method [J].Applied Mathematical Modelling,2011,35(6):2752-2770 [10] Guilhem M,Daniel D,Abdul-Hamid S.Probabilistic analysis of pressurized tunnels against face stability using collocation-based stochastic response surface method [J].Journal of Geotechnical & Geoenvironmental Engineering,2011,137(4):385-397 [11] Pietrzyk K,Hagentoft C.Probabilistic analysis of air infiltration in low-rise building [J].Building and Environment,2008,43(4):537-549 [12] Lü Q,Low B K.Probabilistic analysis of underground rock excavations using response surface method and SORM [J].Computers and Geotechnics,2011,38(8):1008-1021 [13] Pugh C E,Richard Bass B,Dickson T L.Role of probabilistic analysis in integrity assessments of reactor pressure vessels exposed to pressurized thermal-shock conditions [J].Engineering Failure Analysis,2007,14(8):501-517 [14] Hu Dianying,Wang Rongqiao,Tao Zhi.Probabilistic design for turbine disk at high temperature[J].Aircraft Engineering and Aerospace Technology,2011,83(4):199-207 [15] Chen Jianbing,Li Jie.Dynamic response and reliability analysis of non-linear stochastic structures [J].Probabilistic Engineering Mechanics,2005,20(1):33-44 [16] Nakamura T,Fuji K.Probabilistic transient thermal analysis of an atmospheric reentry vehicle structure [J].Aerospace Science and Technology,2006,10(4):346-354 [17] 李昌,韩兴.基于响应面法齿轮啮合传动可靠性灵敏度分析 [J].航空动力学报,2011,26(3):711-715 Li Chang,Han Xing.Analysis of reliability sensitivity for gear engagement based on response surface methods [J].Journal of Aerospace Power,2011,26(3):711-715(in Chinese)
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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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