A compact layout folding unmanned helicopter is characterized in that a flight control module is responsible for stability of an aircraft in folding and unfolding processes, and flight control of the aircraft in different directions is realized through variable pitch control rotors and tail rotors; rotors of the power modules are driven by motors to rotate around hollow spindles to provide lift force for the aircraft, and tail rotors are driven by the motors to provide yaw moment. The sensor module is used for sensing information such as position, speed and attitude of the aircraft; the ejection module is used for loading the unmanned helicopter and ejecting the unmanned helicopter from a launch canister to realize rapid deployment so as to form all-directional coverage and efficient coping capacity to the surrounding environment; the load module can be provided with detection equipment, weapons, food, drugs and the like according to different requirements of flight missions. According to the unmanned helicopter, through flexible folding of the rotors and the tail rotors, storage of the tubular fuselage is achieved, and the storage and transportation cost of the unmanned helicopter is reduced; rapid catapult-assisted take-off can be achieved through the gunpowder launching device, and the rapid deployment capacity and maneuverability of the unmanned helicopter are improved.
一种紧凑型布局折叠无人直升机,飞行控制模块负责飞行器在折叠和展开过程中的稳定性,同时通过变距操纵旋翼和尾桨实现飞行器不同方向的飞行控制;动力模块的旋翼由电机驱动绕空心主轴旋转为飞行器提供升力,尾桨由电机驱动提供偏航力矩;传感器模块用于感知飞行器的位置、速度、姿态等信息;弹射模块用于将无人直升机装入并从发射筒弹出,实现快速部署以形成对周围环境的全方位覆盖和高效应对能力;载荷模块可根据飞行任务的不同需求,安装探测设备、武器、食品药品等。本无人直升机通过旋翼与尾桨的灵活折叠,实现管式机身存储,降低无人直升机的存储运输成本;并且能够通过火药发射装置实现快速弹射起飞,提高无人直升机快速部署能力和机动性。
Compact-layout tubular folding unmanned helicopter
一种紧凑布局管式折叠无人直升机
2025-02-14
Patent
Electronic Resource
Chinese
IPC: | B64U |
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