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Materials and method for improving dimensional stability of precision electronic optical photonic and spacecraft components and structures

机译:用于提高精密电子光学光子和航天器部件和结构的尺寸稳定性的材料和方法

摘要

Composite materials of the invention contain a bulk resin and a filler material. The filler material is in the form of a particle having a particle size less than about 10 micrometers, preferably less than about 1 micrometer, and more preferably less than about 500 nanometers. The composite material is made of three phases—a bulk resin phase, a filler particle phase, and an interphase. The size and extent of the interphase is dependent on the amount and particle size of the filler material and the nature of the resin. The coefficient of thermal expansion or other property of the interphase region is intermediate between that of the bulk resin and the filler particles, and tend to be biased toward those of the filler particles. In a preferred embodiment, the filler material has a coefficient of thermal expansion lower than the coefficient of thermal expansion of the bulk resin.
机译:本发明的复合材料包含块状树脂和填充材料。填充材料为粒径小于约10微米,优选小于约1微米,更优选小于约500纳米的颗粒形式。该复合材料由三相-本体树脂相,填料颗粒相和中间相制成。相间的大小和程度取决于填充材料的数量和粒径以及树脂的性质。相间区域的热膨胀系数或其他性质介于本体树脂和填料颗粒之间,并且倾向于偏向填料颗粒。在一个优选的实施方案中,填充材料的热膨胀系数低于本体树脂的热膨胀系数。

著录项

  • 公开/公告号US2003187117A1

    专利类型

  • 公开/公告日2003-10-02

    原文格式PDF

  • 申请/专利权人 STARKOVICH JOHN A.;

    申请/专利号US20020109828

  • 发明设计人 JOHN A. STARKOVICH;

    申请日2002-03-29

  • 分类号B29B11/16;C08K3/10;

  • 国家 US

  • 入库时间 2022-08-22 00:08:53

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