发明名称 Composite panel adapted for point compressive loads and method for making same
摘要 A method for making a composite panel includes the step (26) of providing a panel having elongated channels (14) that are positioned along areas of anticipated point compression loading. The panel (10) has a reinforcing fabric layer (41) attached to a non-woven fabric layer (43) forming an outside layer (12). The composite panel has foam core (8,9) within the outside layer. The method further comprises the step (27) of providing structural foam channel inserts (16) having an outer fabric layer (18), wherein the channel inserts have a cross section which matches the cross-sectional profile of each of the elongated channels of the panel. Resin is then applied to the outside layer of the panel and outer fabric layer of the channel inserts such the channel inserts are positioned within the channels of the panel (29 and 31). The resin is then allowed to cure (33) forming a composite structure.
申请公布号 US6755998(B1) 申请公布日期 2004.06.29
申请号 US20000697465 申请日期 2000.10.26
申请人 COMPSYS, INC. 发明人 REICHARD RONNAL P.;LEWIT SCOTT M.;MACKANESS MILES P.;ROHAN NEIL A.
分类号 B29C44/12;B32B5/18;B32B5/26;(IPC1-7):B29C44/06 主分类号 B29C44/12
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