利索-全球专利检索

  1. 登录
  2. 注册
发明公开
CN102658687A 用于飞行器外部防护的环境稳定的混合织物系统 有权

用于飞行器外部防护的环境稳定的混合织物系统
摘要：
一种为飞行器（10）形成外部表面防护结构（12）的方法，包括将具有载体（51）的受载表面料（52）结合到混合预浸渍基材（32）。所述预浸渍基材（32）包括带有集成导电部件（48）的碳织物（44），并结合到基体基材（30），其中所述集成导电部件具有金属导电性范围内的导电性。固结所述受载表面料（52）和所述预浸渍基材（32），包括交界粘结所述受载表面料（52）和所述预浸渍基材（32）之间的材料。一种用于飞行器（10）外部（14）的防护织物系统（12）包括基体基材（30）。所述预浸渍基材（32）耦接到所述基体基材（30）。所述带有载体（51）的受载表面料（52）交界粘结到所述预浸渍基材。
摘要（英）：

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.

公开/授权文献
0/0