The invention discloses a tilting rotorcraft and a power transmission device thereof, and relates to the field of aviation aircrafts. The tilting rotorcraft comprises a rotorcraft body, the head of the rotorcraft body is provided with an airflow rectification grating cover, and the tail of the rotorcraft body is provided with a wind driven generator which is electrically connected with a built-in power supply of the rotorcraft body. The airflow rectification grating cover is connected with the air inlet end of the wind driven generator through an airflow channel; a motor is arranged at the head of the body, an output shaft of the motor is connected with the propeller, and the motor is electrically connected with a body built-in power supply; the power output end of the engine is connected with tilting rotor power transmission boxes located on the tops of the outer ends of the left wing and the right wing of the aircraft body through overrun clutches. The control, the safety, the energy-saving utilization and the like are greatly changed and obviously improved; by integrating the system performance, the airplane generates qualitative change and progress.

    本发明公开了一种倾转旋翼机及其动力传动装置,涉及航空飞行器领域,包括机体,机体的头部设有气流整流格栅罩,机体的尾部设有风力发电机,风力发电机电连接机体内置电源,气流整流格栅罩和风力发电机的进风端之间通过气流通道连接;所述机体的头部还设有电动机,电动机的输出轴连接螺旋桨,电动机电连接机体内置电源;所述机体内设置发动机,发动机的动力输出端通过超越离合器连接位于机体左右两翼外端顶部的倾转旋翼动力传动箱。本发明在操控、安全性、节能利用等方面均有较大变化和显著提高;综合其系统性能,飞机产生了质的变化和进步。


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    Title :

    Tilting rotorcraft and power transmission device thereof


    Additional title:

    一种倾转旋翼机及其动力传动装置


    Contributors:
    ZHU SHIYOU (author)

    Publication date :

    2021-07-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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