Invention Grant
- Patent Title: Nacelle of a turbojet comprising a reverser flap and a deployment system with delay
-
Application No.: US16714986Application Date: 2019-12-16
-
Publication No.: US11215142B2Publication Date: 2022-01-04
- Inventor: Olivier Pautis
- Applicant: Airbus Operations SAS
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR1873541 20181220
- Main IPC: F02K1/72
- IPC: F02K1/72 ; F02K1/08 ; F02K1/76

Abstract:
A bypass turbojet nacelle comprising a fixed structure, a fixed cowl and a cowl movable in translation between advanced and withdrawn positions by a ram with a reverser flap movable thereon, and a deployment system comprising a first slider integral with the movable cowl, a first groove comprising a first part and a curved, second part integral with the fixed structure, a second slider movable in translation in the second groove part, a first connecting rod rotatable on the first slider and on the second slider, and a second connecting rod articulated on both the first connecting rod first end and the reverser flap. The ram rod is articulated on the first connecting rod. Moving the first slider from the advanced to the withdrawn position moves the second slider along the first part and, when the first slider reaches the withdrawn position, the second slider moves along the second part.
Public/Granted literature
- US20200240360A1 NACELLE OF A TURBOJET COMPRISING A REVERSER FLAP AND A DEPLOYMENT SYSTEM WITH DELAY Public/Granted day:2020-07-30
Information query
IPC分类: