NOSECAP
    3.
    发明申请
    NOSECAP 审中-公开

    公开(公告)号:US20160273451A1

    公开(公告)日:2016-09-22

    申请号:US15032517

    申请日:2014-10-15

    Abstract: The present disclosure relates generally to a nosecap for a gas turbine engine. The nosecap may be injection molded in an embodiment. The nosecap may have bolt holes surrounded by bolt pockets that are asymmetric about a plane passing through a geometric center of the nosecap and passing through and dividing the bolt hole in an embodiment.

    Abstract translation: 本公开总体上涉及燃气涡轮发动机的喷嘴。 在一个实施例中,可以注射成型。 螺栓孔可以具有螺栓孔,螺栓孔围绕穿过螺栓孔的几何中心的平面不对称,并且在一个实施例中通过并分隔螺栓孔。

    Nosecap
    5.
    发明授权
    Nosecap 有权

    公开(公告)号:US10352236B2

    公开(公告)日:2019-07-16

    申请号:US15032517

    申请日:2014-10-15

    Abstract: The present disclosure relates generally to a nosecap for a gas turbine engine. The nosecap may be injection molded in an embodiment. The nosecap may have bolt holes surrounded by bolt pockets that are asymmetric about a plane passing through a geometric center of the nosecap and passing through and dividing the bolt hole in an embodiment.

    FAN BLADE PLATFORM SPACER MOUNTING
    8.
    发明申请
    FAN BLADE PLATFORM SPACER MOUNTING 审中-公开
    风扇平面平面安装

    公开(公告)号:US20170030205A1

    公开(公告)日:2017-02-02

    申请号:US15039880

    申请日:2014-11-07

    Abstract: In a featured embodiment, a fan rotor comprises a platform. Clevises extend radially inwardly of the platform. Each clevis has an aperture. A hub has hub lugs positioned intermediate spaced ends of the clevises, and apertures. A pin extends through the apertures in the hub and the clevises to connect the platform to the hub. The apertures in the clevises are formed to have an inner surface for supporting the pin. A method of forming a fan blade platform is also disclosed.

    Abstract translation: 在特征实施例中,风扇转子包括平台。 夹具在平台的径向内侧延伸。 每个U形夹具有一个孔。 轮毂具有定位在U形夹的中间间隔的端部处的毂凸耳和孔。 销延伸穿过轮毂中的孔和套筒将平台连接到轮毂。 夹头中的孔形成为具有用于支撑销的内表面。 还公开了一种形成风扇叶片平台的方法。

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