INTERIOR AIRCRAFT COMPONENTS AND METHODS OF MANUFACTURE
    1.
    发明申请
    INTERIOR AIRCRAFT COMPONENTS AND METHODS OF MANUFACTURE 有权
    内部飞机组件及其制造方法

    公开(公告)号:US20150197632A1

    公开(公告)日:2015-07-16

    申请号:US14154737

    申请日:2014-01-14

    Abstract: A aircraft component comprises a polycarbonate composition comprising: a first polycarbonate selected from a polycarbonate homopolymer, a poly(aliphatic ester-carbonate), or a combination thereof; a second polymer different from the first polycarbonate, the second polymer comprising a poly(carbonate-siloxane) copolymer, a polydialkylsiloxane, a silicone graft copolymer, or a combination thereof, wherein siloxane units in the second polymer are present in the polycarbonate composition in an amount of 0.3 to 3 wt. %, based on the total weight of the polycarbonate composition; and 10 to 50 wt. % of glass fiber, based on the total weight of the polycarbonate composition.

    Abstract translation: 飞机部件包括聚碳酸酯组合物,其包含:选自聚碳酸酯均聚物,聚(脂肪族酯 - 碳酸酯)或其组合的第一聚碳酸酯; 不同于第一聚碳酸酯的第二聚合物,第二聚合物包含聚(碳酸酯 - 硅氧烷)共聚物,聚二烷基硅氧烷,硅氧烷接枝共聚物或其组合,其中第二聚合物中的硅氧烷单元以聚碳酸酯组合物存在于聚碳酸酯组合物中 量为0.3〜3重量% %,基于聚碳酸酯组合物的总重量; 和10〜50wt。 %的玻璃纤维,基于聚碳酸酯组合物的总重量。

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