- Patent Title: Turbojet engine comprising a nacelle equipped with reverser flaps
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Application No.: US16017634Application Date: 2018-06-25
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Publication No.: US10550796B2Publication Date: 2020-02-04
- Inventor: Olivier Pautis , Laurent Tizac , Frédéric Ridray , Lionel Czapla , Frédéric Piard
- 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: FR1756037 20170629
- Main IPC: F02K1/72
- IPC: F02K1/72 ; F02K1/76 ; F02K3/06

Abstract:
A turbofan comprising a fan casing and a nacelle comprising a cowl translatable between an advanced position and a pushed-back position in which the mobile cowl and the fan casing define a window therebetween. The nacelle also comprises reverser flaps, each reverser flap being mounted in a linked manner on the mobile assembly between a closed position in which it obstructs the window and an open position in which it does not obstruct the window. The nacelle also has an impelling mechanism comprising a lever arm rotatable on the mobile assembly and having a roller, a connecting rod mounted rotatably between the reverser flap and the lever arm, and a channel receiving the roller, the channel having a front part parallel with the translation direction and a rear part extending after the front part and oriented inward as it progresses from the front toward the rear.
Public/Granted literature
- US20190003421A1 TURBOJET ENGINE COMPRISING A NACELLE EQUIPPED WITH REVERSER FLAPS Public/Granted day:2019-01-03
Information query
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