复合材料前机身典型结构件整体成型  

Integral Molding on Typical Structure of Composites Forward Fuselage

作　　者：常海峰[1] 梁宪珠[1] 李黎[2] 

机构地区：[1]北京航空制造工程研究所 [2]成都飞机设计研究所

出　　处：《航空制造技术》2009年第S1期48-49,52,共3页Aeronautical Manufacturing Technology

摘　　要：介绍了前机身典型结构件的研制过程,阐述了胶接共固化和二次胶接等成型方法在研制过程中的应用及相关工艺方案的选择与设计,通过工艺效果评估,证明了本方案是切实可行的。The development process of typical structure of the forward fuselage is described,the emphasis is placed on the application of bonding co-curing and secondary bonding methods in the development process and the selection and design of associated process plan.It is proved that the program is practicable through the assessment of process effect.

关 键 词：典型结构件 胶接共固化 整体结构 π加筋 

分 类 号：V261[航空宇航科学与技术—航空宇航制造工程]