The invention discloses a multi-wing layout solar aircraft and a control method thereof. The multi-wing layout solar aircraft comprises an aircraft body, front wings, motors, paddles, front ailerons, middle wings, rear wings, rear ailerons, vertical empennages and an energy system. The front wings are mounted on two sides of the front part of the fuselage, the middle wings are mounted on two sides of the middle part of the fuselage, and the rear wings are mounted on two sides of the rear part of the fuselage; motors are mounted on the front wing, the middle wing and the rear wing, and are connected with and drive the paddles; the rear edge of the front wing is connected with the front aileron, and the rear edge of the rear wing is connected with the rear aileron; a power device composed of the motors and the paddles is used for controlling the working states of the motors on the front wing, the middle wing and the rear wing, and the yawing action of the aircraft is controlled by controlling the rotating speed difference of the motors on the two sides of the aircraft body. The aircraft is provided with three pairs of wings, the rigidity and the crosswind resistance of the aircraft wings and the longitudinal stability and the transverse lateral stability of the aircraft are improved, the cruise lift coefficient of the aircraft is increased through the design of the multi-wing layout, and the cruise efficiency of the aircraft is improved.
本发明公开了一种多机翼布局的太阳能飞机及其控制方法,包括机身、前机翼、电机、桨叶、前副翼、中机翼、后机翼、后副翼、垂直尾翼及能源系统;前机翼安装在机身的前部两侧,中机翼安装在机身的中部两侧,后机翼安装在机身的后部两侧;前机翼、中机翼、后机翼上均安装有电机,电机连接并驱动桨叶;前机翼的后缘连接前副翼,后机翼的后缘连接后副翼;电机和桨叶组成动力装置用于控制前机翼、中机翼、后机翼上的电机的工作状态,通过控制机身两侧的电机转速差来控制飞机的偏航动作。本发明有三对机翼,提高了飞机机翼的刚度和抗侧风能力,飞机的纵向稳定性和横侧向稳定性,且多机翼布局的设计提高了飞机的巡航升力系数,提高了飞机的巡航效率。
Solar aircraft with multi-wing layout and control method thereof
一种多机翼布局的太阳能飞机及其控制方法
22.04.2025
Patent
Elektronische Ressource
Chinesisch
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