The invention relates to a multi-power-mode fixed-wing aircraft. The aircraft comprises an aircraft body, a left wing, a right wing, a left aileron, a right aileron, an empennage, and tilting engines;the left wing and the right wing are symmetrically arranged on two sides of the aircraft body; the left aileron is arranged on the left wing; the right aileron arranged on the right wing; the empennage is arranged at the tail part of the aircraft body; the tilting engines are arranged on the left wing, the right wing or the empennage; the number of the tilting engines is three or more; the tilting engines are fixed on tilting wing plates; and the tilting wing plates are connected with the left wing, the right wing or the empennage through rotating motors. According to the multi-power-mode fixed-wing aircraft of the invention, the power mode of the aircraft under take-off, landing and in-transit flight can be switched among a fixed wing power mode, a helicopter power mode and a hybrid power mode according to load change conditions; and heavy-load catapult-assisted take-off and no-load vertical landing modes are particularly suitable for field or narrow space efficient operation such asagricultural plant protection or logistics delivery.

    本发明涉及一种多动力模式固定翼飞行器,包括机身、对称设置在机身两侧的左机翼和右机翼、设置在左机翼上的左副翼、设置在右机翼上的右副翼、设置在机身尾部的尾翼、以及设置在左机翼、右机翼或尾翼上的倾转发动机,倾转发动机的数量为三个或以上,倾转发动机固定在倾转翼板上,倾转翼板通过旋转电机与左机翼、右机翼或尾翼连接。本发明提供一种多动力模式固定翼飞行器,起降及在途飞行动力模式随负载变化情况可在固定翼动力模式、直升机动力模式和混合动力模式间切换,重载弹射起飞、空载垂直降落的模式尤其适用于农业植保或物流投送等野外或狭小空间高效作业。


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    Titel :

    Multi-power-mode fixed-wing aircraft


    Weitere Titelangaben:

    一种多动力模式固定翼飞行器


    Beteiligte:
    CHEN HOURAN (Autor:in)

    Erscheinungsdatum :

    2020-08-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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