Invention Grant
US08484848B2 Method for the orbital assembly of aircraft sections made of composite material
有权
用复合材料制成的飞机部件的轨道组装方法
- Patent Title: Method for the orbital assembly of aircraft sections made of composite material
- Patent Title (中): 用复合材料制成的飞机部件的轨道组装方法
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Application No.: US12995535Application Date: 2009-05-26
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Publication No.: US08484848B2Publication Date: 2013-07-16
- Inventor: Guillaume Gallant , Jean-Claude Lacombe
- Applicant: Guillaume Gallant , Jean-Claude Lacombe
- 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: FR0803009 20080602
- International Application: PCT/FR2009/050972 WO 20090526
- International Announcement: WO2009/156637 WO 20091230
- Main IPC: B21D53/88
- IPC: B21D53/88

Abstract:
A method for assembling two structural elements, at least one of the two structural elements being tube-shaped and including a skin made of a fiber-reinforced composite material. The ability of the element to adapt to the shape and perimeter of a junction interface is improved by providing longitudinal grooves distributed on the circumference of the junction interface. The grooves are of a sufficient length to provide the junction interface with the flexibility to accommodate, through relative radial movement of each portion located between two grooves, differences in shape and perimeter among the junction interfaces of the two structural elements.
Public/Granted literature
- US20110185555A1 METHOD FOR THE ORBITAL ASSEMBLY OF AIRCRAFT SECTIONS MADE OF COMPOSITE MATERIAL Public/Granted day:2011-08-04
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