公开(公告)号：US20210301762A1

公开(公告)日：2021-09-30

申请号：US17209323

申请日：2021-03-23

Applicant: Airbus Operations SAS

Inventor： Fabien MENOU ,  Stéphanie FESQUET

IPC: F02K1/72 ,  F02K1/76

Abstract: A bypass turbofan engine comprising a nacelle surrounding a flow path for a secondary flow and comprising a fixed structure, a mobile assembly with a slide capable of translational movement on the fixed structure and bearing a mobile cowl and a frame capable of translational movement on the fixed structure and bearing deflectors. The mobile assembly is able to move between a forward position and a retreated position making it possible to open a passage between the flow path and the outside through the deflectors. A differentiation mechanism ensures a length of travel of the slide that is different from the length of travel of the frame, and actuators providing a translational travel of the slide. Fitting a differentiation mechanism means that the length of travel of the deflectors with respect to the length of travel of the mobile cowl can be regulated.