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纤维缠绕圆筒压力容器结构分析
引用本文:陈汝训.纤维缠绕圆筒压力容器结构分析[J].固体火箭技术,2004,27(2):105-107.
作者姓名:陈汝训
作者单位:中国航天科技集团公司四院,西安,710025
摘    要:对具有内衬的纤维缠绕圆筒压力容器进行了结构分析。将内衬作为各向同性材料,纤维缠绕圆筒作为正交异性材料处理。在内压作用下,得到了内衬和纤维缠绕圆筒的弹性应力和应变。讨论了内衬和纤维缠绕圆筒材料选取和结构设计准则,即应选取弹性模量很低,强度较高和塑性良好的材料作内衬;选取模量和强度都较高的纤维缠绕圆筒;内衬壁厚应尽可能薄,且与纤维缠绕圆筒粘接牢固。算例表明,弹性应力分析结果与测试值符合良好。

关 键 词:纤维缠绕壳体  压力容器  内衬  应力  固体火箭发动机
文章编号:1006-2793(2004)02-0105-03
修稿时间:2003年11月24

Structure analysis for filament-wound cylinder pressure vessel
CHEN Ru-xunThe Fourth Academy of CASC,Xi'an,China..Structure analysis for filament-wound cylinder pressure vessel[J].Journal of Solid Rocket Technology,2004,27(2):105-107.
Authors:CHEN Ru-xunThe Fourth Academy of CASC  Xi'an  China
Institution:CHEN Ru-xunThe Fourth Academy of CASC,Xi'an710025,China.
Abstract:The structure analysis of the filament-wound cylinder pressure vessel with internal liner are performed.In the analysis,the liner is regarded as an isotropic material and the filament-wound cylinder is orthotropic material.The elastic stress and strain in the liner and the filament-wound cylinder caused by internal pressure are obtained.The criteria for the material selection and structure design of the filament-wound vessel are discussed.It is suggested that the liner material should be of low modulus,high strength and excellent plasticity,and the filament-wound cylinder shoule be of high modulus and high strength.The liner thickness should be thiner and the adhesion between the filament-wound cylinder and the liner must be secure.The calculation example shows that the elastic stress analysis agrees with the results of the test.
Keywords:filament-wound case  pressure vessel  liner  stress  
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