Invention Grant
- Patent Title: Nacelle of a turbojet engine comprising an outer thrust-reversing door
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Application No.: US16253035Application Date: 2019-01-21
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Publication No.: US10941729B2Publication Date: 2021-03-09
- Inventor: Patrick Oberle
- Applicant: Airbus SAS
- Applicant Address: FR Blagnac
- Assignee: Airbus SAS
- Current Assignee: Airbus SAS
- Current Assignee Address: FR Blagnac
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR1850928 20180205
- Main IPC: F02K1/76
- IPC: F02K1/76 ; F02K1/70 ; F02K1/72 ; B64D29/06 ; F02K1/56 ; F02K1/60

Abstract:
A nacelle for a dual-flow turbojet engine comprises a structure, a fixed cowl, a cowl translationally mobile on the structure, a window open between a secondary jet and the outside of the nacelle, and delimited by the fixed and mobile cowls, an outer thrust-reversing door rotationally mobile and a driving mechanism. The driving mechanism comprises a single power cylinder arranged at the level of a median plane and having a first end mounted articulated on the structure, a shaft with the second end of the power cylinder mounted articulated on the shaft, a first yoke joint secured to the outer thrust-reversing door and free to rotate on the shaft, and a second yoke joint secured to the mobile cowl, and where each of the two flanks of the second yoke joint has a groove in each of which the shaft is mounted to slide parallel to the median plane.
Public/Granted literature
- US20190242329A1 NACELLE OF A TURBOJET ENGINE COMPRISING AN OUTER THRUST-REVERSING DOOR Public/Granted day:2019-08-08
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