Invention Grant
- Patent Title: Integrated ribs for central wing box
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Application No.: US15255639Application Date: 2016-09-02
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Publication No.: US10399663B2Publication Date: 2019-09-03
- Inventor: Denis Soula , Matthieu Plet , Javier Maqueda Lahoz
- 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: FR1558205 20150904
- Main IPC: B64C3/18
- IPC: B64C3/18 ; B64C1/06 ; B64C1/26 ; B64C3/22

Abstract:
A central wing box for an aircraft, including a top panel, a bottom panel, a front spar, a rear spar, and at least one secondary rib. A secondary rib includes two stiffeners, a first stiffener extending adjacent to the top panel and to one of the front spar and the rear spar, and a second stiffener extending adjacent to the bottom panel and to the other of the front spar and the rear spar. A reduced number of components can be employed, thereby simplifying the construction of the central wing box of an aircraft, particularly the installation of the secondary ribs.
Public/Granted literature
- US20170066520A1 INTEGRATED RIBS FOR CENTRAL WING BOX Public/Granted day:2017-03-09
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