发明名称 INTERNALLY STIFFENED COMPOSITE PANELS AND METHODS FOR THEIR MANUFACTURE
摘要 Internally stiffened composite panels and associated manufacturing methods. In one embodiment, an internally stiffened composite panel includes a first face sheet, a second face sheet offset from the first face sheet, and at least one core portion sandwiched between the first and second face sheets. In one aspect of this embodiment, the composite panel further includes a stiffener disposed between the first and second face sheets adjacent to the core portion. The stiffener can have a first attachment portion attached to the first face sheet, a second attachment portion attached to the second face sheet, and an intermediate portion extending between the first and second attachment portions. In another aspect of this embodiment, one or both of the first and second attachment portions is configured to engage a fastener, such as a blind fastener, for attaching a part to the composite panel.
申请公布号 US2010252681(A1) 申请公布日期 2010.10.07
申请号 US20070626766 申请日期 2007.01.24
申请人 THE BOEING COMPANY 发明人 GRILLOS EMMANUEL J.
分类号 B64C1/00;B21D53/88;B64C1/12;B64C3/20;E04C2/36 主分类号 B64C1/00
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