发明名称 COMPOSITE AIRCRAFT FLOOR SYSTEM
摘要 <p>An aircraft floor system includes a composite panel which generally includes an inboard layer, an inboard interlock layer, a core layer, an outboard interlock layer and an outboard layer. The advanced sandwich core material may include K-Cor or X-Cor which is pinned through at least one ply of dry composite reinforcement to provide a mechanical lock between the pins and an inboard and outboard interlock layer. Bonding of the locked-in ply with the inboard and outboard results in improved structural performance and damage tolerance.</p>
申请公布号 WO2008020881(A2) 申请公布日期 2008.02.21
申请号 WO2007US02730 申请日期 2007.01.31
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 CARSTENSEN, THOMAS, A.;COURNOYER, DAVID, M.;URSENBACH, DAN, O.
分类号 E04B1/00 主分类号 E04B1/00
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