Invention Grant
- Patent Title: Supporting set for a wing flap system of an aircraft
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Application No.: US14661144Application Date: 2015-03-18
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Publication No.: US09637220B2Publication Date: 2017-05-02
- Inventor: Sébastien De Conto , Fabrice Rival , Romain Bernes , Frédéric Coll
- Applicant: Airbus Operations (S.A.S.)
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations (S.A.S.)
- Current Assignee: Airbus Operations (S.A.S.)
- Current Assignee Address: FR Toulouse
- Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
- Priority: FR1452376 20140321
- Main IPC: B64C9/16
- IPC: B64C9/16 ; B64C9/02

Abstract:
The support assembly comprises a fixing system which comprises a first connection rod which is connected via a first end to a support component and which is configured to generate a primary force path and a second connection rod which is connected via a first end to the support component and which is configured to generate a secondary force path, the fixing system further comprising a beam which is fixed to a structural component, the second end of the first connection rod and the second end of the second connection rod being connected to the beam, which is arranged so that the directions of the first and second connection rods are oriented in accordance with a plane substantially orthogonal to the plane of the support component.
Public/Granted literature
- US20150266562A1 SUPPORTING SET FOR A WING FLAP SYSTEM OF AN AIRCRAFT Public/Granted day:2015-09-24
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