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11. 发明授权

US06431830B1 Nozzle ring for a gas turbine 失效
标题翻译：用于燃气轮机的喷嘴环
公开(公告)号：US06431830B1
公开(公告)日：2002-08-13
申请号：US09643066
申请日：2000-08-21
申请人： Karl-Hermann Richter , Josef Reischl , Hans Juergen Schmuhl , Klaus Breitschwerdt , Ulrich Knott , Siegfried Boettcher , Karlheinz Manier , Werner Humhauser
发明人： Karl-Hermann Richter , Josef Reischl , Hans Juergen Schmuhl , Klaus Breitschwerdt , Ulrich Knott , Siegfried Boettcher , Karlheinz Manier , Werner Humhauser
IPC分类号： F01D900
CPC分类号： F01D9/042 , Y02T50/673 , Y10T29/49321 , Y10T29/49323
摘要： A worked nozzle ring for a gas turbine, in particular an aircraft engine, having at least one shroud and at least one blade sheet arranged thereon, whereby, in order to create a worked nozzle ring that is easy to manufacture, the blade sheet comprises, at the frontal side, at least one two-dimensionally profiled connecting space region that is placed in a profiled opening formed in the shroud by beam cutting and is connected therewith.
摘要翻译：一种用于燃气涡轮机，特别是飞机发动机的加工喷嘴环，其具有至少一个护罩和布置在其上的至少一个叶片，由此，为了形成易于制造的加工喷嘴环，在前侧，至少一个二维轮廓的连接空间区域，其通过光束切割放置在形成在罩中的成型开口中并与其连接。

12. 发明授权

US06663784B1 Method for producing three-dimensional structures by means of an etching process 失效
标题翻译：通过蚀刻工艺制备三维结构的方法
公开(公告)号：US06663784B1
公开(公告)日：2003-12-16
申请号：US09890080
申请日：2002-02-04
申请人： Nils Kummer , Roland Mueller-Fiedler , Klaus Breitschwerdt , Andre Mueller , Frauke Driewer , Andreas Kern
发明人： Nils Kummer , Roland Mueller-Fiedler , Klaus Breitschwerdt , Andre Mueller , Frauke Driewer , Andreas Kern
IPC分类号： H01L2100
CPC分类号： B81C1/00412
摘要： A method is proposed for producing three-dimensional structures, especially microlenses, in a substrate using an etching process, at least one original shape having a known original surface shape being present initially on the substrate in a plurality of places. The etching process has at least one first etching removal rate a1 and a second etching removal rate a2 which are material-dependent, and of which at least one is changeable as a function of time. The original shape is converted to a target shape by the etching process, the original surface shape of the original shape and the target surface shape of the target shape to be reached being known before the beginning of the etching process. In order to achieve the target surface shape, at least one of the etching rates a2 or a1 is set by a change of at least one etching parameter calculated before the beginning of the etching process as a function of the etching time.
摘要翻译：提出了一种使用蚀刻工艺在衬底中制造三维结构，特别是微透镜的方法，至少一种具有已知原始表面形状的原始形状最初存在于多个位置的衬底上。蚀刻工艺具有与材料有关的至少一个第一蚀刻去除速率a1和第二蚀刻去除速率a2，其中至少一个可随时间变化。原始形状通过蚀刻处理转换为目标形状，原始形状的原始表面形状和待形成的目标形状的目标表面形状在蚀刻工艺开始之前是已知的。为了实现目标表面形状，蚀刻速度a2或a1中的至少一个通过蚀刻工艺开始之前计算的至少一个蚀刻参数的变化来设定，作为蚀刻时间的函数。

13. 发明申请

US20090169372A1 METHOD OF PRODUCING A PROTECTIVE COATING, PROTECTIVE COATING, AND COMPONENT WITH A PROTECTIVE COATING 审中-公开
标题翻译：保护性涂料的生产方法，保护涂料和具有保护涂料的组分
公开(公告)号：US20090169372A1
公开(公告)日：2009-07-02
申请号：US12067274
申请日：2006-09-16
申请人： Christian Friedrich , Klaus Breitschwerdt
发明人： Christian Friedrich , Klaus Breitschwerdt
IPC分类号： F01D25/00 , C23C4/10
CPC分类号： C23C4/00 , C23C4/01 , Y02T50/67 , Y02T50/6765 , Y10T428/12486
摘要： A method for producing a wear-resistant, temperature-resistant, and corrosion-resistant protective coating for a component, in particular for components of a gas turbine, using thermal spraying, wherein during the application onto the component of the protective coating, which consists of a hard material-metal combination, in order to produce an abrasive surface a structuring of that surface of the protective coating that faces away from the component takes place, the hard material or materials consisting of boron nitride particles, titanium carbide particles, tungsten carbide particles, chromium carbide particles, and zirconium oxide particles, or a mixture thereof, and the hard materials having a particle size of 0.1 μm-200 μm, and the protective coating having a thickness of 10 μm-6.0 mm.
摘要翻译：一种用于制造用于组件的耐磨损，耐温和耐腐蚀的保护涂层的方法，特别是对于使用热喷涂的燃气轮机的部件，其中在施加到保护涂层的部件上时，其包括的硬质材料 - 金属组合，为了产生研磨表面，保护涂层的表面远离组分发生的结构，由氮化硼颗粒，碳化钛颗粒，碳化钨组成的硬质材料或材料颗粒，碳化铬颗粒和氧化锆颗粒或其混合物，以及具有0.1μm〜200μm的粒度的硬质材料，并且保护涂层的厚度为10μm〜6.0mm。

14. 发明申请

US20060097388A1 Electrical system, especially a microelectronic or microelectromechanical high frequency system 审中-公开
标题翻译：电气系统，特别是微电子或微机电高频系统
公开(公告)号：US20060097388A1
公开(公告)日：2006-05-11
申请号：US10520218
申请日：2003-06-24
申请人： Klaus Breitschwerdt , Markus Ulm , Andrea Urban , Mathias Reimann
发明人： Klaus Breitschwerdt , Markus Ulm , Andrea Urban , Mathias Reimann
IPC分类号： H01L23/34
CPC分类号： H01L23/66 , H01L2223/6616 , H01L2223/6627 , H01L2924/15313 , H01L2924/16152 , H01L2924/1903 , H01L2924/3011 , H01P1/047 , H01P11/00
摘要： An electrical component is proposed, in particular a high-frequency microelectronic or microelectromechanical component having a base element that is provided with a feedthrough, a first conductive structure extending on an upper side of the base element being connected by the feedthrough, continuously for high-frequency electromagnetic waves, to a second conductive structure extending on a lower side of the base element. The feedthrough has the form of a right prism or cylinder, and the first and/or the second conductive structure is embodied as a planar waveguide, in particular as a coplanar waveguide. Also proposed is a method for producing an electrical component having a feedthrough for high-frequency electromagnetic waves through a base element, an electrically conductive layer being applied on an upper side of the base element and an etching mask being applied on a lower side of the base element; a trench, having at least almost perpendicular sidewalls and penetrating through the base element, then being etched into the base element in a plasma etching step; an electrically conductive layer being applied on the lower side after the etching and after removal of the etching mask; and the trench lastly being filled or lined with an electrically conductive material.
摘要翻译：提出了一种电气元件，特别是具有设置有馈通的基座元件的高频微电子或微机电元件，在基座元件的上侧延伸的第一导电结构，通过馈通连接，到基底元件的下侧延伸的第二导电结构。馈通具有右棱镜或圆筒的形式，并且第一和/或第二导电结构被实施为平面波导，特别是作为共面波导。还提出了一种用于制造具有通过基底元件的高频电磁波的馈通的电气元件的方法，将导电层施加在基底元件的上侧，并且将蚀刻掩模施加在基底元件的下侧基本元素沟槽，具有至少几乎垂直的侧壁并穿过基底元件，然后在等离子体蚀刻步骤中蚀刻到基底元件中; 在蚀刻之后和去除蚀刻掩模之后，在下侧施加导电层; 并且沟槽最后被填充或衬有导电材料。

15. 发明授权

US6119339A Nozzle ring for a gas turbine and method of manufacture thereof 有权
标题翻译：一种用于燃气轮机的喷嘴环及其制造方法
公开(公告)号：US6119339A
公开(公告)日：2000-09-19
申请号：US281987
申请日：1999-03-29
申请人： Karl-Hermann Richter , Josef Reischl , Hans Juergen Schmuhl , Klaus Breitschwerdt , Ulrich Knott , Siegfried Boettcher , Karlheinz Manier , Werner Humhauser
发明人： Karl-Hermann Richter , Josef Reischl , Hans Juergen Schmuhl , Klaus Breitschwerdt , Ulrich Knott , Siegfried Boettcher , Karlheinz Manier , Werner Humhauser
IPC分类号： F01D9/02 , F01D9/04 , B21D53/78
CPC分类号： F01D9/042 , Y02T50/673 , Y10T29/49321 , Y10T29/49323
摘要： A worked nozzle ring for a gas turbine, in particular an aircraft engine, having at least one shroud and at least one blade sheet arranged thereon, whereby in order to create a worked nozzle ring that is easy to manufacture, the blade sheet comprises, at the frontal side, at least one two-dimensionally profiled connecting space region that is placed in a profiled opening formed in the shroud by means of beam cutting and is connected therewith.
摘要翻译：一种用于燃气涡轮机，特别是飞机发动机的加工喷嘴环，其具有至少一个护罩和布置在其上的至少一个刀片，由此为了形成易于制造的加工喷嘴环，刀片包括在前侧，至少一个二维轮廓的连接空间区域，其通过光束切割放置在形成在护罩中的成型开口中并与其连接。

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