The invention relates to the field of aircrafts, and discloses an electric vertical take-off and landing tilt rotor aircraft which comprises an aircraft body 1, a front fixed wing 2, a rear fixed wing 3, a ducted coaxial double-rotor tilt assembly 4, an aircraft take-off and landing supporting frame 5, a power battery 6 and a flight control system 7. According to the electric vertical take-off and landing tilt rotor aircraft, directional thrust is provided through ducted coaxial double rotor tilting, and the aircraft can be transited to a transition mode from a hovering mode, then to a forward flying mode and then returns to the hovering mode. The aircraft can vertically take off and land, hover and fly forwards, special airports and runways are not needed, the use cost is reduced, the carbon emission is remarkably reduced, the manufacturing difficulty is reduced, the flight efficiency is high, the flight speed is high, and the flight stability is high.

    本发明涉及航空器领域,公开了一种电动垂直起降倾转旋翼航空器,包括机身1、前固定翼2、后固定翼3、涵道式共轴双旋翼倾转组件4、航空器起落支撑架5、动力电池6、飞行控制系统7;所述电动垂直起降倾转旋翼航空器通过涵道式共轴双旋翼倾转提供定向推力,航空器可以从悬停模式过渡到过渡模式,然后到前飞模式,再回到悬停模式。所述航空器能垂直起降、悬停、前飞,不需要专门的机场和跑道,减小使用成本,显著减少碳排放量,降低制造难度,飞行效率高,飞行速度快,飞行稳定性高等。


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    Titel :

    Electric vertical take-off and landing tilt rotor aircraft


    Weitere Titelangaben:

    一种电动垂直起降倾转旋翼航空器


    Beteiligte:
    WANG SHUIHAO (Autor:in)

    Erscheinungsdatum :

    14.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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