The invention discloses a double-duct aircraft power system improved structure which comprises an aircraft frame body and a battery used for providing electric energy, the center of the aircraft frame body is arranged to be a driving and taking position, a propeller power system is arranged on the aircraft frame body, and the propeller power system comprises a left duct spiral assembly and a right duct spiral assembly. The left ducted spiral assembly and the right ducted spiral assembly are arranged at the left side end and the right side end of a riding position of the aircraft frame body respectively. The aircraft is simple in structure and convenient to use, the motor is adopted as a power source, the propeller of the aircraft is directly driven to work through the driving motor, the aircraft can ascend and fly, the driving motor is adopted as the power source, the stability and safety of propeller operation can be effectively guaranteed, and the aircraft is more stable and reliable. And whether the driving motors need to operate at the same time or not can be controlled manually, the direction of airflow is changed in cooperation with a flow guide assembly below, good controllability and maneuverability are achieved, and the aircraft can fly stably.
本发明公开了一种双涵道飞行器动力系统改进结构,包括飞行器架体及用于提供电力能源的电池,飞行器架体的中心设置为驾乘位,飞行器架体上设有螺旋桨动力系统,螺旋桨动力系统包括左涵道螺旋组件和右涵道螺旋组件,左涵道螺旋组件和右涵道螺旋组件分别设置在飞行器架体的驾乘位左右两侧端;本发明结构简单、使用方便,通过采用电机来作为动力源,使得飞行器的螺旋桨直接通过驱动电机来驱动工作,使飞行器能够上升飞行,采用驱动电机作为动力源,能够有效保证螺旋桨运行的稳定性和安全性,还能通过人工来控制驱动电机是否需要同时运行,并搭配下方的导流组件对气流的方向进行改变,具有良好的操控性和机动性,能够使飞行器平稳飞行。
Improved structure of power system of double-duct aircraft
一种双涵道飞行器动力系统改进结构
2024-07-05
Patent
Electronic Resource
Chinese
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