Lightweight fuselage for flapping-wing flying robot and flapping-wing flying robot

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Lightweight fuselage for flapping-wing flying robot and flapping-wing flying robot

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XU WENFU / HU XIAOKUN / ZHONG SIPING / YAN LEI

The invention discloses a lightweight fuselage for a flapping-wing flying robot, and the lightweight fuselage comprises a fuselage main rod which extends in the front-back direction and is provided with a cavity; the driving mounting frame is arranged at the front end of the fuselage main rod, and the driving mounting frame is used for mounting the flapping wing driving mechanism; the power supply mounting plate is arranged in the middle of the machine body main rod and used for mounting a power supply assembly; the empennage mounting frame is arranged at the rear end of the fuselage main rod and used for mounting an empennage assembly; by applying the fuselage, the energy consumption of the ornithopter can be effectively reduced; the invention further provides a flapping-wing flying robot.

本发明公开了一种用于扑翼飞行机器人的轻量化机身，包括：机身主杆，机身主杆沿前后方向延伸，机身主杆开设有空腔；驱动安装框架，设置在机身主杆前端，驱动安装框架用于安装扑翼驱动机构；电源安装板，设置在机身主杆中部，电源安装板用于安装电源组件；尾翼安装架，设置在机身主杆后端，尾翼安装架用于安装尾翼组件；应用上述机身能够有效降低扑翼飞行器的能耗；本发明还提供一种扑翼飞行机器人。