The invention discloses a booster separation mechanism which comprises an unmanned aerial vehicle, a passive separation mechanism and a booster, one end of the booster is fixedly connected with a front ejector rod, the two sides of the unmanned aerial vehicle are fixedly connected with mounting blocks and fuselage rear hanging shafts, and a fuselage front ball socket is formed in the bottom side wall of each mounting block; the passive separation mechanism comprises two adapter side plates, an adapter front baffle is fixedly connected between the bottoms of the two adapter side plates, and the two ends of the upper side of each adapter side plate are fixedly connected with a first fixing block and a second fixing block. When the belly space of the fuselage is insufficient, the booster can be transversely installed, installation is easy and convenient, the booster can be automatically separated after stopping working, the separation track is controllable and does not interfere with the unmanned aerial vehicle, the separation time is shortened, the influence on the attitude of the unmanned aerial vehicle is reduced, it is ensured that a boosting engine can be controllably separated in time, and the reliability of the unmanned aerial vehicle is improved. The surface of the separated unmanned aerial vehicle is kept complete.
本发明公开了一种助推器分离机构,包括无人机、被动分离机构和助推器,所述助推器的一端固定连接有前顶杆,所述无人机的两侧均固定连接有安装块和机身后挂轴,每个所述安装块的底侧壁上开设有机身前球窝;所述被动分离机构包括两个适配器侧板,两个所述适配器侧板底部之间固定连接有适配器前挡板,每个所述适配器侧板的上侧两端均固定连接有第一固定块和第二固定块。本发明能够在机身腹部空间不足时,能够横向安装助推器,且安装简便,助推器停止工作后能够自动分离,分离轨迹可控且不与无人机发生干涉,缩短分离时间,减小对无人机姿态的影响,确保助推发动机能够及时、可控地分离,分离后无人机表面保持完整。
Booster separation mechanism
一种助推器分离机构
2022-08-12
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |