|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/110D ; 244/113 ; 244/213 ; 239/26529|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 3 인용 특허 : 0|
Reverser doors on an aircraft are to be opened, closed and splayed to effect pitch and yaw control in combination with reverse thrust. A first actuator achieves open and close control. A second actuator achieves splay control through a linkage, with the first actuator located within the linkage.
A reverser door actuating mechanism for an aircraft having at least two reverser door sets, each door set having two doors, two fixed door pivots at spaced locations with one of said doors secured to each pivot, said doors sized to close a space between said pivots, comprising: a first actuator; a first actuator linkage connected to said first actuator and to each door set for contra-rotating said doors of each door set; a second actuator; and a second linkage connected to said second actuator and to each door of said door sets for rotating said doors of...