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. Ribs are formed on a smooth hard base tool. Expansion blocks are placed in the shallow cavities formed by the ribs and the base tool, and held in place by a synthetic elastomer-based adhesive while a skin is placed over the ribs, expansion blocks, and base tool. The assembly is then placed in a vacuum bag and autoclave cured. After cooling, the expansion blocks are removed and the formed structure is removed from the hard base tool. This abstract is provided to comply with the rules requiring an abstract, and is intended to allow a searcher or other reader to quickly ascertain the subject matter of the technical disclosure. It is submitted with the understanding that it will not be used to interpret or limit the scope or meaning of the claims.
申请公布号 US7479201(B1) 申请公布日期 2009.01.20
申请号 US20050239453 申请日期 2005.09.27
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 WEGNER PETER M.;GANLEY JEFFREY M.;JOHNSON BRICE A.;VAN WEST BARRY P.
分类号 B29D99/00;B27N3/10;B28B7/22;B29C45/14;B29C53/58;B29C53/80;B29C69/00;B29C70/86;B29D22/00;B32B27/00;B65C3/26;B65H81/00 主分类号 B29D99/00
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