发明名称 INTEGRATED AIRCRAFT STRUCTURAL FLOOR
摘要 <p>A number of integrated floor structures made of lightweight composite materials for use in an aircraft are disclosed. Generally, each of such floors includes a top-layer skin, a bottom-layer skin disposed below the top-layer skin and a first structural core disposed between the top-layer skin and the bottom-layer skin, the first structural core being composed of a honeycomb composite material. One or more denser structural cores can also be incorporated at strategic locations.</p>
申请公布号 EP1871662(A1) 申请公布日期 2008.01.02
申请号 EP20060738754 申请日期 2006.03.16
申请人 THE BOEING COMPANY 发明人 WESTRE, WILLARD, N.;EVANS, DAVID, W.
分类号 B64C1/18;B61D17/04;B62D25/20;B64D11/06 主分类号 B64C1/18
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