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    • 4. 发明申请
    • CEMENTITIOUS PANEL WITH BASALT FIBER REINFORCED MAJOR SURFACE(S)
    • 具有基础纤维增强主要表面的面板(S)
    • WO02033191A1
    • 2002-04-25
    • PCT/US2001/042778
    • 2001-10-16
    • E04C2/04
    • E04C2/043Y10T442/134Y10T442/141Y10T442/143Y10T442/171Y10T442/197
    • A cementitious panel having a basalt fiber-containing reinforcing web embedded in at least one major surface, preferably both major surfaces, of the panel. The basalt fibers containing reinforcing webs preferably are in the form of a mesh or scrim comprising spaced basalt fiber strands in both the warp and fill directions, each strand made from a plurality of aligned, continuous basalt fibers. The basalt fiber reinforcing webs also can be in the form of woven or non-woven fabrics of basalt fibers, having aligned or randomly oriented staple and/or micro fibers, so long as the fabrics have sufficient void area to permit a cementitious core material to penetrate the fabric when the fabric is embedded in one or both major surfaces of the cementitious panel before the cementtitious core material hardens.
    • 一种具有嵌入板的至少一个主表面,优选两个主表面的含玄武岩纤维增强网的水泥板。 含有增强网的玄武岩纤维优选为网状或稀松布的形式,其包括在经向和填充方向上分开的玄武岩纤维束,每条链由多个对准的连续的玄武岩纤维制成。 玄武岩纤维增强网也可以是具有对准或随机定向的短纤维和/或微纤维的玄武岩纤维的织造或非织造织物的形式,只要织物具有足够的空隙面积以允许水泥核心材料 在将粘结的芯材硬化之前,将织物嵌入水泥质板的一个或两个主表面时,渗透织物。
    • 9. 发明申请
    • COMPOSITE MATERIALS AND APPLICATIONS THEREOF AND METHODS OF MAKING COMPOSITE MATERIALS
    • 复合材料及其制备方法及制备复合材料的方法
    • WO2014062991A1
    • 2014-04-24
    • PCT/US2013/065566
    • 2013-10-18
    • PPG INDUSTRIES OHIO, INC.
    • MORRIS, Steven, JohnPETERS, James, Carl
    • B32B18/00C04B33/36F41H5/04
    • E04C5/073B32B18/00C04B14/42C04B28/34C04B35/447C04B35/62844C04B35/82C04B2111/00612C04B2111/0075C04B2235/5256C04B2237/34C04B2237/36C04B2237/70C04B2237/704Y10T442/133Y10T442/14Y10T442/153Y10T442/171C04B14/06C04B32/02C04B20/1029
    • Various embodiments of the present invention provide composite materials and methods of making the same. In some embodiments, the composite materials comprise high temperature resistant composite materials and methods of making high temperature resistant composite materials. In some embodiments, high temperature resistant composite materials of the present invention can be fabricated into landing pads, components used in landing pads to provide a structure to support the take-off and landing of aircraft, roadways or similar travel paths for heavy equipment, and/or components used in roadways or similar travel paths for heavy equipment. In one embodiment, a composite material comprises an inorganic ceramic matrix having a top surface in facing opposition to a bottom surface and at least one side surface between the top surface and the bottom surface, a first open weave fabric comprising a plurality of fibers disposed in the matrix proximate the bottom surface of the matrix, and at least one additional open weave fabric comprising a plurality of fibers disposed in the matrix between the first open weave fabric and the top surface of the matrix, wherein the at least one additional open weave fabric is positioned closer to the bottom surface than the top surface of the matrix.
    • 本发明的各种实施方式提供复合材料及其制造方法。 在一些实施方案中,复合材料包括耐高温复合材料和制备耐高温复合材料的方法。 在一些实施方案中,本发明的耐高温复合材料可以制成着陆​​垫,用于着陆垫中的部件,以提供用于支撑用于重型设备的飞行器,道路或类似行进路径的起飞和着陆的结构,以及 /或用于重型设备的道路或类似行驶路径中的部件。 在一个实施方案中,复合材料包括无机陶瓷基体,其具有面向底表面的顶表面和顶表面和底表面之间的至少一个侧表面,第一开口编织织物,其包括多个布置在 所述基体接近所述基体的底表面,以及至少一个额外的开放编织织物,其包含布置在所述基质中的所述第一开口编织织物和所述基质的顶表面之间的多个纤维,其中所述至少一个另外的开放编织织物 位于比矩阵的顶表面更靠近底表面的位置。