公开(公告)号：US20160273489A1

公开(公告)日：2016-09-22

申请号：US14643555

申请日：2015-03-10

Applicant: AIRCELLE

Inventor： Serge BUNEL ,  Alexandre Bellanger

IPC: F02K1/72 ,  B64D27/18

Abstract: The present disclosure relates to a thrust reverser device for a turbo jet engine nacelle including a fixed thrust reverser support structure having a longitudinal support half beam able to support a thrust reverser half-cowl, and the thrust reverser half-cowl mounted such that it can slide on the fixed structure in a direction substantially parallel to a longitudinal axis of the device via a guidance assembly, between a direct-jet position and a reverse-thrust position. In particular, the fixed structure includes a structure for offsetting the guidance assembly that guides the half-cowl circumferentially in a plane radial to the longitudinal axis between its various positions with respect to the half-beam on which the half-cowl is mounted.

Abstract translation: 本发明涉及一种用于涡轮喷气发动机机舱的推力反向器装置，其包括具有能够支撑推力反向器半罩的纵向支撑半梁的固定推力反向器支撑结构，并且安装推力反向器半罩，使得其可以 在直接喷射位置和反向推力位置之间经由引导组件在基本上平行于装置的纵向轴线的方向上在固定结构上滑动。 特别地，固定结构包括用于抵消引导组件的结构，该引导组件相对于安装有半罩的半光束在其各个位置之间的纵向轴线的径向周向上引导半罩。