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
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