The invention discloses a double-wing unmanned aerial vehicle launching platform which comprises two side plates, the same first reinforcing plate is fixed between the two side plates, the same aircraft supporting frame is rotationally arranged at the top between the two side plates and used for placing a double-wing unmanned aerial vehicle, and a mounting base is arranged at the top between the two side plates and used for mounting the double-wing unmanned aerial vehicle. A sucker mechanism is mounted at the bottom of the mounting seat, a swing mechanism for driving the mounting seat and the sucker mechanism to move up and down is mounted on the outer wall of one side plate, and a driving mechanism for moving the aircraft supporting frame is mounted on the aircraft supporting frame. The driving mechanism comprises a bidirectional motor fixed to the outer wall of the aircraft supporting frame, an output shaft of the bidirectional motor is connected with a shaft rod through a transmission mechanism, the two ends of the shaft rod are each fixedly provided with two fourth gears in a penetrating mode, and two symmetrical arc-shaped plates are installed between the two side plates. According to the invention, continuous launching tasks are realized, effective power-assisted launching is realized, and the launching efficiency is better and more efficient.
本发明公开了双翼无人机发射平台,包括两个侧板,两个侧板之间固定有同一个第一加强板,两个侧板之间的顶部转动设置有同一个飞机支撑架,飞机支撑架用于放置双翼无人机,两个侧板之间的顶部设置有安装座,安装座的底部安装有吸盘机构,其中一个侧板的外壁安装有驱动安装座和吸盘机构实现上下移动的摆动机构,飞机支撑架上安装有实现飞机支撑架移动的驱动机构;驱动机构包括固定在飞机支撑架外壁的双向电机,双向电机的输出轴通过传动机构连接有轴杆,轴杆的两端均固定穿设有两个第四齿轮,两个侧板之间安装有两个对称的弧形板。本发明实现连续的发射任务,并起到有效的助力发射,发射效率更好,更高效。
Launching platform of double-wing unmanned aerial vehicle
双翼无人机发射平台
2024-02-27
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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