The invention relates to the technical field of aerospace, in particular to a special-shaped multi-star distributor, the lower end face of a special-shaped force bearing structure of the special-shaped multi-star distributor is in butt joint with the upper end face of a conical section force bearing structure of the special-shaped multi-star distributor, the lower end face of the special-shaped force bearing structure is a round end face, and the upper end face of the special-shaped force bearing structure is an oval end face; the bearing beam is fixed in a mounting cavity of the special-shaped bearing structure; the top satellite installation support is fixed to the upper end of the special-shaped force bearing structure, and the side satellite installation support is fixed to the outer side face of the special-shaped force bearing structure and is perpendicular to the long diameter direction of the upper end face of the special-shaped force bearing structure. The irregular satellite installation support is fixed to the outer side face of the special-shaped force bearing structure and is perpendicular to the short diameter direction of the upper end face of the special-shaped force bearing structure. The regular-shaped satellites are fixedly mounted on the top satellite mounting bracket and/or the side satellite mounting brackets, and the irregular satellites are fixedly mounted on the irregular satellite mounting brackets. According to the method, the protruding point of the satellite can be enveloped into the safe enveloping range, and the size of the fairing is prevented from being increased.
本申请涉及航空航天技术领域,尤其涉及一种异形多星分配器,其异形承力结构的下端面与其锥段承力结构的上端面对接,异形承力结构的下端面为圆形端面,异形承力结构的上端面为椭圆形端面;其承力梁固定于异形承力结构的安装腔内;顶部卫星安装支架与异形承力结构的上端固定,侧面卫星安装支架固定于异形承力结构的外侧面,且与异形承力结构的上端面的长径方向垂直;不规则卫星安装支架固定于异形承力结构的外侧面,且与异形承力结构的上端面的短径方向垂直;规则形状卫星固定安装至顶部卫星安装支架和/或侧面卫星安装支架上,不规则卫星固定安装至不规则卫星安装支架上。本申请可使卫星的凸出点被包络至安全包络范围内,且避免增大整流罩尺寸。
Special-shaped multi-satellite distributor and irregular satellite installation tool and method thereof
一种异形多星分配器及其不规则卫星安装工装、安装方法
28.06.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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