Invention Grant
US08746621B2 Connector for stiffening frames between an aircraft fuselage and a wing box
有权
用于在飞机机身和翼盒之间加固框架的连接器
- Patent Title: Connector for stiffening frames between an aircraft fuselage and a wing box
- Patent Title (中): 用于在飞机机身和翼盒之间加固框架的连接器
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Application No.: US13348110Application Date: 2012-01-11
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Publication No.: US08746621B2Publication Date: 2014-06-10
- Inventor: Jean Pierre Cabanac , Jerome Colmagro , Jean Marc Durand , Ludovic Fournie , Julien Guillemaut , Francois Loyant
- Applicant: Jean Pierre Cabanac , Jerome Colmagro , Jean Marc Durand , Ludovic Fournie , Julien Guillemaut , Francois Loyant
- Applicant Address: FR Toulouse
- Assignee: AIRBUS Operations S.A.S.
- Current Assignee: AIRBUS Operations S.A.S.
- Current Assignee Address: FR Toulouse
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1150678 20110128
- Main IPC: B64C1/06
- IPC: B64C1/06
Abstract:
The stiffening frames (14) of an aircraft fuselage (2) remain continuous while passing through an upper panel (5) of the wing box and extend over the ribs (3) situated in that box. The overall mechanical strength of the assembly is improved, despite the notches it is necessary to make in the panel (5).
Public/Granted literature
- US20120193475A1 CONNECTOR FOR STIFFENING FRAMES BETWEEN AN AIRCRAFT FUSELAGE AND A WING BOX Public/Granted day:2012-08-02
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