发明名称 Method for fabricating rib-stiffened composite structures
摘要 A method for fabricating a grid-stiffened structure from fiber-reinforced composite materials. A skin is applied to a smooth, hard base tool. Ribs comprised of carbon-fiber tows are formed on the skin, and shallow cavities are formed between the ribs and the skin. An expansion block is placed in each of the cavities, and is held in place by an elastomeric contact adhesive having adhesive properties that are substantially diminished when the adhesive is heated to an elevated curing temperature. The assembly is then autoclave cured. After cooling, the formed structure is separated from the base tool and the expansion blocks are removed from the cavities. A grid-stiffened sandwich structure is formed by applying an outer skin over the ribs and expansion blocks, before curing the assembly. After cooling, the outer skin is removed to allow extraction of the blocks, and subsequently bonded to the ribs.
申请公布号 US8435375(B1) 申请公布日期 2013.05.07
申请号 US201213559559 申请日期 2012.07.26
申请人 WEGNER PETER M.;GANLEY JEFFREY M.;JOHNSON BRICE A.;VAN WEST BARRY P.;THE UNITED STATES AS REPRESENTED BY THE SECRETARYOF THE AIRFORCE 发明人 WEGNER PETER M.;GANLEY JEFFREY M.;JOHNSON BRICE A.;VAN WEST BARRY P.
分类号 B29C53/80;B29D99/00;B27N3/10;B28B7/22;B29C45/14;B29C53/58;B29C69/00;B29C70/86;B29D22/00;B32B27/00;B32B37/24;B65H81/00 主分类号 B29C53/80
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