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基于阻抗法的径向均压槽气浮支承承载力研究
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国家自然科学基金项目(51705378);湖北省自然科学基金项目(2018CFB757);武汉科技大学国防预研基金项目(GF201908).


Research on Bearing Capacity of Aerostatic Bearing with Radial Pressure Groove by Impedance Method
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    摘要:

    为提高气浮支承计算效率,以气浮表面布置径向均压槽的气浮支承为研究对象,提出一种计算径向均压槽气浮支承承载力的阻抗模型,利用CFD数值仿真验证阻抗模型的可行性,并分析均压槽深度、半径及角度对阻抗模型的影响。结果表明:该阻抗模型可计算不同截面形状的径向均压槽和无均压槽2种模型的承载力,且利用阻抗模型计算气浮支承承载力与CFD数值仿真计算结果具有较好的一致性;在气膜较小时,气浮支承表面布置均压槽结构能提高系统的阻抗系数,可有效提高气浮支承承载力;均压槽的深度、半径对系统的阻抗系数影响较大,而均压槽角度对系统的阻抗系数影响较小。

    Abstract:

    In order to improve the calculation efficiency of the aerostatic bearing,an impedance model for calculating the loading capacity of the aerostatic bearing with the radial pressure groove arranged on the surface was presented,and the feasibility of the impedance model was verified by CFD numerical simulation,and the influence of the depth,radius and angle of the pressure groove on the impedance model was analyzed.The results show that the impedance model can be used to calculate the loading capacity of radial pressure groove and non-pressure groove with different section shapes,and the results of CFD numerical simulation are in good agreement with those of the impedance model.When the air film is small,the system impedance coefficient and bearing capacity of the air aerostatic bearing can be improved by arranging the pressure groove on the surface of the aerostatic bearing.The depth and radius of the pressure groove have great influence on the impedance coefficient of the system while the angle of the pressure groove has little influence on the impedance coefficient of the system.

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夏巨兴,于普良,胡回,姜庆,鲜小东.基于阻抗法的径向均压槽气浮支承承载力研究[J].润滑与密封,2021,46(12):86-92.
XIA Juxing, YU Puliang, HU Hui, JIANG Qing, XIAN Xiaodong. Research on Bearing Capacity of Aerostatic Bearing with Radial Pressure Groove by Impedance Method[J]. Lubrication Engineering,2021,46(12):86-92.

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  • 在线发布日期: 2022-04-07
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