Performance testing of attitude control wheel under ceramic bearing support and grease lubricating for micro-small satellites

BAI Yue; CAO Ping; GAO Qing-jia; HUANG Dun-xin; WU Yi-hui

doi:10.3788/OPE.20101809.2016

您当前的位置：

首页 >

文章列表页 >

Performance testing of attitude control wheel under ceramic bearing support and grease lubricating for micro-small satellites

Article | 更新时间：2020-08-12

- Performance testing of attitude control wheel under ceramic bearing support and grease lubricating for micro-small satellites
- Optics and Precision Engineering Vol. 18, Issue 9, Pages: 2016-2021(2010)
- 作者机构：
  
  1. 中国科学院长春光学精密机械与物理研究所, 吉林长春 130033
  2. 长春工程学院理学院,吉林长春 130022
- 作者简介：
- 基金信息：
- DOI：10.3788/OPE.20101809.2016
  CLC： V448.222;TH133.7
- Received：21 December 2009，
  
  Revised：01 March 2010，
  
  Published Online：29 September 2010，
  
  Published：20 September 2010
- 稿件说明：
移动端阅览
白越, 曹萍, 高庆嘉, 黄敦新, 吴一辉. 微小卫星用陶瓷轴承脂润滑姿控飞轮的性能试验[J]. 光学精密工程, 2010,18(9): 2016-2021

BAI Yue, CAO Ping, GAO Qing-jia, HUANG Dun-xin, WU Yi-hui. Performance testing of attitude control wheel under ceramic bearing support and grease lubricating for micro-small satellites[J]. 光学精密工程, 2010,18(9): 2016-2021
白越, 曹萍, 高庆嘉, 黄敦新, 吴一辉. 微小卫星用陶瓷轴承脂润滑姿控飞轮的性能试验[J]. 光学精密工程, 2010,18(9): 2016-2021 DOI： 10.3788/OPE.20101809.2016.

BAI Yue, CAO Ping, GAO Qing-jia, HUANG Dun-xin, WU Yi-hui. Performance testing of attitude control wheel under ceramic bearing support and grease lubricating for micro-small satellites[J]. 光学精密工程, 2010,18(9): 2016-2021 DOI： 10.3788/OPE.20101809.2016.

摘要

为解决微小卫星姿态控制执行元件姿控飞轮的轻量化、高效支撑及润滑问题

提出了应用脂润滑陶瓷轴承为微小卫星姿控飞轮提供支撑和润滑的方法。试验研究了陶瓷轴承脂润滑姿控飞轮的启动、摩擦功耗、温度特性、抗振动性能及寿命特性

试验结果显示:与同型号钢制球轴承相比

陶瓷球轴承在静态摩擦力矩及功耗方面性能更优良

可以有效减小姿控飞轮的启动电流和摩擦功耗。陶瓷轴承脂润滑姿控飞轮在-30~50 ℃具有良好的启动性能

低于卫星最低工作温度20 ℃时仍能保持良好的启动特性

无冷焊问题

完全满足卫星发射时抵抗振动的要求。振动试验后的姿控飞轮在4年的地面真空试验中功耗电流变化率在有真空度和温度变化的影响下小于1%

验证了陶瓷轴承脂润滑姿控飞轮使用寿命优于4年

满足国内微小卫星对姿控飞轮轻量化和使用寿命的要求。

Abstract

In order to solve the problems on lightweight

efficient support and lubricating for the attitude control wheel in a micro-small satellite

a method using grease lubricated ceramic bearing to support and lubricate the attitude control wheel was proposed. The static frication torque

power loss

anti-temperature

anti-vibration and life of the wheel using ceramic bearing support and grease lubricating were analyzed through experiments. The results show that the static frication torque and power loss of the ceramic bearing under grease lubricating are less than those of all-steel bearings

and the starting characteristics of the proposed wheel are very well at the temperature from -30 ℃ to 50 ℃. Moreover

the vibration resistance performances of the wheel under the testing conditions equal to the conditions when a satellite is launched perfectly. After the vibration testing

the wheel has been tested for four years under a vacuum degree of 0.02 Pa and a rotation speed of 5 000 min/s and results show the variations of current are less than 1%

which proves that the life of the attitude control wheel has more than four years and can meet the lightweight and life requirements of micro-small satellites in space.

关键词

Keywords

references

尤政,张高飞. 基于MEMS的微推进系统的研究现状与展望

. 微细加工技术,2004(1):1-7. YOU ZH, ZHANG G F. The review of micro propulsion system based on MEMS

. Micr of Abrication Technology, 2004(1):1-7. (in Chinese)

余文革,钟先信,李晓毅,等. 皮卫星发展展望

. 压电与声光,2004,26(4):289-292. YU W G, ZHONG X X, LI X Y,et al.. Prospects of picosat development

. Piezoelectrics ＆ Acoustooptics, 2004,26(4):289-292. (in Chinese)

武俊峰,安静,徐春剑,等. 姿控飞轮控制系统设计及转速过零分析

. 光学精密工程,2009,17(4):801-806. WU J F, AN J, XU CH J, et al. Design of control system of flywheel and analysis on approach to zero speed

. Opt. Precision Eng., 2009,17 (4):801-806. (in Chinese)

白越,吴一辉,韩邦成. 飞轮单轴姿态控制及储能系统

. 光学精密工程, 2008,16(8):1446-1451. BAI Y, WU Y H, HAN B CH. Single axis attitude control and energy storage system with two flywheels

. Opt. Precision Eng., 2008,16(8):1446-1451. (in Chinese)

白越,杨作起,黎海文,等. 储能/姿控一体化飞轮能耗试验研究

. 光学精密工程, 2007,15(2):243 - 247. BAI Y, YANG Z Q, LI H W, et al.. Experimental study on power loss of integrated energy storage and attitude control flywheel

. Opt. Precision Eng., 2007,15(2):243-247. (in Chinese)

刘治华,白越,黎海文,等. 单轴飞轮储能与姿态控制系统误差分析

. 光学精密工程, 2006,14(1):127-132. LIU ZH H, BAI Y, LI H W, et al.. Analysis on errors of single axis energy storage/attitude control system with double flywheel

. Opt. Precision Eng., 2006,14(1):127-132. (in Chinese)

程颢,葛升民,刘付成,等. 反作用飞轮力矩模式控.制系统设计

. 宇航学报, 2006(6):1248-1253. CHENG H, GE SH M, LIU F CH, et al.. The design of torque mode control for reaction wheel system

. Journal of Astronautics,2006(6):1248-1253. (in Chinese)

黄敦新,白越,黎海文,等. 飞轮轴系润滑剂损失及寿命分析

. 润滑与密封, 2009, 34(9):20-24. HUANG D X, BAI Y, LI H W, et al.. Analysis of molecular diffusion of lubricants and lubrication life of flywheel shafting

. Lubrication Engineering, 2009,34(9):20-24. (in Chinese)

钱桂山,郭景良. 美国军事空间应用技术的基本趋势和重要军用卫星系统

. 国外卫星动态,2004,3:4-11. QIAN G SH, GUO J L. The basic trend of applied space technology of U.S. and the important military satellite system

. Foreign Satellite Trends, 2004,3:4-11. (in Chinese)

ZHONG SH, HOU P M. Review of space information technology

. Journal of System Engineering and Electronics, 2006,17(2):237-244.

WILLIAM R J, MARK J J. Lubrication for space applications . Glenn: NASA Glenn Research Center, 2005.

陈晓伟,梁宇翔. 液体空间润滑剂的现状与发展

. 润滑与密封, 2006(6):176-179. CHEN X W, LIANG Y X. Status and development of liquid space lubricant

.Lubrication Engineering, 2006(6):176-179. (in Chinese)

WILLIAM M, J J ROAMER E P. Evaluation of temperature and material combinations on several lubricants for use in the geostationary operational environmental satellite (GOES) mission filter wheel bearings . Glenn: NASA Glenn Research Center, 2001.

Views

324

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

No data

Related Author

No data

Related Institution

No data

AI问答

Address：No.3888 Dong Nanhu Road, Changchun, Jilin, China Postal code：130033
Tel：0431-86176855 Email：gxjmgc@ciomp.ac.cn
Technical support is provided by Beijing Founder electronics co., LTD 吉ICP备11002662号-17 京公网安备11010802024621
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰