公开(公告)号：US20170022935A1

公开(公告)日：2017-01-26

申请号：US15283591

申请日：2016-10-03

Applicant: AIRCELLE

Inventor： HUE Corentin ,  Rodolphe DENIS ,  Denis GUILLOIS ,  Sarah TISSOT

IPC: F02K1/76 ,  F02K1/62

CPC classification number: F02K1/766 ,  F02K1/60 ,  F02K1/62 ,  F02K1/70 ,  F02K1/763 ,  F05D2220/323 ,  F05D2260/52

Abstract: The present disclosure relates to a system for locking the position of the flaps of a thrust reverser of a turbojet nacelle, said flaps being controlled by actuators, each one swinging about a tranverse pivot in order to partially close off the air stream so as to guide it forwards, further including locks for locking the flaps in an intermediate opening position, between the closed position and the open position.

Abstract translation: 本公开涉及一种用于锁定涡轮喷气发动机舱的推力反向器的翼片的位置的系统，所述翼片由致动器控制，每个翼片围绕横向枢轴摆动以部分地关闭空气流，以便引导 其进一步包括用于将襟翼锁定在中间打开位置中的锁定件，在关闭位置和打开位置之间。

公开(公告)号：US20130056554A1

公开(公告)日：2013-03-07

申请号：US13662926

申请日：2012-10-29

Applicant: AIRCELLE

Inventor： Denis GUILLOIS ,  Laurent Albert BLIN ,  Löic CHAPELAIN

IPC: B63H11/10

CPC classification number: F02K1/60 ,  B64D33/04 ,  F02K1/70 ,  F02K1/763 ,  Y02T50/671

Abstract: A thrust reverser with doors having at least one stationary structure is provided, on which at least one door is mounted pivoting between a closed position in which the door closes the reverser and makes up an outer cowling part, and an open position in which the door opens a passage in the stationary structure and can at least partially block a flow of air generated by a turbojet engine so as to reorient the door. The stationary structure includes at least two sets of cascade vanes that can be covered by the door when in the closed position.

Abstract translation: 提供具有至少一个固定结构的门的推力反向器，其上安装有至少一个门，枢转在关闭位置之间，门关闭反向器并构成外整流罩部分，以及打开位置，其中门 打开固定结构中的通道并且可以至少部分地阻挡由涡轮喷气发动机产生的空气流，以便重新定向门。 固定结构包括至少两组级联叶片，当组合叶片处于关闭位置时可以被门覆盖。