The invention discloses an energy-saving semi-rotating free flapping rotor aircraft, which is characterized in that supports are symmetrically fixed to the two sides of an aircraft body, a clutch control system, a brake and a navigation control system are fixed to the support on each side of the aircraft body, meanwhile, flapping rotors and navigation driving force generating devices are symmetrically arranged on the two sides of the aircraft body through the supports, and the flapping rotor and the navigation driving force generating device on each side of the aircraft body are connected through a clutch; during rising, under the control of the controller, the navigation control system drives the navigation driving force generating device to work, and the clutch control system controls the clutch to combine the flapping rotor with the navigation driving force generating device; and during navigation, under the control of the controller, the navigation control system drives the navigation driving force generating device to work, and the clutch control system controls the clutch to separate the flapping rotor from the navigation driving force generating device.
一种节能型半转自由扑旋翼航空器,机身的两侧对称固定有支架,机身每侧的支架上均固定离合器控制系统、制动器和航行控制系统,同时扑旋翼和航行驱动力产生装置均通过支架对称设置在机身的两侧,且机身每侧的扑旋翼和航行驱动力产生装置均通过离合器连接;上升时,在控制器的控制下,航行控制系统驱动航行驱动力产生装置工作,且离合器控制系统控制离合器将扑旋翼和航行驱动力产生装置结合;航行时,在控制器的控制下,航行控制系统驱动航行驱动力产生装置工作,且离合器控制系统控制离合器将扑旋翼和航行驱动力产生装置分离。
Energy-saving semi-rotating free flapping rotor aircraft
一种节能型半转自由扑旋翼航空器
2021-03-05
Patent
Electronic Resource
Chinese