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1. 发明申请

US20090317228A1 APPARATUS AND METHOD FOR CONTROLLING A BLADE TIP CLEARANCE FOR A COMPRESSOR 有权
标题翻译：用于控制压缩机叶片间隙的装置和方法
公开(公告)号：US20090317228A1
公开(公告)日：2009-12-24
申请号：US11477294
申请日：2006-06-29
申请人： Andre Werner
发明人： Andre Werner
IPC分类号： F01D11/14
CPC分类号： F01D11/22 , F05D2220/3216 , F05D2240/11 , F05D2270/65 , F05D2300/431 , F05D2300/437 , F05D2300/501
摘要： An apparatus and method for controlling a blade tip clearance for a compressor of a turbo-engine, in particular of an aircraft engine, is disclosed. A blade tip clearance control device, which has a rotor and a housing surrounding the rotor forming a blade tip clearance, includes a sealing element that is movable into the blade tip clearance and an actuator unit, where the sealing element is designed as a circumferential shroud liner made of a flexible rubbery material in which at least one tubular diaphragm that is also circumferential is arranged. The diaphragm is acted upon with hydraulic fluid via the actuator unit. This makes it possible to counteract degradation that occurs during operation due to erosion, aging, etc. As a result, efficiency is maintained and the pump limit interval is retained.
摘要翻译：公开了一种用于控制涡轮发动机，特别是飞机发动机的压缩机的叶片顶端间隙的装置和方法。叶片顶端间隙控制装置具有转子和围绕转子的壳体，形成叶片顶端间隙，包括可移动到叶片顶端间隙中的密封元件和致动器单元，其中密封元件被设计为周向护罩衬垫由柔性橡胶材料制成，其中至少一个也是周向的管状隔膜被布置。隔膜通过致动器单元与液压流体作用。这使得可以抵消由于腐蚀，老化等而在操作期间发生的劣化。结果，保持效率并保持泵的限制间隔。

2. 发明申请

US20090202379A1 METHOD FOR PRODUCING AN INLET LINING 审中-公开
标题翻译：生产入口衬里的方法
公开(公告)号：US20090202379A1
公开(公告)日：2009-08-13
申请号：US12093395
申请日：2006-11-10
申请人： Andre Werner
发明人： Andre Werner
IPC分类号： B22F3/11 , B22F7/04
CPC分类号： C23C30/00 , C23C10/02 , C23C10/18 , C23C10/26 , C23C10/30 , C23C10/52 , C23C18/1204 , C23C18/127 , C23C18/1295
摘要： The invention relates to a method for producing an inlet lining on a stator-sided component of a turbine engine, in particular, a gas turbine, with at least the following steps: a) providing a stator-sided component of a turbine engine, this component being provided with an inlet lining; b) providing a mixture consisting of a solvent; particles of a metallic parent material for the inlet lining, said particles being insoluble in the solvent; and a filler, this filler having at least one constituent that is soluble in the solvent; c) applying the mixture to the stator-sided component; d) drying the stator-sided component and the mixture, applied to the component, while at least partially expelling the solvent in order to provide a porous green body in the area of the applied and dried mixture; e) diffusion heat treating the component for inwardly diffusing aluminum and/or chromium and for forming the intermetallic phases in the resulting inlet lining.
摘要翻译：本发明涉及一种用于在涡轮发动机，特别是燃气轮机的定子侧部件上制造入口衬里的方法，至少具有以下步骤：a）提供涡轮发动机的定子侧部件，该部件设有入口衬里; b）提供由溶剂组成的混合物; 用于入口衬里的金属母材的颗粒，所述颗粒不溶于溶剂; 和填料，该填料具有至少一种可溶于溶剂的组分; c）将混合物施加到定子侧部件上; d）干燥施加到部件上的定子侧部件和混合物，同时至少部分排出溶剂，以便在施加和干燥的混合物的区域中提供多孔生坯; e）对组分进行扩散热处理以使铝和/或铬向内扩散，并在所得到的入口衬里中形成金属间相。

3. 发明申请

US20120128875A1 Method for Producing an Inlet Lining 审中-公开
标题翻译：生产进口衬里的方法
公开(公告)号：US20120128875A1
公开(公告)日：2012-05-24
申请号：US13300385
申请日：2011-11-18
申请人： Andre Werner
发明人： Andre Werner
IPC分类号： B05D7/22
CPC分类号： C23C30/00 , C23C10/02 , C23C10/18 , C23C10/26 , C23C10/30 , C23C10/52 , C23C18/1204 , C23C18/127 , C23C18/1295
摘要： The invention relates to a method for producing an inlet lining on a stator-sided component of a turbine engine, in particular, a gas turbine, with at least the following steps: providing a stator-sided component of a turbine engine with an inlet lining; providing a mixture consisting of a solvent, particles of a metallic parent material for the inlet lining, the particles being insoluble in the solvent, and a filler having at least one constituent soluble in the solvent; applying the mixture to the stator-sided component; drying the stator-sided component and the mixture applied to the component while at least partially expelling the solvent to provide a porous green body in the area of the applied and dried mixture; and diffusion heat treating the component for inwardly diffusing aluminum and/or chromium and for forming the intermetallic phases in the resulting inlet lining.
摘要翻译：本发明涉及一种用于在涡轮发动机，特别是燃气轮机的定子侧部件上制造入口衬里的方法，至少具有以下步骤：提供具有入口衬套的涡轮发动机的定子侧部件 ; 提供由溶剂组成的混合物，用于入口衬里的金属母体材料的颗粒，不溶于溶剂的颗粒和具有至少一种可溶于溶剂的组分的填料; 将混合物施加到定子侧部件上; 干燥定子侧部件和施加到部件上的混合物，同时至少部分地排出溶剂以在施加和干燥的混合物的区域中提供多孔生坯; 以及扩散热处理所述部件以向内扩散铝和/或铬并在所得到的入口衬里中形成金属间相。

4. 发明授权

US07797179B2 Method and apparatus for planning major outages for gas turbines 有权
标题翻译：用于规划燃气轮机重大停运的方法和装置
公开(公告)号：US07797179B2
公开(公告)日：2010-09-14
申请号：US11237436
申请日：2005-09-28
申请人： Amit Chakraborty , Andre Werner , Venkatraman Gurumurthi , Ammaiappan Balasubramanian , Robin Hoeher , Michael Rindler , Michael Lange
发明人： Amit Chakraborty , Andre Werner , Venkatraman Gurumurthi , Ammaiappan Balasubramanian , Robin Hoeher , Michael Rindler , Michael Lange
IPC分类号： G06F9/44
CPC分类号： G06Q10/06 , G06Q10/0631 , G06Q40/12 , Y04S10/54
摘要： A system and method for planning outages for a power generation installation comprising a gas turbine power plant. The system and method utilizes a computer to receive requests from users to create maintenance plans for the power plant by generating templates, applying the templates to a database containing gas turbine data for the power generation installation; and receiving data from users to create maintenance package plans. Users can select either modular or turnkey maintenance plans. Modular maintenance package options enable a user to specifically select and obtain price quote information for parts and technicians who perform the maintenance tasks, and to specify particular shift options for the technicians.
摘要翻译：一种用于计划包括燃气轮机发电厂的发电设备的停电的系统和方法。该系统和方法利用计算机接收用户的请求，通过生成模板，将模板应用于包含用于发电设备的燃气轮机数据的数据库，为电厂创建维护计划; 并从用户接收数据来创建维护包计划。用户可以选择模块化或交钥匙维护计划。模块化维护包选项使用户能够为执行维护任务的部件和技术人员特别选择并获取价格报价信息，并为技术人员指定特定的换档选项。

5. 发明授权

US07654791B2 Apparatus and method for controlling a blade tip clearance for a compressor 有权
标题翻译：用于控制压缩机的叶片顶端间隙的装置和方法
公开(公告)号：US07654791B2
公开(公告)日：2010-02-02
申请号：US11477294
申请日：2006-06-29
申请人： Andre Werner
发明人： Andre Werner
IPC分类号： F01D11/20
CPC分类号： F01D11/22 , F05D2220/3216 , F05D2240/11 , F05D2270/65 , F05D2300/431 , F05D2300/437 , F05D2300/501
摘要： An apparatus and method for controlling a blade tip clearance for a compressor of a turbo-engine, in particular of an aircraft engine, is disclosed. A blade tip clearance control device, which has a rotor and a housing surrounding the rotor forming a blade tip clearance, includes a sealing element that is movable into the blade tip clearance and an actuator unit, where the sealing element is designed as a circumferential shroud liner made of a flexible rubbery material in which at least one tubular diaphragm that is also circumferential is arranged. The diaphragm is acted upon with hydraulic fluid via the actuator unit. This makes it possible to counteract degradation that occurs during operation due to erosion, aging, etc. As a result, efficiency is maintained and the pump limit interval is retained.
摘要翻译：公开了一种用于控制涡轮发动机，特别是飞机发动机的压缩机的叶片顶端间隙的装置和方法。叶片顶端间隙控制装置具有转子和围绕转子的壳体，形成叶片顶端间隙，包括可移动到叶片顶端间隙中的密封元件和致动器单元，其中密封元件被设计为周向护罩衬垫由柔性橡胶材料制成，其中至少一个也是周向的管状隔膜被布置。隔膜通过致动器单元与液压流体作用。这使得可以抵消由于腐蚀，老化等而在操作期间发生的劣化。结果，保持效率并保持泵的限制间隔。

6. 发明申请

US20070093988A1 Method and apparatus for planning major outages for gas turbines 有权
标题翻译：用于规划燃气轮机重大停运的方法和装置
公开(公告)号：US20070093988A1
公开(公告)日：2007-04-26
申请号：US11237436
申请日：2005-09-28
申请人： Amit Chakraborty , Andre Werner , Venkatraman Gurumurthi , Ammaiappan Balasubramanian , Robin Hoeher , Michael Rindler
发明人： Amit Chakraborty , Andre Werner , Venkatraman Gurumurthi , Ammaiappan Balasubramanian , Robin Hoeher , Michael Rindler
IPC分类号： G06F17/18 , G06F19/00 , G06F15/00
CPC分类号： G06Q10/06 , G06Q10/0631 , G06Q40/12 , Y04S10/54
摘要： A system and method for planning outages for a power generation installation comprising a gas turbine power plant. The system and method utilizes a computer to receive requests from users to create maintenance plans for the power plant by generating templates, applying the templates to a database containing gas turbine data for the power generation installation; and receiving data from users to create maintenance package plans. Users can select either modular or turnkey maintenance plans. Modular maintenance package options enable a user to specifically select and obtain price quote information for parts and technicians who perform the maintenance tasks, and to specify particular shift options for the technicians.
摘要翻译：一种用于计划包括燃气轮机发电厂的发电设备的停电的系统和方法。该系统和方法利用计算机接收用户的请求，通过生成模板，将模板应用于包含用于发电设备的燃气轮机数据的数据库，为电厂创建维护计划; 并从用户接收数据来创建维护包计划。用户可以选择模块化或交钥匙维护计划。模块化维护包选项使用户能够为执行维护任务的部件和技术人员特别选择并获取价格报价信息，并为技术人员指定特定的换档选项。

7. 发明申请

US20100330271A1 METHOD OF REPAIRING RUN-IN COATINGS 有权
标题翻译：修复运行涂层的方法
公开(公告)号：US20100330271A1
公开(公告)日：2010-12-30
申请号：US12308523
申请日：2007-06-14
申请人： Manfred A. Daeubler , Andre Werner , Heinrich Walter
发明人： Manfred A. Daeubler , Andre Werner , Heinrich Walter
IPC分类号： B05D3/02
CPC分类号： F01D11/12 , B23P6/007 , C23C10/16 , C23C10/18 , C23C26/00 , F05C2201/0463 , F05C2201/0466 , F05D2220/762 , F05D2230/10 , F05D2230/22 , F05D2230/30 , F05D2230/40 , F05D2230/80 , F05D2300/11 , F05D2300/224 , F05D2300/228
摘要： The present invention relates to a method of repairing intake coatings (12), in particular intake coatings for use in compressor and turbine components, wherein the process comprises the following steps: a) filling of a damaged place (10) of the inlet coating (12) with a material (18) whose material composition corresponds to that of the intake coating (12) or is comparable to this or whose materials properties are comparable to the materials properties of the intake coating (12); b) drying of the material (18) introduced into the damaged place (10); c) application of a diffusion donor layer (20) over the region of the damaged place (10) and onto the introduced material (18); and d) heat treatment of the intake coating (12) at least in the region of the damaged place (10) to effect local diffusion of at least one metallic element from the diffusion donor layer (20) into the introduced material (18).
摘要翻译：本发明涉及一种修复进口涂层（12）的方法，特别是用于压缩机和涡轮机部件的进料涂层，其中该方法包括以下步骤：a）填充入口涂层的损坏场所（10）（ 12）与其材料成分对应于进料涂层（12）的材料（18）或与其相当或其材料性质与进料涂层（12）的材料性质相当的材料（18）; b）干燥引入损坏场所（10）的材料（18）; c）在损坏的地方（10）的区域上施加扩散施主层（20）并且到引入的材料（18）上; 以及d）至少在损坏处（10）的区域中对进气涂层（12）进行热处理，以使至少一种金属元素从扩散施主层（20）局部扩散到引入材料（18）中。

8. 发明申请

US20100119706A1 METHOD FOR THE PRODUCTION OF AN ABRADABLE COATING 审中-公开
标题翻译：生产不可磨损涂料的方法
公开(公告)号：US20100119706A1
公开(公告)日：2010-05-13
申请号：US12597163
申请日：2008-04-12
申请人： Andre Werner
发明人： Andre Werner
IPC分类号： B05D1/12
CPC分类号： C23C26/02 , B22F1/025 , B22F3/22 , B22F7/06 , B22F7/062 , B22F2003/247 , B22F2998/10 , C23C4/067 , C23C4/18 , C23C10/28 , C23C10/60 , C23C24/08 , C23C24/10 , C23C26/00 , B22F1/0074 , B22F3/1021 , B22F3/24
摘要： A method for producing an abradable coating for a component of a turbo-machine is disclosed. The method includes a) a powdery material is pretreated; b) a processable preliminary product is produced which is to be applied to a component that is to be coated; c) the preliminary product is applied to the component that is to be coated; d) a synthetic binder contained in the preliminary product is burned off; e) the component is sintered; and f) the component is post-processed. The method for producing an abradable coating for a turbo-machine eliminates the drawbacks of the solutions known from the prior art. In particular, the method is inexpensive, can easily be combined with other production process steps, for example, thermal treatments that have to be carried out anyway, and is also suitable as a method for repairs.
摘要翻译：公开了一种用于制造用于涡轮机的部件的可磨损涂层的方法。该方法包括：a）预处理粉状材料; b）生产将要涂覆的组分的可加工的预制品; c）将初步产品施加到待涂覆的部件上; d）预备产品中所含的合成粘合剂被烧掉; e）组分烧结; 和f）组件被后处理。用于制造用于涡轮机的可磨损涂层的方法消除了现有技术已知的解决方案的缺点。特别地，该方法便宜，可以容易地与其他生产工艺步骤组合，例如，必须执行的热处理，并且也适合作为修理的方法。

9. 发明申请

US20090311552A1 COMPONENT WITH A REINFORCING PLATING 审中-公开
标题翻译：具有增强镀层的组件
公开(公告)号：US20090311552A1
公开(公告)日：2009-12-17
申请号：US12296985
申请日：2007-04-04
申请人： Karl-Heinz Manier , Josef Linska , Andre Werner
发明人： Karl-Heinz Manier , Josef Linska , Andre Werner
IPC分类号： C22C19/05
CPC分类号： C23C28/027 , C23C4/073 , C23C4/129 , C23C4/18 , C23C28/022 , C25D15/02 , F01D5/288 , Y10T428/12486
摘要： A component, in particular a rotor blade of a gas turbine, having a blade tip plating, the plating including a cover layer that is formed of abrasive particles embedded in a metallic matrix material, and the cover layer being applied onto a surface of the component with the intermediate situation of a metallic bonding layer, wherein the metallic bonding layer is fashioned as a bonding layer applied to the component by high-speed flame spraying, and that the metallic matrix material of the cover layer is galvanically deposited.
摘要翻译：一种具有叶片顶板的组件，特别是燃气轮机的转子叶片，所述镀层包括由嵌入在金属基体材料中的磨料颗粒形成的覆盖层，并且所述覆盖层被施加到所述部件的表面上在金属接合层的中间情况下，通过高速火焰喷涂将金属接合层形成为施加到部件上的接合层，并且覆盖层的金属基体材料被电镀沉积。

10. 发明授权

US4700311A System for optimizing process parameters in photoactive semiconductor manufacturing in-situ 失效
标题翻译：光源半导体制造原位工艺参数优化系统
公开(公告)号：US4700311A
公开(公告)日：1987-10-13
申请号：US694932
申请日：1985-01-25
申请人： Helmut Tributsch , Gerhard Beck , Marinus Kunst , Udo Kuppers , Hans-Joachim Lewerenz , Jochen Lilie , Andre Werner
发明人： Helmut Tributsch , Gerhard Beck , Marinus Kunst , Udo Kuppers , Hans-Joachim Lewerenz , Jochen Lilie , Andre Werner
IPC分类号： H01L21/66 , H01L21/205 , H01L31/04 , H01L31/20 , C30B25/16 , H01L31/18
CPC分类号： H01L31/202 , Y02E10/50 , Y02P70/521 , Y10S136/29
摘要： Materials and systems substantially having photoactive properties are produced with a high quality output and without time losses in the fabrication process. To determine the quality of the photoactive material in situ, conductivity is induced in the material by exciting charge carriers through irradiation, and an electromagnetic field influenced thereby is measured, with the result of the measurement being evaluated by a computer with a corresponding control of actuating members such as valves and controllers. Optimum process parameters are thus found and used for the process.
摘要翻译：基本上具有光敏性质的材料和系统在制造过程中以高质量的输出产生并且没有时间损失。为了在原位确定光活性材料的质量，通过照射激发载流子，在材料中诱发电导率，并且测量受影响的电磁场，其结果是通过计算机进行评估，计算机具有相应的致动控制会员如阀门和控制器。因此找到最佳工艺参数并用于该过程。

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