报告题目：Design and analysis of a multi-part composite frangible cover

报告人：蔡登安 博士(航空宇航学院 航空航天交叉研究院)

报告时间：2018年5月8日（星期二）14:30PM

报告地点：明故宫校区A18-209

主办单位：航空航天交叉研究院、航空宇航学院

报告摘要：

As an important part of a missile storage and launch system, a missile-launch canister cover is a storage device of an inner missile to protect a warhead to avoid damage and to prevent a leak of inert gas before the missile is launched. In the process of missile launch, the cover should be opened timely, not affecting a normal launch. Due to overweight of the blown part when the frangible cover is opened by the gas flow, it may cause a threat to the surrounding equipment. Therefore, a new multi-part composite frangible cover is proposed and analysed. The multi-part frangible cover is divided into three parts: a frame, weak zones and multi-part blown parts. The effect of structure parameters on the strength of weak zone in the multi-part frangible cover is discussed. Based on the equal-strength design principle, a weak zone selection scheme is developed, and the failure process of the multi-part frangible cover is simulated. The numerical results show that the multi-part blown parts are separated almost simultaneously, which agree well with the experiments.

报告人简介：

蔡登安，讲师，2017年12月于南京航空航天大学获得博士学位，主要从事纤维增强复合材料力学行为分析、结构设计与试验验证等方面研究。以第一作者发表SCI论文5篇、EI论文3篇，授权发明专利4项。