|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/75R ; 91/464 ; 91/509|
|우선권정보||FR-0000206 (1984-01-09); FR-0000207 (1984-01-09)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 15 인용 특허 : 0|
Flight control system for aircraft of the type provided with ailerons, elevators, upper surface spoilers, and upper surface air-brakes, a rudder and horizontal stabilizers with variable angle of incidence, said system comprising an electric control, in some cases without any mechanical emergency control for said upper surface spoilers and air-brakes. According to the invention: the ailerons and elevators are electrically controlled without any mechanical aid, the rudder is mechanically controlled, and the horizontal stabilizers with variable angle of inc...
In an aircraft, an electrical-mechanical compound flight control system comprising: piloting means (12); computer means (21, 22) receiving piloting orders from said piloting means (12); ailerons (6), upper surface spoilers (7) and upper surface air-brakes (8); first, second and third actuator means (13, 14, 20) for respectively actuating said ailerons (6), said upper surface spoilers (7) and said upper surface air-brakes (8), said first, second and third actuator means being electrically controlled by said computer means (21, 22) and said ailerons (6) be...