Thermoplastic-toughened cyanate ester resin composites with low heat release properties
    3.
    发明授权
    Thermoplastic-toughened cyanate ester resin composites with low heat release properties 有权
    具有低放热性能的热塑性增韧氰酸酯树脂复合材料

    公开(公告)号:US08404777B2

    公开(公告)日:2013-03-26

    申请号:US13611812

    申请日:2012-09-12

    IPC分类号: C08G18/28 C08G59/14 C08L79/04

    摘要: Composite materials that contain thermoplastic-toughened cyanate ester resins as the resin matrix. The composite materials exhibit low levels of heat release when burned. The matrix resins are composed of from 50 to 80 weight percent of a cyanate ester resin component. The matrix resin composition also includes from 10 to 40 weight percent of a thermoplastic blend that is composed of polyetherimide and polyamideimide. The epoxy resin composition further includes from 1 to 10 weight percent of a curative agent. The composite materials may be used for primary structures in aircraft and other load-bearing structures.

    摘要翻译: 含有热塑性增韧氰酸酯树脂作为树脂基体的复合材料。 复合材料在燃烧时表现出低的放热水平。 基质树脂由50-80重量%的氰酸酯树脂组分组成。 基质树脂组合物还包括10-40重量%的由聚醚酰亚胺和聚酰胺酰亚胺组成的热塑性共混物。 环氧树脂组合物还包含1至10重量%的治疗剂。 复合材料可用于飞机和其他承重结构中的主要结构。

    Power-saving and context-showing display information converting system and corresponding apparatus
    5.
    发明授权
    Power-saving and context-showing display information converting system and corresponding apparatus 有权
    省电和上下文显示信息转换系统及相应设备

    公开(公告)号:US08957886B2

    公开(公告)日:2015-02-17

    申请号:US13005540

    申请日:2011-01-13

    IPC分类号: G09G5/00 G09G3/32 G09G3/20

    摘要: A context-showing and power-saving display information converting system and a corresponding apparatus are provided for lowering the power consumption of displaying images on a pixel self-emissive display device. The display information converting system includes a context-showing module and a power-saving conversion module. The context-showing module receives display information that describes the content of an image, wherein the display information includes one or more elements, and each element corresponds to a plurality of pixels displayed by a display device. In addition, the context-showing module determines a relevance of the one or more elements according to the viewing interest of the user. The power-saving conversion module converts the display information in unit of the one or more elements according to the relevance and provides the converted display information to the display device.

    摘要翻译: 提供一种上下文显示和省电显示信息转换系统和相应的装置,用于降低在像素自发显示装置上显示图像的功耗。 显示信息转换系统包括上下文显示模块和省电转换模块。 上下文显示模块接收描述图像内容的显示信息,其中显示信息包括一个或多个元素,并且每个元素对应于由显示设备显示的多个像素。 此外,上下文显示模块根据用户的观看兴趣确定一个或多个元素的相关性。 省电转换模块根据相关性将一个或多个元件单元的显示信息转换,并将转换的显示信息提供给显示设备。

    Thermoplastic-toughened cyanate ester resin composites with low heat release properties
    6.
    发明授权
    Thermoplastic-toughened cyanate ester resin composites with low heat release properties 有权
    具有低放热性能的热塑性增韧氰酸酯树脂复合材料

    公开(公告)号:US08283408B2

    公开(公告)日:2012-10-09

    申请号:US12713534

    申请日:2010-02-26

    IPC分类号: C08G18/28 C08G59/14 C08L79/04

    摘要: Composite materials that contain thermoplastic-toughened cyanate ester resins as the resin matrix. The composite materials exhibit low levels of heat release when burned. The matrix resins are composed of from 50 to 80 weight percent of a cyanate ester resin component. The matrix resin composition also includes from 10 to 40 weight percent of a thermoplastic blend that is composed of polyetherimide and polyamideimide. The epoxy resin composition further includes from 1 to 10 weight percent of a curative agent. The composite materials may be used for primary structures in aircraft and other load-bearing structures.

    摘要翻译: 含有热塑性增韧氰酸酯树脂作为树脂基体的复合材料。 复合材料在燃烧时表现出低的放热水平。 基质树脂由50-80重量%的氰酸酯树脂组分组成。 基质树脂组合物还包括10-40重量%的由聚醚酰亚胺和聚酰胺酰亚胺组成的热塑性共混物。 环氧树脂组合物还包含1至10重量%的治疗剂。 复合材料可用于飞机和其他承重结构中的主要结构。

    Thermoplastic-Toughened Cyanate Ester Resin Composites With Low Heat Release Properties
    7.
    发明申请
    Thermoplastic-Toughened Cyanate Ester Resin Composites With Low Heat Release Properties 有权
    具有低热释放性能的热塑性增韧氰酸酯树脂复合材料

    公开(公告)号:US20110212292A1

    公开(公告)日:2011-09-01

    申请号:US12713534

    申请日:2010-02-26

    IPC分类号: C08L33/24 B32B5/12

    摘要: Composite materials that contain thermoplastic-toughened cyanate ester resins as the resin matrix. The composite materials exhibit low levels of heat release when burned. The matrix resins are composed of from 50 to 80 weight percent of a cyanate ester resin component. The matrix resin composition also includes from 10 to 40 weight percent of a thermoplastic blend that is composed of polyetherimide and polyamideimide. The epoxy resin composition further includes from 1 to 10 weight percent of a curative agent. The composite materials may be used for primary structures in aircraft and other load-bearing structures.

    摘要翻译: 含有热塑性增韧氰酸酯树脂作为树脂基体的复合材料。 复合材料在燃烧时表现出低的放热水平。 基质树脂由50-80重量%的氰酸酯树脂组分组成。 基质树脂组合物还包括10-40重量%的由聚醚酰亚胺和聚酰胺酰亚胺组成的热塑性共混物。 环氧树脂组合物还包含1至10重量%的治疗剂。 复合材料可用于飞机和其他承重结构中的主要结构。

    THERMOPLASTIC-TOUGHENED CYANATE ESTER RESIN COMPOSITES WITH LOW HEAT RELEASE PROPERTIES
    9.
    发明申请
    THERMOPLASTIC-TOUGHENED CYANATE ESTER RESIN COMPOSITES WITH LOW HEAT RELEASE PROPERTIES 有权
    具有低热释放性能的热塑性增韧氰化酯树脂复合材料

    公开(公告)号:US20130005898A1

    公开(公告)日:2013-01-03

    申请号:US13611812

    申请日:2012-09-12

    IPC分类号: C08L79/08 C08K7/06

    摘要: Composite materials that contain thermoplastic-toughened cyanate ester resins as the resin matrix. The composite materials exhibit low levels of heat release when burned. The matrix resins are composed of from 50 to 80 weight percent of a cyanate ester resin component. The matrix resin composition also includes from 10 to 40 weight percent of a thermoplastic blend that is composed of polyetherimide and polyamideimide. The epoxy resin composition further includes from 1 to 10 weight percent of a curative agent. The composite materials may be used for primary structures in aircraft and other load-bearing structures.

    摘要翻译: 含有热塑性增韧氰酸酯树脂作为树脂基体的复合材料。 复合材料在燃烧时表现出低的放热水平。 基质树脂由50-80重量%的氰酸酯树脂组分组成。 基质树脂组合物还包括10-40重量%的由聚醚酰亚胺和聚酰胺酰亚胺组成的热塑性共混物。 环氧树脂组合物还包含1至10重量%的治疗剂。 复合材料可用于飞机和其他承重结构中的主要结构。