The invention discloses a combined type vertical take-off and landing fixed-wing unmanned aerial vehicle, which has a canard wing configuration having a cabin attached to a left main wing and a right main wing. A left front wing and a right front wing are connected together to form a one-piece front wing. There is a left linear support connecting the left front wing to the left main wing and a right linear support connecting the right front wing to the right main wing. A plurality of propellers are disposed on the left and right linear supports.
本发明公开了一种复合式垂直起降固定翼无人机,其具有鸭式机翼配置,所述鸭式机翼配置具有附接到左主翼和右主翼的舱。一个左前翼和一个右前翼连接在一起,形成一个单件式前翼。有一个将左前翼连接到左主翼的左线性支撑件,以及一个将右前翼连接到右主翼的右线性支撑件。多个螺旋桨布置在左侧和右侧线性支撑件上。
Combined type vertical take-off and landing fixed-wing unmanned aerial vehicle
一种复合式垂直起降固定翼无人机
28.12.2021
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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