公开(公告)号：US20140301837A1

公开(公告)日：2014-10-09

申请号：US14310184

申请日：2014-06-20

Applicant: AIRCELLE

Inventor： Nicolas DEZEUSTRE ,  Xavier HERT ,  Luc QUERNET

IPC: F02K1/56

CPC classification number: F02K1/566 ,  F02K1/60 ,  F02K1/605 ,  F02K1/62 ,  F02K1/70 ,  F02K1/763 ,  F05D2260/50 ,  F05D2260/52 ,  Y02T50/671

Abstract: A door for a door-type thrust reverser is pivotally mounted on a stationary structure of a thrust reverser. The door includes an inner surface integrated to a flow path of an air flow generated by a turbojet engine, an outer surface providing an outer aerodynamic continuity of a nacelle equipped with the thrust reverser, a spoiler to deflect the air flow disposed at an upstream end of the door, and an actuator actuating the spoiler. The spoiler is movably mounted, in rotation around a rotation axis substantially perpendicular to a front frame of the door, between a retracted and a deployed position. In particular, the actuator includes a first rod connected to the spoiler, a second rod connected to the first rod and the front frame, and a third rod connected to the first and second rods as well as to the spoiler.

Abstract translation: 门式推力反向器的门枢转地安装在推力反向器的固定结构上。 门包括与涡轮喷气发动机产生的空气流的流动路径相整合的内表面，提供装备有推力反向器的机舱的外部空气动力学连续性的外表面，用于使设置在上游端的气流偏转的扰流板 的门，以及致动扰流板的致动器。 扰流器围绕基本上垂直于门的前框架的旋转轴线在缩回和展开位置之间可旋转地安装。 特别地，致动器包括连接到扰流板的第一杆，连接到第一杆和前框架的第二杆以及连接到第一杆和第二杆以及扰流器的第三杆。