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1. 发明授权

US07874791B2 Turbomachine 有权
标题翻译：涡轮机
公开(公告)号：US07874791B2
公开(公告)日：2011-01-25
申请号：US11530065
申请日：2006-09-08
申请人： Joergen Ferber , James Ritchie
发明人： Joergen Ferber , James Ritchie
IPC分类号： F01D5/22 , F01D9/04 , F01D5/30
CPC分类号： F01D5/225 , F05D2240/40 , F05D2260/30 , Y02T50/672 , Y02T50/673
摘要： A turbomachine (1), in particular a turbine or compressor, includes a rotor (2) which has at least one moving blade row (4) with a plurality of moving blades (5), and a stator (3) which has at least one guide vane row (6) with a plurality of guide vanes (7), at least in one of the blade or vane rows (4, 6) all the blades or vanes (5, 7) each having a shroud plate (10). In order to simplify the maintenance of the turbo-machine (1), the shroud plates (10) are separate components with respect to the respective blade or vane (5, 7) and are mounted on the respective blade or vane (5, 7), shroud plates (10) adjacent in the circumferential direction (9) being coupled to one another for the transmission of tensile forces in the circumferential direction (9).
摘要翻译：涡轮机（1），特别是涡轮机或压缩机，包括具有至少一个具有多个活动叶片（5）的至少一个活动叶片排（4）的转子（2）和至少具有至少具有多个导向叶片（7）的一个导向叶片排（6），至少在叶片或叶片排（4,6）之一中，所有叶片或叶片（5,7）均具有护罩板（10）。为了简化涡轮机（1）的维护，护罩板（10）相对于相应的叶片或叶片（5,7）是分离的部件，并且安装在相应的叶片或叶片（5,7）上），沿圆周方向（9）相邻的护罩板（10）彼此联接以在周向（9）上传递张力。

2. 发明授权

US06818034B2 Device for separating dirt and debris in flowing media 有权
标题翻译：用于分离流动介质中的污物和碎屑的装置
公开(公告)号：US06818034B2
公开(公告)日：2004-11-16
申请号：US10292492
申请日：2002-11-13
申请人： Gordon Anderson , Joergen Ferber
发明人： Gordon Anderson , Joergen Ferber
IPC分类号： B01D4512
CPC分类号： B04C5/185 , B01D45/12 , B04C5/14
摘要： The present invention relates to a device for separating dirt and debris in flowing media by making use of centrifugal forces, said device comprising a separation chamber (1), and a dirt collection chamber (3) connected with said separation chamber (1) by at least one dirt discharge opening (2). Arranged in the region of dirt discharge opening (2) within dirt collection chamber (3) are one or more flow guide elements (4, 5, 6), which make the backflow of dirt and debris into separation chamber (1) difficult. In the present device the danger of backflow of dirt and debris particles from the dirt collection chamber into the separation chamber is reduced.
摘要翻译：本发明涉及一种用于通过利用离心力分离流动介质中的污物和碎屑的装置，所述装置包括分离室（1）和与所述分离室（1）连接的污物收集室（3）至少一个排污口（2）。在污物收集室（3）内的排污口（2）区域内布置有一个或多个流动引导元件（4,5,6），这使得污物和碎屑回流到分离室（1）中困难。本装置减少了灰尘和碎屑颗粒从污物收集室回流到分离室中的危险。

3. 发明授权

US08821116B2 Abradable coating system 有权
标题翻译：耐磨涂层系统
公开(公告)号：US08821116B2
公开(公告)日：2014-09-02
申请号：US12915978
申请日：2010-10-29
申请人： Sophie Duval , Piero-Daniele Grasso , Sven Olliges , Joergen Ferber , Alexander Stankowski
发明人： Sophie Duval , Piero-Daniele Grasso , Sven Olliges , Joergen Ferber , Alexander Stankowski
IPC分类号： F01D11/12 , F01D5/00 , F01D5/28
CPC分类号： F01D11/122 , F01D5/005 , F01D5/284 , F01D11/125 , F05D2230/90 , F05D2300/21 , F05D2300/6012 , F05D2300/603 , F05D2300/612 , F05D2300/615 , Y02T50/67 , Y02T50/672
摘要： An abradable coating system (2-8) for a turbine or a compressor is proposed has at least one layer of woven or non-woven tissue (15) or foam made of: ceramic, glass, glass-ceramic, ceramic-metal composite and combinations thereof. A free-standing preformed element (18) has at least one layer of such a woven or non-woven tissue or foam is filled with fillers and/or binder. A method prepares such a system. Finally, a method for the repair of an abradable coating portion of a turbine or the compressor component (9) includes in a first optional step that the damaged portion is at least partly removed and/or cleaned and/or surface treated, and in a second step at least one free-standing preformed abradable coating element (18) or a complete abradable coating system is attached to the component (9), preferably by using a matrix, wherein for example only a center part (2) or a fraction of a center part (2) is replaced.
摘要翻译：提出了一种用于涡轮机或压缩机的可磨损涂层系统（2-8），其具有至少一层机织或非织造组织（15）或由陶瓷，玻璃，玻璃陶瓷，陶瓷 - 金属复合材料制成的泡沫或泡沫其组合。独立的预成型元件（18）具有至少一层这样的机织或非织造组织或泡沫填充有填料和/或粘合剂。一种方法准备这样的系统。最后，用于修复涡轮机或压缩机部件（9）的可磨损涂覆部分的方法包括在第一任选步骤中，损伤部分至少部分地被去除和/或清洁和/或表面处理，并且在第二步，优选通过使用基质将至少一个独立的预成形的可磨损涂层元件（18）或完整的可磨损涂层系统附接到部件（9），其中例如仅仅是中心部分（2）或部分更换中心部分（2）。

4. 发明申请

US20070212215A1 TURBOMACHINE 有权
标题翻译：涡轮机
公开(公告)号：US20070212215A1
公开(公告)日：2007-09-13
申请号：US11530065
申请日：2006-09-08
申请人： Joergen Ferber , James Ritchie
发明人： Joergen Ferber , James Ritchie
IPC分类号： F04D29/08
CPC分类号： F01D5/225 , F05D2240/40 , F05D2260/30 , Y02T50/672 , Y02T50/673
摘要： A turbomachine (1), in particular a turbine or compressor, includes a rotor (2) which has at least one moving blade row (4) with a plurality of moving blades (5), and a stator (3) which has at least one guide vane row (6) with a plurality of guide vanes (7), at least in one of the blade or vane rows (4, 6) all the blades or vanes (5, 7) each having a shroud plate (10). In order to simplify the maintenance of the turbo-machine (1), the shroud plates (10) are separate components with respect to the respective blade or vane (5, 7) and are mounted on the respective blade or vane (5, 7), shroud plates (10) adjacent in the circumferential direction (9) being coupled to one another for the transmission of tensile forces in the circumferential direction (9).
摘要翻译：涡轮机（1），特别是涡轮机或压缩机，包括具有至少一个具有多个活动叶片（5）的至少一个活动叶片排（4）的转子（2）和至少具有至少具有多个导向叶片（7）的一个导向叶片排（6），至少在叶片或叶片排（4,6）之一中，所有叶片或叶片（5,7）均具有护罩板（10）。为了简化涡轮机（1）的维护，护罩板（10）相对于相应的叶片或叶片（5,7）是分离的部件，并且安装在相应的叶片或叶片（5,7）上），沿圆周方向（9）相邻的护罩板（10）彼此联接以在周向（9）上传递张力。

5. 发明申请

US20110103940A1 ABRADABLE COATING SYSTEM 有权
标题翻译：不可磨损的涂层系统
公开(公告)号：US20110103940A1
公开(公告)日：2011-05-05
申请号：US12915978
申请日：2010-10-29
申请人： Sophie Duval , Piero-Daniele Grasso , Sven Olliges , Joergen Ferber , Alexander Stankowski
发明人： Sophie Duval , Piero-Daniele Grasso , Sven Olliges , Joergen Ferber , Alexander Stankowski
IPC分类号： F01D11/12 , B32B37/16
CPC分类号： F01D11/122 , F01D5/005 , F01D5/284 , F01D11/125 , F05D2230/90 , F05D2300/21 , F05D2300/6012 , F05D2300/603 , F05D2300/612 , F05D2300/615 , Y02T50/67 , Y02T50/672
摘要： An abradable coating system (2-8) for a turbine or a compressor is proposed has at least one layer of woven or non-woven tissue (15) or foam made of: ceramic, glass, glass-ceramic, ceramic-metal composite and combinations thereof. A free-standing preformed element (18) has at least one layer of such a woven or non-woven tissue or foam is filled with fillers and/or binder. A method prepares such a system. Finally, a method for the repair of an abradable coating portion of a turbine or the compressor component (9) includes in a first optional step that the damaged portion is at least partly removed and/or cleaned and/or surface treated, and in a second step at least one free-standing preformed abradable coating element (18) or a complete abradable coating system is attached to the component (9), preferably by using a matrix, wherein for example only a center part (2) or a fraction of a center part (2) is replaced.
摘要翻译：提出了一种用于涡轮机或压缩机的可磨损涂层系统（2-8），其具有至少一层机织或非织造组织（15）或由陶瓷，玻璃，玻璃陶瓷，陶瓷 - 金属复合材料制成的泡沫或泡沫其组合。独立的预成型元件（18）具有至少一层这样的机织或非织造组织或泡沫填充有填料和/或粘合剂。一种方法准备这样的系统。最后，用于修复涡轮机或压缩机部件（9）的可磨损涂覆部分的方法包括在第一任选步骤中，损伤部分至少部分地被去除和/或清洁和/或表面处理，并且在第二步，优选通过使用基质将至少一个独立的预成形的可磨损涂层元件（18）或完整的可磨损涂层系统附接到部件（9），其中例如仅仅是中心部分（2）或部分更换中心部分（2）。

6. 发明申请

US20090214355A1 FIXING METHOD FOR A TIP WINGLET AND REDUCED TIP LEAKAGE BLADE 审中-公开
标题翻译：固定方式用于提IP ET。AND。。。。。。。。。。。。。。
公开(公告)号：US20090214355A1
公开(公告)日：2009-08-27
申请号：US12390538
申请日：2009-02-23
申请人： Michele Pereti , Joergen Ferber
发明人： Michele Pereti , Joergen Ferber
IPC分类号： F01D5/18 , B23P6/00
CPC分类号： F01D5/20 , B23P6/002 , F01D5/005 , F01D5/141 , F01D5/145 , F05D2230/232 , F05D2230/80 , Y10T29/49318
摘要： Reducing the tip leakage for an existing compressor or turbine blade (10), including internally cooled blades, can be achieved by retrofitted the blade with a tip leakage-reducing device in the form of a winglet (12). The winglet (12) can be fixed onto the tip portion by bonding the winglet onto the face or faces of the blade by a key and slot arrangement.
摘要翻译：减小现有的包括内部冷却叶片的压缩机或涡轮叶片（10）的尖端泄漏可以通过用小翼（12）形式的尖端泄漏减少装置进行改装来实现。小翼（12）可以通过键和槽布置将小翼粘合到叶片的面或面上而固定在尖端部分上。

7. 发明申请

US20080298970A1 Turbo Machine 审中-公开
标题翻译：涡轮机
公开(公告)号：US20080298970A1
公开(公告)日：2008-12-04
申请号：US12045895
申请日：2008-03-11
申请人： Joergen Ferber , James Ritchie , Slawomir Slowik
发明人： Joergen Ferber , James Ritchie , Slawomir Slowik
IPC分类号： F01D5/22
CPC分类号： F01D5/225 , F05B2240/33 , F05D2230/60 , F05D2260/30 , Y02T50/671 , Y02T50/673
摘要： A turbo machine (1, 101), in particular turbine or compressor, includes a rotor (2, 102) which has at least one moving blade row (4, 104) with a plurality of moving blades (5, 105), and a stator (3) which has at least one guide vane row (6, 106) with a plurality of guide vanes (7, 107), at least one moving blade row (4, 104) having a shroud (8, 108). The shroud (8, 108) is designed to be self-supporting in such a way that it can at least partially absorb the centrifugal forces arising during operation and discharge them in the circumferential direction.
摘要翻译：特别是涡轮机或压缩机的涡轮机（1,101）包括具有至少一个具有多个活动叶片（5,105）的活动叶片排（4,104）的转子（2,102），以及定子（3）具有至少一个具有多个导向叶片（7,107）的导向叶片排（6,106），至少一个具有护罩（8,108）的活动叶片排（4,104）。护罩（8,108）被设计成自支撑，使得其可以至少部分地吸收在操作过程中产生的离心力并在圆周方向上排出它们。

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