直升机板-蜂窝夹层结构件表面成型质量研究  

Panel-Honeycomb Sandwich Structure Composite Part Surface Forming Quality

作　　者：潘永生[1] 

机构地区：[1]海军驻哈尔滨地区航空军事代表室,哈尔滨150066

出　　处：《纤维复合材料》2016年第3期12-16,共5页Fiber Composites

摘　　要：对金属板与蜂窝夹层结构复合材料件,成型后在板-板胶接区、蜂窝胶接区产生大量胶瘤的表面成型缺陷进行了改进。通过增加扒皮布、粘贴胶带保护等方法,提高了产品的表面质量,减少了产品表面的补加工,防止对产品强度、后续工序造成影响。For metal plate and honeycomb sandwich structure composite part improvement are made in panel-panel bonding area after forming, plenty of resin accumulation after curing surface forming defects. Surface quality has been improved by adding peel cloth, bonding tape etc. , reduce the repair of product surface, prevent the impact of product strength and following process.

关 键 词：成型质量 蜂窝夹层结构 复合材料工艺 粘接 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计] V262