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1. 发明授权

US08309232B2 Running-in coating for gas turbines and method for production thereof 有权
标题翻译：用于燃气轮机的运行涂层及其生产方法
公开(公告)号：US08309232B2
公开(公告)日：2012-11-13
申请号：US10581147
申请日：2004-11-12
申请人： Manfred A. Daeubler , Klaus Schweitzer
发明人： Manfred A. Daeubler , Klaus Schweitzer
IPC分类号： B32B15/01 , B32B15/00 , F01D25/00
CPC分类号： C23C4/02 , C23C4/06 , C23C30/00 , Y10T428/12063 , Y10T428/12861 , Y10T428/12937 , Y10T428/12944
摘要： A running-in coating for gas turbines and a method for production of a running-in coating are provided. The running-in coating serves to seal a radial gap between a housing (11) of the gas turbine and the rotating blades (10) themselves, whereby the running-in coating (13) is applied to the housing. The running-in coating is made from a CoNiCrAIY-hBN material. The CoNiCrAIY-hBN material can be applied by thermal spraying, in particular plasma spraying.
摘要翻译：提供了用于燃气轮机的流入式涂层和用于生产流入式涂层的方法。运行的涂层用于密封燃气涡轮机的壳体（11）与旋转叶片（10）本身之间的径向间隙，由此将进入的涂层（13）施加到壳体。进入涂层由CoNiCrAIY-hBN材料制成。 CoNiCrAIY-hBN材料可以通过热喷涂，特别是等离子体喷涂来应用。

2. 发明申请

US20080282933A1 Running-In Coating for Gas Turbines and Method for Production Thereof 有权
标题翻译：燃气轮机运行涂层及其生产方法
公开(公告)号：US20080282933A1
公开(公告)日：2008-11-20
申请号：US10581147
申请日：2004-11-12
申请人： Manfred A. Daeubler , Klaus Schweitzer
发明人： Manfred A. Daeubler , Klaus Schweitzer
IPC分类号： C23C30/00 , C23C4/06 , C23C4/02
CPC分类号： C23C4/02 , C23C4/06 , C23C30/00 , Y10T428/12063 , Y10T428/12861 , Y10T428/12937 , Y10T428/12944
摘要： A running-in coating for gas turbines and a method for production of a running-in coating are provided. The running-in coating serves to seal a radial gap between a housing (11) of the gas turbine and the rotating blades (10) themselves, whereby the running-in coating (13) is applied to the housing. The running-in coating is made from a CoNiCrAIY-hBN material. The CoNiCrAIY-hBN material can be applied by thermal spraying, in particular plasma spraying.
摘要翻译：提供了用于燃气轮机的流入式涂层和用于生产流入式涂层的方法。运行的涂层用于密封燃气涡轮机的壳体（11）与旋转叶片（10）本身之间的径向间隙，由此将进入的涂层（13）施加到壳体。进入涂层由CoNiCrAIY-hBN材料制成。 CoNiCrAIY-hBN材料可以通过热喷涂，特别是等离子体喷涂来应用。

3. 发明授权

US5232789A Structural component with a protective coating having a nickel or cobalt basis and method for making such a coating 失效
标题翻译：具有镍或钴基保护层的结构部件和制造这种涂层的方法
公开(公告)号：US5232789A
公开(公告)日：1993-08-03
申请号：US845763
申请日：1992-03-02
申请人： Albin Platz , Klaus Schweitzer , Peter Adam
发明人： Albin Platz , Klaus Schweitzer , Peter Adam
IPC分类号： C23C4/10 , C23C4/18 , C23C30/00 , F01D5/28
CPC分类号： F01D5/288 , C23C30/00 , C23C4/10 , C23C4/18 , Y10S428/937 , Y10T428/12646 , Y10T428/12931
摘要： A structural component made of a base metal composition on a nickel or cobalt basis is provided with a protective coating against oxidation, corrosion, and thermal fatigue. The protective coating and the base metal are made of chemically the same or identical material, whereby the bonding of the protective coating is increased, the tendency to crack is reduced, and the resistance to thermal fatigue is improved. The grain size of the coating is substantially smaller than the grain size of the base metal composition.
摘要翻译：由基于镍或钴的贱金属组合物制成的结构部件具有防氧化，腐蚀和热疲劳的保护涂层。保护涂层和母材由化学相同或相同的材料制成，由此保护涂层的粘结增加，裂纹的倾向减小，耐热疲劳性得到改善。涂层的晶粒尺寸显着小于贱金属组合物的晶粒尺寸。

4. 发明授权

US07178808B2 Layer system for the rotor/stator seal of a turbomachine 有权
标题翻译：涡轮机转子/定子密封层系统
公开(公告)号：US07178808B2
公开(公告)日：2007-02-20
申请号：US10456959
申请日：2003-06-09
申请人： Richard Grunke , Lothar Peichl , Klaus Schweitzer
发明人： Richard Grunke , Lothar Peichl , Klaus Schweitzer
IPC分类号： F16J15/447
CPC分类号： C23C28/3215 , C23C28/3455 , C23C28/36 , F01D11/122 , F05D2230/90 , F05D2300/2118 , F05D2300/506 , F05D2300/611 , Y02T50/67
摘要： A layer system for the rotor/stator seal of a turbomachine, in particular of a gas turbine, is applied to a metallic component and can be run in with respect to a further component which can move relative to the metallic component, which, in order to improve the service life and run-in properties, is characterized by a bonding layer which is applied to the metallic component and a run-in coating which is applied to the bonding layer and comprises at least two layers, the first layer, which adjoins the bonding layer, being harder than the second layer, and the second layer having run-in properties.
摘要翻译：用于涡轮机，特别是燃气轮机的转子/定子密封件的层系统被施加到金属部件，并且可以相对于可相对于金属部件移动的另一部件运行，顺序为了提高使用寿命和磨合性能，其特征在于：施加到金属部件的接合层和施加到接合层并且包括至少两层的延伸涂层，第一层邻接所述粘结层比所述第二层硬，所述第二层具有磨合特性。

5. 发明授权

US06737110B1 Method for producing a heat insulating layer 失效
标题翻译：绝热层的制造方法
公开(公告)号：US06737110B1
公开(公告)日：2004-05-18
申请号：US09868447
申请日：2001-11-30
申请人： Ralf Stolle , Thomas Cosack , Klaus Schweitzer , Michael Pulver , Georg Wahl
发明人： Ralf Stolle , Thomas Cosack , Klaus Schweitzer , Michael Pulver , Georg Wahl
IPC分类号： C23C1640
CPC分类号： C23C16/405
摘要： A process for producing a thermal barrier coating, in which organometal complexes of zirconium and at least one stabilizing element selected from the group of the alkaline earth metals or rare earths are provided as starting substances, the starting substances are evaporated by heating and the coating gases that are generated in this manner are transported to a component to be coated, which is heated at a deposition temperature, where they are broken down so that a layer is deposited, in which process, in order to produce a thermal barrier coating with a columnar structure and a sufficient layer thickness, the starting substances are heated, at a process pressure of 0.5 to 50 mbar, to at most 250° C. so that the coating gases are formed, and the coating gases are transported to the component to be coated, the surface of which is heated at a deposition temperature of between 300° C. and 1100° C.
摘要翻译：提供了一种制备热障涂层的方法，其中提供锆和选自碱土金属或稀土族中的至少一种稳定元素的有机金属络合物作为起始物质，起始物质通过加热蒸发，并且涂覆气体以这种方式产生的被传送到待涂覆的部件，其在沉积温度下被加热，在那里它们被分解，使得沉积一层，以便在其中生产具有柱状的热障涂层结构和足够的层厚度，起始物质以0.5至50毫巴的加工压力加热至至多250℃，从而形成涂覆气体，并将涂覆气体输送到待涂覆的部件，其表面在300℃至1100℃的沉积温度下加热。

6. 发明授权

US4629397A Structural component for use under high thermal load conditions 失效
标题翻译：在高热负荷条件下使用的结构部件
公开(公告)号：US4629397A
公开(公告)日：1986-12-16
申请号：US627291
申请日：1984-07-02
申请人： Klaus Schweitzer
发明人： Klaus Schweitzer
IPC分类号： F01D5/18 , B23K1/19 , B32B15/04 , B32B18/00 , F01D5/28 , F01D11/12 , F01D25/00 , B32B7/00
CPC分类号： F01D11/12 , F01D25/005 , F01D5/284 , Y10S165/907 , Y10T428/12444 , Y10T428/12611
摘要： A structural component which is coolable for use under high thermal load conditions, such as a turbine blade, has a metallic support core with cooling ducts separated by lands in its surface. The core and its cooling ducts and lands are enclosed by an inner layer of metal felt and an outer layer of heat insulating ceramic material which partially penetrates into the metal felt to form a bonding zone between the felt and the ceramic material. Thus, any heat passing through the ceramic layer is introduced into the large surface area of the metal felt enabling the latter to efficiently introduce the heat into a cooling medium flowing in the ducts, thereby preventing thermal loads from adversely affecting the metal core to any appreciable extent.
摘要翻译：可在诸如涡轮叶片的高热负荷条件下使用的可冷却的结构部件具有金属支撑芯，其冷却管道在其表面上由焊盘分开。芯体及其冷却管道和焊盘由金属毡内层和绝热陶瓷材料外层所包围，部分渗入金属毡中，以形成毡和陶瓷材料之间的接合区。因此，通过陶瓷层的任何热量被引入到金属毡的大表面区域中，使其能够有效地将热量引入到在管道中流动的冷却介质中，从而防止热负荷对金属芯不利地影响到任何明显的程度。

7. 发明授权

US4242294A Method for encapsulating a molded ceramic member 失效
标题翻译：封装模制陶瓷构件的方法
公开(公告)号：US4242294A
公开(公告)日：1980-12-30
申请号：US930730
申请日：1978-08-03
申请人： Werner Huther , Klaus Schweitzer , Axel Rossmann
发明人： Werner Huther , Klaus Schweitzer , Axel Rossmann
IPC分类号： B22F3/12 , C04B33/00 , C04B35/593 , C04B35/645 , C04B33/34 , C04B37/00
CPC分类号： C04B33/32 , B22F3/1225 , B22F3/125 , B22F3/1266 , C04B33/00 , C04B35/593 , C04B35/6455
摘要： For encapsulating a ceramic molded member for high-temperature isostatic pressing (HIP), a generally porous coating of glass and/or ceramic is applied on the molded member of ceramic and sintered under a vacuum into a pressure-tight capsule encompassing the molded member.
摘要翻译：为了封装用于高温等静压（HIP）的陶瓷模制构件，将玻璃和/或陶瓷的通常多孔的涂层施加在陶瓷的模制构件上并在真空下烧结成包围模制构件的耐压胶囊。

8. 发明授权

US5114797A Metal structural component having a heat insulating titanium fire inhibiting protective coating 失效
标题翻译：金属结构部件具有耐热绝缘耐火保护涂层
公开(公告)号：US5114797A
公开(公告)日：1992-05-19
申请号：US693818
申请日：1991-04-30
申请人： Thomas Uihlen , Klaus Schweitzer
发明人： Thomas Uihlen , Klaus Schweitzer
IPC分类号： B32B15/01 , C23C4/02
CPC分类号： C23C4/02 , B32B15/01 , Y10T428/12056 , Y10T428/12063 , Y10T428/12069 , Y10T428/12618
摘要： A metal structure component is provided with a protective coating including three layers. A first layer on the surface of the metal structural component is a bond improving metallic base layer on which an intermediate heat insulating oxidic layer is applied, followed by a titanium fire inhibiting metallic cover layer. Due to this arrangement of three layers, it is possible for the advantageous characteristics of the individual layers to cooperate to provide a good bonding and heat insulating protection of the intermediate layer in combination with the titanium fire inhibiting protection of the outer layer, whereby the structural component achieves a prolonged operational life without a substantial weight increase as compared to conventional protection layers provided only for heat insulation purposes. This layer structure also minimizes any adverse influence on the structural strength of the metal structural component.
摘要翻译：金属结构部件具有包括三层的保护涂层。金属结构部件的表面上的第一层是施加了中间绝热氧化层的接合改善金属基层，其后是防止钛的阻火金属覆盖层。由于这种三层布置，单个层的有利特性可以协调，以提供中间层与外层的钛防火保护结合的良好的结合和隔热保护，由此结构与仅用于隔热目的提供的常规保护层相比，组件实现了延长的操作寿命而没有显着的重量增加。该层结构还可以最小化对金属结构部件的结构强度的任何不利影响。

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