Process for manufacturing a honeycomb seal
    2.
    发明授权
    Process for manufacturing a honeycomb seal 有权
    蜂窝状密封件的制造方法

    公开(公告)号:US08434663B2

    公开(公告)日:2013-05-07

    申请号:US11578875

    申请日:2005-03-31

    申请人: Reinhold Meier

    发明人: Reinhold Meier

    IPC分类号: B23K101/02

    摘要: A process for manufacturing a honeycomb seal is disclosed. The process includes the following steps: a) the honeycomb structure is brought to the desired three-dimensional form and is fixed in this form; b) then the honeycomb structure is filled with a filler material; c) then the honeycomb structure filled with the filler material is machined on a side on which a carrier element is arranged, such that this side has the desired contour and that the end edges of the honeycomb structure are sealed flushly with the filler compound; d) then the side contoured in this way is coated with a coating; e) next the carrier element is applied to the coating, preferably by laser powder build-up welding.

    摘要翻译: 公开了一种制造蜂窝密封件的方法。 该方法包括以下步骤:a)将蜂窝结构体形成所需的三维形状并以此形式固定; b)然后蜂窝结构填充填料; c)然后,填充有填充材料的蜂窝结构体在其上布置有载体元件的一侧被加工,使得该侧具有期望的轮廓,并且蜂窝结构的端边缘与填料混合物密封; d)然后以这种方式形成的侧面涂覆有涂层; e)接下来,将载体元件施加到涂层上,优选地通过激光粉末堆积焊接。

    GUIDE BLADE SEGMENT OF A GAS TURBINE AND METHOD FOR ITS PRODUCTION
    3.
    发明申请
    GUIDE BLADE SEGMENT OF A GAS TURBINE AND METHOD FOR ITS PRODUCTION 审中-公开
    燃气轮机的指导刀片及其生产方法

    公开(公告)号:US20090304497A1

    公开(公告)日:2009-12-10

    申请号:US12162307

    申请日:2007-01-19

    IPC分类号: F01D11/00

    摘要: A guide blade segment of a gas turbine, having at least one guide blade and having an inner cover band assigned to the radially inner end of the or each guide blade, is disclosed. An integral constituent part of the inner cover band of the guide blade segment is a sealing element, which serves to seal a radially inner gap between the guide blade segment and a gas turbine rotor.

    摘要翻译: 公开了一种燃气轮机的导向叶片段,其具有至少一个导向叶片并且具有分配给该导向叶片或每个导向叶片的径向内端的内盖带。 引导叶片段的内盖带的整体构成部分是密封元件,其用于密封导向叶片段和燃气轮机转子之间的径向内部间隙。

    Sealing Device
    4.
    发明申请
    Sealing Device 审中-公开
    密封装置

    公开(公告)号:US20070273103A1

    公开(公告)日:2007-11-29

    申请号:US10588141

    申请日:2005-01-28

    申请人: Reinhold Meier

    发明人: Reinhold Meier

    IPC分类号: F01D11/12

    摘要: A sealing device is e.g., for a gas turbine, such as an aircraft engine. The sealing device, is used for sealing a gap between a rotor and a stator, e.g., for sealing a gap between radially inside ends of fixed vanes and a rotor and/or a gap between radially outer ends of rotating rotor blades and a fixed housing, a honeycomb seal including a plurality of honeycomb seal cells being assigned to the stator, and the honeycomb seal cells being separated from one another by walls. At least the walls of the honeycomb seal cells that extend transversely to the direction of rotation of the rotor are placed radially at a slant in the direction of rotation of the rotor.

    摘要翻译: 例如,用于燃气轮机的密封装置,例如飞行器发动机。 密封装置用于密封转子和定子之间的间隙,例如用于密封固定叶片的径向内端和转子之间的间隙和/或旋转的转子叶片的径向外端之间的间隙和固定壳体 ,蜂窝状密封件,其包括分配给定子的多个蜂窝密封单元,蜂窝状密封单元通过壁彼此分离。 至少沿着转子的旋转方向横向延伸的蜂窝状密封单元的壁沿转子的旋转方向径向放置。

    Method For Connecting Components
    5.
    发明申请
    Method For Connecting Components 审中-公开
    连接组件的方法

    公开(公告)号:US20070271759A1

    公开(公告)日:2007-11-29

    申请号:US11659870

    申请日:2005-08-03

    申请人: Reinhold Meier

    发明人: Reinhold Meier

    IPC分类号: B21D53/02

    摘要: The invention relates to a method for the connecting of components, namely for the connecting of at least one pipe-shaped or rod-shaped component with a wall-type component, with the following steps: a) providing a wall-type component (11), whereby the wall-type component (11) comprises a sandwich-type structure of two plate-shaped or pipe-shaped elements (12, 13) with a layer (14) of an expandable foamable metal material positioned therebetween; b) providing at least one pipe-shaped or rod-shaped component (10); c) introducing at least one opening in the wall-type component (11) for the receiving of the or each pipe-shaped or rod-shaped component (10); d) inserting of the or each pipe-shaped or rod-shaped component (10) in a corresponding opening of the wall-type component (11); e) heating of the arrangement of the wall-type component (11) and the or each pipe-shaped or rod-shaped component (10) with foaming-up expansion of the expandable foamable metal material for the connecting of the or each pipe-shaped or rod-shaped component (10) with the wall-type component (11).

    摘要翻译: 本发明涉及一种用于连接部件的方法,即用于将至少一个管状或棒状部件与壁型部件连接起来的方法,步骤如下:a)提供壁式部件(11 ),由此壁型部件(11)包括两个板状或管状元件(12,13)的夹层结构,其间具有位于其间的可膨胀发泡金属材料层(14); b)提供至少一个管状或棒状部件(10); c)在所述壁式部件(11)中引入至少一个开口,用于容纳所述或每个管状或棒状部件(10); d)将所述或每个管状或棒状部件(10)插入所述壁式部件(11)的相应开口中; e)通过膨胀发泡金属材料的膨胀膨胀来加热壁型部件(11)和管状或棒状部件(10)的布置,用于连接管状或棒状部件 带状或杆状部件(10)与壁型部件(11)。

    Halogen incandescent lamp having U-shaped inner supply lead held mechanically in a fold in the foil
    7.
    发明授权
    Halogen incandescent lamp having U-shaped inner supply lead held mechanically in a fold in the foil 失效
    卤素白炽灯具有机械地保持在箔片中的折叠中的U形内部供应引线

    公开(公告)号:US06291934B1

    公开(公告)日:2001-09-18

    申请号:US09267810

    申请日:1999-03-12

    IPC分类号: H01J1718

    摘要: A supply lead (7) for a halogen incandescent lamp is bent in a U-shaped fashion and comprises a base (15) and two limbs (16). The ends of the limbs engage in the end region (6) of the luminous element by means of hook parts (20). A section (11) at the end, on the side of the luminous element, of the associated foil is folded back and forms a fold (12) in which the base (15) is held mechanically.

    摘要翻译: 用于卤素白炽灯的供应引线(7)以U形的方式弯曲,并且包括基座(15)和两个支脚(16)。 四肢的端部通过钩部件(20)接合在发光元件的端部区域(6)中。 在相关联的箔的发光元件侧的端部的部分(11)被折回并形成其中基部(15)机械地保持的折叠(12)。

    Component and method for joining metal elements
    8.
    发明授权
    Component and method for joining metal elements 有权
    用于连接金属元素的组分和方法

    公开(公告)号:US09333589B2

    公开(公告)日:2016-05-10

    申请号:US12225350

    申请日:2007-03-14

    摘要: A component, in particular a component of a gas turbine, is described composed of at least two metallic structural elements, the first structural element having a first joining surface, and the second structural element having a second joining surface, and the structural elements being joined via their joining surfaces by an inductive high-frequency pressure welding. One of the joining surfaces is shaped to widen peripherally in comparison to the other joining surface, and an upsetting deformation produced in a join region in response to the joining of the structural elements rests virtually entirely within and, in particular, on a peripheral collar formed by the peripheral widening of the one joining surface. A method is described for joining metallic structural elements, in particular structural elements of a gas turbine, an inductive high-frequency pressure welding being used to join corresponding joining surfaces of the structural elements.

    摘要翻译: 描述了一种组件,特别是燃气轮机的部件,其由至少两个金属结构元件组成,第一结构元件具有第一接合表面,第二结构元件具有第二接合表面,并且结构元件被连接 通过其接合表面通过感应式高频压力焊接。 其中一个接合表面被成形为与其它接合表面相比在外围加宽,并且响应于结构元件的接合而在连接区域中产生的镦锻变形基本上完全搁置在并且特别地在形成的外围套环上 通过一个连接表面的外围加宽。 描述了用于连接金属结构元件,特别是燃气轮机的结构元件的方法,用于连接结构元件的相应接合表面的感应式高频压力焊接。

    Method for joining blades to blade roots or rotor disks when manufacturing and/or repairing gas turbine blades or integrally bladed gas turbine rotors
    10.
    发明授权
    Method for joining blades to blade roots or rotor disks when manufacturing and/or repairing gas turbine blades or integrally bladed gas turbine rotors 失效
    在制造和/或修理燃气轮机叶片或整体叶片燃气轮机转子时,将叶片连接到叶片根部或转盘上的方法

    公开(公告)号:US07634854B2

    公开(公告)日:2009-12-22

    申请号:US10570418

    申请日:2005-06-30

    申请人: Reinhold Meier

    发明人: Reinhold Meier

    IPC分类号: B23P6/00 B23P19/04

    摘要: A method is provided for joining blades to blade roots or rotor disks when manufacturing and/or repairing gas turbine blades or integrally bladed gas turbine rotors. A blade and a blade root or rotor disk that is to be joined to the blade are supplied, and provided with a thickening in sections that are to be joined together. The sections of the blade and the blade root or rotor disk that are to be joined together are machined so as to form recesses and; c) are then aligned relative to each other, opposite recesses defining at least one groove-shaped seam preparation. The blade and the blade root or rotor disk are joined in the area of the or each seam preparation by means of laser power build-up welding and the joined blade and blade root or rotor disk are machined so as to provide a gas turbine blade or an integrally bladed gas turbine rotor having a predefined geometrical profile.

    摘要翻译: 提供了一种用于在制造和/或修理燃气涡轮叶片或整体叶片燃气轮机转子时将叶片接合到叶片根部或转子盘的方法。 供给要连接到叶片的叶片和叶片根部或转子盘,并且设置有要连接在一起的部分的增厚部。 要连接在一起的叶片和叶片根部或转子盘的部分被加工成形成凹部; c)然后相对于彼此对准,相对的凹部限定至少一个槽形接缝制备。 叶片和叶片根部或转子盘通过激光发电焊接在该接缝制备区域或每个接缝制备区域中接合,并且对加入的叶片和叶片根部或转子盘进行加工,以便提供燃气轮机叶片或 具有预定几何轮廓的整体叶片燃气轮机转子。