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轴承腔中均匀流体/壁面油膜分层流动分析 被引量:4

Analysis of Homogeneous Fluid/wall Oil Film Two-phase Stratified Flow in an Aeroengine Bearing Chamber
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摘要 航空发动机轴承腔精确的润滑与换热设计依赖于对其内油气两相润滑介质流动与换热本质的认识。针对轴承腔内复杂的油气两相润滑介质流动状态,建立轴承腔均匀流体/壁面油膜分层流动分析模型,开展腔内油气两相润滑介质流动特性研究,探讨转子转速和润滑油供油量对均匀流体和壁面油膜两相介质压力、速度以及温度分布的影响。分析模型中,气相介质(含油滴)的等效物理特征参数通过离散油滴和气相介质的组分比例关系确定,各固体壁面与流体介质的对流换热系数根据其各自的传热特性确定。研究结果表明,均匀流体与壁面油膜两相介质的压力随着润滑油供油量的增加而增大,受转子转速的影响较为复杂;均匀流体与壁面油膜两相介质的速度随着转子转速的增高而增大,受润滑油供油量影响较小;均匀流体的温度随着润滑油供油量的增加而减小,受转子转速的影响较小;与均匀流体温度不同,壁面油膜的温度随着转子转速的增加而增大,随着润滑油供油量的增加而减小。建立了轴承腔试验台系统,开展了轴承腔油气两相流动状态下的压力和温度测试,压力和温度试验结果与理论计算结果均具有较好的吻合性,验证了提出的理论分析方法的可靠性。 The accurate lubrication and heat transfer designs of an aeroengine bearing chamber require an understanding of the complex air/oil two-phase flow characteristics in the chamber. A homogeneous fluid/wall oil film two-phase stratified flow model is proposed to investigate the air/oil two-phase lubrication medium flow in an aeroengine bearing chamber, and the effects of shaft speed and oil mass flow rate on the pressure, flow velocity and temperature for the homogeneous fluid and wall oil film are discussed in detail. In the model, the equivalent physical feature parameters of air (containing droplets) are determined by the component rate of droplets and air in the mixture of air and droplets, and the convection heat transfer coefficients between relevant walls and fluid medium in the bearing chamber are calculated by their convection heat transfer characteristics, respectively. The calculation results show preliminarily that the pressures of the homogenous fluid and wall oil film increase with increasing oil mass flow rate, and are influenced complexly by shaft speed;that the flow velocities of the homogenous fluid and wall oil film increase with increasing shaft speed, and are influenced insignificantly by oil mass flow rate;that the homogenous fluid temperature decreases with increasing oil mass flow rate, and are influenced slightly by shaft speed;and that the wall oil film temperature increases with increasing shaft speed and decreasing oil mass flow rate. Finally, a bearing chamber experimental facility is built, and the pressure and temperature under the air/oil two-phase flow condition are measured in the bearing chamber. The calculation results agree well with experimental data.
出处 《机械工程学报》 EI CAS CSCD 北大核心 2014年第21期164-173,共10页 Journal of Mechanical Engineering
基金 国家自然科学基金资助项目(51275411 50975233)
关键词 航空发动机 轴承腔 均匀流体 壁面油膜 油气两相 aeroengine bearing chamber homogeneous fluid wall oil film air/oil two-phase
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参考文献20

  • 1LEE C W, PALMA P C, SIMMONS K, et al. Comparison of computational fluid dynamics and particle image velocimetry data for the airflow in an aeroengine bearing chamber [J]. Journal of Engineering for Gas Turbines and Power, 2005, 127(4): 697-703.
  • 2AIDARINIS J, MISSIRLIS D, YAKINTHOS K, et al. CFD modelling and LDA measurements for the air-flow in an aeroengine front bearing chamber [J]. Journal of Engineering for Gas Turbines and Power, 2011, 133(8): 0825041-0825048.
  • 3陈薄,陈国定,张永红,孙恒超.航空发动机轴承腔气相速度场数值模拟[J].机械科学与技术,2012,31(8):1241-1246. 被引量:7
  • 4GLAHN A, KURRECK M, WILLMANN M, et al. Feasibility study on oil droplet flow investigations inside aeroengine bearing chambers--PDPA techniques in combination with numerical approaches [J]. Journal of Engineering for Gas Turbines and Power, 1996, 118(4): 749-755.
  • 5GLAHN A, BUSAM S, BLAIR M F, et al. Droplet generation by disintegration of oil films at the rim of a rotating disk [J]. Journal of Engineering for Gas Turbines andPower, 2002, 124(1): 117-124.
  • 6GORSE P, DULLENKOPF K, BAUER H J, et al. An experimental study on droplet generation in bearing chambers caused by roller bearings[C].// Proceedings of theASME Turbo Expo 2008: Power for Land, Sea, and Air, June 9-13, 2008, Berlin, Germany, 2008: 1681-1692.
  • 7FARRALL M, SIMMONS K, HIBBERD S, et al. 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.
  • 8GORSE P, BUSAM S, DULLENKOPF K. Influence of operating condition and geometry on the oil film thickness in aeroengine bearing chambers [J]. Journal of Engineering for Gas Turbines and Power, 2006, 128(1): 103-110.
  • 9HASHMI A A, DULLENKOPF K, BAUER H J, et al. Experimental investigation of lubrication oil film dynamics in a typical aero-engine bearing chamber environment[C].//Proceedings of the ASME Turbo 2011: Turbine Technical Conference and Exposition, June 6-10, 2011, Vancouver, British Columbia, Canada, 2011: 797-807.
  • 10WANG C, MORVAN H P, HIBBERD S, et al. Thin film modelling for aero-engine bearing chambers [C]. // Proceedings of the ASME Turbo 2011 : Turbine Technical Conference and Exposition, June 6-10, 2011, Vancouver, British Columbia, Canada, 2011: 277-286.

二级参考文献37

  • 1田保红,徐滨士,马世宁,刘世参,梁秀兵.高速电弧喷涂3Cr13钢雾化粒子温度和飞行速度数值模拟[J].机械工程学报,2005,41(7):169-173. 被引量:4
  • 2吴昊天,陈国定.轴承腔中润滑油气液两相分层流动研究[J].中国机械工程,2007,18(15):1800-1803. 被引量:8
  • 3Glahn A, Kurreck M, Willmann M, et al. Feasibility Study on Oil Droplet Flow Investigations inside Aero Engine Bearing Chambers PDPA Techniques in Combination with Numerical Approaches. Journal of Engineering for Gas Turbines and Power, 1996, 118(4): 749-755.
  • 4Farrall M, Simmons K, Hibberd S, et al. A numerical Model for Oil Film Flow in an Aeroengine Bearing Chamber and Comparison Experimental Data. Journal of Engineering for Gas Turbines and Power, 2006,128 ( 1 ) : 111 - 117.
  • 5Farrall M, Hibberd S, Simmons K. The Effect of Initial Injection Conditions on the Oil Droplet Motion in a Simplified Bearing Chamber. Journal of Engineering for Gas Turbines and Power, 2008, 130( 1 ) :012501-1 - 012501-7.
  • 6Farrall M, Hibberd S, Simmons K. Prediction of Air Oil Exit Flows in a Commercial Aero-Engine Bearing Chamber. Journal of Aerospace Engineering, 2006, 220(3 ). 197 - 202.
  • 7刘亚军.航空发动机轴承腔油膜流动及油气两相流型特征分析:[硕士学位论文].西安:西北工业大学,2010.
  • 8Gorse P, Busam S, Dullenkopf K. Influence of Operating Condition and Geometry on the Oil Film Thickness in Aerocngine Bearing Chambers. Journal of Engineering for Turbines and Power,2006, 128 ( 1 ) : 103 - 110.
  • 9Wittig S,Glahn A,Himmelsbach J.Influence of high rotational speeds on heat transfer and oil film thickness in aero-engine bearing chamber[J].Journal of Engineering for Gas and Turbines and Power,1994,116(2):395-401.
  • 10Glahn A,Wittig S.Two-phase air/oil flow in aero-engine bearing chambers assessment of an analytical prediction method the internal wall heat transfer[J].International Journal of Rotating Machinery,1999,5(3):155-165.

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