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
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