|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/110B ; 239/265.23 ; 602/262|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 28 인용 특허 : 6|
An improved pivoting door thrust reverser system for a turbofan aircraft jet engine having a non-translatable housing and at least one thrust reverser door being pivotable between a stowed forward thrust position and a deployed reverse thrust position. The thrust reverser door is pivotable about a first axis and a kicker plate is hinged to the door at a second axis. As the door is deployed by an actuator a spring loaded roller clamp means keeps the kicker plate clamped to the actuator body until a portion of the kicker plate positively engages the thrust...
[ What is claimed is:] [1.]1. A thrust reverser for a turbofan aircraft jet engine having a non-translatable housing extending around a longitudinal axis of the cowl of the core jet engine with an exterior surface, an interior surface defining an outer boundary of a cold air flow duct and defining a lateral opening, the thrust reverser comprising:at least one thrust reversing door pivotally attached to the housing so as to be movable between a first, forward thrust position wherein an outer surface of the door is substantially flush with the exterior sur...