The invention discloses a control device of a variable-pitch aircraft, which structurally comprises a controller, a dispersing device, a driving shaft, a propeller hub, a butt joint piece and a radiator, when the control device is used, a propeller is connected to the propeller hub, and each extension head corresponds to a motor for driving the propeller to rotate; guiding wires, needing to be connected, of all motors extend out of the wiring adjusting pieces in a penetrating mode, power lines are connected with power supply connecting points, signal lines are connected with receivers, lines between electronic speed regulators and extending heads are connected to electronic speed controller connecting points, and the power lines and the signal lines connected to the multiple electronic speed controllers are dispersed through the multiple wiring adjusting pieces. Therefore, a user can quickly check the wire of each motor.

    本发明公开了一种变距飞行器的控制装置,其结构包括控制器、分散装置、驱动轴、桨毂、对接件、散热器,本发明进行使用时,将螺旋桨连接在桨毂上,每个延伸头分别对应于一个驱动该螺旋桨转动的电机,将每个电机需要连接的导向贯穿伸出接线调件上,将电源线与电源连接点相接,将信号线与接收器相接,将电子调速器与延伸头之间的线路连接到电调连接点上,通过多个接线调件将多个电调上连接的电源线和信号线进行分散开,使得使用者可以快速查看到每个电机的导线。


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    Title :

    Control device of variable-pitch aircraft


    Additional title:

    一种变距飞行器的控制装置


    Contributors:

    Publication date :

    2022-12-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    H01R Elektrisch leitende Verbindungen , ELECTRICALLY-CONDUCTIVE CONNECTIONS / B64C AEROPLANES , Flugzeuge



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