The invention provides a rocket body turning-over device and a rocket hoisting system. The rocket body turning-over device comprises end journals, a connecting plate and a hoisting device; at least two end journals are clamped on the outer circumferential surface of a rocket body and are arranged in the axial direction of the rocket body at intervals; the connecting plate is arranged in the axialdirection of the rocket body and is erected on the plurality of end journals; and at least two hoisting ends of the hoisting device are connected to the connecting plate. According to the rocket bodyturning-over device, the plurality end journals are arranged on the rocket body, the connecting plate is arranged on the end journals, the hoisting device performing hoisting at the two positions of the connecting plate, and the rocket body can be turned over by adjusting the hoisting height of two hoisting points; and the structure is simple, the cost is low, corresponding ancillary facility needed by the above structure is extremely few, a rocket can be erected in a non-special launching field, the construction cost of a special launching site is reduced, and the requirements on the rocket launching environment are reduced.
本发明中提供了一种箭体翻转装置及火箭吊装系统,一种箭体翻转装置包括端轴颈,至少两个端轴颈卡装在箭体的外周面上,且沿箭体的轴向间隔设置;连接板,沿箭体的轴向设置且架装在若干端轴颈上;起吊装置,其至少两处起吊端连接在连接板上。本发明中的箭体翻转装置仅需要通过在箭体上设置若干个端轴颈,端轴颈上设置连接板,起吊装置起吊在连接板的两处位置,通过调节两处起吊点的起吊高度,即可实现对火箭箭体的翻转,结构简单,成本低,且上述结构需要相应的配套设施极少,可完全实现在非专用发射场地内对火箭进行起竖操作,降低专用发射场地的建设成本,降低对火箭发射环境的要求。
Rocket body turning-over device and rocket hoisting system
箭体翻转装置及火箭吊装系统
2020-04-28
Patent
Electronic Resource
Chinese
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