发明名称 Method for the orbital assembly of aircraft sections made of composite material
摘要 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.
申请公布号 US8484848(B2) 申请公布日期 2013.07.16
申请号 US20090995535 申请日期 2009.05.26
申请人 GALLANT GUILLAUME;LACOMBE JEAN-CLAUDE;AIRBUS OPERATIONS S.A.S. 发明人 GALLANT GUILLAUME;LACOMBE JEAN-CLAUDE
分类号 B21D53/88 主分类号 B21D53/88
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