发明名称 Honeycomb spliced multilayer foam core aircraft composite parts and method for making same
摘要 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.
申请公布号 US4687691(A) 申请公布日期 1987.08.18
申请号 US19860856896 申请日期 1986.04.28
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 KAY, BRUCE F.
分类号 B29C44/12;B29C44/18;B32B3/12;B64C3/20;B64C27/473;E04C2/20;(IPC1-7):B32B3/26;B32B31/20 主分类号 B29C44/12
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