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1.发明授权Protective coating for application to a substrate and method for manufacturing a protective coating 失效用于基材的保护涂层和用于制造保护涂层的方法公开(公告)号：US07422769B2
公开(公告)日：2008-09-09
申请号：US11181284
申请日：2005-07-14
CPC分类号： C23C4/18 , C23C4/12 , C23C10/02 , Y02T50/67 , Y10T428/12458 , Y10T428/12611 , Y10T428/12931
摘要： A refractory, oxidation-resistant, and corrosion-resistant protective coating for application to a substrate, in particular for application to parts of turbines or aircraft propulsion engines, is described, including a spray coating made of a thermally sprayed, primarily metallic material, the coating being at least partially subjected to a thermochemical aluminum (Cr, Si) deposition process having a specifically high aluminum deposition activity after the application of the protective coating to the substrate, in such a way that the protective coating has alloy gradients of Al (Cr, Si) which increase from the substrate surface to the coating surface and isolated globulitic metal oxide particles. Furthermore, a method for manufacturing this protective coating and its use are described.
摘要翻译： 描述了一种适用于基材，特别是用于涡轮机或飞机推进发动机的部件的耐火，耐氧化和耐腐蚀的保护涂层，包括由喷涂的主要金属材料制成的喷涂， 涂层至少部分地经受在将保护涂层施加到基底之后具有特别高的铝沉积活性的热化学铝（Cr，Si）沉积工艺，使得保护涂层具有Al（Cr ，Si），其从衬底表面增加到涂层表面和分离的球状金属氧化物颗粒。 此外，描述了制造该保护涂层的方法及其用途。
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2.发明申请Protective coating for application to a substrate and method for manufacturing a protective coating 失效用于基材的保护涂层和用于制造保护涂层的方法公开(公告)号：US20060292390A1
公开(公告)日：2006-12-28
申请号：US11181284
申请日：2005-07-14
CPC分类号： C23C4/18 , C23C4/12 , C23C10/02 , Y02T50/67 , Y10T428/12458 , Y10T428/12611 , Y10T428/12931
摘要： A refractory, oxidation-resistant, and corrosion-resistant protective coating for application to a substrate, in particular for application to parts of turbines or aircraft propulsion engines, is described, including a spray coating made of a thermally sprayed, primarily metallic material, the coating being at least partially subjected to a thermochemical aluminum (Cr, Si) deposition process having a specifically high aluminum deposition activity after the application of the protective coating to the substrate, in such a way that the protective coating has alloy gradients of Al (Cr, Si) which increase from the substrate surface to the coating surface and isolated globulitic metal oxide particles. Furthermore, a method for manufacturing this protective coating and its use are described.
摘要翻译： 描述了一种适用于基材，特别是用于涡轮机或飞机推进发动机的部件的耐火，耐氧化和耐腐蚀的保护涂层，包括由喷涂的主要金属材料制成的喷涂， 涂层至少部分地经受在将保护涂层施加到基底之后具有特别高的铝沉积活性的热化学铝（Cr，Si）沉积工艺，使得保护涂层具有Al（Cr ，Si），其从衬底表面增加到涂层表面和分离的球状金属氧化物颗粒。 此外，描述了制造该保护涂层的方法及其用途。
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公开(公告)号：US07294361B2
公开(公告)日：2007-11-13
申请号：US10250974
申请日：2002-01-09
IPC分类号： C23C16/00
摘要： A process for gas diffusion coating of metallic components; in which a component surface which is to be coated is brought into contact with a metal halide as coating gas, to form a diffusion layer with a defined layer thickness and a defined coating metal content in % by weight in the component surface, working on the basis of a nominal concentration of the metal halide at the component surface which, at a defined coating temperature, leads to a defined coating time, wherein a first concentration, which is higher than the nominal concentration, for the metal halide is established for a first time, and at least one second concentration, which is at or below the nominal concentration, is established at the component surface for at least one second time, the first and the at least one second time being selected in such a way that their sum is shorter than the coating time with the nominal concentration. Also disclosed is a device for the process.
摘要翻译： 一种金属部件的气体扩散涂覆工艺; 将要被涂覆的组分表面与作为涂覆气体的金属卤化物接触，以形成具有限定的层厚度的限定涂层金属含量和在组分表面中的重量％的限定涂层金属含量，在 在组分表面处的金属卤化物的标称浓度的基础，其在限定的涂布温度下导致限定的涂布时间，其中为第一种金属卤化物建立高于标称浓度的第一浓度 时间，并且处于或低于标称浓度的至少一个第二浓度在组分表面处建立至少一秒钟，第一和至少一个第二时间被选择为使得它们的和为 比标称浓度的涂布时间短。 还公开了用于该过程的装置。
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公开(公告)号：US20130139852A1
公开(公告)日：2013-06-06
申请号：US13816910
申请日：2011-08-06
摘要： A method for removing a layer made of a first material from a surface of a body made of a second material is disclosed. The body is subjected to a pressurized jet containing a blasting medium composed of particles, where the pressurized jet at least intermittently has an Almen intensity of at most 0.35 Almen A, preferably at most 0.3 Almen A and particularly preferably at most 0.25 Almen A.
摘要翻译： 公开了一种从由第二材料制成的主体表面去除由第一材料制成的层的方法。 经受包含由颗粒组成的喷射介质的加压射流，其中加压射流至少间歇地具有至多0.35Almen A的Almen强度，优选至多0.3Almen A，特别优选至多0.25 Almen A.
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5.发明申请公开(公告)号：US20110058952A1
公开(公告)日：2011-03-10
申请号：US12877018
申请日：2010-09-07
CPC分类号： F01D5/288 , C23C10/06 , C23C10/08 , C23C10/10 , Y02T50/671
摘要： A method for producing a high-temperature protective layer containing metal on a metallic high-temperature material is disclosed. The metal is deposited on the high-temperature material via the gaseous phase to form the high-temperature protective layer. The high-temperature material is held at a diffusion temperature for a specific length of time so that at least a portion of the deposited metal is diffused into the high temperature material to form a diffusion zone and where the high-temperature material is not in contact with solids or liquids in the region of the surface to be coated, but merely has a solid/gas interface. Also disclosed is a component made of a high-temperature material with a hot-gas anti-corrosive layer containing chromium. There is a coating layer containing chromium applied to the surface of the high-temperature material, a diffusion layer in the high-temperature material, and a build-up zone between the coating layer and the diffusion layer.
摘要翻译： 公开了一种在金属高温材料上生产含有金属的高温保护层的方法。 金属通过气相沉积在高温材料上，形成高温保护层。 将高温材料在扩散温度下保持特定长度的时间，使得沉积的金属的至少一部分扩散到高温材料中以形成扩散区，并且其中高温材料不接触 在待涂覆表面的区域中具有固体或液体，但仅具有固体/气体界面。 还公开了由具有含有铬的热气体防腐蚀层的高温材料制成的部件。 在高温材料的表面上涂布含有铬的涂层，高温材料中的扩散层，以及涂层与扩散层之间的积聚区域。
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6.发明申请COATING FOR GAS TURBINE COMPONENTS, AND METHOD AND DEVICE FOR PROVIDING A COATING 审中-公开用于气体涡轮机组件的涂料，以及用于提供涂料的方法和装置公开(公告)号：US20100098971A1
公开(公告)日：2010-04-22
申请号：US12527823
申请日：2008-02-14
CPC分类号： C23C10/02 , C23C16/08 , C23C16/4488 , C23C28/021 , C23C28/023 , C23C28/028 , F01D5/288 , F05D2230/90 , Y10T428/12944
摘要： A coating, in particular for gas turbine components produced of a superalloy, is disclosed. The coating has an outer layer and an inner layer. The outer layer constitutes 10% to 60% of the overall coating and is substantially made of a β-NiAl phase having an Al proportion between 23 and 35 percent by weight. The inner layer constitutes 90% to 40% of the overall coating and is substantially made of a γ-NiAl phase having an Al proportion of a maximum of 15 percent by weight.
摘要翻译： 公开了一种涂层，特别是用于由超级合金制造的燃气轮机部件。 涂层具有外层和内层。 外层构成整个涂层的10％至60％，并且基本上由具有23至35重量％之间的Al比例的Ni-Al相制成。 内层构成整个涂层的90％至40％，并且基本上由Al比例最大为15重量％的γ-NiAl相制成。
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公开(公告)号：US09333623B2
公开(公告)日：2016-05-10
申请号：US13816910
申请日：2011-08-06
摘要： A method for removing a layer made of a first material from a surface of a body made of a second material is disclosed. The body is subjected to a pressurized jet containing a blasting medium composed of particles, where the pressurized jet at least intermittently has an Almen intensity of at most 0.35 Almen A, preferably at most 0.3 Almen A and particularly preferably at most 0.25 Almen A.
摘要翻译： 公开了一种从由第二材料制成的主体表面去除由第一材料制成的层的方法。 经受包含由颗粒组成的喷射介质的加压射流，其中加压射流至少间歇地具有至多0.35Almen A的Almen强度，优选至多0.3Almen A，特别优选至多0.25 Almen A.
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公开(公告)号：US06709711B1
公开(公告)日：2004-03-23
申请号：US09485082
申请日：2000-04-19
申请人： Gerhard Wydra , Martin Thoma , Horst Pillhoefer
发明人： Gerhard Wydra , Martin Thoma , Horst Pillhoefer
IPC分类号： B05D136
摘要： The invention is directed to a method for producing a corrosion-resistant and oxidization-resistant layer that is applied onto a component part, whereby the method can be simply and cost-beneficially implemented in fabrication-oriented terms and comprises the steps: a) producing a slip by mixing powder containing at least one of the elements Cr, Ni or Ce with a binding agent; b) applying the slip onto the component part; c) drying the slip at temperatures from room temperature through 300° C.; and d) alitizing the slip layer.
摘要翻译： 本发明涉及一种用于制造施加到部件上的耐腐蚀和耐氧化层的方法，由此该方法可以以制造为导向的术语简单且成本有益地实现，并且包括以下步骤：a） 将含有至少一种元素Cr，Ni或Ce的粉末与粘合剂混合的粉末; b）将所述滑移物施加到所述组分部分上; c）在室温至300℃的温度下干燥所述滑移物; andd）使滑动层疏通。
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公开(公告)号：US4878952A
公开(公告)日：1989-11-07
申请号：US243424
申请日：1988-09-12
申请人： Horst Pillhoefer
发明人： Horst Pillhoefer
IPC分类号： C22F1/10
CPC分类号： C22F1/10
摘要： Cast structural components of nickel alloys are heat treated by heating to a temperature above the incipient melting temperature of the carbidic .gamma./.gamma.' eutectic phase, whereby homogenizing and complete solution annealing of the material structure is acheived. Thereafter, the resultant fusion pores are closed at low temperature.
摘要翻译： 将镍合金的铸造结构部件通过加热至高于碳化γ/γ'共晶相的初始熔融温度的温度进行热处理，从而实现材料结构的均化和完全固溶退火。 此后，所得的熔融孔在低温下封闭。
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公开(公告)号：US10006298B2
公开(公告)日：2018-06-26
申请号：US12877007
申请日：2010-09-07
申请人： Heinrich Walter , Horst Pillhoefer , Michael Strasser , Karlheinz Manier , Max Morant , Richard Lange
发明人： Heinrich Walter , Horst Pillhoefer , Michael Strasser , Karlheinz Manier , Max Morant , Richard Lange
CPC分类号： F01D5/288 , C23C10/32 , F01D5/3092 , F01D25/007 , F05D2300/132 , Y10T29/49337
摘要： A method for coating a turbine blade of a gas turbine is disclosed. The method includes applying a lacquer coat to a region of the turbine blade, where the lacquer coat includes chromium particles and/or chromium alloy particles, halides, and a binding agent. The method further includes drying the applied lacquer coat at a temperature between 50° C. and 600° C. with disintegration of the binding agent and subsequent reactive connection at a temperature between 900° C. and 1160° C.
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