|국가/구분||United States(US) Patent 등록|
|§371/§102 date||19820929 (19820929)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 43 인용 특허 : 1|
A variable wing tip (18) for securing to a variable camber leading edge portion (12) of an aircraft wing (10). The wing tip has a normal fore and aft camber in an upper position and is adapted to have an increased camber curvature in a deflected down position. In the down position, the wing tip has a compound curvature, is shortened in the fore and aft direction ad is generally thickened in depth in a substantial portion of the wing tip. By operation of an actuator (96) in the leading edge (21), a multiple of generally parallel scissor plates (30,32) are...
In an aircraft wing, a variable camber wing tip forming an outboard and forward portion of said wing, said wing tip comprising: an inboard generally fore and aft extending end of the wing tip being secured along a complementary outer end of a variable camber leading edge portion of the wing; a trailing edge of the wing tip extending along a fixed outboard forwardly facing edge of the wing; said wing tip having a normal camber on its upper surface in an upper position and being adapted to have an increased camber curvature in a deflected down position; sa...