机器人2012，Vol.34Issue(2)：204-210,7.DOI:10.3724/SP.J.1218.2012.00204
带有均压槽的气体静压推力轴承设计
Design of an Aerostatic Thrust Bearing with Pressure-equalizing Grooves
摘要
Abstract
To solve the problem in the space robot's microgravity simulation experiment that lateral interference force/moment exists and the workbench is uneven, a high load capacity, high stiffness round aerostatic thrust bearing with circumferential and radial pressure-equalizing grooves is designed and manufactured, and its load capacity is modeled and numerically analyzed using deformational Reynolds equation. In order to validate the theoretical calculation results, simulation analysis using Fluent is carried out to get the load capacity characteristics, and the influence of the impact created by the high pressure gas on the load capacity is analyzed. Finally, an experiment about the bearing's load capacity characteristics is performed on the standard test platform, and the result is compared with the data of bearing without grooves. It turns out that the structure design and theoretical analysis are correct.关键词
气体静压推力轴承/均压槽/Fluent仿真/承载力/冲击力Key words
aerostatic thrust bearing/pressure-equalizing groove/Fluent simulation/load capacity/impulsive force分类
机械制造引用本文复制引用
冯永可,张延恒,孙汉旭,贾庆轩,艾晨光..带有均压槽的气体静压推力轴承设计[J].机器人,2012,34(2):204-210,7.基金项目
中央高校基本科研业务费专项资金资助项目(2011PTB-00-11) （2011PTB-00-11）
国家863计划资助项目(2010AA7090304). （2010AA7090304）
