摘要
复合材料在设计性、工艺性、结构减重等方面有着很大的优势,其在飞机制造中的应用比重也越来越大。以某型飞机为例,详细分析和探讨了垂直尾翼根部整流罩结构基于复合材料的设计过程,具体包括整流罩结构的总体布置、复合材料面板的铺层设计、气动密封件设计、表面防护设计、装配设计等方面的内容。
Composite material has so much superiority in the field of design, technology and loss of structure weight that its rate of application in the aircraft manufacturing is higher and higher. The composite material based design procedure of the root fairing of vertical tail has been analyzed and discussed detailedly in this article, and it concretely contains the general arrangement of fairing, the spread design of composite material based panel, the de- sign of aerodynamic seals, the design of surface protection, the design of assembly, etc.
出处
《民用飞机设计与研究》
2014年第1期18-21,共4页
Civil Aircraft Design & Research
关键词
复合材料
垂直尾翼
整流罩
机身
Composite Material
Vertical Tail
Fairing
Fuselage
