公开(公告)号：US20180372025A1

公开(公告)日：2018-12-27

申请号：US16007761

申请日：2018-06-13

Applicant: Airbus Operations (S.A.S.)

Inventor： Frédéric Ridray ,  Lionel Czapla ,  Frédéric Piard

IPC: F02K1/72 ,  B64D29/06 ,  B64D33/04 ,  F02K1/76

Abstract: A jet engine including a motor with a fan casing and a nacelle which includes a mobile cowl and a main slider that is mobile in translation between an advanced position and a retracted position in which the mobile cowl and the fan casing define, between them, a window. The nacelle also includes reverser flaps and exterior flaps, each one being mounted articulated on the main slider between a stowed position in which it obstructs the window and a deployed position in which it does not obstruct the window, a secondary slider that is mobile in translation on the main slider between a first position and a second position, a transmission system making each reverser flap and exterior flap pass from the stowed position to the deployed position when the secondary slider passes from the first position to the second position, and a set of actuators that bring about a movement in translation of the main slider and of the secondary slider.