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1. 发明授权

US08951606B2 Method for producing a component by calculating a load line of the component 有权
标题翻译：通过计算部件的负载线来制造部件的方法
公开(公告)号：US08951606B2
公开(公告)日：2015-02-10
申请号：US13577876
申请日：2011-01-29
申请人： Manuel H. Hertter , Andreas Jakimov , Marcin Olbrich , Mihaela-Sorina Seitz , Juergen Kraus , Bertram Kopperger , Klaus Broichhausen , Hans Banhirl , Erwin Bayer , Wolfgang Werner , Eberhard Knodel
发明人： Manuel H. Hertter , Andreas Jakimov , Marcin Olbrich , Mihaela-Sorina Seitz , Juergen Kraus , Bertram Kopperger , Klaus Broichhausen , Hans Banhirl , Erwin Bayer , Wolfgang Werner , Eberhard Knodel
IPC分类号： B05D1/02 , B05D1/32 , C23C24/04 , F01D5/28
CPC分类号： B05D1/02 , C23C24/04 , F01D5/288 , Y10T428/239 , Y10T428/24 , Y10T428/24479
摘要： A method for producing a component is disclosed. The method includes calculating a load line of the component as a result of a load to be absorbed by the component and applying a layer on a core by gas dynamic cold spraying, where the layer has a layer section and where the layer section runs along the calculated load line.
摘要翻译：公开了一种制造组件的方法。该方法包括计算作为由部件吸收的负荷的结果的部件的负荷线，并且通过气体动态冷喷涂在芯上施加层，其中该层具有层部分，并且层部分沿着计算负载线。

2. 发明申请

US20130084421A1 METHOD FOR PRODUCING A COMPONENT AND SUCH A COMPONENT 有权
标题翻译：用于生产组分和其组分的方法
公开(公告)号：US20130084421A1
公开(公告)日：2013-04-04
申请号：US13577876
申请日：2011-01-29
申请人： Manuel H. Hertter , Andreas Jakimov , Marcin Olbrich , Mihaela-Sorina Seitz , Juergen Kraus , Bertram Kopperger , Klaus Broichhausen , Hans Banhirl , Erwin Bayer , Wolfgang Werner , Eberhard Knodel
发明人： Manuel H. Hertter , Andreas Jakimov , Marcin Olbrich , Mihaela-Sorina Seitz , Juergen Kraus , Bertram Kopperger , Klaus Broichhausen , Hans Banhirl , Erwin Bayer , Wolfgang Werner , Eberhard Knodel
IPC分类号： B05D1/02
CPC分类号： B05D1/02 , C23C24/04 , F01D5/288 , Y10T428/239 , Y10T428/24 , Y10T428/24479
摘要： The invention relates to a component, which has a layer applied by gas dynamic cold spray, said layer having at, least one layer section or a reinforcing element, the material and orientation of which are selected according to a load line, and to a method for producing such a component by gas dynamic cold spray.
摘要翻译：本发明涉及一种具有通过气体动态冷喷涂施加的层的部件，所述层具有根据负载线选择其材料和取向的至少一个层部分或增强元件，并且涉及一种方法用于通过气体动态冷喷雾生产这种组分。

3. 发明申请

US20130129976A1 COATING PLASTIC COMPONENTS BY MEANS OF KINETIC COLD GAS SPRAYING 审中-公开
标题翻译：通过动态冷气喷涂来涂装塑料成分
公开(公告)号：US20130129976A1
公开(公告)日：2013-05-23
申请号：US13509577
申请日：2010-11-11
申请人： Manuel Hertter , Andreas Jakimov , Mihaela-Sorina Seitz , Marcin Olbrich , Juergen Kraus , Bertram Kopperger , Klaus Broichhausen , Hans Banhirl , Erwin Bayer , Wolfgang Werner , Eberhard Knodel
发明人： Manuel Hertter , Andreas Jakimov , Mihaela-Sorina Seitz , Marcin Olbrich , Juergen Kraus , Bertram Kopperger , Klaus Broichhausen , Hans Banhirl , Erwin Bayer , Wolfgang Werner , Eberhard Knodel
IPC分类号： C23C4/12
CPC分类号： C23C4/12 , C23C24/04 , C23C28/321 , C23C28/322 , C23C28/324 , C23C28/347 , Y10T428/24355
摘要： A method for coating a plastic surface and a plastic component is disclosed. The method includes applying a base layer to a plastic surface. A layer of a coating is applied by kinetic cold gas spraying on the base layer. The base layer is applied by a method that is different from the kinetic cold gas spraying. The base layer adheres to the plastic surface and the layer of the coating applied by kinetic cold gas spraying is deposited on the base layer by the kinetic cold gas spraying.
摘要翻译：公开了一种涂覆塑料表面和塑料部件的方法。该方法包括将基底层施加到塑料表面。通过动态冷气喷涂在基层上施加一层涂层。通过与动态冷气喷射不同的方法施加基层。基层粘附到塑料表面，并且通过动态冷气喷涂在基层上沉积通过动态冷气喷涂施加的涂层层。

4. 发明申请

US20110166798A1 DEVICE AND METHOD FOR SERVICE-LIFE MONITORING 审中-公开
标题翻译：用于维修生命监控的设备和方法
公开(公告)号：US20110166798A1
公开(公告)日：2011-07-07
申请号：US12998054
申请日：2009-09-09
申请人： Eberhard Knodel , Hans-Peter Borufka , Hernan Victor Arrieta
发明人： Eberhard Knodel , Hans-Peter Borufka , Hernan Victor Arrieta
IPC分类号： G06F19/00
CPC分类号： F01D21/003 , F05D2270/11 , G05B23/0283 , Y02T50/671
摘要： In the case of a device and a method for monitoring the service life of an engine or of a turbine having a compressor blisk and/or a turbine blisk, momentary stresses of blisk substructures, such as the blade (1), the disk (2), and the join region (3) between the blade (1) and the disk (2), are calculated on the basis of operating parameters that are measured in the course of engine or turbine operation; and accumulated damage to the individual substructures, that was caused by the momentary stresses, is estimated.
摘要翻译：在用于监测发动机或具有压缩机叶片和/或涡轮叶片的涡轮机的使用寿命的装置和方法的情况下，叶片子结构（例如叶片（1）），盘（2）的瞬时应力）和叶片（1）和盘（2）之间的连接区域（3）基于在发动机或涡轮机操作过程中测量的操作参数来计算; 并估计了由瞬时压力造成的各个子结构的累积损失。

5. 发明授权

US07267527B2 Rotor for a turbomachine 有权
标题翻译：转子用于涡轮机
公开(公告)号：US07267527B2
公开(公告)日：2007-09-11
申请号：US11095556
申请日：2005-04-01
申请人： Martin Fischer , Wilfried Weidmann , Eberhard Knodel
发明人： Martin Fischer , Wilfried Weidmann , Eberhard Knodel
IPC分类号： F01D5/00
CPC分类号： F01D5/066 , F16B5/02
摘要： The invention relates to a rotor for a turbomachine, in particular a low-pressure turbine rotor for a gas turbine, having at least one stage, each stage comprising a rotor disk having rotor blades attached to the rotor disk, and the rotor disk of each stage being removably connected either to oppositely situated rotor disks of adjoining stages or to a rotor connection of a rotor shaft by at least one respective attachments. According to the invention, the, or each of the, attachment means extends through the rotor disk of at least one stage, whereby the, or each of the, attachment means is guided with radial play into at least one borehole passing through the respective rotor disk, so that an interior borehole surface is not subjected to load or force.
摘要翻译：本发明涉及一种用于涡轮机的转子，特别是用于燃气轮机的低压涡轮转子，具有至少一个级，每个级包括具有附接到转子盘的转子叶片的转子盘，以及每个转子盘的转子盘阶段可拆卸地连接到相邻位置的相邻位置的转子盘或通过至少一个相应的附件连接到转子轴的转子连接。根据本发明，所述附接装置中的每一个或每个附接装置延伸穿过至少一个台的转子盘，由此，附接装置中的每个或每个附接装置以径向游隙的形式被引导到穿过相应转子的至少一个钻孔中使得内部钻孔表面不受负载或力的影响。

6. 发明申请

US20050226730A1 Rotor for a turbomachine 有权
标题翻译：转子用于涡轮机
公开(公告)号：US20050226730A1
公开(公告)日：2005-10-13
申请号：US11095556
申请日：2005-04-01
申请人： Martin Fischer , Wilfried Weidmann , Eberhard Knodel
发明人： Martin Fischer , Wilfried Weidmann , Eberhard Knodel
IPC分类号： B63H1/20 , F01D5/02 , F01D5/06 , F16B5/02
CPC分类号： F01D5/066 , F16B5/02
摘要： The invention relates to a rotor for a turbomachine, in particular a low-pressure turbine rotor for a gas turbine, having at least one stage, each stage comprising a rotor disk having rotor blades attached to the rotor disk, and the rotor disk of each stage being removably connected either to oppositely situated rotor disks of adjoining stages or to a rotor connection of a rotor shaft by at least one respective attachments. According to the invention, the, or each of the, attachment means extends through the rotor disk of at least one stage, whereby the, or each of the, attachment means is guided with radial play into at least one borehole passing through the respective rotor disk, so that an interior borehole surface is not subjected to load or force.
摘要翻译：本发明涉及一种用于涡轮机的转子，特别是用于燃气轮机的低压涡轮转子，具有至少一个级，每个级包括具有附接到转子盘的转子叶片的转子盘，以及每个转子盘的转子盘阶段可拆卸地连接到相邻位置的相邻位置的转子盘或通过至少一个相应的附件连接到转子轴的转子连接。根据本发明，所述附接装置中的每一个或每个附接装置延伸穿过至少一个台的转子盘，由此，附接装置中的每个或每个附接装置以径向游隙的形式被引导到穿过相应转子的至少一个钻孔中使得内部钻孔表面不受负载或力的影响。

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