The invention belongs to the field of rocket launching, and particularly relates to a low-resilience combined buffering device. The device comprises a plunger barrel, a piston rod, buffering honeycombs, a bottom end baffle and a bottom end baffle locking mechanism when the piston rod moves reversely. The buffering honeycombs comprise the forward stroke buffering honeycombs and the reverse stroke buffering honeycombs. The piston rod comprises two cylinders separated by a middle partition plate. A positive stroke buffering honeycomb playing a positive stroke buffering role is arranged between the plunger barrel and the partition plate of the piston rod; and a reverse stroke buffering honeycomb playing a reverse stroke buffering role is arranged between the partition plate of the piston rod and the bottom end baffle. The problem that an oil gas buffer device commonly used at present rebounds after completing a buffer energy absorption task is solved; and a carrier can be more stable in the recovery landing process, and instability overturning of the carrier is avoided.
本发明属于火箭发射领域,具体涉及一种低回弹组合缓冲装置。包括柱塞筒,活塞杆,缓冲蜂窝,底端挡板和活塞杆反行程运动时的底端挡板锁定机构;缓冲蜂窝包括正行程缓冲蜂窝和反行程缓冲蜂窝,所述活塞杆包括由中部分隔板分隔的两个圆筒;柱塞筒和活塞杆的分隔板之间设有起到正行程缓冲作用的正行程缓冲蜂窝;活塞杆的分隔板和底端挡板之间设有起到反行程缓冲作用的反行程缓冲蜂窝。本发明解决当前常用的油气缓冲装置在完成缓冲吸能任务后会产生回弹的问题;可以让运载器在回收着陆过程中更加稳定,避免运载器发生失稳倾覆。
Low-resilience combined buffering device
一种低回弹组合缓冲装置
2021-07-27
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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