会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 6. 发明专利
    • Multiple-resin composite structures and methods of producing the same
    • 多层树脂复合结构及其生产方法
    • JP2014167083A
    • 2014-09-11
    • JP2013125019
    • 2013-06-13
    • Boeing Coザ・ボーイング・カンパニーThe Boeing Company
    • CHRISTOPHER P HENRY
    • C08J5/04B64C1/00B64C1/12C08J5/24
    • B32B5/12B29B15/10B29B15/105B29K2063/00B29K2083/00B64C1/12D06M15/55D06M15/643D06M17/00Y10T156/10Y10T428/24107Y10T428/2481Y10T428/24983Y10T442/2098Y10T442/3301
    • PROBLEM TO BE SOLVED: To provide materials suitably flexible to cover or form an aircraft skin and having a mechanical stability appropriate to force typically applied to the aircraft skin.SOLUTION: Flexible composite structures include a textile arrangement of at least one textile layer constructed of textile fibers and having a distribution of pores formed therein, with a first resin filling pores having a pore diameter equal to or less than a pore diameter threshold, and a second resin bonded to the first resin and substantially filling inter-fiber pores having a pore diameter greater than the pore diameter threshold. Embodiments include a rigid first resin such as an epoxy resin, and a flexible second resin such as a silicone. Methods of producing composite structures may include selectively filling, in a textile layer having a number of pores formed therein, only those pores having a pore diameter equal to or less than a pore diameter threshold, with a first resin, and substantially filling the remaining pores in the textile layer with a second resin.
    • 要解决的问题:提供适当灵活的材料以覆盖或形成飞行器皮肤并具有适于通常施加到飞行器皮肤上的力的机械稳定性。解决方案:柔性复合结构包括由纺织品构成的至少一个纺织层的织物布置 纤维,其中形成有孔的分布,第一树脂填充孔径等于或小于孔径阈值的孔,以及第二树脂,其结合到第一树脂上并基本上填充具有孔径的纤维间孔隙 大于孔径阈值。 实施例包括诸如环氧树脂的刚性第一树脂和诸如硅酮的柔性第二树脂。 制备复合结构的方法可以包括在第一树脂中选择性地填充其中形成有多个孔的织物层中仅具有孔径等于或小于孔直径阈值的孔,并且基本上填充剩余的孔 在具有第二树脂的织物层中。