公开(公告)号：US09188015B2

公开(公告)日：2015-11-17

申请号：US12437075

申请日：2009-05-07

申请人： Fathi Ahmad ,  Stefan Krause ,  Oliver Lüsebrink

发明人： Fathi Ahmad ,  Stefan Krause ,  Oliver Lüsebrink

IPC分类号： B32B5/12 ,  F01D5/28 ,  B22D27/04 ,  C22C19/05 ,  C22F1/10

CPC分类号： F01D5/286 ,  B22D27/045 ,  B23P15/02 ,  C22C19/05 ,  C22F1/10 ,  F05D2240/121 ,  F05D2240/303 ,  F05D2300/606 ,  Y02T50/67 ,  Y10T428/24074

摘要： A component, designed so that the longitudinal grain which experiences the greatest stress has a larger grain width than the other grains, is provided. This longitudinal grain is usually on the edge of the component. The component includes longitudinal grains that are directionally solidified in a rod-crystalline form along the longitudinal axis of the component.

摘要翻译： 提供了一种被设计成使得经受最大应力的纵向颗粒具有比其它颗粒更大的晶粒宽度的部件。 该纵向颗粒通常位于组件的边缘上。 该组件包括纵向晶粒，其沿组件的纵轴以杆状晶体形式定向凝固。

公开(公告)号：US20090280291A1

公开(公告)日：2009-11-12

申请号：US12437075

申请日：2009-05-07

申请人： Fathi Ahmad ,  Stefan Krause ,  Oliver Lüsebrink

发明人： Fathi Ahmad ,  Stefan Krause ,  Oliver Lüsebrink

IPC分类号： B32B5/12

CPC分类号： F01D5/286 ,  B22D27/045 ,  B23P15/02 ,  C22C19/05 ,  C22F1/10 ,  F05D2240/121 ,  F05D2240/303 ,  F05D2300/606 ,  Y02T50/67 ,  Y10T428/24074

摘要： A component, designed so that the longitudinal grain which experiences the greatest stress has a larger grain width than the other grains, is provided. This longitudinal grain is usually on the edge of the component. The component includes longitudinal grains that are directionally solidified in a rod-crystalline form along the longitudinal axis of the component.

摘要翻译： 提供了一种被设计成使得经受最大应力的纵向颗粒具有比其它颗粒更大的晶粒宽度的部件。 该纵向颗粒通常位于组件的边缘上。 该组件包括纵向晶粒，其沿组件的纵轴以杆状晶体形式定向凝固。

公开(公告)号：US20120118524A1

公开(公告)日：2012-05-17

申请号：US13275460

申请日：2011-10-18

申请人： Fathi Ahmad ,  Winfried Esser ,  Giuseppe Gaio ,  Waldemar Heckel ,  Rudolf Küperkoch ,  Oliver Lüsebrink ,  Thorsten Mattheis ,  Mirko Milazar ,  Artur Mol ,  Uwe Paul ,  Oliver Ricken ,  Oliver Schneider

发明人： Fathi Ahmad ,  Winfried Esser ,  Giuseppe Gaio ,  Waldemar Heckel ,  Rudolf Küperkoch ,  Oliver Lüsebrink ,  Thorsten Mattheis ,  Mirko Milazar ,  Artur Mol ,  Uwe Paul ,  Oliver Ricken ,  Oliver Schneider

IPC分类号： B22D45/00 ,  B21K21/16

CPC分类号： B22C7/06 ,  B22C9/10 ,  Y10T29/49716

摘要： A core die is provided. The core die includes a first half and a second half where a cavity is formed between the two. Pins are arranged on the halves and the pins are replaceable. By virtue of the modular inner structure of a core die, the core die may be matched to the desired changes of the core, by small changes, more quickly and more easily than would be the case if the core die had only one part or if the pins were a fixed component of the core die halves.

摘要翻译： 提供一个核心模具。 芯模具包括在两者之间形成空腔的第一半和第二半部。 引脚布置在一半上，引脚是可更换的。 由于芯模的模块化内部结构，芯模可以通过小的变化与芯的期望变化相匹配，比如果芯模只有一个部分或如果 销钉是芯半模的固定部件。

公开(公告)号：US09238976B2

公开(公告)日：2016-01-19

申请号：US13145353

申请日：2010-01-05

申请人： Fathi Ahmad ,  Giuseppe Gaio ,  Holger Grote ,  Christian Lerner ,  Mirko Milazar ,  Mathias Stutt ,  Thomas-Dieter Tenrahm ,  Bernd Vonnemann

发明人： Fathi Ahmad ,  Giuseppe Gaio ,  Holger Grote ,  Christian Lerner ,  Mirko Milazar ,  Mathias Stutt ,  Thomas-Dieter Tenrahm ,  Bernd Vonnemann

IPC分类号： F01D9/04 ,  F01D25/24

CPC分类号： F01D25/246 ,  F01D9/023 ,  F05D2230/80

摘要： A turbine guide vane system, in particular for a gas turbine is provided. The turbine guide vane system includes a number of guide vane rows and a guide vane carrier, to enable particularly simple replacement of guide vanes, while maintaining a particularly high degree of efficiency, and thus designed for particularly short repair durations. For this purpose, the guide vane carrier has a number of segments, wherein a segment extends over the entire radial extension of the guide vane carrier and the connection of the remaining segments may be detached, and wherein the turbine guide vane carrier includes at least two sections along the axial extension thereof that are connected to one another and have a different number of segments.

摘要翻译： 提供了一种特别用于燃气轮机的涡轮导叶系统。 涡轮引导叶片系统包括多个导向叶片行和导向叶片载体，以便能够特别简单地更换导向叶片，同时保持特别高的效率，并因此设计为特别短的修理持续时间。 为此目的，导向叶片承载件具有多个段，其中，一个段在导向叶片承载件的整个径向延伸部分上延伸，并且其余段的连接可以被拆卸，并且其中该涡轮导向叶片承载件包括至少两个 其轴向延伸部分彼此连接并且具有不同数量的段。

公开(公告)号：US08865255B2

公开(公告)日：2014-10-21

申请号：US13576405

申请日：2011-02-23

申请人： Fathi Ahmad ,  Knut Halberstadt ,  Christian Lerner

发明人： Fathi Ahmad ,  Knut Halberstadt ,  Christian Lerner

IPC分类号： C23C16/00 ,  B05D7/22 ,  C23C10/00 ,  C23C10/18 ,  C23C10/06 ,  C23C10/48

CPC分类号： C23C10/00 ,  C23C10/06 ,  C23C10/18 ,  C23C10/48 ,  Y02T50/67 ,  Y10T428/13

摘要： A process for setting the average flow rate within a hollow component is provided. The process includes setting a relatively small wall thickness in a first region with a relatively large flow cross section using a first diffusion coating process and setting a relatively large wall thickness by a second different diffusion process in a second region with a relatively small flow cross section. The use of different diffusion coatings in a component allows the flow of coolant through a component to be set in a controlled manner.

摘要翻译： 提供了一种用于设定中空部件内的平均流量的方法。 该方法包括使用第一扩散涂覆工艺在具有相对大的流动横截面的第一区域中设置相对小的壁厚，并且在具有相对小的流动横截面的第二区域中通过第二不同扩散过程设定相对较大的壁厚 。 在组件中使用不同的扩散涂层允许通过部件的冷却剂流以受控的方式设定。

公开(公告)号：US20120070310A1

公开(公告)日：2012-03-22

申请号：US13258624

申请日：2010-03-25

申请人： Fathi Ahmad

发明人： Fathi Ahmad

IPC分类号： F01D5/18

CPC分类号： F01D5/087 ,  F01D25/12 ,  F05D2260/201

摘要： An axial turbomachine rotor is provided. The rotor includes a rotor disk and a rotor blade ring, which includes a plurality of rotor blades, each of which include a blade root, with which the rotor blade is fixed radially outward on the rotor disk, wherein the blade root is engaged with the rotor disk at the outer edge of the rotor disk in a form-closed manner in such a way that during operation of the rotor, a gap is formed between the rotor blade and the rotor disk at a predetermined surface area of the rotor disk, in which area, a plurality of impingement cooling openings is arranged, through which a cooling medium may flow from the interior of the rotor disk into the gap whereby the rotor blade is cooled using the cooling medium by means of impingement cooling.

摘要翻译： 提供轴向涡轮机转子。 转子包括转子盘和转子叶片环，其包括多个转子叶片，每个转子叶片包括叶片根部，转子叶片通过该叶片根部径向向外固定在转子盘上，其中叶片根部与叶片根部 转子盘在转子盘的外边缘处以形式关闭的方式，使得在转子的操作期间，在转子叶片的预定表面区域处在转子叶片和转子盘之间形成间隙， 设置多个冲击冷却开口，冷却介质可从转子盘的内部流动到间隙中，由此通过冲击冷却使用冷却介质冷却转子叶片。

公开(公告)号：US20120039716A1

公开(公告)日：2012-02-16

申请号：US13145353

申请日：2010-01-05

申请人： Fathi Ahmad ,  Giuseppe Gaio ,  Holger Grote ,  Christian Lerner ,  Mirko Milazar ,  Matthias Stutt ,  Thomas-Dieter Tenrahm ,  Bernd Vonnemann

发明人： Fathi Ahmad ,  Giuseppe Gaio ,  Holger Grote ,  Christian Lerner ,  Mirko Milazar ,  Matthias Stutt ,  Thomas-Dieter Tenrahm ,  Bernd Vonnemann

IPC分类号： F01D5/02

CPC分类号： F01D25/246 ,  F01D9/023 ,  F05D2230/80

摘要： A turbine guide vane system, in particular for a gas turbine is provided. The turbine guide vane system includes a number of guide vane rows and a guide vane carrier, to enable particularly simple replacement of guide vanes, while maintaining a particularly high degree of efficiency, and thus designed for particularly short repair durations. For this purpose, the guide vane carrier has a number of segments, wherein a segment extends over the entire radial extension of the guide vane carrier and the connection of the remaining segments may be detached, and wherein the turbine guide vane carrier includes at least two sections along the axial extension thereof that are connected to one another and have a different number of segments.

摘要翻译： 提供了一种特别用于燃气轮机的涡轮引导叶片系统。 涡轮引导叶片系统包括多个导向叶片行和导向叶片载体，以便能够特别简单地更换导向叶片，同时保持特别高的效率，并因此设计为特别短的修理持续时间。 为此目的，导向叶片承载件具有多个段，其中，一个段在导向叶片承载件的整个径向延伸部分上延伸，并且其余段的连接可以被拆卸，并且其中该涡轮导向叶片承载件包括至少两个 其轴向延伸部分彼此连接并且具有不同数量的段。

公开(公告)号：US20100129554A1

公开(公告)日：2010-05-27

申请号：US12596780

申请日：2008-04-10

申请人： Fathi Ahmad

发明人： Fathi Ahmad

IPC分类号： B05D3/12

CPC分类号： F01D5/288 ,  F01D5/16 ,  F01D5/187 ,  F05D2230/10 ,  F05D2230/80 ,  F05D2250/19 ,  Y10T29/49318 ,  Y10T29/49336 ,  Y10T29/49337 ,  Y10T29/49339 ,  Y10T29/49726

摘要： A method for producing a coated turbine blade, with which the frequency property thereof can be particularly easily adjusted to the required boundary conditions is provided. Recesses are introduced into a blade tip of the blade leaf of the turbine blade after coating of turbine blade. In one aspect a plurality of bores are made which are distributed along the blade leaf center line.

摘要翻译： 提供一种用于制造涂覆的涡轮叶片的方法，其特征在于能够将其频率特性容易地调整到所需的边界条件。 在涡轮叶片涂覆之后，将凹陷物引入涡轮机叶片叶片的叶片尖端。 在一个方面，制成沿叶片叶中心线分布的多个孔。

公开(公告)号：US20090229101A1

公开(公告)日：2009-09-17

申请号：US12227447

申请日：2007-02-15

申请人： Fathi Ahmad ,  Michael Dankert

发明人： Fathi Ahmad ,  Michael Dankert

IPC分类号： B22D19/10

CPC分类号： B23K1/0018 ,  B23K2101/001 ,  B23P6/005 ,  B23P6/045 ,  F01D5/005 ,  F05D2230/237 ,  F05D2230/238 ,  F05D2230/80 ,  Y02T50/67 ,  Y10T29/49746

摘要： A method for the crack repair of a component having a crack on a surface, including excavating a hollow around the crack, wherein the hollow has two recesses and the recesses are arranged at the height of the surface and are open at the height of the surface, and wherein the recesses are arranged around the circumference of the hollow and further including filling the hollow with a braze. A component having a crack on a surface is also provided with a hollow which is excavated around the crack, the hollow has two recesses and the recesses are arranged at the height of the surface and are open at the height of the surface, and the recesses are arranged around the circumference of the hollow, wherein the hollow is filled with the braze.

摘要翻译： 一种用于在表面上具有裂缝的部件的裂纹修复的方法，包括在所述裂纹周围挖出一个中空部，其中所述中空部具有两个凹部，并且所述凹部布置在所述表面的高度处并且在所述表面的高度处开放 并且其中所述凹部围绕所述中空部的圆周布置，并且还包括用钎焊填充所述中空部。 在表面具有裂缝的部件还设置有围绕裂缝挖掘的中空部，中空部具有两个凹部，凹部布置在表面的高度处并且在表面的高度处开口，并且凹部 围绕中空的圆周布置，其中中空部填充有钎焊。

公开(公告)号：US07465150B2

公开(公告)日：2008-12-16

申请号：US11479183

申请日：2006-06-30

申请人： Fathi Ahmad

发明人： Fathi Ahmad

IPC分类号： F01D9/06 ,  F01D25/10 ,  F01D25/12

CPC分类号： F01D25/10 ,  F01D5/18 ,  F01D9/041 ,  F05D2220/3212 ,  F05D2260/85 ,  F05D2270/114

摘要： Described is a cooled gas turbine guide blade for a gas turbine, with a hollow blade profile which comprises an onflow edge onto which a working medium is capable of flowing, and with, for guiding a cooling medium, an onflow edge duct running inside the blade profile along the onflow edge. Furthemore, to the use of such a gas turbine guide blade and to a method for operating a gas turbine with an abovementioned gas turbine guide blade. In order to provide a gas turbine guide blade with an increased lifetime by means of the invention, it is proposed that, in the onflow edge duct, an electrical heating element be provided, which extends approximately completely over the entire length of the onflow edge duct and through which a heating current flows, before the operation of the gas turbine, for the preheating of the gas turbine guide blade.

摘要翻译： 描述了一种用于燃气轮机的冷却式燃气涡轮引导叶片，其具有中空叶片轮廓，该中空叶片轮廓包括流入工作介质能够流动的向上流动边缘，以及用于引导冷却介质，在叶片内运行的流出边缘管道 沿着边缘的轮廓。 对于使用这样的燃气轮机引导叶片以及使用上述燃气轮机引导叶片来操作燃气轮机的方法更是如此。 为了通过本发明提供具有增加的寿命的燃气轮机引导叶片，提出在流出边缘管道中设置电加热元件，该电加热元件大致完全延伸在流出边缘管道的整个长度上 并且在燃气轮机的运行之前加热电流通过其流动，用于燃气涡轮引导叶片的预热。