|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/219 ; 244/215|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 36 인용 특허 : 0|
A variable camber apparatus for the leading and/or trailing edge of an airfoil that is operable for lift variation at high airspeeds of a jet aircraft such as for maneuvering of fighter aircraft. The cambering apparatus comprises an upper surface flexible skin panel which is supported along its inner edge by a wing spar assembly and along its outermost edge, by an airfoil edge forming structure. A hinged rib member, through a kinematic linkage mechanism associated between itself and the structure at the outermost edge of the airfoil section, bends and to...
A variable camber apparatus for the trailing edge portion of an airfoil, comprising: a trailing edge structure; an aerodynamically continuous upper surface having an inner-end connected to relatively rigid structure of the airfoil and an outer-end fixedly connected to the trailing edge structure; a rib member pivotally mounted about its inner-end to an axis fixed with respect to rigid structure of the airfoil; linkage means interconnecting the trailing edge structure with the rib member such that the rib member supports the outer-end of the upper surface...