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    Run-in coating for gas turbines and method for producing same
    2.
    发明申请
    Run-in coating for gas turbines and method for producing same 有权
    燃气轮机的润滑涂层及其制造方法

    公开(公告)号：US20090110560A1

    公开(公告)日：2009-04-30

    申请号：US10568394

    申请日：2004-07-28

    申请人： Erwin Bayer ,  Wilfried Smarsly

    发明人： Erwin Bayer ,  Wilfried Smarsly

    IPC分类号： F01D5/14 ,  B05D3/02 ,  C09D1/00 ,  B32B3/00

    CPC分类号： F01D11/122 ,  Y10T428/12389

    摘要： A run-in coating is for gas turbines. The run-in coating is used for sealing a radial gap between a housing of the gas turbine and rotating rotor blades of same, the run-in coating being applied onto the housing. The run-in coating is made of an intermetallic titanium-aluminum material.

    摘要翻译： 磨损涂层用于燃气轮机。 该外接涂层用于密封燃气涡轮机壳体与其旋转的转子叶片之间的径向间隙，该引入式涂层施加到壳体上。 导入涂层由金属间钛 - 铝材料制成。

    FORGED TiAl COMPONENTS, AND METHOD FOR PRODUCING SAME
    3.
    发明申请
    FORGED TiAl COMPONENTS, AND METHOD FOR PRODUCING SAME 审中-公开
    锻造TiAl组分及其制造方法

    公开(公告)号：US20140202601A1

    公开(公告)日：2014-07-24

    申请号：US14237929

    申请日：2012-08-09

    申请人： Dietmar Helm ,  Falko Heutling ,  Ulrike Habel ,  Wilfried Smarsly

    发明人： Dietmar Helm ,  Falko Heutling ,  Ulrike Habel ,  Wilfried Smarsly

    IPC分类号： C22F1/18 ,  C22C14/00

    CPC分类号： C22F1/183 ,  C22C14/00 ,  F01D5/28 ,  F05D2300/174

    摘要： The present invention relates to a method for producing forged components of a TiAl alloy, in particular turbine blades, wherein the components are forged and undergo a two-stage heat treatment after the forging process, the first stage of the heat treatment comprising a recrystallization annealing process for 50 to 100 minutes at a temperature below the γ/α transition temperature, and the second stage of the heat treatment comprising a stabilization annealing process in the temperature range of from 800° C. to 950° C. for 5 to 7 hrs, and the cooling rate during the first heat treatment stage being greater than or equal to 3° C./sec, in the temperature range between 1300° C. to 900° C.

    摘要翻译： 本发明涉及一种用于生产TiAl合金，特别是涡轮叶片的锻造部件的方法，其中锻件在锻造之后被锻造并进行两级热处理，第一阶段的热处理包括再结晶退火 在低于γ/α转变温度的温度下处理50至100分钟，第二阶段的热处理包括在800℃至950℃的温度范围内的稳定退火工艺5至7小时 在1300℃〜900℃的温度范围内，第一热处理阶段的冷却速度大于或等于3℃/秒。

    Method for the production of cast components
    6.
    发明申请
    Method for the production of cast components 有权
    铸件的生产方法

    公开(公告)号：US20070151696A1

    公开(公告)日：2007-07-05

    申请号：US10585978

    申请日：2004-12-22

    申请人： Manfred Renkel ,  Wilfried Smarsly

    发明人： Manfred Renkel ,  Wilfried Smarsly

    IPC分类号： B22D27/00 ,  B22D41/00

    CPC分类号： C22F1/183 ,  C22C1/02 ,  C22C14/00

    摘要： The invention relates to a method for the production of a cast component, in particular a gas turbine component. The inventive method comprises at least the following steps: a) a crucible and at least one semi-finished product is prepared from an intermetallic titanium-aluminium material; b) the or each semi-finished product made of intermetallic titanium-aluminium material is melted in the crucible; c) at least one additional element or an additional compound is added to the melt, whereby the or each element and/or the or each compound is introduced into the melt according to the melting temperature thereof; d) a casting mould is prepared; e) the casting mould is filled with the melt; f) the melt is solidified in the casting mould; g) the casting component is extracted from the casting mould.

    摘要翻译： 本发明涉及一种用于生产铸造部件，特别是燃气轮机部件的方法。 本发明的方法至少包括以下步骤：a）坩埚，并且从金属间钛 - 铝材料制备至少一种半成品; b）由金属间钛 - 铝材料制成的每个半成品在坩埚中熔化; c）将至少一种另外的元素或另外的化合物加入到熔体中，由此根据其熔融温度将这些或每种元素和/或每种化合物引入熔体中; d）制备铸模; e）铸模中填充有熔体; f）熔体在铸模中固化; g）铸造部件从铸模中取出。

    Component for a gas turbine and a method for the production of the component
    8.
    发明授权
    Component for a gas turbine and a method for the production of the component 有权
    用于燃气轮机的组件和用于生产组件的方法

    公开(公告)号：US08882442B2

    公开(公告)日：2014-11-11

    申请号：US12998411

    申请日：2009-10-14

    申请人： Wilfried Smarsly ,  Joachim Bamberg ,  Joerg Esslinger

    发明人： Wilfried Smarsly ,  Joachim Bamberg ,  Joerg Esslinger

    IPC分类号： F01D5/34 ,  B23K20/12 ,  B23P15/00

    CPC分类号： F01D5/34 ,  B23K20/1205 ,  B23K2101/001 ,  B23K2103/14 ,  B23P15/006 ,  F05B2230/239 ,  F05C2201/0466 ,  F05D2230/50 ,  F05D2300/133 ,  Y10T29/49336 ,  Y10T29/49337 ,  Y10T29/49968

    摘要： A component for a gas turbine, especially a blisk or a bling, whereby the component includes a rotor base (12) made of a high temperature-resistant nickel alloy and a plurality of turbine blades (14) joined to the rotor base, whereby each turbine blade includes a rotor blade (16) made of a titanium alloy and a blade root. The blade root is configured as an adapter element (18) that is made of a material that can be welded to the titanium alloy as well as to the high temperature-resistant nickel alloy and that is integrally joined to the rotor base (12) and to the rotor blade (16) fusion. A method for the production of the component is also described.

    摘要翻译： 一种用于燃气轮机的部件，特别是叶片或叶片，其中部件包括由耐高温镍合金制成的转子基座（12）和与转子基座接合的多个涡轮机叶片（14），由此 涡轮叶片包括由钛合金和叶片根部制成的转子叶片（16）。 叶片根部被配置为由能够焊接到钛合金以及耐高温镍合金并且与转子基座（12）整体接合的材料制成的适配器元件（18），并且 到转子叶片（16）的融合。 还描述了用于制造组件的方法。

    MATERIAL FOR COMPONENTS OF A GAS TURBINE
    9.
    发明申请
    MATERIAL FOR COMPONENTS OF A GAS TURBINE 有权
    气体涡轮机组件的材料

    公开(公告)号：US20090202381A1

    公开(公告)日：2009-08-13

    申请号：US12158202

    申请日：2006-12-15

    申请人： Wilfried Smarsly ,  Gerhard Sauthoff

    发明人： Wilfried Smarsly ,  Gerhard Sauthoff

    IPC分类号： C22C38/18 ,  F01D25/00 ,  C22C38/06 ,  C22C30/00

    CPC分类号： C22C38/18 ,  C22C38/002 ,  C22C38/005 ,  C22C38/06 ,  C22C38/12

    摘要： The presently described technology relates to a material for components of a gas turbine, in particular for components of a gas turbine aircraft engine, having a matrix of an iron-based alloy material, wherein the matrix of the iron-based alloy material being hardened by means of an intermetallic material of the Laves phase.

    摘要翻译： 目前描述的技术涉及一种用于燃气涡轮机的部件的材料，特别是用于具有铁基合金材料的基体的燃气涡轮机飞机发动机的部件，其中铁基合金材料的基体被 Laves相的金属间化合物的手段。

    Method for Producing a Cast Component
    10.
    发明申请
    Method for Producing a Cast Component 有权
    生产铸件的方法

    公开(公告)号：US20070261813A1

    公开(公告)日：2007-11-15

    申请号：US11632774

    申请日：2005-07-16

    申请人： Manfred Renkel ,  Wilfried Smarsly

    发明人： Manfred Renkel ,  Wilfried Smarsly

    IPC分类号： B22D23/06

    CPC分类号： B22D23/06 ,  B22D21/005 ,  B22D21/007 ,  B22D27/15 ,  B22D39/02

    摘要： The invention relates to a method for producing a cast component, particularly a gas turbine component, by casting. According to the invention, the method comprises at least the following steps: a) preparing a melting crucible; b) preparing a semifinished granular material from an intermetallic titanium/aluminum material; c) filling the melting crucible with the semifinished granular material, whereby the quantity of the semifinished granular material placed inside the melting crucible corresponds to the quantity necessary for casting the component; d) melting the semifinished granular material made of the intermetallic titanium/aluminum material inside the melting crucible; e) preparing a casting mold; f) pouring the melt into the casting mold; g) solidifying the melt inside the casting mold, and; h) removing the cast component from the casting mold.

    摘要翻译： 本发明涉及通过铸造生产铸件，特别是燃气轮机件的方法。 根据本发明，该方法至少包括以下步骤：a）制备熔化坩埚; b）从金属间钛/铝材料制备半成品颗粒材料; c）用半成品颗粒材料填充熔化的坩埚，由此放置在熔化坩埚内部的半成品颗粒材料的量相当于铸造组分所需的量; d）在熔融坩埚内熔化由金属间钛/铝材料制成的半成品粒状材料; e）制备铸模; f）将熔体倒入铸模中; g）固化铸模内部的熔体， h）从铸模中去除铸造组件。