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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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