| 摘要 |
Wing parts ( 20, 21 ) which influence the lift of aircraft wings ( 1 ), especially wings ( 1 ) with a cross section and an angle of attack which is suitable for high-speed flight, which parts can be moved out of an aerodynamically inactive servicing position within the aircraft fuselage ( 30 ) or out of chambers ( 40 ) mounted on the wings ( 1 ) into an aerodynamically efficient active position and from the active position back into the servicing position, are assigned to the wings ( 1 ). These wing parts ( 20, 21 ) in their active position are located on the top ( 3 ) and optionally also on the bottom ( 4 ) of the wings ( 1 ) and are shaped for example such that the wing parts ( 21 ) located in their active position on the bottom ( 4 ) of the wings ( 1 ) jointly with the wing parts ( 20 ) located in their active position on the top ( 3 ) of the wings ( 1 ) increase the lift and optionally at the same time change the angle of attack of the wing.
|
