METHOD FOR 3-D PRINTING A PATTERN FOR THE SURFACE OF A TURBINE SHROUD
    3.
    发明申请
    METHOD FOR 3-D PRINTING A PATTERN FOR THE SURFACE OF A TURBINE SHROUD 有权
    3-D打印涡轮机表面图案的方法

    公开(公告)号:US20150093506A1

    公开(公告)日:2015-04-02

    申请号:US14043031

    申请日:2013-10-01

    Abstract: A method of making an article of manufacture is provided and includes the steps of spraying a first coating onto a substrate, and depositing a second coating on the first coating by 3-D printing a material disposed in a pattern. The pattern includes ridges disposed at a base surface of a turbine part. Each ridge defined by first and second sidewalls, each sidewall having a first and second end. The ends extend from the base surface, the sidewalls slope toward each other until meeting at second ends of respective first and second sidewalls defining a centerline and a top portion of the ridge. The sidewalls are inclined with substantially equal but opposite slopes with respect to the base surface. The ridges correspond to a back portion of a turbine bucket and are oriented at a first angle with respect to an axis of rotation of the bucket.

    Abstract translation: 提供了一种制造制品的方法,包括以下步骤:将第一涂层喷涂到基材上,并通过3D印刷以图案布置的材料在第一涂层上沉积第二涂层。 该图案包括设置在涡轮部分的基面处的脊。 每个脊由第一和第二侧壁限定,每个侧壁具有第一和第二端。 所述端部从所述基部表面延伸,所述侧壁朝向彼此倾斜,直到在限定所述脊的中心线和顶部的相应的第一和第二侧壁的第二端处相遇。 侧壁相对于基面具有大致相等但相反的倾斜倾斜。 脊对应于涡轮机叶片的后部并相对于铲斗的旋转轴线以第一角度定向。

    UNITARY BODY TURBINE SHROUD FOR TURBINE SYSTEMS

    公开(公告)号:US20200248559A1

    公开(公告)日:2020-08-06

    申请号:US16263596

    申请日:2019-01-31

    Abstract: A turbine shroud for turbine systems are disclosed. The shrouds may include a unitary body including a support portion coupled directly to a turbine casing of the turbine system, and forward hook(s) and aft hook(s) formed integral with the support portion. The unitary body may also include an intermediate portion formed integral with and extending from the support portion. The intermediate portion may include a non-linear segment extending from the support portion, and a forward segment formed integral with the non-linear segment. The forward segment of the intermediate portion may be positioned axially upstream of the forward hook(s). Additionally the unitary body may include a seal portion formed integral with the intermediate portion, opposite the support portion. The seal portion may include a forward end formed integral with the intermediate portion. The forward end may be positioned axially upstream of the forward hook(s).

    COLLIMATOR GRID AND AN ASSOCIATED METHOD OF FABRICATION
    8.
    发明申请
    COLLIMATOR GRID AND AN ASSOCIATED METHOD OF FABRICATION 有权
    COLLIMATOR网格和相关的制造方法

    公开(公告)号:US20140177781A1

    公开(公告)日:2014-06-26

    申请号:US13723275

    申请日:2012-12-21

    CPC classification number: G21K1/02 A61B6/4233 A61B6/4291 Y10T29/49989

    Abstract: A collimator grid and a method of fabricating the collimator grid are disclosed. The method includes molding a plurality of plates, each plate includes a plurality of grooves in a first surface, a plurality of fin tips in a second surface disposed opposite to the first surface, plurality of ribs on a first pair of peripheral sides, a plurality of first fiducials formed on the plurality of ribs, and a plurality of second fiducials formed on a second pair of peripheral sides. The method includes machining the second surface to form the plurality of fins having predefined dimensions. Further, the method includes stacking the plurality of plates overlapping each other based on the plurality of first fiducials, and machining the plurality of ribs and first fiducials to form the collimator grid.

    Abstract translation: 公开了准直器栅格和制造准直器栅格的方法。 该方法包括成型多个板,每个板包括在第一表面中的多个槽,在与第一表面相对设置的第二表面中的多个翅片尖端,在第一对外围侧上的多个肋,多个 形成在所述多个肋上的第一基准以及形成在第二对外围侧上的多个第二基准。 该方法包括加工第二表面以形成具有预定尺寸的多个翅片。 此外,该方法包括基于多个第一基准堆叠彼此重叠的多个板,并且加工多个肋和第一基准以形成准直器格栅。

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