Experimental Study on Plane Cross Joint of Air Static Thrust Bearing with Small Orifice Throttling

被引:0
作者
Wang P. [1 ]
Long W. [1 ]
Xin X. [1 ]
Gao H. [1 ]
Wang J. [1 ]
机构
[1] Faculty of Mechanical and Electrical Engineering, Kunming University of Science and Technology, Kunming, Yunnan
来源
Mocaxue Xuebao/Tribology | 2023年 / 43卷 / 11期
关键词
aerostatic thrust bearing; buffer effect of stagnation zone; micro-vibration characteristic; plane straddle joint; static bearing characteristic;
D O I
10.16078/j.tribology.2023223
中图分类号
学科分类号
摘要
In microgravity simulations in the aerospace fields, the aerostatic thrust bearings affect the static and micro-vibration characteristics of the thrust bearings due to the addition of a time-varying exit boundary at the air film during the completion of the planar spanning-gap test, and the flow field inside the supporting air film varies with the change in the position of the time-varying exit boundary, thus affecting the static and micro-vibration characteristics of the thrust bearings. In order to clarify the service characteristics of aerostatic thrust bearings in the process of spanning the gap, the air film of aerostatic thrust bearings changes at any time when the change in the exit boundary of the macro-performance, this paper was based on the theory of hydrostatic gas lubrication, to build aerostatic thrust bearings planar spanning the gap of the laboratory bench, and carried out experimental research on the disc-type small-orifice throttling aerostatic thrust bearings with central air supply and three throttle orifices uniform distribution. The static and micro-vibration characteristics of bearings under different air supply pressures, different air film thicknesses, and different slot positions were analyzed. It was found that when the plane of the aerostatic thrust bearing spanned the gap, it was equivalent to adding a time-varying outlet boundary to the support air film. Moreover, there would be a high-pressure gas leakage phenomenon, which would lead to a reduction in the bearing capacity of the air bearing. When the throttle orifice faced the gap directly between the experimental tables, the self-excited micro-vibration amplitude of the bearing was the smallest. In the process of plane cross-seam of aerostatic bearing, under the same air film thickness, with the increase of air supply pressure, the static bearing capacity and static stiffness of the bearing were improved. With the load increasing, the micro-vibration amplitude of the air bearings with the throttle orifice directly above the splicing gap reduced. © 2023 Science Press. All rights reserved.
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页码:1310 / 1318
页数:8
相关论文
共 20 条
[1]  
Li Haiyue, Cheng Ze, Zhao Danni, Et al., Research on multi-degreeof-freedom microgravity simulation deployment test system based on suspension method and air flotation method, Chinese Journal of Engineering Design, 27, 4, pp. 508-515, (2020)
[2]  
Qi Naiming, Sun Kang, Wang Yaobing, Et al., Micro/low gravity simulation and experiment technology for spacecraft, Journal of Astronautics, 41, 6, pp. 770-779, (2020)
[3]  
Gao Shanghan, Nong Shenglong, Xu Wubin, Studies on the evolution of shock wave in gas film clearance for aerostatic thrust bearing, Progress in Computational Fluid Dynamics: An International Journal, 20, 4, (2020)
[4]  
Santaguida L, Zhu Z H., Development of air-bearing microgravity testbed for autonomous spacecraft rendezvous and robotic capture control of a free-floating target[J], Acta Astronautica, 203, pp. 319-328, (2023)
[5]  
Sun Ang, Ma Wenqi, Wang Zuwen, A review on the application equation in gas lubrication of high supply pressure, China Mechanical Engineering, 19, 17, pp. 2090-2094, (2008)
[6]  
Hu Xiaoru, Design and analysis of six-degree-of-freedom motion simulation system for spacecraft on-orbit service, (2022)
[7]  
Yoshimoto S, Yamamoto M, Toda K., Numerical calculations of pressure distribution in the bearing clearance of circular aerostatic thrust bearings with a single air supply inlet[J], Journal of Tribology, 129, 2, pp. 384-390, (2007)
[8]  
Long Wei, Bao Gang, Analysis of orifice compensated aerostatic bearing with supersonic flow, Hydraulics Pneumatics & Seals, 28, 4, pp. 64-68, (2008)
[9]  
Guo Liangbin, Peng Baolin, Load characteristics of parallel circular aerostatic thrust bearing in adiabatic perfect gas, Journal of Wuhan University of Science and Technology, 34, 1, pp. 62-68, (2011)
[10]  
Yang He, Study on static load-bearing characteristics of aerostatic thrust bearing across joints, (2012)