|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||24/4217 ; 24/409.0R|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 44 인용 특허 : 6|
An aircraft aileron system unique in its construction, method of deployment and the functional results obtained, is comprised of two panels located at the rear portion of the wing, in a spanwise direction and aligned with the wing's trailing edge. The panels are independently hinged at their leading edges and rotate to make angular deflections with respect to the wing. The upper, aileron panel is restricted to upward deflection only from its neutral position and in operation is deployed independently as an aileron. The lower, auxiliary flap panel is capa...
[ What is claimed is:] [1.] An aerodynamic control system for control of an aircraft around a longitudinal axis of the aircraft, comprising an aileron assembly disposed on each wing of the aircraft, each aileron assembly having an upper panel and a lower panel each pivotally attached adjacent to the trailing edge of the wing, with the upper surface of the upper panel forming a continuation of the wing's upper surface when the upper panel is in a neutral position and the lower surface of the lower panel forming a continuation of the wing's lower surface w...