发明名称 HONEYCOMB SPLICED MULTILAYER FOAM CORE AIRCRAFT COMPOSITE PARTS AND METHOD FOR MAKING SAME
摘要 <p>Aircraft composite components having foam cores comprising at least two foam sheets joined with a sheet of honeycomb to form a foam-honeycomb-foam sandwich. The layers of sheet foam are in contact with each other and the honeycomb cells extend a substantially equal depth into and generally perpendicular to the sheet foam layers. The composite component has increased shear strength. The aircraft composite component can be made by aligning a layer of honeycomb between and generally perpendicular to two layers of sheet foam. A compressive force is applied generally perpendicular to at least one layer of sheet foam so that the honeycomb cells penetrate each of the two layers of sheet foam to a substantially equal depth so that the layers of foam contact each other to form a foam-honeycomb-foam sandwich. The foam core is surrounded by resin impregnated fibers and cured.</p>
申请公布号 GB2189447(B) 申请公布日期 1989.12.13
申请号 GB19870007806 申请日期 1987.04.01
申请人 * UNITED TECHNOLOGIES CORPORATION 发明人 BRUCE F * KAY
分类号 B29C44/12;B29C44/18;B32B3/12;B64C3/20;B64C27/473;E04C2/20 主分类号 B29C44/12
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