论文:2013,Vol:31,Issue(1):71-76
引用本文:
孙恒超, 陈国定, 陈薄. 航空发动机涡轮前支承轴承腔油气两相物理场分析[J]. 西北工业大学
Sun Hengchao, Chen Guoding, Chen Bo. Physical Fields of Oil/Air Two-Phase in Aeroengine Bearing Chamber in front of Turbine[J]. Northwestern polytechnical university

航空发动机涡轮前支承轴承腔油气两相物理场分析
孙恒超, 陈国定, 陈薄
西北工业大学 机电学院, 陕西 西安 710072
摘要:
处在航空发动机热区的涡轮前支承轴承腔的油气两相物理场分析是进行二次流及润滑系统设计的重要基础工作。文章结合某型发动机涡轮前轴承腔的结构和工况参数,构建了适用于发动机全运行状态下的轴承腔油气两相物理场理论计算模型,求解获得了轴承腔内油气两相介质流动的物理场。探讨了轴承腔内油气两相流动的速度、压力、温度及壁面油膜厚度在腔内不同位置的分布情况;分析了发动机运行状态对上述物理场的影响规律;与试验数据的比较支持了文中理论分析方法的正确性。提出的轴承腔油气两相物理场分析方法对于航空发动机主轴支承轴承腔的润滑与换热设计具有应用价值。
关键词:    航空发动机    轴承腔    两相流    物理场    对流换热    油膜厚度   
Physical Fields of Oil/Air Two-Phase in Aeroengine Bearing Chamber in front of Turbine
Sun Hengchao, Chen Guoding, Chen Bo
Department of Mechanical Engineering,Northwestern Polytechnical University,Xi'an 710072,China
Abstract:
The analysis of physical fields of oil/air two-phase flow of in bearing chamber in front of turbine and athot zone of aeroengine is an important and basic work in designing lubrication and secondary air systems.Accordingto the geometry and operating parameters of bearing chamber equipped on a certain turbofan engine, a theoreticalcalculation model for analyzing oil/air physical fields in bearing chamber for all operating states of aeroengine isbuilt, the oil/air two-phase flow physical fields are obtained.The velocity, pressure, temperature and oil filmthickness distributions of oil/air two-phase flow in bearing chamber are discussed.The effect of aeroengine operat-ing sates on physical fields is analyzed.The comparison of calculated values and experimental data supports the cor-rectness of the present theoretical methods.The theoretical methods for analyzing oil/air two-phase physical fieldsand the calculated results presented in this paper are, we believe, applicable to bearing chamber lubrication andheat transfer engineering design and academic research.
Key words:    aircraft engines    calculations    design    experiments    heat convection    heat transfer    mathematicalmodels    pressure distribution    temperature distribution    velocity distribution    two phase flow;bear-ing chamber    convection heat transfer    physical fields   
收稿日期: 2012-04-19     修回日期:
DOI:
基金项目: 国家自然科学基金(50975233、51275411);西北工业大学研究生创业种子基金(Z2012051)资助
通讯作者:     Email:
作者简介: 孙恒超(1987-),西北工业大学博士研究生,主要从事航空发动机润滑系统设计研究。
相关功能
PDF(666KB) Free
打印本文
把本文推荐给朋友
作者相关文章
孙恒超  在本刊中的所有文章
陈国定  在本刊中的所有文章
陈薄  在本刊中的所有文章

参考文献:
[1] Wittig S,Glahn A,Himmelsbach J.Influence of High Rotational Speeds on Heat Transfer and Oil Film Thickness in Aero-En-gine Bearing Chambers.Journal of Engineering for Gas Turbines and Power.1994,116(2): 395-401
[2] Glahn A,Busam S,Wittig S.Local and Mean Heat Transfer Coefficients along the Internal Housing Walls of Aero Engine Bear-ing Chambers.ASME Paper,1997(97-GT): 261
[3] Busam S,Glahn A,Wittig S.Internal Bearing Chamber Wall Heat Transfer as a Function of Operating Conditions and ChamberGeometry.Journal of Engineering for Gas and Turbines and Power,2000,122(2): 314-320
[4] Gorse P,Busam S,Dullenkopf K.Influence of Operating Condition and Geometry on the Oil Film Thickness in Aero-EngineBearing Chambers.Journal of Engineering for Gas and Turbines and Power,2006,128(1): 103-110
[5] Glahn A,et al.Feasibility Study on Oil Droplet Flow Investigations inside Aero Engine Bearing Chambers-PDPA Techniques inCombination with Numerical Approaches.Journal of Engineering for Gas and Tarbines and Power,1996,118(4): 749-755
[6] Farrall M,Hibberd S,Simmons K.Modelling Oil Droplet/Film Interaction in an Aero-Engine Bearing Chamber.ICLASS-2003,Sorento,Italy,2003
[7] Chen Guoding,Sun Hengchao,Wang Jun.Research into Configuration and Flow of Wall Oil Film in Bearing Chamber Based onDroplet Size Distribution.Chinese Journal of Aeronautics,2011,24(3): 355-362
[8] 林基恕.航空发动机设计手册第 12 册传动与润滑系统.北京: 航空工业出版社,2002Lin Jishu.Aeroengine Design Manual (Volume 12) Transmission and Lubrication Systems.Beijing: Aviation Industrial Press,2002 (in Chinese)
[9] 陶文铨.传热学.西安: 西北工业大学出版社,2006Tao Wenquan.Heat Transfer.Xi'an: Press of Northwestern Polytechnical University,2006 (in Chinese)
[10] 斯库巴切夫斯基.航空燃气涡轮发动机零件结构与计算.北京:国防工业出版社,1992Skubachevskiy.Aviation Gas Turbine Engine Part Structure and Calculation.Beijing: National Defense Industry Press,1992 (in Chinese)
相关文献:
1.陈国定, 王涛, 刘曼利, 孙恒超, 张永红.轴承腔两相流动流型特征参数及鲁棒性分析[J]. 西北工业大学, 2012,30(2): 155-159