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发明授权
US07402269B2 Environmentally stable hybrid fabric system for exterior protection of an aircraft 有权
用于飞机外部保护的环境稳定的混合织物系统

Environmentally stable hybrid fabric system for exterior protection of an aircraft
摘要：
A method of forming an exterior surface protective structure (12) for an aircraft (10) 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 an aircraft (10) 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).
摘要（中）：

形成用于飞行器（10）的外表面保护结构（12）的方法包括将具有载体（51）的已加载的二次表面（52）结合到混合预浸料基板（32）上。 预浸料衬底（32）包括具有金属导电率范围内具有导电性并且与基底（30）结合的整体导电组件（48）的碳织物（44）。 负载的表面处理剂（52）和预浸料基材（32）被固化，其包括在负载的二面体（52）和预浸料衬底（32）之间的界面粘附物质。 用于飞行器（10）的外部（14）的保护性织物系统（12）包括基底（30）。 混合预浸料基板（32）与基底基板（30）连接。 带有载体（51）的装载的二元化合物（52）与预浸料基材（32）进行界面粘合。

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