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1. 发明申请

US20140178206A1 METHOD FOR CREATING A BLADE FOR A FLOW ENGINE AND BLADE FOR A FLOW FORCE ENGINE 有权
标题翻译：用于制造用于流动发动机的叶片和用于流动力发动机的叶片的方法
公开(公告)号：US20140178206A1
公开(公告)日：2014-06-26
申请号：US14234569
申请日：2012-07-20
申请人： Jens Göhler , Frank Kernstock , Olaf Rehme , Martin Schäfer
发明人： Jens Göhler , Frank Kernstock , Olaf Rehme , Martin Schäfer
IPC分类号： F01D5/14
CPC分类号： F01D5/14 , B22F3/1055 , B22F5/04 , B22F7/08 , B22F2007/068 , B23K26/34 , B23K2101/001 , B23P6/007 , B23P15/04 , F01D5/005 , F01D5/286 , F05D2230/21 , F05D2230/31 , F05D2240/303 , F05D2260/602 , Y02P10/295 , Y10T29/49336
摘要： A method for creating a blade (11) for a turbo-engine and such a blade are disclosed. Components (19) of the blade are produced by an additive production method such as selective laser melting or fusion, while a main body (18) is produced by casting, for example. The blade components (19) may consist of a different material than the basic body (18). The components or body may carry functions such as serving as drainage slots (24). Expense related to the use of additive production methods occurs only for the components (19) in which a complicated geometry, for example, must be implemented. The remaining components in the form of the main body (18), comprising the blade (27), the blade foot (28) and the blade head (29), can be cost-effectively implemented as a cast part or a sheet metal part.
摘要翻译：公开了一种用于涡轮发动机和这种叶片的叶片（11）的制造方法。例如，通过选择性激光熔融或熔融等添加剂制造方法制造刀片的部件（19），而通过铸造制造主体（18）。刀片部件（19）可以由与基体（18）不同的材料组成。部件或主体可以承载诸如用作排水槽（24）的功能。与使用添加剂生产方法相关的费用仅针对必须实施复杂几何的组件（19）。包括刀片（27），刀脚（28）和刀头（29）的主体（18）形式的其余部件可以成本有效地实现为铸件或钣金件。

2. 发明申请

US20130001837A1 TURBINE BLADE AND METHOD FOR ITS PRODUCTION 审中-公开
标题翻译：涡轮叶片及其生产方法
公开(公告)号：US20130001837A1
公开(公告)日：2013-01-03
申请号：US13498415
申请日：2010-09-14
申请人： Jens Göhler , Frank Kernstock , Olaf Rehme , Martin Schäfer
发明人： Jens Göhler , Frank Kernstock , Olaf Rehme , Martin Schäfer
IPC分类号： B29C35/08
CPC分类号： B22F3/1055 , B22F5/04 , B33Y80/00 , Y02P10/295
摘要： A method of producing a turbine blade is provided, wherein the turbine blade is produced by an additive production method. Cavities and/or lattice structures can be produced in one and the same process. The additive production method also allows drainage slots, heating openings, and/or other holes or, as the case may be, recesses to be provided in the turbine blade while the turbine blade is being produced. Holes can furthermore be furnished completely or partially with a lattice structure.
摘要翻译：提供了一种制造涡轮叶片的方法，其中通过添加剂制造方法制造涡轮叶片。腔和/或晶格结构可以在同一过程中产生。添加剂生产方法还允许排气槽，加热开口和/或其他孔，或者视情况而定，在涡轮叶片被制造时要设置在涡轮叶片中的凹槽。孔还可以完全地或部分地配置有格子结构。

3. 发明授权

US09670782B2 Method for creating a blade for a flow engine and blade for a flow force engine 有权
公开(公告)号：US09670782B2
公开(公告)日：2017-06-06
申请号：US14234569
申请日：2012-07-20
申请人： Jens Göhler , Frank Kernstock , Olaf Rehme , Martin Schäfer
发明人： Jens Göhler , Frank Kernstock , Olaf Rehme , Martin Schäfer
IPC分类号： F01D5/14 , B23P6/00 , B22F3/105 , B22F5/04 , B23P15/04 , F01D5/00 , F01D5/28 , B23K26/34 , B23K101/00 , B22F7/08 , B22F7/06
CPC分类号： F01D5/14 , B22F3/1055 , B22F5/04 , B22F7/08 , B22F2007/068 , B23K26/34 , B23K2101/001 , B23P6/007 , B23P15/04 , F01D5/005 , F01D5/286 , F05D2230/21 , F05D2230/31 , F05D2240/303 , F05D2260/602 , Y02P10/295 , Y10T29/49336
摘要： A method for creating a blade (11) for a turbo-engine and such a blade are disclosed. Components (19) of the blade are produced by an additive production method such as selective laser melting or fusion, while a main body (18) is produced by casting, for example. The blade components (19) may consist of a different material than the basic body (18). The components or body may carry functions such as serving as drainage slots (24). Expense related to the use of additive production methods occurs only for the components (19) in which a complicated geometry, for example, must be implemented. The remaining components in the form of the main body (18), comprising the blade (27), the blade foot (28) and the blade head (29), can be cost-effectively implemented as a cast part or a sheet metal part.

4. 发明申请

US20140131921A1 PROCESS FOR SELECTIVE LASER MELTING AND SYSTEM FOR CARRYING OUT SAID PROCESS 审中-公开
标题翻译：选择性激光熔化工艺及其实施过程的系统
公开(公告)号：US20140131921A1
公开(公告)日：2014-05-15
申请号：US14110650
申请日：2012-04-02
申请人： Yves Küsters , Friedrich Lupp , Olaf Rehme , Martin Schäfer
发明人： Yves Küsters , Friedrich Lupp , Olaf Rehme , Martin Schäfer
IPC分类号： B29C67/00
CPC分类号： B29C67/00 , B29C64/153
摘要： A component is manufactured by selective laser melting by a laser having an intensity profile set largely constant by a diffractive optical element, so that the treatment surface which has occurred as a result of this profile is melted uniformly on the surface of the component. Thermal load peaks, such as occur due to an intensity maximum of an unshaped laser, can therefore be advantageously avoided. Moreover, the treatment surface may, for example, have a square shape, so that, in the case of rectangular components, it becomes simpler to produce the corners of the cross section to be manufactured. Overall, as a result, components having improved surface quality can be produced. The system is equipped with suitable optics for generating the intensity profile described.
摘要翻译：通过使用由衍射光学元件大致恒定的强度分布的激光进行选择性激光熔化来制造组件，使得由于该轮廓而发生的处理表面在组件的表面上均匀熔化。因此，可以有利地避免热负荷峰值，例如由于未成形激光器的强度最大值而发生。此外，处理面可以例如为正方形，因此在矩形部件的情况下，制造要制造的截面的角部变得更加简单。总之，结果，可以生产具有改进的表面质量的部件。该系统配备有用于产生所描述的强度分布的合适的光学器件。

5. 发明申请

US20120205996A1 ELECTRICAL MACHINE 有权
标题翻译：电机
公开(公告)号：US20120205996A1
公开(公告)日：2012-08-16
申请号：US13504746
申请日：2010-10-22
申请人： Klaus Büttner , Vladimir Danov , Olaf Rehme , Martin Schäfer
发明人： Klaus Büttner , Vladimir Danov , Olaf Rehme , Martin Schäfer
IPC分类号： H02K9/20
CPC分类号： H02K9/20 , H02K15/00
摘要： The invention relates to an electric machine (100) comprising a stator (107) and a rotor (101), wherein the rotor (101) comprises a hollow shaft (102), wherein a closed hollow space (103) is formed by means of the hollow shaft (102), wherein the closed hollow space (103) is provided for receiving a cooling agent, wherein a three-dimensional transport structure (200) is provided in the closed hollow chamber (103) for transporting the cooling agent. The three-dimensional structure can, for example, be produced by means of applying an adaptive material.
摘要翻译：本发明涉及一种包括定子（107）和转子（101）的电机（100），其中转子（101）包括中空轴（102），其中封闭的中空空间（103）通过空心轴（102），其中设置有用于接收冷却剂的封闭中空空间（103），其中在封闭的中空室（103）中设置有用于输送冷却剂的三维输送结构（200）。例如，可以通过施加自适应材料来生产三维结构。

6. 发明申请

US20120183701A1 METHOD FOR PRODUCING A MARKED OBJECT 审中-公开
标题翻译：生产标记对象的方法
公开(公告)号：US20120183701A1
公开(公告)日：2012-07-19
申请号：US13498228
申请日：2010-09-16
申请人： Heinz Pilz , Olaf Rehme , Martin Schäfer
发明人： Heinz Pilz , Olaf Rehme , Martin Schäfer
IPC分类号： C08J7/04 , B05D5/00
CPC分类号： G06K19/086 , B22F3/1055 , B22F2998/00 , B29C64/00 , B29K2105/203 , B29K2995/0001 , B29L2031/082 , B29L2031/737 , Y02P10/295 , C22C1/08
摘要： A method produces a marked object. To be able to create markings in a particularly flexible way, it is provided that the object is produced by an additive production process, at least one marking being formed in the object during the additive production process. The method makes many degrees of freedom possible in the design of the marking. For example, the method makes it possible in a very simple way for two- or three-dimensional structures to be concealed within the object during the additive production process. In addition or as an alternative, production parameters can be varied, whether stochastically or deterministically, to produce variations in density. For example, a porous microstructure may be produced as a marking. It is also possible for basic material in the object to be left untreated or to be differently treated, so that it forms the marking.
摘要翻译：一种方法产生一个标记对象。为了能够以特别灵活的方式创建标记，条件是通过添加剂生产过程产生物体，在添加剂生产过程中在物体中形成至少一个标记。该方法在标记的设计中可以实现许多自由度。例如，该方法使得在添加剂生产过程中二维或三维结构被隐藏在对象内的非常简单的方式成为可能。另外或作为替代方案，生产参数可以随时改变，也可以确定性地产生密度变化。例如，可以产生多孔微结构作为标记。对象中的基本材料也可以不经处理或被不同地处理，从而形成标记。

7. 发明授权

US09252642B2 Electrical machine 有权
标题翻译：电机
公开(公告)号：US09252642B2
公开(公告)日：2016-02-02
申请号：US13504746
申请日：2010-10-22
申请人： Klaus Büttner , Vladimir Danov , Olaf Rehme , Martin Schäfer
发明人： Klaus Büttner , Vladimir Danov , Olaf Rehme , Martin Schäfer
IPC分类号： H02K9/20
CPC分类号： H02K9/20 , H02K15/00
摘要： The invention relates to an electric machine (100) comprising a stator (107) and a rotor (101), wherein the rotor (101) comprises a hollow shaft (102), wherein a closed hollow space (103) is formed by means of the hollow shaft (102), wherein the closed hollow space (103) is provided for receiving a cooling agent, wherein a three-dimensional transport structure (200) is provided in the closed hollow chamber (103) for transporting the cooling agent. The three-dimensional structure can, for example, be produced by means of applying an adaptive material.
摘要翻译：本发明涉及一种包括定子（107）和转子（101）的电机（100），其中转子（101）包括中空轴（102），其中封闭的中空空间（103）通过空心轴（102），其中设置有用于接收冷却剂的封闭中空空间（103），其中在封闭的中空室（103）中设置有用于输送冷却剂的三维输送结构（200）。例如，可以通过施加自适应材料来生产三维结构。

8. 发明授权

US08960605B2 Supporting pillar for an aircraft's structural component manufactured by a selective laser melting process 有权
标题翻译：通过选择性激光熔化工艺制造的飞机结构部件的支撑柱
公开(公告)号：US08960605B2
公开(公告)日：2015-02-24
申请号：US13061240
申请日：2009-07-30
申请人： Christoph Klahn , Rüdy Gysemberg , Olaf Rehme
发明人： Christoph Klahn , Rüdy Gysemberg , Olaf Rehme
IPC分类号： B64C1/06 , B64C7/00 , B64D11/00
CPC分类号： B64C1/06 , B64C7/00 , B64D11/00 , B64D2011/0076 , Y10T29/49622 , Y10T29/49631
摘要： The invention relates to an elongated supporting pillar for a high-strength structural component, wherein the supporting pillar is designed to absorb bending forces that act transversely to a longitudinal direction of extension of the supporting pillar. The supporting pillar comprises a wall which at least partially encloses an elongated cavity of the supporting pillar. A reinforcement structure is arranged within the cavity and transversely to the direction of longitudinal extension in such a manner that the reinforcement structure can absorb at least some of the bending forces. The reinforcement structure is designed integrally with the wall, wherein both the wall and the reinforcement structure comprise a meltable material.
摘要翻译：本发明涉及一种用于高强度结构部件的细长支撑柱，其中支撑柱被设计成吸收横向于支撑柱延伸的纵向方向作用的弯曲力。支撑柱包括至少部分地包围支撑柱的细长腔的壁。加强结构布置在空腔内并且横向于纵向延伸的方向，使得加强结构能够吸收至少一些弯曲力。加强结构与壁一体设计，其中壁和加强结构都包括可熔融材料。

9. 发明申请

US20110253878A1 SUPPORTING PILLAR FOR AN AIRCRAFT'S STRUCTURAL COMPONENT MANUFACTURED BY A SELECTIVE LASER MELTING PROCESS 有权
标题翻译：用于选择性激光熔化工艺制造的飞机结构部件的支撑支架
公开(公告)号：US20110253878A1
公开(公告)日：2011-10-20
申请号：US13061240
申请日：2009-07-30
申请人： Christoph Klahn , Rüdy Gysemberg , Olaf Rehme
发明人： Christoph Klahn , Rüdy Gysemberg , Olaf Rehme
IPC分类号： B64C1/06 , B21D47/01 , F16M13/00
CPC分类号： B64C1/06 , B64C7/00 , B64D11/00 , B64D2011/0076 , Y10T29/49622 , Y10T29/49631
摘要： The invention relates to an elongated supporting pillar for a high-strength structural component, wherein the supporting pillar is designed to absorb bending forces that act transversely to a longitudinal direction of extension of the supporting pillar. The supporting pillar comprises a wall which at least partially encloses an elongated cavity of the supporting pillar. A reinforcement structure is arranged within the cavity and transversely to the direction of longitudinal extension in such a manner that the reinforcement structure can absorb at least some of the bending forces. The reinforcement structure is designed integrally with the wall, wherein both the wall and the reinforcement structure comprise a meltable material.
摘要翻译：本发明涉及一种用于高强度结构部件的细长支撑柱，其中支撑柱被设计成吸收横向于支撑柱延伸的纵向方向作用的弯曲力。支撑柱包括至少部分地包围支撑柱的细长腔的壁。加强结构布置在空腔内并且横向于纵向延伸的方向，使得加强结构能够吸收至少一些弯曲力。加强结构与壁一体设计，其中壁和加强结构都包括可熔融材料。

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