本发明提供一种垂直起降飞机,包括用于运输乘客和/或负载的机身(2);附接于机身的前机翼(3);附接于机身的后机翼(4),在向前飞行方向上后机翼在前机翼的后方;右连接梁(5a)和左连接梁(5b),该连接梁(5a、5b)在结构上与前机翼和后机翼连接,连接梁与机身间隔开;以及在每个连接梁上的至少两个提升单元(M1‑M6),每个提升单元包括至少一个螺旋桨(6b)和至少一个驱动螺旋桨的马达(6a),优选为电动马达,并且提升单元被布置为其各自的螺旋桨轴线在基本上竖直的方向(z);至少部分前机翼具有掠角γ,45°≤γ≤135°,优选地γ=75°,至少部分后机翼具有掠角β≥30°的前掠,优选地β=65°。

    We propose a VTOL aircraft (1), comprising:a fuselage (2) for transporting passengers and/or load;a front wing (3) attached to the fuselage (2);a rear wing (4) attached to the fuselage (2), behind the front wing (3) in a direction of forward flight (FF);a right connecting beam (5a) and a left connecting beam (5b), which connecting beams (5a, 5b) structurally connect the front wing (3) and the rear wing (4), which connecting beams (5a, 5b) are spaced apart from the fuselage (2); and at least two lifting units (M1-M6) on each one of the connecting beams (5a, 5b), which lifting units (M1-M6) each comprise at least one propeller (6b) and at least one motor (6a) driving said propeller (6b), preferably an electric motor, and are arranged with their respective propeller axis in an essentially vertical orientation (z);wherein the front wing (3), at least in portions thereof, has a sweep angle γ between γ = 45° and γ = 135°, preferably γ = 75°, and the rear wing (4), at least in portions thereof, has a forward sweep with sweep angle β ≥ 30°, preferably, β = 65°.


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    Titel :

    垂直起降飞机


    Erscheinungsdatum :

    04.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge