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航天器复合材料桁架连接增强方法与验证

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大型航天器主承载复合材料桁架局部承受过大的轴向拉伸载荷时,存在接头与杆件拉脱破坏的风险.基于胶接桁架碳纤维分层破坏机理,提出了外套管增强胶接、锥面配合增强胶接和组合增强胶接 3 种连接增强方案,通过优化传力路径达到降低层间应力的目的.针对 3 种连接增强方案,投产了相应的试件开展性能测试.经试验验证,胶接增强设计方法能够有效提高承载能力 33%~66%,极限拉脱力达到 200 kN,可为大型航天器主承载桁架研制提供参考.
Connection Enhancement Method and Its Verification for Spacecraft Composite Truss
When the main bearing composite truss of large spacecraft is subjected to excessive axial tensile load locally,there is a pulling failure risk for bar and joint.Based on layered failure mech-anism of truss adhesive,three kinds of adhesive reinforcement design schemes are proposed:out-er sleeve reinforcement,conical fit reinforcement,and combination reinforcement.By optimizing the force transmission path,the goal of reducing interlayer stress is achieved.Corresponding specimens are put into production to carry out performance tests.Experimental results show that the adhesive reinforced design scheme can effectively increase the bearing capacity by 33%~66%,and the ultimate pull-out force can reach 200kN,which can provide useful reference for the development of the main bearing truss of large spacecraft.

spacecraftcomposite trussadhesive bondingconnection enhancement

马超、王志国、张如变、胡宗文、刘良威、陆晴、陈红飞、胡敏

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上海卫星工程研究所,上海 201109

上海复合材料科技有限公司,上海 201112

上海卫星装备研究所,上海 200240

航天器 复合材料桁架 胶接接头 连接增强

2024

航天器工程
中国空间技术研究院总体部(北京空间飞行器总体设计部)

航天器工程

CSTPCD北大核心
影响因子:0.552
ISSN:1673-8748
年,卷(期):2024.33(3)