直升机复合材料结构装配工艺研究  

Study on Assembly Techniques of Composite Structures of Some Helicopter

作　　者：李子峰[1] 唐义号[2] 吴剑峰[2] 

机构地区：[1]黑龙江工商职业技术学院,黑龙江哈尔滨150001 [2]中国直升机设计研究所,景德镇333001

出　　处：《纤维复合材料》2008年第2期11-13,共3页Fiber Composites

摘　　要：本文详细分析了直升机复合材料关键装配特征,进行了装配工装设计。系统研究了制孔、锪窝、切割加工工艺及铆接、螺接等连接工艺和方法。为今后大型复杂复合材料结构装配奠定了基础。The main assembly factor of some helicopter was analyzed detailed and the assembly tooling was designed. The machining techniques of drilling and countersink and cutting and the techniques of riveting connecting and screw connecting were studied. This study will lay a foundation for the complex composite structures assembly.

关 键 词：复合材料 复合材料机械加工 装配连接工艺 

分 类 号：V262.4[航空宇航科学与技术—航空宇航制造工程]