SURFACE HAVING SPECIALLY FORMED RECESSES AND COMPONENT
    11.
    发明申请
    SURFACE HAVING SPECIALLY FORMED RECESSES AND COMPONENT 审中-公开
    具有特殊成型表面和部件的表面

    公开(公告)号:US20140255652A1

    公开(公告)日:2014-09-11

    申请号:US14352233

    申请日:2012-08-17

    Abstract: A surface having specially formed recesses and component is provided. The component has a layer with a surface, having elongate recesses, which have a longitudinal direction, wherein the recesses are arranged at an angle which differs considerably from 0°, in particular 90°+/−20°, with respect to a direction of overflow over the surface, and are at least partially widened transversely to the longitudinal direction thereof in the region of the surface with respect to the base of the recess, in which the recess is widened proceeding from the base only above a certain height within the recess, and in particular the recess has a constant width before it, in which the recess does not extend through the entire thickness of the layer.

    Abstract translation: 提供具有特别形成的凹部和部件的表面。 该部件具有具有表面的层,其具有纵向方向的细长凹槽,其中凹部被布置成与0°,特别是90°+/- 20°相差大的角度,相对于 在表面的相对于凹部的基部的区域中,横向于其纵向方向至少部分地被加宽,其中凹部从基部开始仅在凹部内的一定高度上方加宽 特别地,凹部在其之前具有恒定的宽度,其中凹部不延伸穿过层的整个厚度。

    METHOD FOR PRODUCING A PROTECTIVE LAYER FOR A ROTOR BLADE
    16.
    发明申请
    METHOD FOR PRODUCING A PROTECTIVE LAYER FOR A ROTOR BLADE 审中-公开
    用于生产用于转子叶片的保护层的方法

    公开(公告)号:US20130330203A1

    公开(公告)日:2013-12-12

    申请号:US14000935

    申请日:2011-12-30

    Abstract: A method for producing a protective layer for a rotor blade of a turbomachine is proposed. The rotor blade has a wear cap wall that in relation to the axis of the turbomachine protrudes radially towards the exterior of the turbomachine beyond a body of the rotor blade. The method enables the entire rotor blade to have a comparatively long service life and at the same time allows the wear cap wall to be thermally insulated in an especially simple manner. For the purpose, a profile producing a positive fit effective in the radial direction is inserted in a radially located region of the wear cap wall, a slip containing metal powder and/or a ceramic slip is applied to the region and the slip in sintered.

    Abstract translation: 提出了一种用于制造涡轮机转子叶片保护层的方法。 转子叶片具有磨损盖壁,其相对于涡轮机的轴线径向朝向涡轮机的外部突出超过转子叶片的主体。 该方法使得整个转子叶片具有相对较长的使用寿命,并且同时允许耐磨帽壁以特别简单的方式被隔热。 为此目的,在径向定位的区域中插入产生沿径向有效的正配合的轮廓,将含有金属粉末和/或陶瓷滑移的滑动件施加到该区域上并将该滑动烧结。

    Liner for a Die Body
    17.
    发明申请
    Liner for a Die Body 审中-公开
    一个模具的衬里

    公开(公告)号:US20120285652A1

    公开(公告)日:2012-11-15

    申请号:US13103338

    申请日:2011-05-09

    CPC classification number: B22D17/22 B22C7/02 B22C9/06 B29C33/68 B29C67/241

    Abstract: A liner for a die body is presented. The liner includes a flexible base material characterized in that reinforcements with lower stretchability compared to the base material are bonded along the extent of the liner. A tool which includes the liner is also provided. The reinforcements may include glass fibers or carbon fibers.

    Abstract translation: 提出了一种用于模具主体的衬垫。 衬套包括柔性基体材料,其特征在于,与基底材料相比,具有较低拉伸性的增强材料沿衬垫的程度粘合。 还提供了包括衬套的工具。 加强件可以包括玻璃纤维或碳纤维。

    PROCESS FOR OPTIMIZING A CORE DIE
    19.
    发明申请
    PROCESS FOR OPTIMIZING A CORE DIE 审中-公开
    优化核心工艺的过程

    公开(公告)号:US20120103554A1

    公开(公告)日:2012-05-03

    申请号:US13287358

    申请日:2011-11-02

    CPC classification number: B22C9/06 B22C9/12 B22C13/12

    Abstract: A process for optimizing a core die is provided. By iteratively modifying the ceramic core without changing the core die, it is possible to ascertain an optimum core without modifying the core die every time. In a last step, an optimum core die is produced using the optimum ceramic core.

    Abstract translation: 提供了一种用于优化芯片的工艺。 通过在不改变芯模的情况下迭代地修改陶瓷芯,可以确定最佳的芯,而不必每次修改芯芯。 在最后一步中,使用最佳陶瓷芯产生最佳的芯模。

    Method for producing a pattern for the precision-cast preparation of a component comprising at least one cavity
    20.
    发明申请
    Method for producing a pattern for the precision-cast preparation of a component comprising at least one cavity 失效
    用于制造用于精密铸造制备包含至少一个腔的部件的图案的方法

    公开(公告)号:US20100294451A1

    公开(公告)日:2010-11-25

    申请号:US12517889

    申请日:2007-09-21

    Applicant: Uwe Paul

    Inventor: Uwe Paul

    CPC classification number: B22C7/026 B22C9/04 B22C9/10 B33Y80/00

    Abstract: A method for producing a pattern for the precision-cast representation of a component having a cavity is provided. In the method wherein the component is a turbine component having a cavity, the finished pattern comprises a core and an outer contour pattern, the outer contour pattern at least partially surrounds the core and at least partially defines the outer contour of the turbine component. The core is produced from a curable core material, which cures during the course of the method, and the outer contour pattern is produced from a material which can be burned or melted out. In this case, first the outer contour pattern is produced with a cavity corresponding to the cavity of the turbine component and subsequently the curable core material is filled into the cavity and cured to produce the core.

    Abstract translation: 提供了一种用于制造具有空腔的部件的精密铸造表面的图案的方法。 在其中所述部件是具有空腔的涡轮机部件的方法中,所述精加工图案包括芯部和外部轮廓图案,所述外部轮廓图案至少部分地围绕所述芯部并且至少部分地限定所述涡轮机部件的外部轮廓。 芯由可固化的芯材制成,其在该方法的过程中固化,并且外轮廓图案由可燃烧或熔化的材料制成。 在这种情况下,首先利用对应于涡轮机部件的空腔的空腔来制造外部轮廓图案,随后将可固化的芯材料填充到腔体中并固化以产生芯部。

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