基于有限元的高速储能飞轮转子设计

李结冻; 吕东元; 陈军委; 吕奇超

本文已被：浏览 1447次下载 742次

中文摘要: 利用解析法计算出高速储能飞轮转子护套所需过盈量的范围,利用有限元软件进行静止状态和工作状态下护套的应力分析,仿真结果与解析计算结果基本吻合,验证了结果的有效性。分析了装配过程中,护套加热产生的热变形,为护套的过盈安装提供了依据。最后, 对飞轮转子的模态进行了仿真和实验, 两者结果的误差为0.6%。

中文关键词: 解析法有限元热变形过盈

Abstract:The range of interference required by the rotor sheath of high-speed energy storage flywheel is calculated by analytic method. The stress analysis of the sheath in static state and working state is carried out by finite element software. The simulation results are in good agreement with the analytical results, and the validity of the results is verified. The thermal deformation caused by the heating for the sheath during the assembly process is analyzed, which provides the basis for the interference fit of the sheath. Finally, the model of flywheel rotor is simulated and tested, and the error of simulation and experiment is 0.6 %.

keywords: analytic method finite element thermal deformation interference

文章编号：20180309 中图分类号： 文献标志码：

基金项目:

作者	单位
李结冻	上海航天控制技术研究所·上海·201109 上海市空间智能控制技术重点实验室·上海·201109
吕东元	上海航天控制技术研究所·上海·201109 上海市空间智能控制技术重点实验室·上海·201109
陈军委	上海航天控制技术研究所·上海·201109 上海市空间智能控制技术重点实验室·上海·201109
吕奇超	上海航天控制技术研究所·上海·201109 上海市空间智能控制技术重点实验室·上海·201109

Author Name	Affiliation
LI Jiedong	Shanghai Aerospace Control Technology Institute,Shanghai 201109 Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai 201109
LYU Dongyuan	Shanghai Aerospace Control Technology Institute,Shanghai 201109 Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai 201110
CHEN Junwei	Shanghai Aerospace Control Technology Institute,Shanghai 201109 Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai 201111
LYU Qichao	Shanghai Aerospace Control Technology Institute,Shanghai 201109 Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai 201112

引用文本：
李结冻,吕东元,陈军委,吕奇超.基于有限元的高速储能飞轮转子设计[J].飞控与探测,2018,(3):47-53.