Invention Application
- Patent Title: JET ENGINE NACELLE HAVING A REVERSER FLAP
-
Application No.: US15883260Application Date: 2018-01-30
-
Publication No.: US20180216574A1Publication Date: 2018-08-02
- Inventor: Eric HARAMBURU , Patrick OBERLE , Nicolas JOLIVET
- Applicant: Airbus Operations SAS , Airbus SAS
- Priority: FR1750798 20170131
- Main IPC: F02K1/76
- IPC: F02K1/76 ; F02K1/72

Abstract:
A nacelle comprising a fixed cowl and a movable cowl movable in translation, a window delimited by the fixed cowl and the movable cowl, a reverser flap movable in rotation and a drive mechanism coordinating the movements of the reverser flap with those of the movable cowl. The drive mechanism comprises two bearings fixed to the nacelle, for each bearing, a lever arm with one end movable in rotation on the bearing and one end articulated on the reverser flap, for each lever arm, a rail comprising a straight portion and a curved portion, for each lever arm, a rod with one end articulated on the lever arm, and for each rail, a slider that is movable in translation on the rail and is articulated to one end of the rod.
Information query