UNIVERSAL SEAL
    2.
    发明申请
    UNIVERSAL SEAL 审中-公开
    通用密封件

    公开(公告)号:US20150315924A1

    公开(公告)日:2015-11-05

    申请号:US14735530

    申请日:2015-06-10

    Abstract: A seal for a gas turbine engine includes a top, a bottom, a left side, a right side, a back and a front. The back is parallel to the front and the left side is parallel to the right side such that a non-square shape is formed by the intersection of the back, the left side, the front and the right side. The top includes a first vane mating surface and the bottom includes a second vane mating surface.

    Abstract translation: 用于燃气涡轮发动机的密封件包括顶部,底部,左侧,右侧,后部和前部。 背面平行于前侧,左侧平行于右侧,从而通过背面,左侧,前部和右侧的交点形成非正方形形状。 顶部包括第一叶片配合表面,底部包括第二叶片配合表面。

    Method of Casting Parts Using Heat Reservoir, Gating Used by Such Method, and Casting Made Thereby
    3.
    发明申请
    Method of Casting Parts Using Heat Reservoir, Gating Used by Such Method, and Casting Made Thereby 有权
    使用这种方法使用的蓄热器浇口的方法和由此制造的铸件的方法

    公开(公告)号:US20140090383A1

    公开(公告)日:2014-04-03

    申请号:US13929289

    申请日:2013-06-27

    Inventor: Bradley T. Duelm

    Abstract: A casting, mold and method for producing a casting are disclosed. The casting may have an area of small thermal mass and an area of large thermal mass. The method may comprise providing a casting having a work product and an appendage engaged to, and suspended over, the work product between the area of small thermal mass and the area of large thermal mass, and controllably cooling the work product using the appendage.

    Abstract translation: 公开了一种用于制造铸件的铸造,模具和方法。 该铸件可以具有小的热质量区域和大的热质量面积。 该方法可以包括提供具有工件和附属物的铸件,所述工件与附属物接合并悬挂在小热量区域和大热质区域之间的工件上,并且使用附件可控制地冷却工件。

    Multi-Airfoil Split and Rejoin Method
    10.
    发明申请
    Multi-Airfoil Split and Rejoin Method 审中-公开
    多翼分裂和重合法

    公开(公告)号:US20150369070A1

    公开(公告)日:2015-12-24

    申请号:US14762630

    申请日:2013-12-16

    Abstract: A method for working an airfoil cluster is disclosed. The method may include attaching a first datum to a first portion of the airfoil cluster, and joining a second portion of the airfoil cluster to the first portion, the second portion having a second datum substantially aligned with the first datum in a common plane spaced away from the first and second portions.

    Abstract translation: 公开了一种用于加工翼型组的方法。 该方法可以包括将第一基准附接到翼型群的第一部分,以及将翼型群的第二部分连接到第一部分,第二部分具有基本上与第一基准对准的公共平面间隔开的第二基准 从第一和第二部分。

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