INTERIOR AIRCRAFT COMPONENTS AND METHODS OF MANUFACTURE
    29.
    发明公开
    INTERIOR AIRCRAFT COMPONENTS AND METHODS OF MANUFACTURE 有权
    内华达州赫尔辛基

    公开(公告)号:EP3094679A1

    公开(公告)日:2016-11-23

    申请号:EP15708576.2

    申请日:2015-01-14

    摘要: 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.

    摘要翻译: 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至50wt。 %的玻璃纤维,基于聚碳酸酯组合物的总重量。