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21. 发明申请

US20100158691A1 Component and Method for Joining Metal Elements 有权
标题翻译：用于连接金属元件的组件和方法
公开(公告)号：US20100158691A1
公开(公告)日：2010-06-24
申请号：US12225350
申请日：2007-03-14
申请人： Herbert Hanrieder , Alexander Gindorf , Reinhold Meier
发明人： Herbert Hanrieder , Alexander Gindorf , Reinhold Meier
IPC分类号： F01D5/14 , B32B15/01 , B23K13/01
CPC分类号： B23K20/021 , B23K2101/001 , F01D5/3061 , F05D2230/232 , Y10T428/12493
摘要： A component, in particular a component of a gas turbine, is described composed of at least two metallic structural elements, the first structural element having a first joining surface, and the second structural element having a second joining surface, and the structural elements being joined via their joining surfaces by an inductive high-frequency pressure welding. One of the joining surfaces is shaped to widen peripherally in comparison to the other joining surface, and an upsetting deformation produced in a join region in response to the joining of the structural elements rests virtually entirely within and, in particular, on a peripheral collar formed by the peripheral widening of the one joining surface. A method is described for joining metallic structural elements, in particular structural elements of a gas turbine, an inductive high-frequency pressure welding being used to join corresponding joining surfaces of the structural elements.
摘要翻译：描述了一种组件，特别是燃气轮机的部件，其由至少两个金属结构元件组成，第一结构元件具有第一接合表面，第二结构元件具有第二接合表面，并且结构元件被连接通过其接合表面通过感应式高频压力焊接。其中一个接合表面被成形为与其它接合表面相比在外围加宽，并且响应于结构元件的接合而在连接区域中产生的镦锻变形基本上完全搁置在并且特别地在形成的外围套环上通过一个连接表面的外围加宽。描述了用于连接金属结构元件，特别是燃气轮机的结构元件的方法，用于连接结构元件的相应接合表面的感应式高频压力焊接。

22. 发明申请

US20090096138A1 Method for Production of a Honeycomb Seal 审中-公开
标题翻译：蜂窝密封的生产方法
公开(公告)号：US20090096138A1
公开(公告)日：2009-04-16
申请号：US12225981
申请日：2007-03-29
申请人： Reinhold Meier
发明人： Reinhold Meier
IPC分类号： B28B1/24 , C04B33/32 , B22F5/10
CPC分类号： B22F3/225 , B22F5/009 , B22F2998/10 , B28B11/006 , B28B2003/203 , C04B38/0012 , C04B2111/00982 , F01D11/127 , F02C7/045 , F05D2230/00 , C04B35/00 , C04B38/08 , B22F3/1112 , B22F3/10
摘要： A method for manufacturing a honeycomb seal by powder-metallurgical injection molding is described wherein, during the powder-metallurgical injection molding; mixing a metal powder and/or a ceramic powder with at least one binding agent to produce a homogeneous mass; subsequently fabricating a molded article for the honeycomb seal having honeycomb-structured cells from the homogeneous mass by injection molding; subsequently performing a debindering process on the molded article; and, subsequently thereto, compacting the molded article via a sintering process to form the honeycomb seal having the desired geometric properties. Prior to the sintering process, partially filling at least some of the cells of the molded article in each case with at least one hollow body, subsequently sintering the molded article together with the hollow bodies that have been introduced into the cells.
摘要翻译：描述了一种通过粉末冶金注射成型制造蜂窝密封件的方法，其中在粉末冶金注射成型期间; 将金属粉末和/或陶瓷粉末与至少一种粘合剂混合以产生均匀的质量; 随后通过注射成型从均质物质制造具有蜂窝结构的蜂窝状蜂窝状密封体的模制品; 随后对模塑制品进行脱粘工艺; 随后通过烧结工艺压制模塑制品以形成具有所需几何性能的蜂窝状密封件。在烧结过程之前，用至少一个中空体在每种情况下部分地填充模塑制品的至少一些细胞，随后将模制品与已经引入细胞的中空体一起烧结。

23. 发明申请

US20080244905A1 Method For Joining Blades to Blade Roots or Rotor Disks When Manufacturing and/or Repairing Gas Turbine Blades or Integrally Bladed Gas Turbine Rotors 失效
标题翻译：在制造和/或修理燃气轮机叶片或整体叶片燃气轮机转子时将叶片连接到叶片根或转子盘的方法
公开(公告)号：US20080244905A1
公开(公告)日：2008-10-09
申请号：US10570418
申请日：2005-06-30
申请人： Reinhold Meier
发明人： Reinhold Meier
IPC分类号： B23P15/04
CPC分类号： B23P6/002 , B23K26/24 , B23K33/004 , B23K2101/001 , B23P15/006 , F01D5/005 , F01D5/3061 , Y02T50/673 , Y10T29/49316 , Y10T29/49318 , Y10T29/49321 , Y10T29/49336 , Y10T29/49728
摘要： A method is provided for joining blades to blade roots or rotor disks when manufacturing and/or repairing gas turbine blades or integrally bladed gas turbine rotors. A blade and a blade root or rotor disk that is to be joined to the blade are supplied, and provided with a thickening in sections that are to be joined together. The sections of the blade and the blade root or rotor disk that are to be joined together are machined so as to form recesses and; c) are then aligned relative to each other, opposite recesses defining at least one groove-shaped seam preparation. The blade and the blade root or rotor disk are joined in the area of the or each seam preparation by means of laser power build-up welding and the joined blade and blade root or rotor disk are machined so as to provide a gas turbine blade or an integrally bladed gas turbine rotor having a predefined geometrical profile.
摘要翻译：提供了一种用于在制造和/或修理燃气涡轮叶片或整体叶片燃气轮机转子时将叶片接合到叶片根部或转子盘的方法。供给要连接到叶片的叶片和叶片根部或转子盘，并且设置有要连接在一起的部分的增厚部。要连接在一起的叶片和叶片根部或转子盘的部分被加工成形成凹部; c）然后相对于彼此对准，相对的凹部限定至少一个槽形接缝制备。叶片和叶片根部或转子盘通过激光发电焊接在该接缝制备区域或每个接缝制备区域中接合，并且加工接合的叶片和叶片根部或转子盘以提供燃气轮机叶片或具有预定几何轮廓的整体叶片燃气轮机转子。

24. 发明申请

US20080135602A1 Process for Manufacturing a Honeycomb Seal 有权
标题翻译：蜂窝密封制造工艺
公开(公告)号：US20080135602A1
公开(公告)日：2008-06-12
申请号：US11578875
申请日：2005-03-31
申请人： Reinhold Meier
发明人： Reinhold Meier
IPC分类号： B23K26/34
CPC分类号： B23K35/0244 , B23K26/32 , B23K26/342 , B23K35/3033 , B23K35/3046 , B23K35/3053 , B23K2101/02 , B23K2103/02 , B23K2103/26 , B23K2103/50
摘要： A process for manufacturing a honeycomb seal is disclosed. The process includes the following steps: a) the honeycomb structure is brought to the desired three-dimensional form and is fixed in this form; b) then the honeycomb structure is filled with a filler material; c) then the honeycomb structure filled with the filler material is machined on a side on which a carrier element is arranged, such that this side has the desired contour and that the end edges of the honeycomb structure are sealed flushly with the filler compound; d) then the side contoured in this way is coated with a coating; e) next the carrier element is applied to the coating, preferably by laser powder build-up welding.
摘要翻译：公开了一种制造蜂窝密封件的方法。该方法包括以下步骤：a）将蜂窝结构体形成所需的三维形状并以此形式固定; b）然后蜂窝结构填充填料; c）然后，填充有填充材料的蜂窝结构体在其上布置有载体元件的一侧被加工，使得该侧具有期望的轮廓，并且蜂窝结构的端边缘与填料混合物密封; d）然后以这种方式形成的侧面涂覆有涂层; e）接下来，将载体元件施加到涂层上，优选地通过激光粉末堆积焊接。

25. 发明申请

US20080090093A1 Method for the Production of a Composite Component Comprising Two Component Sections with a Basic Adhesive Nickel Layer Located Between the Two Component Sections 审中-公开
标题翻译：用于生产包含位于两个部件部分之间的基本粘合剂镍层的两个部件部分的复合部件的方法
公开(公告)号：US20080090093A1
公开(公告)日：2008-04-17
申请号：US11950202
申请日：2007-12-04
申请人： Reinhold Meier
发明人： Reinhold Meier
IPC分类号： B29C65/48 , B29C65/06 , B32B7/04
CPC分类号： B23K1/19 , B23K10/027 , B23K20/2275 , B23K26/32 , B23K26/342 , B23K35/002 , B23K35/004 , B23K35/005 , B23K35/0244 , B23K35/3033 , B23K2101/00 , B23K2101/001 , B23K2103/02 , B23K2103/10 , B23K2103/14 , B23K2103/15 , B23K2103/18 , B23K2103/20 , B23K2103/26 , B23K2103/50 , Y10T156/10 , Y10T428/12229
摘要： The present technology generally relates to a method for producing a composite component, preferably, a composite gas turbine component, wherein the composite component exhibits a first component section made of a magnesium-based material or an aluminum-based material and a second component section made of a high-strength material, preferably, made of an iron-based or nickel-based or titanium-based or cobalt-based material. The method comprises at least the following steps: a) providing the first component section (11) made of the magnesium-based material or the aluminum-based material; b) coating the first component section (11) made of the magnesium-based material or the aluminum-based material with an adhesive layer (12) in at least one fusion area for the second component section, where a nickel-based material, preferably, a nickel alloy material, is used as the coating material for the adhesive layer; c) providing the second component section (13) made of the high-strength material, preferably, made of the iron-based or nickel-based or titanium-based or cobalt-based material; d) joining the second component section (13) made of the high-strength material to the fusion area, which is coated with the adhesive layer (12) and is part of the first component section (11) made of the magnesium-based material or the aluminum-based material.
摘要翻译：本发明技术通常涉及复合成分的制造方法，优选复合燃气轮机部件，其中复合部件呈现由镁基材料或铝基材料构成的第一部件部分和第二部件部分的高强度材料，优选由铁基或镍基或钛基或钴基材料制成。该方法至少包括以下步骤：a）提供由镁基材料或铝基材料制成的第一部件部分（11）; b）在第二组分部分的至少一个熔融区域中用粘合剂层（12）涂覆由镁基材料或铝基材料制成的第一组分部分（11），其中优选镍基材料使用镍合金材料作为粘合剂层的涂料; c）提供由高强度材料制成的第二部件部分（13），优选由铁基或镍基或钛基或钴基材料制成; d）将由高强度材料制成的第二组分部分（13）连接到涂覆有粘合剂层（12）的熔融区域，并且是由镁基材料制成的第一组分部分（11）的一部分或铝基材料。

26. 发明申请

US20070235505A1 Method for Repairing or Manufacturing a Component 失效
标题翻译：修理或制造零件的方法
公开(公告)号：US20070235505A1
公开(公告)日：2007-10-11
申请号：US11632356
申请日：2005-07-16
申请人： Reinhold Meier
发明人： Reinhold Meier
IPC分类号： B23K1/06 , B23K31/00
CPC分类号： B23P6/002 , B23K26/342 , B23K33/00 , B23K35/0244 , B23K2101/001 , B23P15/04 , F01D9/044 , F05D2230/234 , F05D2230/31 , F05D2230/80 , Y10T29/49734
摘要： The invention relates to a method for repairing a structural component, especially a stator-side structural component of a gas turbine such as a housing or a guide vane ring, whereby a damaged section is separated-out from the structural component, and whereby a new section that replaces the damaged as well as separated-out section is fixedly or rigidly connected with the structural component by welding. According to the invention, the damaged section is separated-out from the structural component to be repaired in such a manner so that the length of a separating seam and therewith a later weld seam is minimized, whereby depending on the material thickness distribution along the separating seam, for providing a most uniform possible material thickness along the later weld seam, material is removed from the structural component, and whereby after the connecting of the structural component with the new section, at least the removed material is renewed by laser powder deposit welding.
摘要翻译：本发明涉及一种用于修理结构部件，特别是诸如外壳或导向叶片环之类的燃气轮机的定子侧结构部件的方法，其中损坏部分与结构部件分离，由此新的通过焊接将损坏和分离部分替换为结构部件固定或刚性连接。根据本发明，损伤部分从被修复的结构部件中分离开，使得分离缝的长度和随后的焊缝的长度最小化，由此取决于沿着分离的材料厚度分布接缝，用于沿着后续焊缝提供最均匀的可能的材料厚度，从结构部件移除材料，并且由此在结构部件与新部分连接之后，至少通过激光粉末沉积焊接来更新所移除的材料。

27. 发明申请

US20070172319A1 Milling tool and method for milling recesses 失效
标题翻译：铣削刀具和铣削凹槽的方法
公开(公告)号：US20070172319A1
公开(公告)日：2007-07-26
申请号：US10578702
申请日：2004-10-23
申请人： Reinhold Meier , Georg Moosrainer , Wilfried Schuette
发明人： Reinhold Meier , Georg Moosrainer , Wilfried Schuette
IPC分类号： B26D1/12
CPC分类号： B23C5/08 , B23C3/18 , B23C3/34 , B23C2220/366 , Y10T29/49318 , Y10T29/49325 , Y10T29/49995 , Y10T407/19 , Y10T409/303808 , Y10T409/304424
摘要： A milling tool which is used to mill recesses, in particular, circular-shaped grooves, in a workpiece is provided. The milling tool (10) is disposed on a disk-shaped or plate-shaped base body (14) and on at least one cutting body (15) arranged on the outer periphery of the base body (14). The cutting body or each cutting body (15) is inclined in relation to the disk-shaped base body or the plate-shaped base body (14).
摘要翻译：提供了用于在工件中研磨凹部，特别是圆形凹槽的铣削工具。铣刀（10）设置在盘状或板状的基体（14）上，以及配置在基体（14）的外周的至少一个切割体（15）上。切割体或每个切割体（15）相对于盘形基体或板状基体（14）倾斜。

28. 发明申请

US20070119830A1 Method for connecting components 审中-公开
标题翻译：组件连接方法
公开(公告)号：US20070119830A1
公开(公告)日：2007-05-31
申请号：US10588538
申请日：2005-01-28
申请人： Reinhold Meier
发明人： Reinhold Meier
IPC分类号： B23K26/34 , B23K15/00
CPC分类号： B23K15/0053 , B23K26/144 , B23K26/24 , B23K26/342 , B23K2101/001 , F05B2230/234
摘要： A method for connecting dynamically loaded components, especially gas turbine components is provided. At least two components (10, 11; 14, 15) to be interconnected are connected by means of laser powder build-up welding.
摘要翻译：提供了用于连接动态加载的部件，特别是燃气轮机部件的方法。要互连的至少两个组件（10,11; 14,15）通过激光粉末堆积焊接连接。

29. 发明申请

US20070090152A1 Method for cladding the blade tips of rotor blades of a gas turbine power plant and device for carrying out the method 审中-公开
标题翻译：用于包覆燃气轮机发电厂的转子叶片的叶片尖端的方法以及用于实施该方法的装置
公开(公告)号：US20070090152A1
公开(公告)日：2007-04-26
申请号：US10560564
申请日：2004-06-04
申请人： Reinhold Meier , Mario Schmidt
发明人： Reinhold Meier , Mario Schmidt
IPC分类号： A47J36/02
CPC分类号： F01D5/286 , B23K35/0233 , B23K35/327 , C23C2/04 , C23C26/02
摘要： A method is for the cladding of blade tips of compressor blades of a gas turbine power plant, using a blank, which is made up of a solder foil provided with a metal layer having embedded hard particles and which is adapted to the geometry of the blade tip that is to be clad, which blank is melted onto the blade tip while applying pressure, and in the process obtains, impressed into it, a ribbed or pimpled structure.
摘要翻译：一种方法是用燃料涡轮机动力装置的压缩机叶片的叶片尖端进行包层，该坯料使用由设置有具有嵌入的硬质颗粒的金属层并且适于叶片几何形状的焊料箔构成的坯料要被包覆的尖端，该空白在施加压力的同时熔化在叶片尖端上，并且在该过程中，将其压入其中，形成有肋或者是疙瘩的结构。

30. 发明申请

US20060131815A1 Honeycomb seal 审中-公开
标题翻译：蜂窝密封
公开(公告)号：US20060131815A1
公开(公告)日：2006-06-22
申请号：US10537504
申请日：2003-11-21
申请人： Reinhold Meier
发明人： Reinhold Meier
IPC分类号： F16J15/447
CPC分类号： F01D11/127 , B22F2998/00 , F02C7/28 , F16J15/444 , Y02T50/671 , B22F3/225 , B22F5/009
摘要： A honeycomb seal which is manufactured by powder metallurgical injection molding is disclosed. The honeycomb seal is composed preferably of several segments. Each segment is embodied as a single piece and has a base element as well as honeycomb elements that are embodied as a single piece with the base element.
摘要翻译：公开了一种通过粉末冶金注射成型制造的蜂窝状密封件。蜂窝密封件优选地由多个部分组成。每个片段被实施为单件，并且具有基本元件以及被实施为具有基本元件的单件的蜂窝元件。

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