The invention relates to the field of aircraft impact reduction equipment, and discloses a one-way impact isolation device suitable for a microsatellite, which comprises a lower base plate, a positioning plate mounted at the upper end of the lower base plate, an upper base plate mounted at the upper end of the positioning plate, a top buffer part mounted at the upper end of the upper base plate, and a mounting plate mounted at the upper end of the top buffer part, a connecting piece penetrating through the lower base plate, the positioning plate and the upper base plate is installed on the lower base plate, a bottom connecting base is arranged on the lower portion of the connecting piece, and an energy absorption mechanism is arranged on the lower portion of the lower base plate. The impact force buffering and isolating device has the effect that the problems that an existing buffering and isolating device is simple in structural design and poor in impact force buffering and isolating effect are effectively solved.
本申请涉及飞行器减冲击设备的领域,公开了一种适用于微小卫星的单向冲击隔离装置,其包括下基板,在下基板的上端安装有定位板,在定位板的上端安装有上基板,在上基板的上端安装有顶缓冲件,在顶缓冲件的上端安装有安装板,在下基板上安装有贯穿下基板、定位板,以及上基板的连接件,在连接件下部设置有底连接座,在下基板的下部设置有吸能机构。本申请具有有效改善现有的缓冲隔离装置结构设计简单,对冲击力的缓冲隔离效果差的问题的效果。
One-way impact isolation device suitable for microsatellite
一种适用于微小卫星的单向冲击隔离装置
08.04.2022
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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