The invention discloses a tilt rotor aircraft, and relates to the field of aerospace. The tilt rotor aircraft comprises a fuselage, and a tilt multi-rotor system, a sensing device and a flight controller which are carried on the fuselage; the tilting multi-rotor system comprises a plurality of tilting rotors; in each tilting rotor, one end of a machine arm is fixed on the machine body, and a tilting driving device is mounted at the other end of the machine arm; a motor is mounted on the tilting driving device; the motor is connected with the paddle and used for driving the paddle to rotate according to a preset rotating speed; the tilting driving device is used for driving the motor and the blades to tilt by a preset angle. In the flight control process, the sensing device measures actual attitude data of the fuselage; the flight controller is used for analyzing and judging the actual attitude data, and when the actual attitude of the fuselage does not accord with the expected attitude, the attitude of the fuselage is adjusted by controlling the tilting angle of the blades and the rotating speed of the motor, so that the flight energy consumption can be remarkably reduced, and the flight cruising ability, the flight speed, the wind resistance, the stability and the safety are improved.

    本申请公开了一种倾转旋翼飞行器,涉及航空航天领域。倾转旋翼飞行器包括机身以及搭载在机身上的倾转多旋翼系统、传感装置和飞行控制器;倾转多旋翼系统包括多个倾转旋翼;每个倾转旋翼中,机臂的一端固定在机身上,机臂的另一端安装有倾转驱动装置;倾转驱动装置上安装有电机;电机与桨叶连接,用于驱动桨叶按照预设转速旋转;倾转驱动装置用于带动电机和桨叶倾转预设角度。飞行控制过程中,传感装置测量机身的实际姿态数据;飞行控制器用于对实际姿态数据进行分析判断,当机身实际姿态与期望姿态不符时,通过控制桨叶倾转角度和电机转速来调整机身姿态,能够显著降低飞行能耗,提高飞行续航能力、飞行速度、抗风性、稳定性以及安全性。


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    Titel :

    Tilt-rotor aircraft


    Weitere Titelangaben:

    一种倾转旋翼飞行器


    Beteiligte:
    SU ZHENGYI (Autor:in) / QIU DIANCHEN (Autor:in) / WU HUAYAN (Autor:in) / CHEN HONGYUN (Autor:in)

    Erscheinungsdatum :

    30.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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