公开(公告)号：US09816462B2

公开(公告)日：2017-11-14

申请号：US15017931

申请日：2016-02-08

Applicant: AIRCELLE

Inventor： Philipe Guerin ,  Olivier Kerbler ,  Jean-Paul Rami

IPC: F02K1/76 ,  F02K1/72 ,  F02K1/62 ,  F02K1/70 ,  F02K1/09 ,  F02K3/06

CPC classification number: F02K1/72 ,  F02K1/09 ,  F02K1/62 ,  F02K1/625 ,  F02K1/70 ,  F02K1/76 ,  F02K1/763 ,  F02K1/766 ,  F02K3/06

Abstract: The present disclosure provides a thrust reverser device that is integrated in an aircraft nacelle. Blocking flaps are stored inside a mobile cowl disposed in a downstream section of the nacelle, under deflection cascade assemblies during direct-jet operation of the nacelle. Various devices are provided for executing the passage from direct-jet operation to reverse-jet operation in two stages: the mobile cowl moves in translation towards the downstream end of the nacelle; and each flap is then deployed in the main air flow path.