The invention discloses a vertical take-off and landing transport aircraft. Front wings are arranged between the nose of a fuselage and a middle fuselage; rear wings are arranged at the rear part of the middle fuselage; the rear wings are higher than the front wings; front wing ducted fans are arranged at the two ends of the front wings; rear wing ducted fans are arranged at the two ends of the rear wings; front wing ailerons and front wing flaps are arranged at the rear edges of the front wings to form two front wing operation control surfaces respectively; the rear wing ailerons and the rearwing flaps are arranged at the rear edge of the rear wings; two rear wing operation control surfaces are respectively arranged; the front wing distributed propellers are arranged below the front partof the front wings and are arranged in an array along the wingspan direction; and rear wing distributed propellers are arranged below the front part of rear wing and are arranged in an array along the wingspan direction. According to the aircraft, a double-upper-single-wing and distributed propeller power device mode is adopted, high cruise lift-drag characteristics can be obtained in a wide speed domain range, the battlefield viability of the aircraft is improved, and the structural weight of the aircraft body is effectively reduced.
本发明公开了一种垂直起降运输机,前翼设置在机身的机头及中机身之间,后翼机身的中机身后部,后翼高度比前翼高,前翼涵道风扇设置在所述的前翼两端,后翼涵道风扇设置在后翼两端,前翼副翼、前翼襟翼设置在前翼后缘,分别形成两个前翼操作舵面,后翼副翼、后翼襟翼设置在后翼后缘,分别两个后翼操作舵面,前翼分布式螺旋桨设置在前翼前部下方且沿翼展方向呈阵列排布,后翼分布式螺旋桨设置在后翼前部下方且沿翼展方向呈阵列排布,本发明采用双上单翼+分布式螺旋桨动力装置形式,可在较宽速域范围获得较高巡航升阻特性,提升飞机战场生存能力,有效减轻机体结构重量。
Vertical take-off and landing transport aircraft
一种垂直起降运输机
2020-04-17
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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