The invention provides a vertical take-off and landing aircraft comprising a fuselage (2) for transporting passengers and/or loads; a front wing (3) attached to the fuselage; a rear wing (4) attached to the fuselage, the rear wing being rearward of the front wing in the forward flight direction; a right connecting beam (5a) and a left connecting beam (5b), the connecting beams (5a, 5b) being structurally connected to the front and rear wings, the connecting beams being spaced apart from the fuselage; and at least two lifting units (M1-M6) on each connecting beam, each lifting unit comprising at least one propeller (6b) and at least one motor (6a) driving the propeller, preferably an electric motor, and the lifting units being arranged with their respective propeller axes in a substantially vertical direction (z); at least part of the front wing has a sweep angle gamma, 45 DEG < = gamma < = 135 DEG, preferably gamma = 75 DEG, and at least part of the rear wing has a sweep forward with a sweep angle beta > = 30 DEG, preferably beta = 65 DEG.
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°。
Vertical take-off and landing aircraft
垂直起降飞机
2022-09-13
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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