|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/203 ; 244/210 ; 244/214|
|발명자 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 0|
A slat assembly is mounted upon the leading edge of an aircraft wing, and responds automatically to changes in air speed or in the angle of attack of the wing, to increase lift at lower air speeds, and to reduce the stalling speed of the wing. A capability is induced in the aircraft for landing and taking off in short distances. For an aircraft of given size and power, also, there is offered an added safety factor in that the aircraft is permitted to land at slower landing speeds than have heretofore been possible. For the purpose of accomplishing these ...
A leading edge slat assembly for an aircraft wing comprising: (a) a lower strip attachable to said wing in a position in which the lower strip projects forwardly from the leading edge of the wing; (b) an upper strip overlying the lower strip in spaced relation thereto, said upper and lower strips having leading edge portions that are spaced apart forwardly of the leading edge of the aircraft wing to which the lower strip is attached, the upper strip having a trailing edge portion adapted to overlie the upper surface of the leading edge portion of the win...