发明名称 |
AIRCRAFT STRUCTURE FOR HIGH CAPACITY PULL OFF |
摘要 |
A method and product comprising a composite elongate member (402), a channel (428), and a number of composite structures (431). The composite elongate member (402) has a side configured for attachment to a structure. The channel (428) is on the side of the composite elongate member (402) and extends along a length of the composite elongate member (402). The number of composite structures (431) is configured for placement in the channel (428) and to attach a portion of the side of the composite elongate member (402) to the structure (404). The number of composite structures (431) is configured to increase a capacity of the composite elongate member (402) to withstand forces that pull the composite elongate member (402) away from the structure (404). |
申请公布号 |
WO2012158301(A1) |
申请公布日期 |
2012.11.22 |
申请号 |
WO2012US34257 |
申请日期 |
2012.04.19 |
申请人 |
THE BOEING COMPANY;KAMARAJ, MALMURUGAN;MATHESON, DONALD PAUL |
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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