The invention discloses a wing assembly with slats and an aircraft. The wing assembly includes a swept wing body, a leading edge of the wing body extending outward and rearward from a wing root to a wing edge; a first slat selectively movably connected to the wing body; and a second slat selectively movably connected to the wing body, the second slat being disposed outboard of the first slat, a flexible sealing member disposed and connected between the first slat and the second slat; at least a portion of the first slat, at least a portion of the second slat, and at least a portion of the flexible sealing member defining a slat gap therebetween, at least a majority of the slat gap being substantially parallel to a predetermined local airflow direction. An aircraft is also disclosed which includes a fuselage; and two oppositely disposed wing assemblies connected to the fuselage.
带有缝翼的机翼组件和飞机。一种机翼组件,包括:后掠机翼本体,所述机翼本体的前边缘从机翼根部向外并且向后延伸到机翼边缘;选择性地以可移动方式连接到所述机翼本体的第一缝翼;和选择性地以可移动方式连接到所述机翼本体的第二缝翼,所述第二缝翼设置在所述第一缝翼的外侧,柔性密封部件被设置并且连接在所述第一缝翼和所述第二缝翼之间;所述第一缝翼的至少一部分、所述第二缝翼的至少一部分和所述柔性密封部件的至少一部分在它们之间限定缝翼间隙,所述缝翼间隙的至少大部分基本上平行于预定局部气流方向。还公开了一种飞机,所述飞机包括机身;和连接到所述机身的两个相对设置的机翼组件。
WING ASSEMBLY WITH SLATS AND AIRCRAFT
带有缝翼的机翼组件和飞机
2020-12-11
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |