Aircraft engine pylon attachment
    1.
    发明授权
    Aircraft engine pylon attachment 有权
    飞机发动机吊架附件

    公开(公告)号:US08308105B2

    公开(公告)日:2012-11-13

    申请号:US12734233

    申请日:2008-11-19

    IPC分类号: B64D27/00

    CPC分类号: B64D27/18

    摘要: An aircraft engine mounting structure comprising a pylon box having an upper surface and at least one attachment element configured to be attached to a front spar of an aircraft wing box, the front spar having a lower surface, the attachment element being configured to attach the rear face of the pylon box to the front spar such that at least a portion of the upper surface of the pylon box lies above the lower surface of the front spar.

    摘要翻译: 一种飞机发动机安装结构,包括具有上表面的塔架箱和构造成附接到飞机机翼箱的前翼梁的至少一个附接元件,所述前翼梁具有下表面,所述附接元件构造成将后部 将塔柱的表面连接到前翼梁,使得塔架的上表面的至少一部分位于前翼梁的下表面之上。

    AIRCRAFT ENGINE PYLON ATTACHMENT
    2.
    发明申请
    AIRCRAFT ENGINE PYLON ATTACHMENT 有权
    飞机发动机吊坠附件

    公开(公告)号:US20100314491A1

    公开(公告)日:2010-12-16

    申请号:US12734233

    申请日:2008-11-19

    IPC分类号: B64D27/26

    CPC分类号: B64D27/18

    摘要: An aircraft engine mounting structure comprising a pylon box having an upper surface and at least one attachment element configured to be attached to a front spar of an aircraft wing box, the front spar having a lower surface, the attachment element being configured to attach the rear face of the pylon box to the front spar such that at least a portion of the upper surface of the pylon box lies above the lower surface of the front spar.

    摘要翻译: 一种飞机发动机安装结构,包括具有上表面的塔架箱和构造成附接到飞机机翼箱的前翼梁的至少一个附接元件,所述前翼梁具有下表面,所述附接元件构造成将后部 将塔柱的表面连接到前翼梁,使得塔架的上表面的至少一部分位于前翼梁的下表面之上。