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1. 发明申请

US20130174869A1 CLEANING OF A TURBO-MACHINE STAGE 有权
标题翻译：涡轮机清洁度
公开(公告)号：US20130174869A1
公开(公告)日：2013-07-11
申请号：US13813919
申请日：2011-08-03
申请人： Jürgen Rösing , Frank Seidel , Lutz Winkler , Bernd Kriegl , Thomas Uihlein , Martin Dürr , Fabian Moritz
发明人： Jürgen Rösing , Frank Seidel , Lutz Winkler , Bernd Kriegl , Thomas Uihlein , Martin Dürr , Fabian Moritz
IPC分类号： B24C1/00
CPC分类号： B24C1/003 , B08B7/0021 , B08B9/00 , B24C1/086 , B24C3/325 , F01D25/002
摘要： The invention relates to a method for cleaning a turbo-machine stage (100) consisting of at least one of the following steps: a cleaning nozzle (1) is introduced into an opening of a turbo-machine, in particular into an inspection opening (220); and the blade (100) of the stage is acted upon by solid particles, said particles subliming at the blade temperature, in particular into dry ice particles.
摘要翻译：本发明涉及一种用于清洁由以下至少一个步骤组成的涡轮机台（100）的方法：将清洁喷嘴（1）引入涡轮机的开口中，特别是引入到检查开口 220）; 并且所述台的叶片（100）由固体颗粒作用，所述颗粒在叶片温度下升华，特别是干冰颗粒。

2. 发明授权

US09492906B2 Cleaning of a turbo-machine stage 有权
标题翻译：清洗涡轮机台
公开(公告)号：US09492906B2
公开(公告)日：2016-11-15
申请号：US13813919
申请日：2011-08-03
申请人： Jürgen Rösing , Frank Seidel , Lutz Winkler , Bernd Kriegl , Thomas Uihlein , Martin Dürr , Fabian Moritz
发明人： Jürgen Rösing , Frank Seidel , Lutz Winkler , Bernd Kriegl , Thomas Uihlein , Martin Dürr , Fabian Moritz
IPC分类号： B08B7/00 , B24C1/00 , B08B9/00 , B24C1/08 , B24C3/32 , F01D25/00
CPC分类号： B24C1/003 , B08B7/0021 , B08B9/00 , B24C1/086 , B24C3/325 , F01D25/002
摘要： The invention relates to a method for cleaning a turbo-machine stage (100) consisting of at least one of the following steps: a cleaning nozzle (1) is introduced into an opening of a turbo-machine, in particular into an inspection opening (220); and the blade (100) of the stage is acted upon by solid particles, said particles subliming at the blade temperature, in particular into dry ice particles.
摘要翻译：本发明涉及一种用于清洁由以下至少一个步骤组成的涡轮机台（100）的方法：将清洁喷嘴（1）引入涡轮机的开口中，特别是引入到检查开口 220）; 并且所述台的叶片（100）由固体颗粒作用，所述颗粒在叶片温度下升华，特别是干冰颗粒。

3. 发明授权

US08012562B2 Wear-resistant coating 有权
标题翻译：耐磨涂层
公开(公告)号：US08012562B2
公开(公告)日：2011-09-06
申请号：US12163677
申请日：2008-06-27
申请人： Wolfgang Eichmann , Falko Heutling , Thomas Uihlein
发明人： Wolfgang Eichmann , Falko Heutling , Thomas Uihlein
IPC分类号： B32B5/12 , B32B7/00
CPC分类号： C23C14/226 , C23C28/322 , C23C28/34 , C23C28/3455 , C23C28/347 , C23C28/36 , C23C28/42 , F01D5/288 , F05D2230/313 , F05D2300/614 , Y10T428/12542 , Y10T428/12549 , Y10T428/12576 , Y10T428/12611 , Y10T428/12618 , Y10T428/12632 , Y10T428/12875 , Y10T428/24058 , Y10T428/24174 , Y10T428/24355 , Y10T428/24413
摘要： The present technology generally relates to a wear-resistant coating, especially for gas turbine components, comprising a horizontally segmented or multilayered structure, i.e. at least one relatively hard, ceramic layer and at least one relatively soft, metallic layer. The ceramic layer and the metallic layer are alternately arranged on top of each other in such a way that an external layer forming an external surface of the wear-resistant coating is embodied as a ceramic layer. According to the invention, at least the external, ceramic layer is segmented in a column-type manner in a vertical direction.
摘要翻译：本技术通常涉及耐磨涂层，特别是对于燃气轮机部件，包括水平分段或多层结构，即至少一个相对硬的陶瓷层和至少一个相对柔软的金属层。陶瓷层和金属层交替地布置在彼此的顶部上，使得形成耐磨涂层的外表面的外层被实施为陶瓷层。根据本发明，至少外部陶瓷层在垂直方向上以列式方式分段。

4. 发明申请

US20110045264A1 EROSION PROTECTION COATING 有权
标题翻译：防腐保护涂料
公开(公告)号：US20110045264A1
公开(公告)日：2011-02-24
申请号：US12988045
申请日：2009-04-18
申请人： Falko Heutling , Thomas Uihlein , Wolfgang Eichmann
发明人： Falko Heutling , Thomas Uihlein , Wolfgang Eichmann
IPC分类号： B32B7/02
CPC分类号： C23C14/0641 , C23C14/027 , C23C28/044 , C23C28/048 , C23C28/42 , F01D5/284 , F01D5/288 , F05D2300/506 , Y10T428/24975 , Y10T428/24983
摘要： The invention relates to an erosion protection coating (11), in particular, for gas turbine components, having a horizontally segmented and/or multi-layered construction. i.e., having at least one relatively hard layer (12) and having at least one relatively soft layer (13), wherein the relatively hard layer or each relatively hard layer as well as the relatively soft layer or each relatively soft layer are disposed on top of one another in an alternating manner, in such a way that an outer-lying layer, which forms an outer surface of the erosion protection coating, is formed as a relatively hard layer (12). According to the invention, the relatively hard layer or each relatively hard layer (12) as well as the relatively soft layer or each relatively soft layer (13) are formed as a ceramic layer in each case.
摘要翻译：本发明涉及具有水平分段和/或多层结构的用于燃气轮机部件的侵蚀保护涂层（11）。即具有至少一个相对较硬的层（12）并且具有至少一个相对软的层（13），其中相对较硬的层或每个相对硬的层以及相对软的层或每个相对软的层设置在顶部彼此以交替的方式，以形成侵蚀保护涂层的外表面的外层作为相对硬的层（12）形成。根据本发明，在每种情况下，相对硬的层或每个相对硬的层（12）以及相对软的层或每个相对软的层（13）形成为陶瓷层。

5. 发明申请

US20110020548A1 DEVICE AND METHOD FOR THE PARTIAL COATING OF COMPONENTS 审中-公开
标题翻译：组件部分涂层的装置和方法
公开(公告)号：US20110020548A1
公开(公告)日：2011-01-27
申请号：US12867672
申请日：2009-02-04
申请人： Wolfgang Eichmann , Falko Heutling , Thomas Uihlein , Josef Lachner
发明人： Wolfgang Eichmann , Falko Heutling , Thomas Uihlein , Josef Lachner
IPC分类号： B05D1/32 , B05C9/00
CPC分类号： F01D5/288 , C23C4/01 , C23C14/042 , C23C28/00 , C23C28/321 , C23C28/322 , C23C28/34 , C23C28/42 , F01D5/005 , F01D25/007
摘要： A device and method for the partial coating of a component, particularly for the coating of components of a gas turbine or an aircraft engine, is disclosed. The device includes at least one base receptacle for at least partially receiving the component and a first partial region of the component not to be coated. The device further includes at least one plate-shaped cover that can be positioned in the base receptacle, where the cover includes at least one recess or opening for a second partial region of the component to be coated to pass through. The shape of the recess or opening corresponds to the profile of the component in the region between the partial region not to be coated and the partial region to be coated.
摘要翻译：公开了用于部件涂覆部件的装置和方法，特别是用于喷涂燃气轮机或飞行器发动机部件的涂覆。该装置包括用于至少部分地接收该部件的至少一个基座容器和不被涂覆的部件的第一部分区域。该装置还包括至少一个板状盖，其可以定位在基座容器中，其中盖包括用于待涂覆的部件的第二部分区域通过的至少一个凹部或开口。凹部或开口的形状对应于在未被涂覆的部分区域和待涂覆的部分区域之间的区域中的部件的轮廓。

6. 发明申请

US20100263694A1 DECOATING DEVICE FOR AXIALLY SYMMETRIC COMPONENTS, PARTICULARLY FROM AIRCRAFT ENGINES 审中-公开
标题翻译：用于轴对称组件的特殊装置，特别是来自飞机发动机
公开(公告)号：US20100263694A1
公开(公告)日：2010-10-21
申请号：US12312273
申请日：2007-10-27
申请人： Thomas Uihlein , Wolfgang Eichmann , Falko Heutling , Markus Uecker , Thomas Brendel , Georgios Paronis , Anton Albrecht , Manfred Berger
发明人： Thomas Uihlein , Wolfgang Eichmann , Falko Heutling , Markus Uecker , Thomas Brendel , Georgios Paronis , Anton Albrecht , Manfred Berger
IPC分类号： B08B3/00
CPC分类号： C23G3/00 , C23F1/08 , C25F5/00
摘要： A decoating device for axially symmetric components, particularly from aircraft engines is provided, the decoating process being carried out through the use of a decoating fluid-which is brought on a localized basis into contact with the component to be decoated, a receptacle for holding the decoating fluid being provided that rotates at least about one axis of rotation, and the decoating fluid surface forming a rotation paraboloid in response to the rotation, the component(s) to be decoated on a localized basis being accommodated in the receptacle and being dipped on the radially outer side into the decoating fluid. A decoating device is thereby devised which makes it possible for radially symmetric components to be decoated in the radially outer region in a simple process.
摘要翻译：提供了一种用于轴向对称部件的脱色装置，特别是来自飞机发动机的脱色装置，其通过使用与局部基准成一体的脱色液体进行脱色处理，与脱漆部件接触，提供了旋转至少约一个旋转轴线的旋转流体，并且旋转流体表面响应于旋转而形成旋转抛物面，待局部放置的待分解的部件被容纳在容器中并被浸入径向外侧进入脱水流体。从而设计出一种可以在简单的过程中将径向对称的部件在径向外部区域中解体的装置。

7. 发明申请

US20100119376A1 INLET CONE FOR JET ENGINE 审中-公开
标题翻译：喷射发动机入口锥体
公开(公告)号：US20100119376A1
公开(公告)日：2010-05-13
申请号：US12442520
申请日：2007-09-18
申请人： Thomas Uihlein , Markus Uecker , Olivier Seite
发明人： Thomas Uihlein , Markus Uecker , Olivier Seite
IPC分类号： B64C11/14
CPC分类号： F02C7/05 , F02K3/06 , F05D2250/232
摘要： Inlet cone (1) for a jet engine (10) configured as a bypass turbojet engine, which has an engine core area (11) and a casing area (12) that surrounds it, whereby the inlet cone (1) is placed concentrically in the air inlet area of the jet engine (10) and placed on a turnably supported shaft (14), whereby the inlet cone (1) has a conical angle (15) at which solid bodies (16) impinging with the air flow onto the inlet cone (1) ricochet off it in motion paths (17) which lead most of the solid bodies (16) into the casing area (12). Thereby an inlet cone (1) is created in which the entry of solid bodies 16 into the engine core area (11) can be minimized.
摘要翻译：用于喷气发动机（10）的入口锥（1），其构造为旁通涡轮喷气发动机，其具有发动机芯区域（11）和围绕其的壳体区域（12），由此入口锥体（1）同心地放置在喷气发动机（10）的空气入口区域并且放置在可转动地支撑的轴（14）上，由此入口锥体（1）具有锥形角（15），在该锥形角处，实心体（16）撞击空气流动到入口锥体（1）在大部分固体（16）进入套管区域（12）的运动路径（17）中旋转。因此，产生入口锥体（1），其中实体16进入发动机芯部区域（11）的入口锥度可以最小化。

8. 发明申请

US20100108538A1 METHOD FOR STRIPPING A COMPONENT 审中-公开
标题翻译：剥离组件的方法
公开(公告)号：US20100108538A1
公开(公告)日：2010-05-06
申请号：US12451153
申请日：2008-05-02
申请人： Anton Albrecht , Wolfgang Eichmann , Georgios Paronis , Thomas Uihlein
发明人： Anton Albrecht , Wolfgang Eichmann , Georgios Paronis , Thomas Uihlein
IPC分类号： C25F5/00
CPC分类号： C25F5/00 , F01D5/005
摘要： A method for stripping a component, in particular a gas turbine component, to completely or partially remove a multilayer or sandwich antiwear coating from the surface of the component, the antiwear coating including at least one relatively hard ceramic layer and at least one relatively soft metallic layer is disclosed. According to the present invention, in order to remove the multilayer or sandwich antiwear coating, the component is placed in a bath of an alkaline electrolyte, the component placed in the electrolyte being stripped at a current density of between 1 A/dm2 and 20 A/dm2.
摘要翻译：一种用于剥离部件，特别是燃气轮机部件的方法，用于从部件的表面完全或部分地去除多层或夹层抗磨损涂层，所述抗磨损涂层包括至少一个相对硬的陶瓷层和至少一个相对软的金属层被公开。根据本发明，为了去除多层或夹层抗磨损涂层，将组分置于碱性电解液的浴中，放置在电解质中的组分以10A / dm2至20A的电流密度剥离 / dm2。

9. 发明申请

US20100064515A1 METHOD FOR REPAIRING AND/OR REPLACING INDIVIDUAL ELEMENTS OF A GAS TURBINE COMPONENT 审中-公开
标题翻译：修理和/或更换气体涡轮组件的个人元素的方法
公开(公告)号：US20100064515A1
公开(公告)日：2010-03-18
申请号：US12307704
申请日：2007-06-30
申请人： Wolfgang Eichmann , Falko Heutling , Thomas Uihlein , Alexander Gindorf
发明人： Wolfgang Eichmann , Falko Heutling , Thomas Uihlein , Alexander Gindorf
IPC分类号： B23P6/00
CPC分类号： B23P6/005 , B23K13/015 , B23K2101/001 , B23K2101/34 , B23K2103/14 , F01D5/005 , F05D2230/232 , F05D2230/80 , F05D2230/90 , Y02T50/67 , Y10T29/49318
摘要： The present invention relates to a method for repairing and/or replacing individual elements of a gas turbine component (10), particularly for repairing and/or replacing a blade or blade part arranged on a rotor support of a gas turbine, at least some of the components (10) being provided with at least one wear-resistant and/or erosion-resistant layer and the method comprising the following steps: a) a coated or uncoated individual element that is damaged and/or needs to be replaced is removed from the component (10); b) a coated, partially coated or uncoated replacement element (12) is provided; c) the replacement element (12) is fed and aligned relative to the component (10); and d) the replacement element (12) is connected to the component (10), corresponding contact areas (20, 22) of the replacement element (12) and the component (10) being connected by means of an inductive low-frequency or high-frequency pressure welding process.
摘要翻译：本发明涉及一种用于修理和/或更换燃气轮机部件（10）的各个元件的方法，特别是用于修理和/或更换布置在燃气轮机的转子支架上的叶片或叶片部件，至少部分组件（10）设置有至少一个耐磨损和/或抗侵蚀层，并且该方法包括以下步骤：a）被损坏和/或需要更换的涂覆或未涂覆的单独元件从组件（10）; b）提供涂覆的，部分涂覆的或未涂覆的替代元件（12）; c）替换元件（12）相对于部件（10）进给和对准; 以及d）替换元件（12）连接到组件（10），替换元件（12）的相应接触区域（20,22）和组件（10）通过感应低频或高频压焊工艺。

10. 发明授权

US09427937B2 Anti-wear coating 有权
标题翻译：防磨损涂层
公开(公告)号：US09427937B2
公开(公告)日：2016-08-30
申请号：US13880904
申请日：2011-10-25
申请人： Thomas Uihlein , Wolfgang Eichmann , Falko Heutling , Annegret Brendel
发明人： Thomas Uihlein , Wolfgang Eichmann , Falko Heutling , Annegret Brendel
IPC分类号： B32B7/00 , B32B7/02 , C23C28/04 , C23C28/00 , F01D5/28
CPC分类号： B32B7/02 , B32B2250/42 , C04B2237/04 , C04B2237/086 , C04B2237/363 , C04B2237/597 , C23C28/042 , C23C28/044 , C23C28/40 , F01D5/288 , F05D2230/313 , F05D2300/611 , Y10T428/24149
摘要： The invention relates to an anti-wear coating, specifically for components which are subject to erosion under mechanical loading, in particular for gas turbine components, said coating comprising at least two different individual layers which preferably alternate with one another multiply and are applied to a surface of a component which is to be coated. The individual layers comprise a ceramic main layer (45, 46, 47, 48) and a quasi-ductile, non-metallic intermediate layer (41, 42, 43, 44).
摘要翻译：本发明涉及一种抗磨损涂层，特别涉及在机械载荷下遭受侵蚀的部件，特别是对于燃气轮机部件，所述涂层包括至少两个不同的单独层，其优选地彼此交替并被施加到要被涂覆的部件的表面。各层包括陶瓷主层（45,46,47,48）和准延性非金属中间层（41,42,43,44）。

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