航天器复合材料胶接连接工艺分析  

Analysis of Adhesive Technology in Spacecraft Composite Materials

作　　者：沃西源[1] 涂彬[1] 夏英伟[1] 

机构地区：[1]北京空间机电研究所,北京100076

出　　处：《航天返回与遥感》2008年第4期62-66,共5页Spacecraft Recovery & Remote Sensing

摘　　要：文章叙述了航天器复合材料胶接工艺应具备的条件,航天器产品常用胶粘剂及其特性,研制航天器复合材料耐久型胶接结构基本要素及复合材料胶接连接工艺特性和品质控制等内容。This article introduced the conditions which should be provided in the adhesive technology of spacecraft composite materials and the properties of the typical adhesives. Also the basic element of durable adhesive structure, characteristics of the adhesive technology and quality control were mentioned in the paper.

关 键 词：胶接连接 品质控制 复合材料 航天器 

分 类 号：TQ174.758[化学工程—陶瓷工业] TB33[化学工程—硅酸盐工业]