|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/53B ; 55/306 ; 60/39092 ; 60/39093|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 27 인용 특허 : 4|
An actuating linkage is provided for use in an aircraft engine having a double door-type particle separator, anti-icing system installed within its air intake ducts. The actuating linkage interconnects the deflecting vane and the bypass door through a coupler link. The deflecting vane is pivotally connected to a linear link which is connected to an actuator link about a pivot point. Movement of the actuator link varies the relative positions of the deflecting vane and the bypass door between ram mode and anti-icing mode positions. The actuating linkage p...
An anti-icing system for use in an aircraft engine of the type including an air intake duct extending generally longitudinally of the engine and including a top wall, a bottom wall and side walls, said duct having a forward facing open inlet at one end, a side opening in the top wall disposed intermediate the length of the duct, and a discharge outlet at the other end, a deflecting vane rotatably and translatably mounted at one end to the top wall of the intake duct at a point intermediate the forward facing inlet and the side opening, and a bypass door ...