The invention discloses a connecting device, a satellite-rocket separation device and a belting installation method, and solves the technical problems that in the prior art, limiting force changes along with the length, calculation and simulation are complex, and installation is difficult. Comprising two limiting pieces hinged to each other, a first adjusting piece, a second adjusting piece and a separating piece, and the two limiting pieces are used for being hinged to the bag belt; the first adjusting piece comprises a first butt joint end and a first adjusting end connected with the wrapping belt in a limiting mode. The second adjusting part comprises a second butt joint end which is in butt joint with the first butt joint end and a second adjusting end which is in limiting connection with the wrapping belt; the separating piece is arranged at the second butt joint end and the first butt joint end. Transverse limiting can be carried out through the two limiting pieces hinged to each other, the wrapping tape is prevented from colliding with the satellite load, the limiting mode belongs to mechanism connection, the theoretical design difficulty can be effectively lowered, reliability is improved, and the assembly period is shortened.
本申请公开了一种连接装置、星箭分离装置及包带安装方法,解决了现有技术中限位力随长度变化,计算仿真较为复杂,且安装较为困难的技术问题,其中连接装置用于用于连接相邻的包带,包括相互铰接的两个限位件、第一调节件、第二调节件和分离件,其中两个限位件用于与所述包带铰接;第一调节件包括第一对接端和与所述包带限位连接的第一调节端;第二调节件包括与所述第一对接端对接的第二对接端和与所述包带限位连接的第二调节端;分离件设于所述第二对接端和所述第一对接端。通过相互铰接的两个限位件可以进行横向限位,防止包带碰撞卫星载荷,且限位方式属于机构连接,可有效降低理论设计难度,提高可靠性,缩短装配周期。
Connecting device, satellite-rocket separating device and belting mounting method
一种连接装置、星箭分离装置及包带安装方法
2023-06-23
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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