The invention provides an aircraft with an anti-crash function after aerodynamic configuration damage. The aircraft comprises a remote controller, an aircraft body and wings, pressure sensors are arranged on the surface of the aircraft body and the surfaces of the wings, a control center system, a power control system and an auxiliary control system are installed in the aircraft body, and the control center system is in wireless connection with the remote controller. The control center system is connected with the pressure sensor, the power control system and the auxiliary control system. Theauxiliary control system comprises a side cabin door and an auxiliary flight device arranged behind the side cabin door, and the auxiliary flight device is a paraglider; the auxiliary control system is used for receiving working signals to control the side cabin door to be opened and the paraglider to extend out, and the paraglider, the fuselage and the wings form a gliding structure. The problemsthat at present, after the aerodynamic configuration of an aircraft is damaged, the aircraft loses control, a remote controller cannot control the aircraft any more, and the aircraft often falls downto be damaged and even scrapped are solved.
本发明提供一种具有气动外形受损后防坠毁功能的飞行器,包括遥控器、机身和机翼,机身表面和机翼表面均设置有压力传感器,机身内安装有控制中心系统、动力控制系统和辅助控制系统,控制中心系统与遥控器无线连接,控制中心系统分别与压力传感器、动力控制系统和辅助控制系统连接;辅助控制系统包括侧舱门和设置在侧舱门后的辅助飞行装置,辅助飞行装置为滑翔伞;辅助控制系统用于接收工作信号控制侧舱门打开,滑翔伞伸出,滑翔伞、机身和机翼形成滑翔结构。本发明解决了目前当飞行器气动外形受损后,飞行器就会失去控制,遥控器再也无法控制飞行器,飞行器往往会坠落导致损坏,甚至报废的问题。
Aircraft with anti-crash function after aerodynamic configuration damage
一种具有气动外形受损后防坠毁功能的飞行器
2021-03-26
Patent
Electronic Resource
Chinese