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复合材料飞轮结构及强度设计研究进展
引用本文:秦勇,夏源明. 复合材料飞轮结构及强度设计研究进展[J]. 兵工学报, 2006, 27(4): 750-756
作者姓名:秦勇  夏源明
作者单位:中国兵器工业,系统总体部,北京,100089;中国科学技术大学,力学和机械工程系,安徽,合肥,230027
摘    要:复合材料飞轮储能系统结合了新材料技术、磁悬浮技术、高速可逆电机技术等,使得飞轮系统的储能密度大大提高,并引起了各国科技部门的高度关注。飞轮本体的结构和强度设计作为飞轮系统中的理论性的问题一直没有形成系统完整的分析方法,针对这一问题进行了概述,指出了现有模型的不足,为建立系统完整的复合材料飞轮强度设计方法提出了建议。

关 键 词:复合材料  复合材料飞轮  储能密度  结构和强度设计  多环过盈装配  张紧力缠绕
文章编号:1000-1093(2006)04-0750-07
收稿时间:2005-09-05
修稿时间:2005-09-05

A Study on the Structure and Strength of Composite Flywheel
QIN Yong,XIA Yuan-ming. A Study on the Structure and Strength of Composite Flywheel[J]. Acta Armamentarii, 2006, 27(4): 750-756
Authors:QIN Yong  XIA Yuan-ming
Affiliation:1. North China Institute of System Engineering, Beijing 100089, China; 2.Department of Mechanics and Mechnical Engineering, University of Science and Technology of China, Hefei 230027,Anhui, China
Abstract:A composite flywheel system incorporates the use of new material technology, magnetic suspension technology and high-speed reversible electrical engine techonlogy available today. It is enabled to adopt enormously concentrated energies in their various forms, and has attracted the attention of sci-tech authorities in many lands. Yet there remain unsolved many theoretical problems concerning, the systemic and integrated design of structure and strength of composite flywheel. The progress in these areas of the study are given in generalized terms together with some suggestions.
Keywords:composite material   composite flywheel   energy density   design of structure and strength   multi-ring pressfit   tension filament winding
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