Invention Grant
- Patent Title: Turbojet engine nacelle comprising a thrust reverser drive mechanism
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Application No.: US15889778Application Date: 2018-02-06
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Publication No.: US10753314B2Publication Date: 2020-08-25
- Inventor: Eric Haramburu , Patrick Oberle , Eric Masson
- Applicant: Airbus Operations (S.A.S.) , Airbus (S.A.S.)
- Applicant Address: FR Toulouse FR Blagnac
- Assignee: Airbus Operations (S.A.S.),Airbus (S.A.S.)
- Current Assignee: Airbus Operations (S.A.S.),Airbus (S.A.S.)
- Current Assignee Address: FR Toulouse FR Blagnac
- Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@45966823
- Main IPC: F02K1/70
- IPC: F02K1/70 ; F02K1/72 ; B64D29/06 ; B64D27/18

Abstract:
A nacelle includes a fixed structure supporting a fixed cowl and a movable cowl, the movable cowl being movable translationally between a closing position and an opening position. A blocker door is movably mounted rotationally on the nacelle between a closed position and an open position. The nacelle includes a drive mechanism of the blocker door and of the movable cowl between the closed/closing position and the open/opening position of the blocker door/movable cowl, respectively, and vice versa, the drive mechanism includes at least one actuator fixed, to the fixed structure of the nacelle and, to a fitting fixed to the movable cowl. The drive mechanism includes, for each actuator, a flexible member having a first end fixed to the fixed structure of the nacelle and a second end fixed to the fitting.
Public/Granted literature
- US20180230939A1 TURBOJET ENGINE NACELLE COMPRISING A THRUST REVERSER DRIVE MECHANISM Public/Granted day:2018-08-16
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