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1. 发明申请

US20070023392A1 Method for removing at least one area of a layer of a component consisting of metal or a metal compound 失效
标题翻译：用于去除由金属或金属化合物组成的组分的层的至少一个区域的方法
公开(公告)号：US20070023392A1
公开(公告)日：2007-02-01
申请号：US11541253
申请日：2006-09-29
申请人： Norbert Czech , Andre Jeutter , Adrian Kempster , Ralph Reiche , Rolf Wilkenhoner
发明人： Norbert Czech , Andre Jeutter , Adrian Kempster , Ralph Reiche , Rolf Wilkenhoner
IPC分类号： C03C25/68 , B08B7/00
CPC分类号： F01D5/288 , C23C10/30 , C23G5/00 , F01D5/005 , F05D2230/90
摘要： The invention relates to a method for removing an area of a layer of a component consisting of metal or a metal compound. According to prior art, corrosion products of a component are removed in a first step by applying a molten mass or by heating in a voluminous powder bed. This requires high temperatures or a large amount of space. The inventive method for removing corrosion products of a component is characterized in that a cleaning agent is applied locally, which removes the corrosion products by means of a gaseous reaction product.
摘要翻译：本发明涉及一种去除由金属或金属化合物组成的组分的层的面积的方法。根据现有技术，通过在大量粉末床中施加熔融物质或通过加热，在第一步骤中除去组分的腐蚀产物。这需要高温或大量的空间。用于除去组分的腐蚀产物的本发明的方法的特征在于，局部施加清洁剂，其通过气态反应产物除去腐蚀产物。

2. 发明授权

US07138065B2 Method for removing at least one area of a layer of a component consisting of metal or a metal compound 失效
标题翻译：用于去除由金属或金属化合物组成的组分的层的至少一个区域的方法
公开(公告)号：US07138065B2
公开(公告)日：2006-11-21
申请号：US10490567
申请日：2002-05-17
申请人： Norbert Czech , Andre Jeutter , Adrian Kempster , Ralph Reiche , Rolf Wilkenhöner
发明人： Norbert Czech , Andre Jeutter , Adrian Kempster , Ralph Reiche , Rolf Wilkenhöner
IPC分类号： B08B7/00
CPC分类号： F01D5/288 , C23C10/30 , C23G5/00 , F01D5/005 , F05D2230/90
摘要： The invention relates to a method for removing an area of a layer of a component consisting of metal or a metal compound. According to prior art, corrosion products of a component are removed in a first step by applying a molten mass or by heating in a voluminous powder bed. This requires high temperatures or a large amount of space. The inventive method for removing corrosion products of a component is characterized in that a cleaning agent is applied locally, which removes the corrosion products by means of a gaseous reaction product.
摘要翻译：本发明涉及一种去除由金属或金属化合物组成的组分的层的面积的方法。根据现有技术，通过在大量粉末床中施加熔融物质或通过加热，在第一步骤中除去组分的腐蚀产物。这需要高温或大量的空间。用于除去组分的腐蚀产物的本发明的方法的特征在于，局部施加清洁剂，其通过气态反应产物除去腐蚀产物。

3. 发明授权

US07429337B2 Method for removing at least one area of a layer of a component consisting of metal or a metal compound 失效
标题翻译：用于去除由金属或金属化合物组成的组分的层的至少一个区域的方法
公开(公告)号：US07429337B2
公开(公告)日：2008-09-30
申请号：US11541253
申请日：2006-09-29
申请人： Norbert Czech , Andre Jeutter , Adrian Kempster , Ralph Reiche , Rolf Wilkenhöner
发明人： Norbert Czech , Andre Jeutter , Adrian Kempster , Ralph Reiche , Rolf Wilkenhöner
IPC分类号： C03C25/68
CPC分类号： F01D5/288 , C23C10/30 , C23G5/00 , F01D5/005 , F05D2230/90
摘要： The invention relates to a method for removing an area of a layer of a component consisting of metal or a metal compound. According to prior art, corrosion products of a component are removed in a first step by applying a molten mass or by heating in a voluminous powder bed. This requires high temperatures or a large amount of space. The inventive method for removing corrosion products of a component is characterized in that a cleaning agent is applied locally, which removes the corrosion products by means of a gaseous reaction product.
摘要翻译：本发明涉及一种去除由金属或金属化合物组成的组分的层的面积的方法。根据现有技术，通过在大量粉末床中施加熔融物质或通过加热，在第一步骤中除去组分的腐蚀产物。这需要高温或大量的空间。用于除去组分的腐蚀产物的本发明的方法的特征在于，局部施加清洁剂，其通过气态反应产物除去腐蚀产物。

4. 发明授权

US06217668B1 Refurbishing of corroded superalloy or heat resistant steel parts 失效
标题翻译：腐蚀的超合金或耐热钢部件的翻新
公开(公告)号：US06217668B1
公开(公告)日：2001-04-17
申请号：US08190173
申请日：1994-01-31
申请人： Norbert Czech , Adrian Kempster
发明人： Norbert Czech , Adrian Kempster
IPC分类号： C23G102
CPC分类号： C23G5/00 , C23C10/60
摘要： A corroded superalloy or heat resistant steel part, in particular a gas turbine component like a gas turbine blade, having a surface with products or corrosion is refurbished. The invention the surface is cleaned, in particular mechanically or chemically, and an aluminide coating is applied to the cleaned surface. Subsequently, the aluminide coating is removed, whereby all products of corrosion which have still remained in the part to be refurbished are removed as well.
摘要翻译：被腐蚀的超合金或耐热钢部件，特别是具有产品或腐蚀表面的燃气轮机部件，如燃气轮机叶片被翻新。本发明特别是机械地或化学地清洁表面，并且将铝化物涂层施加到清洁表面上。随后，去除铝化物涂层，从而除去仍然保留在待翻新部分中的所有腐蚀产物。

5. 发明授权

US6139976A Article having a superalloy substrate and an enrichment layer placed thereon, and methods of its manufacturing 失效
标题翻译：具有超合金基材和富集层的制品及其制造方法
公开(公告)号：US6139976A
公开(公告)日：2000-10-31
申请号：US327008
申请日：1999-06-07
申请人： Norbert Czech , Knut Halberstadt , John Smith , Adrian Kempster
发明人： Norbert Czech , Knut Halberstadt , John Smith , Adrian Kempster
IPC分类号： C23C10/32 , C23C10/10 , C23C10/28 , C23C16/10 , C23C26/00 , B32B5/14 , C23C16/00 , F02C1/00
CPC分类号： C23C10/28 , C23C26/00 , Y10S428/938 , Y10S428/941 , Y10T428/12458 , Y10T428/12597 , Y10T428/12611 , Y10T428/12646 , Y10T428/12681 , Y10T428/1275 , Y10T428/12854 , Y10T428/12931 , Y10T428/12944
摘要： The invention relates to an article of manufacture comprising: a substrate composed of a superalloy containing chromium and a base element selected from the group consisting of iron, cobalt, and nickel; and an enrichment layer containing chromium and placed on the substrate. Therein, the enrichment layer comprises a continuous matrix composed of a gamma-phase solid solution of chromium in the base element. The invention also relates to the manufacture of such an article. The article may in particular be a gas turbine component.
摘要翻译：本发明涉及一种制品，包括：由含有铬的超级合金和选自铁，钴和镍的基体元素组成的基底; 和含有铬的富集层并置于基材上。其中，富集层包括由基体中的γ相的γ相固溶体构成的连续基体。本发明还涉及这种制品的制造。该制品可以特别地是燃气轮机部件。

6. 发明授权

US5599385A High temperature-resistant corrosion protection coating for a component, in particular a gas turbine component 失效
标题翻译：用于部件，特别是燃气轮机部件的高温耐腐蚀保护涂层
公开(公告)号：US5599385A
公开(公告)日：1997-02-04
申请号：US568017
申请日：1995-12-06
申请人： Norbert Czech , Friedhelm Schmitz
发明人： Norbert Czech , Friedhelm Schmitz
IPC分类号： C23C4/08 , C23C14/16 , C23C30/00 , C09D5/08 , C22C19/07
CPC分类号： C23C30/00 , C23C14/16 , C23C4/08 , Y10T428/31678
摘要： A protective coating resistant to corrosion at medium and high temperatures is applied on a nickel-based or cobalt-based superalloy component. The protective coating essentially consists of the following elements (in percent by weight): 25 to 40% nickel, 28 to 32% chromium, 7 to 9% aluminum, 1 to 2% silicon, 0.3 to 1% of at least one reactive element of the rare earths, at least 5% cobalt; and impurities, as well as selectively from 0 to 15% of at least one of the elements of the group consisting of rhenium, platinum, palladium, zirconium, manganese, tungsten, titanium, molybdenum, niobium, iron, hafnium, and tantalum. The total share of the elements of the group is from 0 to a maximum of 15% and a remainder of at least 5% cobalt. The component and the coating applied thereon have a ductile brittle transition temperature below 500.degree. C.
摘要翻译：在镍基或钴基超级合金部件上施加耐中性和高温腐蚀的保护涂层。保护涂层基本上由以下元素组成（重量百分数）：25-40％镍，28-32％铬，7-9％铝，1-2％硅，0.3-1％至少一种反应性元素的稀土，至少5％的钴; 和杂质，以及选自0至15％的由铼，铂，钯，锆，锰，钨，钛，钼，铌，铁，铪和钽组成的组中的至少一种元素。该组成份的总份数为0至最多15％，其余为钴至少5％。施加在其上的组分和涂层具有低于500℃的延性脆性转变温度。

7. 发明授权

US5582635A High temperature-resistant corrosion protection coating for a component in particular a gas turbine component 失效
标题翻译：特别是燃气轮机部件的高温耐腐蚀保护涂层
公开(公告)号：US5582635A
公开(公告)日：1996-12-10
申请号：US411459
申请日：1995-03-28
申请人： Norbert Czech , Friedhelm Schmitz
发明人： Norbert Czech , Friedhelm Schmitz
IPC分类号： C23C4/08 , C23C14/16 , C23C30/00 , C09D5/08 , B32B15/04 , C22C19/07
CPC分类号： C23C30/00 , C23C14/16 , C23C4/08 , Y10T428/31678
摘要： A protective coating resistant to corrosion at medium and high temperatures is applied on a nickel-based or cobalt-based superalloy component. The protective coating essentially consists of the following elements (in percent by weight): 25 to 40% nickel, 28 to 32% chromium, 7 to 9% aluminum, 1 to 2% silicon, 0.3 to 1% of at least one reactive element of the rare earths, at least 5% cobalt; and impurities, as well as selectively from 0 to 15% of at least one of the elements of the group consisting of rhenium, platinum, palladium, zirconium, manganese, tungsten, titanium, molybdenum, niobium, iron, hafnium, and tantalum. The total share of the elements of the group is from 0 to a maximum of 15% and a remainder of at least 5% cobalt. The component and the coating applied thereon have a ductile brittle transition temperature below 500.degree. C.
摘要翻译：在镍基或钴基超级合金部件上施加耐中性和高温腐蚀的保护涂层。保护涂层基本上由以下元素组成（重量百分数）：25-40％镍，28-32％铬，7-9％铝，1-2％硅，0.3-1％至少一种反应性元素的稀土，至少5％的钴; 和杂质，以及选自0至15％的由铼，铂，钯，锆，锰，钨，钛，钼，铌，铁，铪和钽组成的组中的至少一种元素。该组成份的总份数为0至最多15％，其余为钴至少5％。施加在其上的组分和涂层具有低于500℃的延性脆性转变温度。

8. 发明授权

US5401307A High temperature-resistant corrosion protection coating on a component, in particular a gas turbine component 失效
标题翻译：组件上的耐高温腐蚀保护涂层，特别是燃气轮机部件
公开(公告)号：US5401307A
公开(公告)日：1995-03-28
申请号：US82602
申请日：1993-06-25
申请人： Norbert Czech , Friedhelm Schmitz
发明人： Norbert Czech , Friedhelm Schmitz
IPC分类号： C23C4/08 , C23C14/16 , C23C30/00 , C09D5/08 , B32B15/04 , C22C19/07
CPC分类号： C23C4/08 , C23C14/16 , C23C30/00 , Y10T428/31678
摘要： A protective coating resistant to corrosion at medium and high temperatures is applied on a nickel-based or cobalt-based superalloy component. The protective coating essentially consists of the following elements (in percent by weight): 25 to 40% nickel, 28 to 32% chromium, 7 to 9% aluminum, 1 to 2% silicon, 0.3 to 1% of at least one reactive element of the rare earths, at least 5% cobalt; and impurities, as well as selectively from 0 to 15% of at least one of the elements of the group consisting of rhenium, platinum, palladium, zirconium, manganese, tungsten, titanium, molybdenum, niobium, iron, hafnium, and tantalum. The total share of the elements of the group is from 0 to a maximum of 15% and a remainder of at least 5% cobalt. The component and the coating applied thereon have a ductile brittle transition temperature below 500.degree. C.
摘要翻译：在镍基或钴基超级合金部件上施加耐中性和高温腐蚀的保护涂层。保护涂层基本上由以下元素组成（重量百分数）：25-40％镍，28-32％铬，7-9％铝，1-2％硅，0.3-1％至少一种反应性元素的稀土，至少5％的钴; 和杂质，以及选自0至15％的由铼，铂，钯，锆，锰，钨，钛，钼，铌，铁，铪和钽组成的组中的至少一种元素。该组成份的总份数为0至最多15％，其余为钴至少5％。施加在其上的组分和涂层具有低于500℃的延性脆性转变温度。

9. 发明申请

US20100266409A1 Method for Coating a Blade and Blade of a Gas Turbine 有权
标题翻译：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）。

10. 发明授权

US06575817B2 Process for treating the interior of a hollow component 失效
标题翻译：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。

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