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1. 发明申请

US20120118524A1 CORE DIE WITH VARIABLE PINS AND PROCESS FOR PRODUCING A CORE 审中-公开
标题翻译：具有可变引脚的芯片和用于生产核心的工艺
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。

2. 发明申请

US20120107136A1 SEALING PLATE AND ROTOR BLADE SYSTEM 审中-公开
标题翻译：密封板和转子叶片系统
公开(公告)号：US20120107136A1
公开(公告)日：2012-05-03
申请号：US13258011
申请日：2010-03-25
申请人： Tobias Buchal , Sascha Dungs , Winfried Esser , Birgit Grüger , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Peter Schröder , Waldemar Socha
发明人： Tobias Buchal , Sascha Dungs , Winfried Esser , Birgit Grüger , Oliver Lüsebrink , Mirko Milazar , Nicolas Savilius , Oliver Schneider , Peter Schröder , Waldemar Socha
IPC分类号： F01D5/08
CPC分类号： F01D5/3015 , F01D11/005 , F05D2230/232
摘要： A rotor blade system, for example, of a gas turbine is provided. The rotor blade system includes a plurality of rotor blades which are arranged annularly on a rotor disk. A plurality of sealing plates are arranged on a side surface of the rotor disk. An individual sealing plate is formed from a plurality of metal sheets, wherein two of the metal sheets are arranged opposite each other a distance apart and parallel to a plane of the sealing plate, forming a gap for guiding of cooling air.
摘要翻译：提供了例如燃气轮机的转子叶片系统。转子叶片系统包括环形地设置在转子盘上的多个转子叶片。多个密封板设置在转子盘的侧面上。单个密封板由多个金属板形成，其中两个金属板彼此相隔布置并平行于密封板的平面，形成用于引导冷却空气的间隙。

3. 发明授权

US09957809B2 Modified interface around a hole 有权
公开(公告)号：US09957809B2
公开(公告)日：2018-05-01
申请号：US14356464
申请日：2012-09-14
申请人： Christian Amann , Thomas Beck , Björn Beckmann , Andreas Böttcher , Winfried Esser , Giuseppe Gaio , Rudolf Küperkoch , Eckart Schumann , Rostislav Teteruk
发明人： Christian Amann , Thomas Beck , Björn Beckmann , Andreas Böttcher , Winfried Esser , Giuseppe Gaio , Rudolf Küperkoch , Eckart Schumann , Rostislav Teteruk
IPC分类号： B32B3/24 , F01D5/18 , F01D5/28
CPC分类号： F01D5/186 , F01D5/18 , F01D5/28 , F01D5/288 , F05D2230/90 , F05D2260/22141 , Y02T50/676 , Y10T428/24273 , Y10T428/24322
摘要： A layer system including a substrate and a layer is provided. The layer system has a hole at least in the layer, and wherein at least one recess is present in a surface of the layer in a vicinity around the hole or directly adjoining a boundary line of the hole.

4. 发明申请

US20140349065A1 MODIFIED INTERFACE AROUND A HOLE 有权
标题翻译：孔改良界面
公开(公告)号：US20140349065A1
公开(公告)日：2014-11-27
申请号：US14356464
申请日：2012-09-14
申请人： Christian Amann , Thomas Beck , Bjorn Beckmann , Andreas Böttcher , Winfried Esser , Giuseppe Gaio , Rudolf Küperkoch , Eckart Schumann , Rostislav Teteruk
发明人： Christian Amann , Thomas Beck , Bjorn Beckmann , Andreas Böttcher , Winfried Esser , Giuseppe Gaio , Rudolf Küperkoch , Eckart Schumann , Rostislav Teteruk
IPC分类号： F01D5/18 , F01D5/28
CPC分类号： F01D5/186 , F01D5/18 , F01D5/28 , F01D5/288 , F05D2230/90 , F05D2260/22141 , Y02T50/676 , Y10T428/24273 , Y10T428/24322
摘要： A layer system including a substrate and a layer is provided. The layer system has a hole at least in the layer, and wherein at least one recess is present in a surface of the layer in a vicinity around the hole or directly adjoining a boundary line of the hole.
摘要翻译：提供了包括衬底和层的层系统。层系统至少在该层中具有孔，并且其中至少一个凹部存在于该孔周围的附近的表面中或者直接邻接该孔的边界线。

5. 发明申请

US20090304503A1 STATOR BLADE SEGMENT OF A THERMAL TURBOMACHINE, ASSOCIATED PRODUCTION METHOD AND ALSO THERMAL TURBOMACHINE 失效
标题翻译：热涡轮机的定子叶片分段，相关的生产方法和热涡轮机
公开(公告)号：US20090304503A1
公开(公告)日：2009-12-10
申请号：US12225933
申请日：2007-02-21
申请人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Küperkoch , Thorsten Mattheis , Jan Münzer , Ralf Müsgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
IPC分类号： F01D9/04 , F01D9/02 , B23P11/00
CPC分类号： F01D9/042 , F01D25/246 , F05D2230/23 , F05D2230/238 , F05D2240/10 , F05D2240/80 , F05D2260/30 , Y10T29/49323
摘要： The invention relates to a guide blade segment of a thermal turbomachine, in particular a gas turbine, comprising a number of profiled blades which are arranged on a platform. A plurality of securing elements for securing the guide blade segment to an associated guide blade support are arranged on the side of the platform which is oriented away from the blade. The aim of the invention is to provide a guide blade segment which can be produced in a simple and economical manner avoiding casting problem areas enabling the guide blade segment to be attached in a particularly reliable and secure manner to the associated guide blade support. According to the invention, at least one section of at least one of the securing elements is a separately produced component which is rigidly connected to the platform or to an additional section of the securing element.
摘要翻译：本发明涉及一种热涡轮机的导向叶片段，特别是燃气涡轮机，其包括布置在平台上的多个异型叶片。用于将引导片段固定到相关联的引导叶片支撑件上的多个固定元件布置在平台的远离叶片的侧面上。本发明的目的是提供一种可以以简单和经济的方式制造的导向叶片段，避免了铸造问题区域，使得导向叶片段以特别可靠和可靠的方式附接到相关联的导向叶片支撑件。根据本发明，至少一个固定元件的至少一个部分是单独制造的部件，其刚性地连接到平台或固定元件的附加部分。

6. 发明申请

US20120273153A1 Casting mold having a stabilized inner casting core, casting method and casting part 审中-公开
标题翻译：具有稳定内铸芯，铸造方法和铸造件的铸模
公开(公告)号：US20120273153A1
公开(公告)日：2012-11-01
申请号：US13513308
申请日：2010-05-31
申请人： Fathi Ahmad , Winfried Esser , Uwe Paul
发明人： Fathi Ahmad , Winfried Esser , Uwe Paul
IPC分类号： B28B7/40 , C22C19/07 , B22D25/06 , C22C19/05
CPC分类号： B22D19/08 , B22C9/106
摘要： A casting mold for a metal melt is provided. By coating a core of a casting mold, the core may be mechanically stabilized and an inner coating of the component to be cast may be obtained, wherein the coating preferably serves as an anti-corrosion layer. A method for producing a cast part using the casting mold is also provided.
摘要翻译：提供了一种用于金属熔体的铸模。通过涂覆铸模的芯，芯可以是机械稳定的，并且可以获得要铸造的部件的内涂层，其中涂层优选用作防腐蚀层。还提供了一种使用铸模制造铸造件的方法。

7. 发明申请

US20080267771A1 Gas turbine with a guide vane 失效
标题翻译：燃气轮机带导叶
公开(公告)号：US20080267771A1
公开(公告)日：2008-10-30
申请号：US12009314
申请日：2008-01-17
申请人： Alexander R. Beeck , Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Alexander R. Beeck , Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
IPC分类号： F01D1/02
CPC分类号： F01D9/00 , F01D5/146 , F05D2240/301 , Y02T50/673
摘要： A guide vane for a gas turbine with a vane base body which is of single-piece design and comprises a profiled vane blade extending between a vane root and a cover plate and also the vane root formed integrally with the vane blade and the cover plate formed integrally with the vane blade, is intended, in a relatively simple way to be able to be matched to the individual conditions of use with especially little outlay on apparatus and logistics. For this purpose, according to the invention, a flow-routing body with an advance guide blade that is connected upstream of the vane blade as seen in the direction of flow of the working medium of the gas turbine is joined to the vane base body.
摘要翻译：一种具有叶片基体的燃气轮机的导向叶片，其具有单件式设计，并且包括在叶片根部和盖板之间延伸的异型叶片叶片，以及与叶片和盖板一体形成的叶片根部与叶片一体地，以相对简单的方式旨在能够与单独的使用条件匹配，特别是在设备和物流方面的特别少的费用。为此，根据本发明，在叶片叶片的工作介质的流动方向上观察到连接在叶片叶片的上游的具有前进导向叶片的流动路线体与叶片基体接合。

8. 发明申请

US20100014980A1 Turbine blade 有权
标题翻译：涡轮叶片
公开(公告)号：US20100014980A1
公开(公告)日：2010-01-21
申请号：US11807387
申请日：2007-05-29
申请人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
IPC分类号： F01D5/18
CPC分类号： F01D5/20 , F01D5/147 , F05D2230/232
摘要： There is described a turbine blade with an aerodynamically profiled blade leaf which is produced from two assembled shell elements. The shell elements forming the suction-side and the pressure-side blade leaf wall have been assembled by means of a high-temperature high-pressure bonding process and, under certain circumstances, may come apart at the blade tip. In order to prevent this, in the region of the blade leaf tip, a cramp is provided which hooks the two blade walls together with one another with a form fit.
摘要翻译：描述了具有由两个组装的壳元件制成的具有空气动力学异型叶片叶片的涡轮机叶片。形成吸入侧和压力侧叶片叶壁的壳单元已经通过高温高压接合工艺组装，并且在某些情况下可能在叶片尖端处分离。为了防止这种情况，在叶片叶尖的区域中，设置有将两个叶片壁彼此钩合在一起的抽筋。

9. 发明申请

US20080240927A1 Turbine blade for a turbine with a cooling medium passage 有权
标题翻译：具有冷却介质通道的涡轮机的涡轮叶片
公开(公告)号：US20080240927A1
公开(公告)日：2008-10-02
申请号：US11974895
申请日：2007-10-16
申请人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
发明人： Katharina Bergander , Georg Bostanjoglo , Tobias Buchal , Winfried Esser , Dirk Goldschmidt , Torsten Koch , Rudolf Kuperkoch , Thorsten Mattheis , Jan Munzer , Ralf Musgen , Matthias Oechsner , Ursula Pickert , Volker Vosberg
IPC分类号： F01D5/08 , F01D25/12
CPC分类号： F01D25/12 , F01D5/18 , F05D2230/10 , F05D2230/21 , F05D2230/232 , F05D2230/238 , F05D2240/81 , F05D2260/36
摘要： A turbine blade for a turbine of a thermal power plant, with a platform for partial delimiting of a flow passage in the turbine, wherein the platform has at least one cooling medium passage, which extends inside the platform, for guiding a cooling medium, is characterized according to the invention in that the at least one cooling medium passage emerges from the platform at at least two connecting openings, and the turbine blade has at least one supplementary component which can be fastened on the platform, with a communicating passage, which is designed for interconnecting the connecting openings in a fluid-guiding manner.
摘要翻译：一种用于火力发电厂的涡轮机的涡轮机叶片，具有用于部分限定涡轮机中的流动通道的平台，其中平台具有至少一个在平台内延伸以用于引导冷却介质的冷却介质通道，是根据本发明的特征在于，至少一个冷却介质通道在至少两个连接开口处从平台排出，并且涡轮叶片具有可以紧固在平台上的至少一个辅助部件，连通通道设计用于以流体引导方式互连连接开口。

10. 发明申请

US20120031579A1 Method for producing a negative mold for casting a turbine blade and mold for producing a wax model of a gas turbine 审中-公开
标题翻译：用于制造用于铸造涡轮叶片的负模具和用于制造燃气轮机的蜡模型的模具的方法
公开(公告)号：US20120031579A1
公开(公告)日：2012-02-09
申请号：US13263871
申请日：2010-03-31
申请人： Fathi Ahmad , Winfried Esser
发明人： Fathi Ahmad , Winfried Esser
IPC分类号： B22D25/02 , B22C7/02
CPC分类号： B22C9/04 , B22C7/02 , B22D23/00
摘要： A method for producing a negative mold for casting a turbine blade with a blade platform and at least one fastening element for fastening the turbine blade to a blade fixture is provided. The surface of the fastening element of a platform surface is located at a distance opposite of the blade platform. A wax model of the turbine blade to be produced is produced, a negative model of the turbine blade is created based on the wax model after the wax model has hardened and the wax model is melted out after completion of the negative mold. During hardening and/or during storage and/or during transport of the wax model at least one spacer is arranged between the platform surface of the blade platform and the opposite surface of the fastening element of the wax model.
摘要翻译：提供了一种用于制造用于将具有叶片平台的涡轮叶片铸造的负模具和用于将涡轮机叶片紧固到叶片固定装置的至少一个紧固元件的负模具的方法。平台表面的紧固元件的表面位于与刀片平台相对的距离处。制造要生产的涡轮叶片的蜡模型，在蜡模型硬化之后，基于蜡模型创建涡轮叶片的负模型，并且在模具完成之后蜡模型熔化。在硬化期间和/或在储存期间和/或在运输蜡模型期间，在叶片平台的平台表面和蜡模型的紧固元件的相对表面之间布置有至少一个间隔件。

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