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    Method for Coating a Blade and Blade of a Gas Turbine
    1.
    发明申请
    Method for Coating a Blade and Blade of a Gas Turbine 有权
    燃气轮机叶片涂层方法

    公开(公告)号：US20100266409A1

    公开(公告)日：2010-10-21

    申请号：US12086511

    申请日：2006-12-12

    申请人： Sharad Chandra ,  Norbert Czech

    发明人： Sharad Chandra ,  Norbert Czech

    IPC分类号： F01D5/18 ,  C23C16/06 ,  C23C4/06 ,  C23C28/02

    CPC分类号： C23C10/14 ,  C23C4/073 ,  C23C4/18 ,  C23C10/08 ,  C23C10/60 ,  C23C14/025 ,  C23C14/028 ,  C23C14/083 ,  C23C14/30 ,  C23C28/3215 ,  C23C28/322 ,  C23C28/325 ,  C23C28/3455 ,  C23C30/00 ,  F01D5/187 ,  F01D5/288 ,  F05D2230/312 ,  F05D2300/132 ,  F05D2300/21

    摘要： A method is provided for coating a hollow, internally cooled blade (1) of a gas turbine, in which method an outer coating (5) comprising an MCrAlY-based bonding layer (6) and a ceramic thermal barrier layer (9) of zirconium oxide is applied to the base material (3) of the blade (1) on the outer side of the blade (1) and an inner coating (4) comprising a Cr diffusion layer (7) is applied to the base material (3) of the blade (1) on the inner side of the blade (1). The MCrAlY-based bonding layer (6) is thereby applied to the finished blade (1). At the same time, along with the inner coating (4), the Cr diffusion layer (7) is also applied to the MCrAlY-based bonding layer (6) of the outer coating (5) by chemical vapour deposition. Subsequently, an Al diffusion layer (8) and an outer brittle Al build-up layer are applied by chemical vapour deposition to the bonding layer (6) coated with the Cr diffusion layer (7). After that, the outer brittle Al build-up layer is removed by an abrasive treatment and the ceramic thermal barrier layer (9) is applied to the Al diffusion layer (8).

    摘要翻译： 提供了一种用于涂覆燃气轮机的中空的内部冷却的叶片（1）的方法，其中包括基于MCrAlY的结合层（6）和锆的陶瓷热障层（9）的外涂层（5） 氧化物施加到叶片（1）的外侧上的叶片（1）的基材（3）上，并且将包含Cr扩散层（7）的内涂层（4）施加到基材（3）上， （1）的内侧。 由此将MCrAlY基接合层（6）施加到成品刀片（1）上。 同时，与内涂层（4）一起，通过化学气相沉积也将Cr扩散层（7）施加到外涂层（5）的MCrAlY基结合层（6）上。 随后，通过化学气相沉积将Al扩散层（8）和外部脆性Al累积层施加到涂覆有Cr扩散层（7）的接合层（6）。 之后，通过研磨处理去除外部脆性Al堆积层，并将陶瓷热障层（9）施加到Al扩散层（8）。

    Process for treating the interior of a hollow component
    2.
    发明授权
    Process for treating the interior of a hollow component 失效
    处理中空部件内部的方法

    公开(公告)号：US06575817B2

    公开(公告)日：2003-06-10

    申请号：US09814491

    申请日：2001-03-21

    申请人： Norbert Czech

    发明人： Norbert Czech

    IPC分类号： B24B3100

    CPC分类号： F01D5/288 ,  B23P2700/06 ,  B24B31/116 ,  C23F3/00 ,  F01D5/186

    摘要： A process for machining the interior of a hollow component for high-temperature application is described. The component has a base body made from a base material, and is in particular a blade of a gas turbine. The component has a cavity, in particular cooling channels for cooling air to flow through, which is provided with an internal coating. According to the process, a treating fluid flows through the cavity, solid particles with an abrasive action being added to the treating fluid.

    摘要翻译： 描述了用于加工用于高温应用的中空部件的内部的工艺。 该部件具有由基材制成的基体，特别是燃气轮机的叶片。 该部件具有空腔，特别是用于冷却空气流过的冷却通道，其设置有内部涂层。 根据该方法，处理流体流过空腔，将具有研磨作用的固体颗粒加入到处理流体中。

    Highly corrosion and/or oxidation-resistant protective coating containing rhenium
    5.
    发明授权
    Highly corrosion and/or oxidation-resistant protective coating containing rhenium 失效
    含有铼的高度腐蚀和/或抗氧化保护涂层

    公开(公告)号：US5273712A

    公开(公告)日：1993-12-28

    申请号：US841987

    申请日：1992-02-26

    申请人： Norbert Czech ,  Friedhelm Schmitz

    发明人： Norbert Czech ,  Friedhelm Schmitz

    IPC分类号： C22C19/00 ,  C23C30/00 ,  C22C38/18 ,  C22C19/05 ,  C22C19/07 ,  C22C30/00

    CPC分类号： C22C19/00 ,  C23C30/00

    摘要： A method of protecting and a protective coating for metal components formed of nickel or cobalt-based superalloys are disclosed. The protective coating essentially consists of the following constituents (in percent by weight):1 to 20% rhenium,15 to 50% chromium,0 to 15% aluminum, the share of chromium and aluminum taken together being at least 25% and at most 53%,0.3 to 2% in total of at least one reactive element from the group consisting of the rare earths, and0 to 3% silicon, impurities, as well as the following elective components:0 to 5% hafnium,0 to 12% tungsten,0 to 10% manganese,0 to 15% tantalum,0 to 5% titanium,0 to 4% niobium, and0 to 2% zirconium,the total share of the elective components being from 0 to a maximum of 15%, and a remainder primarily being at least one of the elements iron, nickel, and cobalt. The protective coating is primarily suited for use with metal components in gas turbines and aircraft engines.

    摘要翻译： 公开了一种用于由镍或钴基超级合金形成的金属部件的保护和保护涂层的方法。 保护涂层基本上由以下成分组成（以重量百分比计）：1至20％的铼，15至50％的铬，0至15％的铝，所占的铬和铝的比例至少为25％ 53％，至少一种来自稀土元素的反应性元素和0-3％硅，杂质以及以下选择成分的总和为0.3至2％：0至5％的铪，0至12 ％钨，0〜10％的锰，0〜15％的钽，0〜5％的钛，0〜4％的铌，0〜2％的锆，选择性成分的总量为0〜15％ ，其余主要是铁，镍和钴中的至少一种元素。 保护涂层主要适用于燃气轮机和飞机发动机中的金属部件。

    Heat-insulating protective layer for a component located within the hot gas zone of a gas turbine
    7.
    发明授权
    Heat-insulating protective layer for a component located within the hot gas zone of a gas turbine 有权
    位于燃气轮机热气区内的部件的隔热保护层

    公开(公告)号：US09139896B2

    公开(公告)日：2015-09-22

    申请号：US12084726

    申请日：2006-11-07

    申请人： Sharad Chandra ,  Norbert Czech

    发明人： Sharad Chandra ,  Norbert Czech

    IPC分类号： B32B15/00 ,  C23C10/02 ,  C23C28/00

    CPC分类号： C23C10/02 ,  C23C28/321 ,  C23C28/3215 ,  C23C28/325 ,  C23C28/345 ,  C23C28/3455 ,  Y10T428/31678

    摘要： Disclosed is a heat-insulating protective layer for a component located within the hot gas zone of a gas turbine. Said protective layer is composed of an adhesive layer, a diffusion layer, and a ceramic layer which is applied to the high temperature-resistant basic metal of the component. The adhesive layer comprises a metal alloy [MCrAlY (M=Ni, Co)] containing Ni, Co, Cr, Al, Y, the diffusion layer is produced by calorizing the adhesive layer, and the ceramic layer is composed of ZrO2 which is partially stabilized by means of yttrium oxide. One or several chemical metal elements that have a large atomic diameter and are selected among the group comprising Re, W, Si, Hf, and/or Ta are alloyed to the material of the adhesive layer. The adhesive layer has the following chemical composition after being applied: Co 15 to 30 percent, Cr 15 to 25 percent, Al 6 to 13 percent, Y 0.2 to 0.7 percent, Re up to 5 percent, W up to 5 percent, Si up to 3 percent, Hf up to 3 percent, Ta up to 5 percent, the remainder being composed of Ni.

    摘要翻译： 公开了一种用于位于燃气轮机的热气区内的部件的绝热保护层。 所述保护层由施加到所述部件的耐高温碱性金属的粘合剂层，扩散层和陶瓷层构成。 粘合剂层包含含有Ni，Co，Cr，Al，Y的金属合金[MCrAlY（M = Ni，Co）]，扩散层通过加热粘合剂层而产生，陶瓷层由部分地由ZrO 2组成 通过氧化钇稳定。 具有大原子直径并且选自Re，W，Si，Hf和/或Ta的组中的一种或几种化学金属元素与粘合剂层的材料合金化。 粘合剂层在施用后具有以下化学组成：Co 15〜30％，Cr 15〜25％，Al 6〜13％，Y 0.2〜0.7％，Re：5％以下，W：5％以上，Si： 至3％，Hf高达3％，Ta高达5％，其余由Ni组成。

    Method For Applying A Protective Layer, Component Coated With A Protective Layer, And Gas Turbine Comprising Such A Component
    8.
    发明申请
    Method For Applying A Protective Layer, Component Coated With A Protective Layer, And Gas Turbine Comprising Such A Component 审中-公开
    用于涂覆保护层的方法，涂覆有保护层的组分和包含这种组分的燃气轮机

    公开(公告)号：US20140141276A1

    公开(公告)日：2014-05-22

    申请号：US14122495

    申请日：2012-05-31

    申请人： Norbert Czech ,  Sharad Chandra ,  Roland Herzog

    发明人： Norbert Czech ,  Sharad Chandra ,  Roland Herzog

    IPC分类号： F01D5/28 ,  C23C4/12 ,  C23C4/10

    CPC分类号： F01D5/288 ,  C23C4/02 ,  C23C4/10 ,  C23C4/134 ,  C23C4/18 ,  C23C10/02 ,  C23C10/60 ,  Y10T428/12611

    摘要： A method for applying a protective layer resistant to high-temperature degradation by corrosion and erosion to a base metal, comprises: applying a MCrAlY-based bond layer to the base metal; coating, by overaluminizing with an Al diffusion layer, the bond layer; subjecting the Al diffusion layer (14) to abrasion treatment so that an outer build-up layer is removed from the Al diffusion layer; and applying a ceramic thermal barrier coating of yttria partially stabilized zirconia to the remaining Al diffusion layer. The ceramic thermal barrier coating is applied to the remaining Al diffusion layer by air plasma spraying. The applied bond layer is subjected to a polishing treatment before being overaluminized such that a surface roughness of Ra≦2 μm is produced at the bond layer.

    摘要翻译： 一种通过腐蚀和腐蚀对基底金属施加耐高温劣化的保护层的方法包括：将MCrAlY基接合层施加到母材上; 通过用Al扩散层过度镀覆所述接合层; 对Al扩散层（14）进行磨损处理，从而从Al扩散层除去外积层; 以及将氧化钇部分稳定的氧化锆的陶瓷热障涂层施加到剩余的Al扩散层。 通过空气等离子体喷涂将陶瓷热障涂层施加到剩余的Al扩散层。 施加的接合层在被过度光化之前进行抛光处理，使得在接合层处产生Ra＆lt; NlE;2μm的表面粗糙度。