公开(公告)号：US10443542B2

公开(公告)日：2019-10-15

申请号：US15283591

申请日：2016-10-03

Applicant: AIRCELLE

Inventor： Corentin Hue ,  Rodolphe Denis ,  Denis Guillois ,  Sarah Tissot

IPC: F02K1/72 ,  F02K1/76 ,  F02K1/60 ,  F02K1/70 ,  F02K1/62

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.

公开(公告)号：US10190538B2

公开(公告)日：2019-01-29

申请号：US14841407

申请日：2015-08-31

Applicant: AIRCELLE

Inventor： Patrick Boileau ,  Peter Segat ,  Pierre Caruel ,  Sarah Tissot

IPC: F02K1/72 ,  F02K1/09 ,  F02K1/82

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.