Power source control method for propeller of new energy aircraft

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Power source control method for propeller of new energy aircraft

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FAN YU / YANG YI / WANG YAN'AN

The invention belongs to the technical field of aviation equipment power source control, and particularly relates to a power source control method for a propeller of a new energy aircraft, which comprises the following steps of: calibrating a corresponding relation among a throttle lever angle, required power and output torque through an energy control computer, and performing closed-loop control by taking the throttle lever angle as a target value; according to the method, the design of the whole power source control system is optimized from the design concepts of safety, convenience, greenness, environmental protection, high efficiency and energy conservation of the aircraft, and the thrust of the aircraft is adjusted through the motor controller. And the environmental protection property, the reliability, the comfort, the maintainability and the economical efficiency of the aircraft are greatly improved.

本发明属于航空设备动力源控制技术领域，具体涉及一种新能源飞机的螺旋桨的动力源控制方法，通过能量控制计算机标定油门杆角度与所需功率、输出转矩的对应关系，进而以油门杆角度为目标值进行闭环控制，输出相应的目标功率值和目标扭矩控制，从而通过电动机控制器调节来调节飞机推力大小，本发明从飞机安全便捷、绿色环保、高效节能设计理念出发，优化整个动力源控制系统的设计，极大地提高了飞机的环保性、可靠性、舒适性、维修性和经济性。