The invention discloses an ejector rod adjustable double-rocket booster unmanned aerial vehicle launching device, and belongs to the technical field of unmanned aerial vehicle launching. Comprising a rack, and a pair of ejector rod mechanisms used for jacking the rocket booster are arranged on the rack; the ejector rod mechanism comprises an ejector rod head, a first ejector rod and a second ejector rod; the ejector rod head is hinged to the first ejector rod and can swing up and down relative to the first ejector rod and be limited. The ejector rod head is used for jacking the tail part of the rocket booster; the first ejector rod is connected with the second ejector rod, and the first ejector rod can freely rotate relative to the second ejector rod; and the second ejector rod can axially move and be positioned. A booster rocket bracket is omitted, the bracket and the booster rocket are integrally designed, the rocket is fixed to the launcher through the adjustable ejector rod mechanism, rocket assembling work on a launching site is omitted, and the total weight of the booster rocket can be effectively reduced; the ejector rod mechanism is convenient to adjust and large in adjusting range, the matching precision requirement is obviously lowered, and the ejector rod mechanism can adapt to unmanned aerial vehicle launching in different scenes.
本发明公开了一种顶杆可调式双火箭助推器无人机发射装置,属于无人机发射技术领域。包括台架,台架上设有一对用于顶托火箭助推器的顶杆机构;顶杆机构包括顶杆头、第一顶杆和第二顶杆;顶杆头与第一顶杆铰接,可相对于第一顶杆上下摆动并限位;顶杆头用于顶托火箭助推器的尾部;第一顶杆与第二顶杆连接,第一顶杆可相对于第二顶杆自由转动;第二顶杆可轴向移动并定位。取消助推火箭托架,将托架和助推火箭进行一体化设计,采用可调节的顶杆机构将火箭固定在发射架上,免除了发射现场火箭组装工作且可有效地减轻了助推火箭的总重量;顶杆机构调节方便且调节范围大,明显降低了配合精度要求,可适应不同场景下的无人机发射。
Ejector rod adjustable double-rocket booster unmanned aerial vehicle launching device
顶杆可调式双火箭助推器无人机发射装置
2024-03-26
Patent
Electronic Resource
Chinese
IPC: | B64U |
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