发明名称 COMPOSITE STRUCTURE AND METHOD OF MANUFACTURE
摘要 A method of manufacture of a structural member comprising, providing a number of internal elements (16,18,20), each having an aperture formed therein, sequentially assembling the internal elements onto a longitudinal element (14) such that the longitudinal element passes through the aperture of each internal element, and wrapping an outer skin around the assembled internal elements and longitudinal element. A structural member is thus produced having a number of internal elements, each internal element having a longitudinal axis aligned with the longitudinal axis of the remaining internal elements, and having a continuous outer skin formed over the internal elements.
申请公布号 WO2008009988(A3) 申请公布日期 2009.01.22
申请号 WO2007GB50401 申请日期 2007.07.13
申请人 AIRBUS UK LIMITED;YATES, JOHN;INSTON, DAVID, GRAHAM 发明人 YATES, JOHN;INSTON, DAVID, GRAHAM
分类号 B64C3/18;B29C53/82;B29C70/32;B29C70/86;B64C9/16;B64C9/22 主分类号 B64C3/18
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