公开(公告)号：US20160222917A1

公开(公告)日：2016-08-04

申请号：US15093805

申请日：2016-04-08

Applicant: AIRCELLE

Inventor： Peter SEGAT ,  Sarah TISSOT ,  Xavier BOUTEILLER

IPC: F02K1/76 ,  B64D33/04 ,  F02K1/72

CPC classification number: F02K1/763 ,  B64D33/04 ,  F02K1/09 ,  F02K1/1261 ,  F02K1/72 ,  F02K1/766 ,  F05D2220/323 ,  F05D2240/128 ,  F05D2240/129

Abstract: The present disclosure concerns a nacelle for an aircraft engine, which includes a thrust reverser cowling that is slidably mounted between a direct jet position, and a reversed jet position in which the cowling opens a passage in the nacelle and uncovers a deflection device, and at least one actuator for moving the cowling. The nozzle section of the cowling delimits at least one opening that is combined with a leakage door, the leakage door being movably mounted on the cowling between a closed position in which the door engages with the associated opening to counteract the flow of air through said opening, and an open escape position in which the door is retracted to allow a portion of the air flow to flow through said opening.

Abstract translation: 本公开涉及一种用于飞行器发动机的机舱，其包括可滑动地安装在直接喷射位置和反向喷射位置之间的推力反向器整流罩，在该反向喷射位置中，整流罩打开机舱中的通道并露出偏转装置，并且在 至少一个用于移动整流罩的致动器。 整流罩的喷嘴部分限定了与泄漏门组合的至少一个开口，泄漏门​​可移动地安装在整流罩上，在关闭位置之间，门与相关联的开口啮合以抵消空气流过所述开口 以及敞开的逃逸位置，其中门缩回以允许空气流的一部分流过所述开口。

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：US20160025039A1

公开(公告)日：2016-01-28

申请号：US14841407

申请日：2015-08-31

Applicant: AIRCELLE

Inventor： Patrick BOILEAU ,  Peter SEGAT ,  Pierre CARUEL ,  Sarah TISSOT

IPC: F02K1/72 ,  F02K1/82

CPC classification number: F02K1/72 ,  F02K1/09 ,  F02K1/827 ,  F05D2240/129 ,  F05D2240/90 ,  F05D2250/34

Abstract: A thrust reverser device for an aircraft turbojet engine includes: a movable cowl, translating cascades connected to the movable cowl, a mast; and a front suspension to suspend the turbojet engine. The cascades translates between a direct jet position where the cascades are retracted in a fan casing, and an indirect jet position where the cascades are brought out of the fan casing. In particular, the cascades have a sliding connection with the mast by means of at least one spacer connected to the mast downstream of the front suspension.

Abstract translation: 一种用于飞机涡轮喷气发动机的推力反向装置，包括：可移动整流罩，平移与可移动整流罩连接的级联，桅杆; 以及悬挂涡轮喷气发动机的前悬架。 级联在级联收缩在风扇壳体中的直接喷射位置和级联从风扇壳体离开的间接射流位置之间转换。 特别地，级联通过至少一个连接到前悬架下游的桅杆的间隔件与桅杆滑动连接。