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21. 发明授权

US07147899B2 Process of masking cooling holes of a gas turbine component 有权
标题翻译：掩蔽燃气轮机部件的冷却孔的过程
公开(公告)号：US07147899B2
公开(公告)日：2006-12-12
申请号：US10950640
申请日：2004-09-28
申请人： John Fernihough , Andreas Boegli , Alexander Stankowski
发明人： John Fernihough , Andreas Boegli , Alexander Stankowski
IPC分类号： B05D1/32 , B05D3/06
CPC分类号： F01D5/288 , B23P2700/06 , C23C4/01 , C23C14/042 , C23C16/042 , C25D5/022 , C25D7/00 , F01D5/005 , F05D2230/80 , F05D2230/90 , F05D2260/202
摘要： A process of masking cooling holes (4) of a gas turbine component (1) with an external surface (6), including a cavity (2) and a plurality of cooling holes (4) before coating the gas turbine component (1), includes first applying a mask material (5) to the cooling holes (4) so that the cooling holes are filled at least closest to the external surface (6), whereby the mask material (5) contains a filler material. Then the mask material (5) within the cooling holes (4) is thickening and the coating (8) is applied to the external surface (6) of the component (1) and the masked cooling holes (4). In the end remaining thickened mask material (5a) is removed from the cooling holes (4).
摘要翻译：在涂覆燃气轮机部件（1）之前，将包括空腔（2）和多个冷却孔（4）的外表面（6）的燃气轮机部件（1）的冷却孔（4）包括首先向所述冷却孔（4）施加掩模材料（5），使得所述冷却孔至少与所述外表面（6）最接近，由此所述掩模材料（5）含有填充材料。然后，冷却孔（4）内的掩模材料（5）变厚，将涂层（8）施加到部件（1）的外表面（6）和掩蔽冷却孔（4）上。最后，从冷却孔（4）移除剩余的增厚的掩模材料（5a）。

22. 发明授权

US09353625B2 Device for cleaning oxidized or corroded components in the presence of a halogenous gas mixture 有权
标题翻译：用于在有卤素气体混合物存在下清洁氧化或腐蚀的组分的装置
公开(公告)号：US09353625B2
公开(公告)日：2016-05-31
申请号：US12352641
申请日：2009-01-13
申请人： Ansgar Luttermann , Alexander Stankowski , Karsten Bindernagel
发明人： Ansgar Luttermann , Alexander Stankowski , Karsten Bindernagel
IPC分类号： C23C16/00 , C23F1/00 , H01L21/306 , F01D5/00 , C23G5/00
CPC分类号： F01D5/005 , C23G5/00 , F05D2230/11
摘要： A device for cleaning oxidized or corroded components (26), especially gas turbine components which are exposed to hot gases, in the presence of a halogenous gas, includes a cleaning retort which is designed in the shape of a boiler or cylinder and into which, indirectly or directly, leads a feed line which is connected via a flow control unit to a gas reservoir which stores the halogenous gas, and in which a device for gas distribution is integrated. The flow control unit has a gas volume control valve (5), a heat exchanger unit (9), and also a gas volume measuring unit (6) in sequence along the throughflow direction of the halogenous gas which flows through the feed line. Furthermore, a gas distribution in the retort directs the halogenous gas directly to the components which are to be cleaned.
摘要翻译：一种用于清洁氧化或腐蚀的部件（26）的设备，特别是在存在卤素气体的情况下暴露于热气体的燃气涡轮机部件，包括设计成锅炉或汽缸形式的清洗蒸馏器，间接地或直接地将通过流量控制单元连接的进料管线引导到储存有卤素气体的气体储存器，并且其中集成了用于气体分配的装置。流量控制单元具有气体量控制阀（5），热交换器单元（9），以及气体体积测量单元（6），其顺次沿着流过供给管线的卤素气体的流动方向。此外，蒸馏器中的气体分布将卤素气体直接引导到待清洁的部件。

23. 发明申请

US20110291311A1 PROCESS FOR EXTENDING THE CYCLIC SERVICE LIFE OF THERMAL BARRIER COATINGS, IN PARTICULAR ON GAS TURBINE COMPONENTS 有权
标题翻译：延长热障涂层循环使用寿命的过程，特别是燃气涡轮机组件
公开(公告)号：US20110291311A1
公开(公告)日：2011-12-01
申请号：US13206568
申请日：2011-08-10
申请人： Frigyes Szuecs , Alexander Stankowski
发明人： Frigyes Szuecs , Alexander Stankowski
IPC分类号： B32B43/00 , B29C73/00
CPC分类号： C04B41/009 , C04B41/502 , C04B41/53 , C04B41/5338 , C04B41/85 , C04B41/91 , C23C28/321 , C23C28/3215 , C23C28/345 , C23C28/3455 , F01D5/288 , F05D2300/2118 , C04B41/457 , C04B41/459 , C04B35/48
摘要： A process for extending the cyclic service life of thermal barrier coatings made of yttrium-stabilized zirconium oxide (YSZ) or the like which have been applied to a substrate with an oxidizing bond coat in between includes increasing or long-term stabilizing the strain tolerance of the thermal barrier coating.
摘要翻译：用于延长由钇稳定的氧化锆（YSZ）等制成的热障涂层的循环使用寿命的方法，其已经施加到其间具有氧化粘结涂层的基底上，包括增加或长期稳定应变耐受性热障涂层。

24. 发明申请

US20110264413A1 METHOD FOR REPAIRING AND/OR UPGRADING A COMPONENT OF A GAS TURBINE 审中-公开
标题翻译：修理和/或升级气体涡轮机组件的方法
公开(公告)号：US20110264413A1
公开(公告)日：2011-10-27
申请号：US13030301
申请日：2011-02-18
申请人： Alexander Stankowski , Lukas Emanuel Rickenbacher , Simone Hövel
发明人： Alexander Stankowski , Lukas Emanuel Rickenbacher , Simone Hövel
IPC分类号： G06F17/50
CPC分类号： B23P6/005 , F01D5/005 , F05D2230/23 , F05D2230/238
摘要： In a method for repairing and/or upgrading a component (10′), preferably of a gas turbine, especially a blade (10′), which component has been deformed during operation, a simplification with cost advantages is achieved by a first nominal CAD model (M1) of the non-deformed component (10) being made available, by the deformed component (10′) being measured, and by the first CAD-model (M1), with the aid of the data determined on the deformed component (10′), being transformed into a second CAD model (M2) of the deformed component (10′) by morphing. A cutting line, which determines a cut-out in the component (10′), and also an insert piece, which can be inserted in the cut-out, is established in the second CAD model (M2). A cut-out is introduced into the component (10′) in accordance with the cutting line, an insert piece for inserting in the cut-out is manufactured in accordance with the cutting line, the manufactured insert piece is inserted in the cut-out, and the inserted insert piece is connected to the component (10′) in a materially bonding manner.
摘要翻译：在用于修复和/或升级组件（10'）的方法中，优选地是在操作期间已经变形的燃气轮机，特别是叶片（10'），通过第一标称CAD来实现具有成本优势的简化通过被测量的变形部件（10'）和第一CAD模型（M1），借助于在变形部件上确定的数据使非变形部件（10）的型号（M1）可用，（10'），通过变形转换成变形部件（10'）的第二CAD模型（M2）。在第二CAD模型（M2）中建立了切割线，其确定部件（10'）中的切口以及可插入切口中的插入件。根据切割线将切口引入部件（10'）中，根据切割线制造用于插入切口的插入件，将制造的插入件插入切口并且插入的插入件以物质接合方式连接到部件（10'）。

25. 发明授权

US08021720B2 Process for extending the cyclic service life of thermal barrier coatings, in particular on gas turbine components 有权
标题翻译：延长隔热涂层，特别是燃气轮机组件的循环使用寿命的方法
公开(公告)号：US08021720B2
公开(公告)日：2011-09-20
申请号：US12014893
申请日：2008-01-16
申请人： Frigyes Szuecs , Alexander Stankowski
发明人： Frigyes Szuecs , Alexander Stankowski
IPC分类号： B05D3/10
CPC分类号： C04B41/009 , C04B41/502 , C04B41/53 , C04B41/5338 , C04B41/85 , C04B41/91 , C23C28/321 , C23C28/3215 , C23C28/345 , C23C28/3455 , F01D5/288 , F05D2300/2118 , C04B41/457 , C04B41/459 , C04B35/48
摘要： A process for extending the cyclic service life of thermal barrier coatings made of yttrium-stabilized zirconium oxide (YSZ) or the like which have been applied to a substrate with an oxidizing bond coat in between includes increasing or long-term stabilizing the strain tolerance of the thermal barrier coating.
摘要翻译：用于延长由钇稳定的氧化锆（YSZ）等制成的热障涂层的循环使用寿命的方法，其已经施加到其间具有氧化粘结涂层的基底上，包括增加或长期稳定的应变耐受性热障涂层。

26. 发明申请

US20060266285A1 Masking material for holes of a component 有权
标题翻译：组件孔洞的掩模材料
公开(公告)号：US20060266285A1
公开(公告)日：2006-11-30
申请号：US11501749
申请日：2006-08-10
申请人： John Fernihough , Andreas Boegli , Alexander Stankowski
发明人： John Fernihough , Andreas Boegli , Alexander Stankowski
IPC分类号： B05C11/00
CPC分类号： C23C16/042 , B05B12/26 , B23P2700/06 , C23C4/01 , C23C8/04 , C23C10/04 , C23C14/042 , Y10T29/49318 , Y10T29/49341
摘要： Process of masking cooling holes of a gas turbine component with an external surface, comprising a cavity and a plurality of cooling holes before coating the gas turbine component, comprising the steps of first applying a mask material to the cooling holes so that the cooling holes are filled at least closest to the external surface, whereby the mask material contains a substance which fluoresces under ultraviolet light and a filler material. Then the mask material within the cooling holes is thickening. An inspection using ultraviolet light to locate any unwanted residual mask material on the external surface is carried out and unwanted residual mask material is removed before the coating is applied to the external surface of the component and the masked cooling holes. In the end the mask material is removed from the cooling holes.
摘要翻译：具有外表面的燃气轮机部件的冷却孔的处理，包括在涂覆燃气轮机部件之前的空腔和多个冷却孔，包括以下步骤：首先将掩模材料施加到冷却孔，使得冷却孔为填充至少最接近外表面，由此掩模材料含有在紫外光下发荧光的物质和填充材料。然后冷却孔内的面罩材料变厚。进行使用紫外光的检查以在外表面上定位任何不需要的残留掩模材料，并且在将涂层施加到部件的外表面和掩蔽的冷却孔之前，去除不需要的残留掩模材料。最后，将掩模材料从冷却孔中移出。

27. 发明申请

US20050191422A1 Process of masking cooling holes of a gas turbine component 有权
标题翻译：掩蔽燃气轮机部件的冷却孔的过程
公开(公告)号：US20050191422A1
公开(公告)日：2005-09-01
申请号：US10950640
申请日：2004-09-28
申请人： John Fernihough , Andreas Boegli , Alexander Stankowski
发明人： John Fernihough , Andreas Boegli , Alexander Stankowski
IPC分类号： F01D5/18 , C23C4/00 , C23C14/04 , C23C16/04 , C23C16/455 , C25D5/02 , C25D7/00 , F01D5/00 , F01D5/28 , F01D25/00 , F02C7/00 , F04D29/38 , F04D29/58 , B05D5/00
CPC分类号： F01D5/288 , B23P2700/06 , C23C4/01 , C23C14/042 , C23C16/042 , C25D5/022 , C25D7/00 , F01D5/005 , F05D2230/80 , F05D2230/90 , F05D2260/202
摘要： A process of masking cooling holes (4) of a gas turbine component (1) with an external surface (6), including a cavity (2) and a plurality of cooling holes (4) before coating the gas turbine component (1), includes first applying a mask material (5) to the cooling holes (4) so that the cooling holes are filled at least closest to the external surface (6), whereby the mask material (5) contains a filler material. Then the mask material (5) within the cooling holes (4) is thickening and the coating (8) is applied to the external surface (6) of the component (1) and the masked cooling holes (4). In the end remaining thickened mask material (5a) is removed from the cooling holes (4).
摘要翻译：在涂覆燃气轮机部件（1）之前，将包括空腔（2）和多个冷却孔（4）的外表面（6）的燃气轮机部件（1）的冷却孔（4）包括首先向所述冷却孔（4）施加掩模材料（5），使得所述冷却孔至少与所述外表面（6）最接近，由此所述掩模材料（5）含有填充材料。然后，冷却孔（4）内的掩模材料（5）变厚，将涂层（8）施加到部件（1）的外表面（6）和掩蔽冷却孔（4）上。最后，从冷却孔（4）移除剩余的增厚的掩模材料（5a）。

28. 发明申请

US20050100672A1 Method of protecting a local area of a component 有权
标题翻译：保护组件局部区域的方法
公开(公告)号：US20050100672A1
公开(公告)日：2005-05-12
申请号：US10631846
申请日：2003-08-01
申请人： Alexander Stankowski , Andreas Boegli , John Fernihough
发明人： Alexander Stankowski , Andreas Boegli , John Fernihough
IPC分类号： B23K26/36 , C23C4/00 , F01D5/00 , F01D5/28 , B05D1/32
CPC分类号： F01D5/28 , B23K26/364 , C23C4/01 , F01D5/00
摘要： It is disclosed a method of protecting a local area of components (1) from the effects of thermochemical or mechanical processes carried out on the surface (6) of the component. A masking material (5) containing at least one filler material is applied to the local area so that the local area is protected by the masking material (5). This is at least partially polymerized on the local area. Subsequently the thermochemical or physical processes on the surface (6) of the component (1) are carried out after which the polymerized masking material (5) is removed from the local area of the component (1).
摘要翻译：公开了一种保护组件（1）的局部区域免受在组件的表面（6）上进行的热化学或机械过程的影响的方法。将包含至少一种填充材料的掩模材料（5）施加到局部区域，使得局部区域被掩蔽材料（5）保护。这在局部区域至少部分聚合。随后，在组分（1）的表面（6）上进行热化学或物理过程，然后从组分（1）的局部区域除去聚合的掩蔽材料（5）。

29. 发明授权

US08610027B2 Process for producing a 3-dimensional component by selective laser melting (SLM) 有权
标题翻译：通过选择性激光熔化（SLM）制备三维成分的方法
公开(公告)号：US08610027B2
公开(公告)日：2013-12-17
申请号：US13009941
申请日：2011-01-20
申请人： Simone Hövel , Alexander Stankowski , Lukas Rickenbacher
发明人： Simone Hövel , Alexander Stankowski , Lukas Rickenbacher
IPC分类号： B23K26/14 , B22D27/02
CPC分类号： B22F3/1055 , B22F5/003 , B22F7/00 , B33Y10/00 , B33Y70/00 , Y02P10/295
摘要： A process produces a 3-dimensional component (16) by selective laser melting (SLM), in which the component (16) is formed on a foundation with a surface, e.g., a platform (10) or a support, which in particular is a component of the same type which has already been produced previously, by successively melting layers of a first metal powder to form a sequence of stacked layers. The process is substantially simplified and made more flexible by virtue of the fact that the separation of the finished component (16) from the surface of the platform (10) or the support thereof is simplified by providing a separating layer (11) between the component (16) and the platform (10) or the support, this separating layer making it possible to separate the finished component (16) from the platform (10) or the support without damaging the finished component (16).
摘要翻译：一种方法通过选择性激光熔化（SLM）产生三维组件（16），其中组件（16）形成在具有表面的基础上，例如平台（10）或支撑件，其特别地是通过连续地熔化第一金属粉末的层以形成层叠的顺序的先前已经生产的相同类型的组分。由于通过在组件（16）之间提供分离层（11）来简化最终部件（16）与平台（10）的表面或其支撑件的分离，因此该过程被大大简化并变得更加灵活（16）和平台（10）或支撑件，该分离层使得可以将成品部件（16）与平台（10）或支撑件分离，而不会损坏最终部件（16）。

30. 发明申请

US20130020377A1 BRAZE ALLOY FOR HIGH-TEMPERATURE BRAZING AND METHODS FOR REPAIRING OR PRODUCING COMPONENTS USING A BRAZE ALLOY 有权
标题翻译：用于高温切割的BRAZE合金和使用BRAZE合金修复或生产组件的方法
公开(公告)号：US20130020377A1
公开(公告)日：2013-01-24
申请号：US13232120
申请日：2011-09-14
申请人： Alexander Stankowski , Daniel Beckel
发明人： Alexander Stankowski , Daniel Beckel
IPC分类号： B23K1/20 , B23K35/24 , B22F1/02 , B23K35/12
CPC分类号： B23K1/0018 , B23K35/0244 , B23K35/3033 , B23K35/3046 , B23K2101/001 , B23P6/00 , B23P6/005 , C22C19/03 , C22C19/07 , F01D5/005 , F05D2230/238 , Y10T29/49318 , Y10T428/12181
摘要： In a Ni-based, Co-based, or Ni—Co-based braze alloy (1) for high-temperature brazing of components (7) of modular structure and for repairing damaged components (7) which are formed of single crystal or directionally solidified superalloys using said braze alloy (1), the braze alloy has a first metallic powder component (2) having particle sizes in the nanometer range and a second metallic powder component (3) having particle sizes in the micrometer range. The surface of the particles of the second powder component (3) is thinly coated with particles of the first powder component (2). The braze alloy (1) additionally includes grain boundary stabilizing elements as alloying elements. In addition, melting point depressants can be present in the braze alloy (1) in a commercially common quantity or with a considerably increased proportion. Both the melting temperature of the braze alloy (1) and the probability of recrystallization are advantageously reduced.
摘要翻译：在用于模块化结构的部件（7）的高温钎焊和用于修复由单晶或定向形成的损坏部件（7）的Ni基，Co基或Ni-Co基钎焊合金（1）使用所述钎焊合金（1）的固化超合金，所述钎焊合金具有粒径在纳米范围内的第一金属粉末成分（2）和粒度在微米范围内的第二金属粉末成分（3）。第二粉末组分（3）的颗粒表面被薄的第一粉末组分（2）的颗粒涂覆。钎焊合金（1）还包括作为合金元素的晶界稳定元件。此外，熔点降低剂可以以商业上普遍的量或大大增加的比例存在于钎焊合金（1）中。钎焊合金（1）的熔融温度和重结晶的可能性都有利地降低。

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