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CARBON-BASED BARRIER COATINGS FOR HIGH-TEMPERATURE POLYMER-MATRIX COMPOSITES

机译:高温聚合物基复合材料的碳基阻隔涂料

摘要

A high-temperature polymeric-matrix composite (HTPMC) structure and a method for protecting an HTPMC from exposure to high temperatures in the presence of air, and prevent thermo-oxidative degradation. A thin, lightweight layer of a carbon-based barrier is applied onto a surface of the HTPMC structure. The carbon-based barrier coating is composed of graphene, amorphous carbon, or a mixture comprising a combination of graphene and amorphous carbon, and has coefficient of thermal expansion that is less than 10 times the coefficient of thermal expansion of the HTPMC structure. The carbon-based barrier may be coated with an erosion-barrier.
机译:高温聚合物基复合材料(HTPMC)结构和用于保护HTPMC免于在空气存在下暴露于高温并防止热氧化降解的方法。碳基阻挡层的薄而轻的层被施加到HTPMC结构的表面上。碳基阻挡涂层由石墨烯,无定形碳或包含石墨烯和无定形碳的组合的混合物组成,并且其热膨胀系数小于HTMPC结构的热膨胀系数的10倍。碳基阻挡层可以涂覆有腐蚀阻挡层。

著录项

  • 公开/公告号EP3023248A1

    专利类型

  • 公开/公告日2016-05-25

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20150194467

  • 发明设计人 TSOTSIS THOMAS KARL;

    申请日2015-11-13

  • 分类号B32B27;

  • 国家 EP

  • 入库时间 2022-08-21 14:49:18

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