|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/75R ; 244/90R ; 244/215|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 41 인용 특허 : 5|
An improved linkage for the control surfaces, e.g., flaps, of a fighter airplane. The wing of the fighter aircraft includes a thin flap which has inwardly extending portions that extend inwardly of the wing of the aircraft by an amount sufficient to allow angular displacement of the flap without interrupting the continuity of the skin thereof. The linkage includes a radial fork having a first arm, a second arm and an intermediate portion intermediate the first and second arms. The intermediate portion is adapted to be pivotally mouted to the wing of the ...
An improved linkage for positioning a control surface pivotally mounted to an airfoil of an aircraft wherein the control surface has a linkage compartment at a forward end thereof, the linkage compartment having a substantially curvilinear outer shell portion that extends inwardly of the airfoil on the top and bottom thereof, the linkage for pivoting the control surface such that at least a portion of the outer shell of the linkage compartment is interior of the outer shell of the airfoil for all angular displacements, said linkage comprising: actuator m...