The flexible solar wing supporting and unloading device for the spacecraft is characterized in that a first supporting plate is arranged at the top of a first supporting framework, a first positioning hole is formed in the first supporting plate, a first limiting device is arranged on one side of the first supporting framework, and a first limiting plate of the first limiting device is arranged above the first supporting plate; a second supporting plate is arranged at the top of the second supporting framework, a second positioning hole is formed in the second supporting plate, the second limiting device is arranged on one side of the second supporting framework, and a second limiting plate of the second limiting device is arranged below the second supporting plate; the first supporting framework and the second supporting framework are connected through a connecting piece, and a gap exists between the first supporting framework and the second supporting framework which are connected. According to the invention, precision maintenance of composite substrates with different thicknesses in a horizontal unloading state and a narrow space stitching area and simultaneous tension loading of the two substrates are realized.
本发明提供了一种航天器用柔性太阳翼支撑卸载装置,一号支撑骨架的顶部设有一号支撑板,所述一号支撑板上设有一号定位孔,所述一号限位装置设置的一号支撑骨架的一侧,所述一号限位装置的一号限位板设置在一号支撑板的上方;所述二号支撑骨架的顶部设有二号支撑板,所述二号支撑板上设有二号定位孔,所述二号限位装置设置在二号支撑骨架的一侧,所述二号限位装置的二号限位板设置在二号支撑板的下方;所述一号支撑骨架和二号支撑骨架通过连接件进行连接,连接后的一号支撑骨架和二号支撑骨架之间存在间隙。本发明实现水平卸载状态不同厚度复合基板、狭小空间缝合区域的精度保持及两个基板同时张力加载。
Flexible solar wing supporting and unloading device for spacecraft
一种航天器用柔性太阳翼支撑卸载装置
2025-01-10
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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