The invention provides a spacecraft structure suitable for vertical layout of a rigid flat plate in the technical field of spaceflight. The spacecraft structure comprises a rigid flat plate spacecraft, a force transmission block, a V-shaped clamping block and a wrapping tape. The force transmission block is connected with the rigid plate spacecraft, and the force transmission block is arranged on the rigid plate spacecraft in a pressing manner through a wrapping tape; a connecting ring is fixedly arranged on the rigid plate spacecraft; the V-shaped clamping block is fixedly arranged on the force transmission block, and the force transmission block is arranged on the V-shaped clamping block in a limiting manner; and the outer sides of the V-shaped clamping blocks are fixedly provided with wrapping belts. By arranging the force transmission block, the V-shaped clamping block and the belting connection design as a novel spacecraft connection form, a conventional common main force bearing column structure form is replaced, connection of multiple spacecrafts is achieved, the vertical or oblique layout requirement of the rigid flat plate spacecraft is met, and the design is simple and convenient. The effective utilization rate of the carrying space and the spacecraft launching efficiency are further improved, and the application requirements of one-rocket multi-spacecraft launching and rapid networking at present are met.
本发明提供了航天技术领域一种适用于刚性平板竖向布局的航天器结构,包括刚性平板航天器、传力块、V型卡块以及包带;传力块与刚性平板航天器连接设置,传力块通过包带压紧设置刚性平板航天器;刚性平板航天器上固定设置有连接环;V型卡块固定设置在传力块上,V型卡块限位设置传力块;V型卡块外侧固定设置包带。本发明通过设置传力块、V型卡块以及包带连接设计作为一种新型的航天器连接形式,替代以往常用的主承力柱结构形式,实现多个航天器的连接,满足刚性平板航天器竖向或斜向的布局需求,进一步提升运载空间有效利用率以及航天器发射效率,满足当前一箭多航天器发射以及快速组网的应用需求。
Spacecraft structure suitable for vertical layout of rigid flat plate
适用于刚性平板竖向布局的航天器结构
2023-04-04
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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