发明名称 |
AIRCRAFT STRUCTURE FOR HIGH CAPACITY PULL OFF |
摘要 |
An apparatus comprising a composite elongate member, a channel, and a number of composite structures. The composite elongate member has a side configured for attachment to a surface of a structure. The channel is on the side and extends along a length of the composite elongate member. The number of composite structures is configured for placement in the channel and configured to attach a portion of the side of the composite elongate member to the structure. A composite structure in the number of composite structures comprises layers having different orientations selected to increase a capacity of the composite elongate member to withstand forces that pull the composite elongate member away from the structure. |
申请公布号 |
EP2709830(A1) |
申请公布日期 |
2014.03.26 |
申请号 |
EP20120717011 |
申请日期 |
2012.04.19 |
申请人 |
THE BOEING COMPANY |
发明人 |
KAMARAJ, MALMURUGAN;MATHESON, DONALD PAUL |
分类号 |
B29C70/34;B29L31/00;B29L31/30 |
主分类号 |
B29C70/34 |
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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