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GRAPHENE-AUGMENTED CARBON FIBER FOR AEROSPACE COMPOSITES

机译:用于航空航天复合材料的石墨烯增强型碳纤维

摘要

Composite materials with graphene-augmented carbon reinforcement fibers having a graphene film wrapped about one or more carbon fiber filaments. The graphene film is wrapped about the carbon fiber filaments in a spiral orientation and has amine groups formed on an outer surface of the graphene film and epoxide groups formed on at least one edge of the graphene film. The amine groups are formed in a functionalized area on the outer surface of the graphene film that is within about 10 microns from the at least one edge of the graphene film. The graphene film may also have holes formed through the graphene film. The graphene film may be wrapped around a single carbon fiber filament, a substantially cylindrical bundle of about 19 carbon fiber filaments, or a substantially rectangular bed of carbon fiber filaments formed from a plurality of carbon fiber tows.
机译:具有石墨烯增强的碳增强纤维的复合材料,其中石墨烯薄膜包裹着一根或多根碳纤维长丝。石墨烯膜以螺旋取向围绕碳纤维丝缠绕,并且具有在石墨烯膜的外表面上形成的胺基和在石墨烯膜的至少一个边缘上形成的环氧基。胺基在石墨烯膜的外表面上的功能化区域中形成,该官能化区域距石墨烯膜的至少一个边缘约10微米。石墨烯膜还可以具有穿过石墨烯膜形成的孔。可以将石墨烯膜包裹在单个碳纤维丝,大约19根碳纤维丝的基本圆柱形的束,或由多个碳纤维丝束形成的碳纤维丝的基本矩形的床周围。

著录项

  • 公开/公告号EP3040371B1

    专利类型

  • 公开/公告日2018-02-21

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20150188441

  • 发明设计人 HUMFELD KEITH DANIEL;

    申请日2015-10-05

  • 分类号C08K9/02;D06M11/74;C01B32/19;C08J5/04;C08J5/06;C08K7/06;

  • 国家 EP

  • 入库时间 2022-08-21 13:17:39

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