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.
出处
《航空制造技术》
2009年第S1期48-49,52,共3页
Aeronautical Manufacturing Technology
关键词
典型结构件
胶接共固化
整体结构
π加筋
Typical structure Bonding co-curing Integral structure π stiffener
