碳纤维复合材料在某舱段壳体的应用及验证
Application and Verification of Carbon Fiber Composites on a Certain Type Shell
邱雄 1安梦雷 2段萌 1祁腾飞2
作者信息
- 1. 中国空空导弹研究院,洛阳 471009
- 2. 天津爱思达航天科技有限公司,天津 300302
- 折叠
摘要
本文阐述了碳纤维复合材料在某舱段壳体中的设计制造、仿真分析和试验验证.首先结合复合材料的特点介绍了复材壳体的设计过程和工艺方法,之后运用ABAQUS软件按照载荷工况进行了位移和应变仿真分析,最后通过了静力试验和环境鉴定试验(包括振动、加速度、冲击),验证了碳纤维复合材料在此产品应用的可行性,从而实现了产品轻量化的设计目标.
Abstract
This research describes the design,manufacturing,analysis and tests during carbon fiber composites applied on the shell structure.Combined with the characteristics of composite material,the design process and manufacturing method of this shell are introduced.The software ABAQUS is used to analyze the displacement and the strain according to the forces in working conditions.The static test and environmental test are passed(including vibration,acceleration,impact),verifying the feasibility of the application of carbon fiber composites in this product,and the aim of weight optimization is achieved.
关键词
碳纤维复合材料/设计/仿真/试验/检验Key words
carbon fiber composite material/design/simulation/test/inspectio引用本文复制引用
出版年
2024
NETL
NSTL
万方数据