航天用感应同步器组件胶膜的研制  

Development of Adhesive Film for Aerospace Induction Synchronizer Components

作　　者：叶振东[1] 徐磊[1] 王桢楠[1] YE Zhengdong;XU Lei;WANG Zhennan(No.21 Research Institute of CETC,Shanghai 200233,China)

机构地区：[1]中国电子科技集团公司第二十一研究所,上海200233

出　　处：《微特电机》2022年第7期62-64,共3页Small & Special Electrical Machines

摘　　要：采用双酚A型环氧树脂(E-54)、聚醚胺改性环氧树脂(D37)、聚氨酯预聚体、双氰胺、改性咪唑,研制了一种航天感应同步器组件专用的板-板粘接胶膜。该胶膜采用中温125℃/2 h固化方式,配合真空压合机压合制作感应同步器组件,并成功用于相关航天器型号中,在轨运行效果良好。By using biphenol A epoxy resin(E-54),polyether gum modified epoxy(D37),polyurethane prepolymer,dicyandiamide and modified imidazole,a special film for space induction synchronizer was developed.The film adopted medium temperature 125℃/2 h curing mode,and was pressed together with vacuum press to produce induction synchronizer components,which was successfully applied in relevant spacecraft models,with good effect in orbit operation.

关 键 词：航天用感应同步器组件 胶膜 板-板粘接 

分 类 号：TM305[电气工程—电机]