Nacelle for an aircraft engine
    2.
    发明授权
    Nacelle for an aircraft engine 有权
    飞机发动机的机舱

    公开(公告)号:US09010681B2

    公开(公告)日:2015-04-21

    申请号:US13662905

    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, the beam and the half-frame being formed of composite materials. The half frame has an open section, and the half-structure defines a structure selected from the group consisting of: the beam and the front half-frame form a one-piece part; the beam has an extension with an open section, the shape of which matches that of the front half-frame, the extension being attached to the half frame; and the front half-frame has an extension with an open shape, the shape of which matches the beam, wherein the extension is attached to the beam.

    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前半框架,梁和半框架由复合材料形成。 半框架具有开口部分,并且半结构限定了从由以下组成的组中选择的结构:梁和前半框架形成一体式部件; 梁具有开口部分的延伸部分,其形状与前半框架的形状相匹配,延伸部分附接到半框架; 并且前半框架具有开口形状的延伸部,其形状与梁的形状相匹配,其中延伸部附接到梁上。

    NACELLE FOR AN AIRCRAFT ENGINE
    3.
    发明申请
    NACELLE FOR AN AIRCRAFT ENGINE 有权
    飞机发动机的NACELLE

    公开(公告)号:US20130062462A1

    公开(公告)日:2013-03-14

    申请号:US13662905

    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, the beam and the half-frame being formed of composite materials. The half frame has an open section, and the half-structure defines a structure selected from the group consisting of: the beam and the front half-frame form a one-piece part; the beam has an extension with an open section, the shape of which matches that of the front half-frame, the extension being attached to the half frame; and the front half-frame has an extension with an open shape, the shape of which matches the beam, wherein the extension is attached to the beam.

    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前半框架,梁和半框架由复合材料形成。 半框架具有开口部分,并且半结构限定了从由以下组成的组中选择的结构:梁和前半框架形成一体式部件; 梁具有开口部分的延伸部分,其形状与前半框架的形状相匹配,延伸部分附接到半框架; 并且前半框架具有开口形状的延伸部,其形状与梁的形状相匹配,其中延伸部附接到梁上。

    NACELLE FOR AN AIRCRAFT ENGINE
    5.
    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

Patent Agency Ranking