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一种星载柔性超轻型折叠式碳纤维伸杆
Application NumberCN201710480484.8
杨萱; 梁旭豪;  沈峰;  马鑫;  李涛;  王劲东;  张艺腾;  杨震;  李明涛;  孟新;  刘波;  陶然;  杨根;  魏德超;  杨剑宇
2017-06-22
ClassificationB64G1/22(2006.01)I
Country中国
Abstract本发明公开了一种星载柔性超轻型折叠式碳纤维伸杆,所述碳纤维伸杆包括:柔性伸杆(1),所述柔性伸杆(1)沿杆件轴向设置若干个长圆通孔(3),作为柔性弯曲关节(15)。本发明采用一体化碳纤维材料构型设计,碳纤维伸杆具备超轻质量的特点,适用于大型卫星、小型卫星等不同规模的卫星安装使用,其单位长度重量小于200g;而且由于本发明的碳纤维伸杆采用自动存储、释放弹性势能的柔性弯曲关节设计,其具备无外需能源自展开,并自动展开定型的功能,节省了星上资源的消耗。
Language中文
Document Type专利
Identifierhttp://ir.nssc.ac.cn/handle/122/6103
Collection空间技术部
Affiliation空间技术部
Recommended Citation
GB/T 7714
杨萱,梁旭豪, 沈峰,等. 一种星载柔性超轻型折叠式碳纤维伸杆[P]. 2017-06-22.
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