发明名称 ENVIRONMENTALLY STABLE HYBRID FABRIC SYSTEM FOR EXTERIOR PROTECTION OF AN AIRCRAFT
摘要 A method of forming an exterior surface protective structure (12) includes uniting a loaded surfacer (52) having a carrier (51) to a hybrid prepreg substrate (32). The prepreg substrate (32) includes a carbon fabric (44) with an integral conductive component (48) having conductivity with in a metal conductivity range and is united to a base substrate (30). The loaded surfacer (52) and the prepreg substrate (32) are cured, which includes interfacially adhering matter between the loaded surfacer (52) and the prepreg substrate (32). A protective fabric system (12) for an exterior (14) of a structure includes the base substrate (30). The hybrid prepreg substrate (32) is coupled to the base substrate (30). The loaded surfacer (52) with the carrier (51) is interfacially adhered to the prepreg substrate (32).
申请公布号 EP1940610(B1) 申请公布日期 2016.05.18
申请号 EP20060850532 申请日期 2006.10.24
申请人 THE BOEING COMPANY 发明人 BROWN, ARLENE, M.
分类号 B29C70/08;B29C70/22;B29C70/78;B29C70/88;B29K707/04;B29L31/30;B32B5/26;B32B15/02;B32B15/08;B32B27/04;B32B27/12;B32B27/38 主分类号 B29C70/08
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