A lift module capable of achieving vertical flight in a fixed-wing aircraft and producing low aerodynamic drag during horizontal flight, the lift module essentially comprising: a structural compartment (40); and two covers (41A) and (41B) hinged to a structural compartment (40) by means of arms (41A-1) and (41B-1), said structural compartment containing at least one drive assembly (43) and at least one rotor (42), said rotor being locked when the lift module (4) is closed during horizontal flight and unlocked when the lift module is open to generate lift by rotation of the rotor.

    一种升力模块,其能够在固定翼飞行器中实现垂直飞行并在水平飞行期间产生低空气动力学阻力,该升力模块基本包括:结构隔室(40);和两个盖(41A)和(41B),两个盖借助于臂(41A‑1)和(41B‑1)铰接到结构隔室(40),所述结构隔室包含至少一个驱动组件(43)和至少一个旋翼(42),其中,当升力模块(4)在水平飞行期间关闭时,所述旋翼被锁定,并且当升力模块打开时,旋翼被解锁,以通过旋翼的旋转产生升力。


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    Titel :

    Lift module for vertical take-off and landing aircraft and aircraft comprising such module


    Weitere Titelangaben:

    用于垂直起降飞行器的升力模块和包含这种模块的飞行器


    Beteiligte:

    Erscheinungsdatum :

    28.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge