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轴承腔油气两相流数值模拟的试验验证

汪友勇 王锁芳 艾俊峰 李斌

汪友勇, 王锁芳, 艾俊峰, 李斌. 轴承腔油气两相流数值模拟的试验验证[J]. 航空动力学报, 2013, 28(3): 629-635.
引用本文: 汪友勇, 王锁芳, 艾俊峰, 李斌. 轴承腔油气两相流数值模拟的试验验证[J]. 航空动力学报, 2013, 28(3): 629-635.
WANG You-yong, WANG Suo-fang, AI Jun-feng, LI Bin. Experimental verification of numerical simulation of oil-air two-phase flow in bearing chamber[J]. Journal of Aerospace Power, 2013, 28(3): 629-635.
Citation: WANG You-yong, WANG Suo-fang, AI Jun-feng, LI Bin. Experimental verification of numerical simulation of oil-air two-phase flow in bearing chamber[J]. Journal of Aerospace Power, 2013, 28(3): 629-635.

轴承腔油气两相流数值模拟的试验验证

Experimental verification of numerical simulation of oil-air two-phase flow in bearing chamber

  • 摘要: 为探索一种适于模拟轴承腔油气两相流流动特性的数值计算模型,建立了一套简化结构的轴承腔试验装置,通过试验研究获得了不同工况对轴承腔通风口出气比例和回油口滑油温升的影响规律.应用Fluent软件,采用Mixture多相流模型和Eulerian多相流模型分别搭配标准k-ε湍流模型和RNG(renormalization group) k-ε湍流模型对选定试验工况进行数值模拟.对比结果表明:当转速为2200r/min时,使用Mixture多相流模型搭配RNG k-ε湍流模型计算的滑油温升与试验值的相对误差仅为2.72%,体现了该计算模型在高转速时的精确性,并在此基础上获得了油气两相流速度场、压力场和温度场的分布特征.

     

  • [1] 林基恕,常春江.航空发动机设计手册(第12册):传动及润滑系统[M].北京:航空工业出版社,2002.
    [2] 陈观慈. 航空发动机主轴高速滚动轴承热分析[D]. 哈尔滨:哈尔滨工业大学,2008. CHEN Guanci.Thermal analysis of high-speed rolling bearing used in main shaft of aeroengine[D].Harbin:Harbin Institute of Technology,2008.(in Chinese)
    [3] 林基恕, 张振波.21世纪航空发动机动力传输系统的展望[J]. 航空动力学报, 2001,16(2):108-114,118. LIN Jishu,ZHANG Zhenbo.Prospects of aeroengine power transmission system in the 21st century[J].Journal of Aerospace Power,2001,16(2):108-114,118.(in Chinese)
    [4] Gorse P,Busam S,Dullenkopf K.Influence of operating condition and geometry on the oil film thickness in aero-engine bearing chambers[J].Journal of Engineering for Gas Turbines and Power, 2006,128(1):103- 110.
    [5] Williams J.Thin film rimming flow subject to droplet impact at the surface[D].United Kingdom:The University of Nottingham,2008.
    [6] Glahn A,Busam S,Blair M F.Droplet generation by disintegration of oil films at the rim of rotating disk[J].Journal of Engineering for Gas Turbines and Power,2002,124(1):117-124.
    [7] Glahn A,Busam S,Blair M F.Disintegration of oil films emerging from radial holes in a rotating cylinder[J].Journal of Engineering for Gas Turbines and Power,2003,125(4):1011-1020.
    [8] Glahn A,Busam S,Blair M F.Disintegration of oil jets emerging from axial passages at the face of a rotating cylinder[J].Journal of Engineering for Gas Turbines and Power,2003,125(4):1003-1010.
    [9] Farrall M,Simmons K,Hibberd S.A numerical model for oil film flow in an aeroengine bearing chamber and comparison to experimental data[J].Journal of Engineering for Gas Turbines and Power,2006,128(1):111-117.
    [10] Farrall M,Hibberd S,Simmons K.The effect of initial injection conditions on the oil droplet motion in a simplified bearing chamber[J].Journal of Engineering for Gas Turbines and Power,2008,130(1):1-7.
    [11] 应伟,冯艳,王锁芳.基于小波和神经网络的流型辨识研究[J].机床与液压,2008,36(10):61-62. YING Wei,FENG Yan,WANG Suofang.Research on discrimination gas-liquid two phase flow patterns based on wavelets and BP neural networks[J].Machine ToolL & Hydraulics,2008,36(10):61-62.(in Chinese)
    [12] 李斌,王锁芳,刘勇.轴承腔内油气两相流动与换热的数值模拟[J].重庆理工大学学报:自然科学版,2010,24(11):38-43. LI Bin,WANG Suofang,LIU Yong.Numerical simulation of air-oil two phase flow and heat transfer in a bearing chamber[J].Journal of Chongqing University of Technology:Natural Science,2010,24(11):38-43.(in Chinese)
    [13] 李斌,王锁芳,刘勇.轴承腔综合分析平台与两相流数值模拟[C]//中国航空学会第二届航空发动机数值仿真与数字化设计学术交流会论文集.北京:中国航空学会动力专业分会,2011:130-135.
    [14] 江帆,黄鹏.Fluent高级应用与实例分析[M].北京:清华大学出版社, 2008.
    [15] 张凯,王瑞金,王刚.Fluent技术基础与应用实例[M].北京:清华大学出版社,2010.
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出版历程
  • 收稿日期:  2012-03-28
  • 刊出日期:  2013-03-28

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