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作 者:HUANG Ming-han ZHANG Wen-zhong TONG De-sheng PENG Hong-mei YANG De-quan
机构地区:[1]CCCC-Key Hydrodynamic Laboratory for Coastal Engineering,Tianjin Port Engineering Institute Limited of China Communications Construction Company Limited, Tianjin 300222, China [2]School of Civil Engineering, Tianjin University, Tianjin 300072, China [3]Institute of Physics and Electronic Information,Inner Mongolia University for the Nationalities,Tongliao Inner Mongolia 028043, China
出 处:《航空动力学报》2014年第5期1211-1215,共5页Journal of Aerospace Power
基 金:National Natural Science Foundation of China(11362015)
摘 要:The problem of hydrodynamics of the three-leaf dislocated floating-ring bearing was studied by means of boundary element method.The law including the distribution of pressure on boundary surface(axial,bearing and floating-ring)and its friction loss in different eccentricities was obtained.The results show that the inner friction of three-leaf dislocated bearing increases from 390.875to 1 091.65,and the inner friction of three-leaf dislocated floating-ring bearing increases from 94.2523to 114.5069with eccentricity varying from 0to 0.075in nondimensional.So changing the pressure and flow field of bearing by adding floating-ring is more stability and less wasted work of friction than three-leaf dislocated bearing.The problem of hydrodynamics of the three-leaf dislocated floating-ring bearing was studied by means of boundary element method.The law including the distribution of pressure on boundary surface(axial,bearing and floating-ring)and its friction loss in different eccentricities was obtained.The results show that the inner friction of three-leaf dislocated bearing increases from 390.875to 1 091.65,and the inner friction of three-leaf dislocated floating-ring bearing increases from 94.2523to 114.5069with eccentricity varying from 0to 0.075in nondimensional.So changing the pressure and flow field of bearing by adding floating-ring is more stability and less wasted work of friction than three-leaf dislocated bearing.
关 键 词:三叶错位浮环轴承 流体力学 边界元法 稳定性 内摩擦
分 类 号:V229.2[航空宇航科学与技术—飞行器设计]
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