NACELLE FOR AN AIRCRAFT ENGINE
    1.
    发明申请
    NACELLE FOR AN AIRCRAFT ENGINE 审中-公开
    飞机发动机的NACELLE

    公开(公告)号:US20130062461A1

    公开(公告)日:2013-03-14

    申请号:US13662886

    申请日:2012-10-29

    Applicant: Aircelle

    CPC classification number: B64D29/06

    Abstract: A supporting half-structure for an aircraft engine nacelle is provided that includes at least one longitudinal beam and a front half-frame connected to each other and formed at least partly in composite materials. The half-structure includes a connecting hinge positioned in a junction area of the longitudinal beam and of the half-frame, the hinge being formed by composite materials laid out so that fibres of the composite materials are positioned in alignment with fibres of composite materials forming said front half-frame.

    Abstract translation: 提供了一种用于飞机发动机机舱的支撑半结构,其包括至少一个纵向梁和彼此连接并且至少部分地形成复合材料的前半框架。 半结构包括位于纵向梁和半框架的接合区域中的连接铰链,铰链由复合材料形成,复合材料布置成使得复合材料的纤维与复合材料的纤维成对准 前半帧说

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