Optimal design of rotor rim for magnetically suspended flywheel with vernier gimballing capacity

TANG Ji-qiang; HAN Xue-fei; LIU Qiang

doi:10.3788/OPE.20122009.1991

您当前的位置：

首页 >

文章列表页 >

Optimal design of rotor rim for magnetically suspended flywheel with vernier gimballing capacity

Article | 更新时间：2020-08-12

- Optimal design of rotor rim for magnetically suspended flywheel with vernier gimballing capacity
- Optics and Precision Engineering Vol. 20, Issue 9, Pages: 1991-1998(2012)
- 作者机构：
  
  1. 北京航空航天大学新型惯性仪表与导航系统技术国防重点学科实验室北京,100191
  2. 北京航空航天大学惯性技术重点实验室北京,100191
- 作者简介：
- 基金信息：
- DOI：10.3788/OPE.20122009.1991
  CLC： V414.1;V448.2
- Received：11 April 2012，
  
  Revised：28 May 2012，
  
  Published：10 September 2012
- 稿件说明：
移动端阅览
汤继强, 韩雪飞, 刘强. 微框架效应磁悬浮飞轮转子轮缘优化设计[J]. 光学精密工程, 2012,20(9): 1991-1998

TANG Ji-qiang, HAN Xue-fei, LIU Qiang. Optimal design of rotor rim for magnetically suspended flywheel with vernier gimballing capacity[J]. Editorial Office of Optics and Precision Engineering, 2012,20(9): 1991-1998
汤继强, 韩雪飞, 刘强. 微框架效应磁悬浮飞轮转子轮缘优化设计[J]. 光学精密工程, 2012,20(9): 1991-1998 DOI： 10.3788/OPE.20122009.1991.

TANG Ji-qiang, HAN Xue-fei, LIU Qiang. Optimal design of rotor rim for magnetically suspended flywheel with vernier gimballing capacity[J]. Editorial Office of Optics and Precision Engineering, 2012,20(9): 1991-1998 DOI： 10.3788/OPE.20122009.1991.

摘要

基于由磁阻式锥形磁轴承和洛伦兹力磁轴承组成的五自由度微框架磁悬浮飞轮

对转子轮缘进行了优化设计。根据飞轮转子结构特性

提出以质量为优化目标

对轮缘质量、极转动惯量和一阶共振频率等进行理论分析和研究

确定了优化变量。应用优化设计软件 iSIGHT 集成有限元分析软件 ANSYS

采用序列二次规划算法

以一阶共振频率、极转动惯量、最大等效应力、极惯性矩与赤道惯性矩之比等作为约束条件并考虑轮辐根数对轮缘质量的影响

对轮缘进行了优化计算

得到了相关变量的最优化结果。结果表明

其他变量最优、轮辐根数为3时

轮缘具有最小质量为 2.036 kg

比初始质量 2.226 kg减小了8.54%。提出的优化方法提高了转子设计的合理性和效率

对飞轮系统整体优化设计具有重要意义。

Abstract

A 5 DOF magnetically suspended flywheel with vernier gimballing capacity which is composed of a conoid reluctive bearing and a Lorentz magnetic bear was investigated and its rotor rim was designed optimally. Based on the structure of the rotor and the goal to minimize the mass of the rim

the mass

inertial moment and resonance frequency of the rim were analyzed theoretically to confirm the optimal variables. Consequently

an optimal design was achieved through iSIGHT and ANSYS

and by taking the number of spokes into account

the variables were optimized by the sequential quadratic programming algorithm in the restrain cases of the resonance frequency

inertial moment

maximum equivalent stress

and the ratio of polar inertia moment to equinoctial inertial moment. Those results of optimization indicate that the mass of the rim is decreased from 2.226 kg to 2.036 kg (namely reduced by 8.54%) when the number of spokes is 3 and other design variables are optimal. The proposed optimal design method can improve the rationality and efficiency of rotor design

and will be an important part in the optimal design of flywheel systems.

关键词

Keywords

references

刘虎,房建成,刘刚. 基于磁悬浮动量轮微框架能力的卫星滚动一偏航姿态稳定控制研究[J]. 宇航学报, 2010, 31(4):1063-1069. LIU H, FANG J CH, LIU G. Satellite Roll-yaw axis attitude stable control based on magnetically suspended momentum wheel with vernier gimballing capacity [J]. Journal of Astronautic,2010, 31(4): 1063-1069. (in Chinese)[2] 刘彬,房建成,刘刚,等. 磁悬浮飞轮不平衡振动控制方法与试验研究[J]. 机械工程学报, 2010, 46(12): 188-194. LIU B, FANG J CH, LIU G, et al.. Unbalance vibration control and experiment research of magnetically suspended flywheels [J]. Journal of Mechanical Engineering, 2010, 46(12): 188-194. (in Chinese)[3] 吴一辉,高庆嘉,白越,等. 反作用飞轮驱动电机的电磁设计[J]. 光学精密工程, 2010, 18(6): 1319-1325. WU Y H, GAO Q J, BAI Y, et al.. Electromagnetic design of driving motors in reaction wheels [J]. Opt. Precision Eng., 2010, 18(6): 1319-1325. (in Chinese)[4] 韩邦成,刘强. 基于自锁原理的磁悬浮飞轮电磁锁紧机构[J]. 光学精密工程, 2009, 17(10): 2456-2464. HAN B CH, LIU Q. Electromagnetic locking device based on self-locking for magnetic suspended flywheel [J]. Opt. Precision Eng., 2009, 17(10): 2456-2464. (in Chinese)[5] SAWADA H, HASHIMOTO T, NINOMIYA K. High-stability attitude control of satellites by magnetic bearing wheels [J], Transactions of the Japan Society for Aeronautical and Space Sciences, 2001, 44(145): 133-141.[6] GERLACH B, EHINGER M, RAUE H K. Digital controller for a gimballing magnetic bearing reaction wheel. AIAA Guidance, Navigation, and Control Conference and Exhibit, San Francisco, USA, 2005: 1-6.[7] 刘彬,房建成,刘刚. 一种磁悬浮陀螺飞轮方案设计与关键技术分析[J]. 航空学报, 2011, 32 (8): 1478-1487. LIU B, FANG J CH, LIU G. Design of a magnetically suspended gyrowheel and analysis of key technologies [J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(8): 1478-1487. (in Chinese)[8] 李红,叶全红,韩邦成,等.磁悬浮反作用飞轮密封罩结构的优化设计[J]. 光学精密工程, 2007, 15(10): 1571-1576. LI H, YE Q H, HAN B CH, et al.. Optimization design of sealed cowling structure for magnetic bearing reaction flywheel [J]. Opt. Precision Eng., 2007, 15(10): 1571-1576.(in Chinese)[9] ARVIN A C, BAKIS C E. Optimal design of press-fitted filament wound composite flywheel rotors [J]. Composite Structures, 2006(72): 47-57.[10] RAFIQUE A F, HE L S, KAMRAN A, et al.. Multidisciplinary design of air launched satellite launch vehicle: performance comparison of heuristic optimization methods [J]. Acta Astronautica, 2010, 67: 826-844.[11] 蔡森甫, 刘浩荣. 高等数学上册 [M]. 上海: 同济大学出版社, 1988. CAI S F, LIU H R. Advanced Mathematics Volume1 [M]. Shanghai: Tongji University Press, 1988. (in Chinese)

Views

396

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Optimal design of core parameters of high-power laser systems based on weight analysis

On-line balancing of high-speed magnetic suspended flywheel system under force free control of imbalance

Design of micro-positioning stage with flexure hinge

Kinematical properties and optimal design of 3-DOF precision positioning stage

Static performance evaluation and optimal design of 5-DOF parallel mechanical leg

Related Author

PAN Gang

WANG Bing

QU Weidong

XING Hui

ZHANG Yanxiu

MA Na

Kai ZHANG

Peng-cheng PU

Related Institution

Unit of PLA

Institute of Nuclear and New Energy Technology, Tsinghua University

Collaborative Innovation Center of Advanced Nuclear Energy Technology

The Key Laboratory of Advanced Reactor Engineering and Safety, Ministry of Education

Department of Engineering Physics, Tsinghua University

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