The invention relates to the technical field of aircraft manufacturing, in particular to a deformable wing hair fused annular wing and an electric vertical take-off and landing aircraft, the wing comprises a front wing (1), an arc-shaped side wing (3) and a rear wing (5); one ends of the two front wings (1) located on the two sides of the fuselage are connected with the fuselage through rotating shafts, the other ends of the two front wings (1) are connected with one ends of the two inclined arc-shaped side wings (3) through rotating structures, the other ends of the two inclined arc-shaped side wings (3) are connected with the rear wing on the upper portion of the fuselage through rotating structures, and the front wings (1), the arc-shaped side wings (3) and the rear wing (5) are mutually connected to form an annular wing. The annular wing ensures uniform lift distribution, efficient airflow utilization, enhanced structural strength and compact design.
本发明涉及飞机制造技术领域,特别是指一种可变形翼发融合环形机翼和电动垂直起降飞行器,所述机翼包括:前翼(1)、弧形侧翼(3)和后翼(5);位于机身两侧的两前翼(1)的一端通过转轴与机身相连,两前翼(1)的另一端与两倾斜的弧形侧翼(3)的一端通过转动结构连接,两倾斜的弧形侧翼(3)的另一端与机身上部的后翼通过转动结构连接,前翼(1)、弧形侧翼(3)和后翼(5)相互连接成为环形机翼,所述环形机翼保证了均匀升力分布、高效气流利用、增强结构强度和紧凑设计。
Deformable wing hair fused annular wing and electric vertical take-off and landing aircraft
一种可变形翼发融合环形机翼和电动垂直起降飞行器
13.05.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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