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复合材料空心飞轮多环套装整体变形及应力简化精细分析
Alternative TitleSimplified and fine analyses of the full deformation and stress of pressfit of the hollow multi-ring composite flywheel
秦勇; 夏源明; 毛天祥
Source Publication复合材料学报
2003-10-30
Volume20Issue:5Pages:95-99
ISSN1000-3851
Abstract采用多环过盈装配是解决复合材料飞轮径向强度过低的有效途径之一。本文作者采用平面应力简化模型,提出了计及过盈配合后变形导致实际过盈量增大计算飞轮套装后的初终应力分布的方法;提出了基于叠加原理计算多环过盈装配旋转飞轮应力的方法;提出了保证飞轮旋转时配合界面不脱离的相关临界转速的概念和计算方法。算例分析表明;过盈配合后的变形对初终应力的影响不能忽略;过盈量和套装环数与飞轮的初终应力和相关临界转速有密切的关系。
Keyword复合材料飞轮 过盈量 径向强度 相关临界转速
Indexed ByCSCD
Language中文
Funding Organization国家自然科学基金资助项目(10172085)
CSCD IDCSCD:1196830
Citation statistics
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/42360
Collection力学所知识产出(1956-2008)
Corresponding Author秦勇
Recommended Citation
GB/T 7714
秦勇,夏源明,毛天祥. 复合材料空心飞轮多环套装整体变形及应力简化精细分析[J]. 复合材料学报,2003,20(5):95-99.
APA 秦勇,夏源明,&毛天祥.(2003).复合材料空心飞轮多环套装整体变形及应力简化精细分析.复合材料学报,20(5),95-99.
MLA 秦勇,et al."复合材料空心飞轮多环套装整体变形及应力简化精细分析".复合材料学报 20.5(2003):95-99.
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