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1. 发明申请

US20090094986A1 Combustion Chamber Wall, Gas Turbine Installation and Process for Starting or Shutting Down a Gas Turbine Installation 有权
标题翻译：燃烧室壁，燃气轮机安装和启动或关闭燃气轮机安装的过程
公开(公告)号：US20090094986A1
公开(公告)日：2009-04-16
申请号：US11920397
申请日：2006-05-10
申请人： Andreas Bottcher , Jens Kleinfeld , Claus Krusch
发明人： Andreas Bottcher , Jens Kleinfeld , Claus Krusch
IPC分类号： F23M5/08 , F23R3/00
CPC分类号： F23R3/002 , F23M5/085 , F23R3/50 , F23R3/60
摘要： In a combustion chamber wall for a combustion chamber having a combustion chamber outlet through which a hot combustion exhaust gas can exit the combustion chamber, the combustion chamber wall comprises an outlet end which surrounds the combustion chamber outlet, and the outlet end is provided with a tempering device.
摘要翻译：在具有燃烧室出口的燃烧室的燃烧室壁中，热燃烧废气可以通过燃烧室出口离开燃烧室，燃烧室壁包括围绕燃烧室出口的出口端，并且出口端设有一个回火装置

2. 发明授权

US08869534B2 Burner for a gas turbine 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US08869534B2
公开(公告)日：2014-10-28
申请号：US12520134
申请日：2007-12-20
申请人： Andreas Böttcher , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Sabine Tüschen , Ulrich Wörz
发明人： Andreas Böttcher , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Sabine Tüschen , Ulrich Wörz
IPC分类号： F02C1/00 , F02G3/00 , F23D11/36 , F23R3/28
CPC分类号： F23R3/283 , F23D11/36
摘要： A burner for a gas turbine including a main burner and a pilot burner is provided. The main burner has a supporting structure, a heat shield and a holder for the heat shield, and wherein the holder is at least partially located within the supporting structure and the heat shield is at least partially located within the holder. The heat shield is fastened to the holder by a force-fit and/or a frictional connection.
摘要翻译：提供一种用于包括主燃烧器和引燃燃烧器的燃气轮机的燃烧器。主燃烧器具有支撑结构，隔热罩和用于隔热罩的保持器，并且其中保持器至少部分地位于支撑结构内，并且隔热罩至少部分地位于支架内。隔热罩通过压配合和/或摩擦连接固定在支架上。

3. 发明申请

US20070233913A1 Key-Operated Memory-Programmable Control Coupled to a Personal Computer 有权
标题翻译：键控操作的存储器可编程控制耦合到个人计算机
公开(公告)号：US20070233913A1
公开(公告)日：2007-10-04
申请号：US10583645
申请日：2004-10-12
申请人： Jens Kleinfeld
发明人： Jens Kleinfeld
IPC分类号： G06F13/38
CPC分类号： G05B19/108 , G05B19/05 , G05B2219/15115
摘要： The keys which are used to activate the machine functions are embodied as keys (T1 Tn) which are directly connected to one of the SPS inputs (9). One of the several key planes can be selected by the user interface (13) of the PC coupled to the SPS. A control unit (4), which is connected to the SPS inputs (9) and which processes data in the SPS, is provided. Said control unit contains information about the keyboard layout of the keys (T1 Tn) on the respectively selected key plane by the PC by means of the data interface (8) and comprises a key signal which is arranged on the SPS entry (9).
摘要翻译：用于激活机器功能的键被实施为直接连接到SPS输入（9）之一的按键（T 1 Tn）。可以通过耦合到SPS的PC的用户界面（13）来选择几个关键平面中的一个。提供了连接到SPS输入（9）并且处理SPS中的数据的控制单元（4）。所述控制单元包含由PC通过数据接口（8）分别选择的键平面上的键（T 1 Tn）的键盘布局的信息，并且包括布置在SPS条目（9）上的键信号，。

4. 发明授权

US6085515A Heat shield configuration, particularly for structural parts of gas turbine plants 失效
标题翻译：隔热罩配置，特别适用于燃气轮机厂的结构部件
公开(公告)号：US6085515A
公开(公告)日：2000-07-11
申请号：US208359
申请日：1998-12-10
申请人： Guenther Walz , Jens Kleinfeld , Robert Frantzheld , Helmut Neugebauer
发明人： Guenther Walz , Jens Kleinfeld , Robert Frantzheld , Helmut Neugebauer
IPC分类号： F02C7/00 , F23M5/00 , F23M5/04 , F23R3/00 , F27D1/04 , F27D1/14 , F02C1/00 , F02G3/00
CPC分类号： F27D1/04 , F23M5/04 , F23R3/007 , F27D1/145 , F23M2900/05004
摘要： A heat shield configuration, particularly for protecting supporting structures and structural parts of gas turbine plants against a hot fluid. The heat shield has an inner lining which consists of a heat-resistant material and which is composed of plate-shaped heat-shield elements resistant to high temperatures and are disposed next to one another with gaps in-between. The heat-shield elements cover the entire area of the structural part. The heat shield is anchored so as to be thermally movable to the supporting structures and parts by bolts. The heat-shield element is formed of an erosion-proof and corrosion-proof material. An insulating brick formed of a refractory ceramic is disposed in each case between each heat-shield element and the supporting structure or parts.
摘要翻译：隔热结构，特别是用于保护燃气轮机设备的支撑结构和结构部件免受热流体的影响。隔热罩具有由耐热材料构成的内衬，该内衬由耐高温的板状隔热元件构成，彼此间隔开设置。隔热元件覆盖结构部件的整个区域。隔热板被锚定，以便通过螺栓可热移动到支撑结构和部件。隔热元件由防腐蚀和防腐蚀材料形成。在每个隔热元件和支撑结构或部件之间，每个壳体都设置由难熔陶瓷形成的绝缘砖。

5. 发明授权

US09488105B2 Gas turbine assembly and method therefor 有权
标题翻译：燃气轮机组件及其方法
公开(公告)号：US09488105B2
公开(公告)日：2016-11-08
申请号：US13885710
申请日：2011-11-30
申请人： Andreas Böttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
发明人： Andreas Böttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
IPC分类号： F02C7/22 , F23R3/28 , F02C7/20
CPC分类号： F02C7/20 , F23R3/283 , F23R3/286 , F23R2900/00005 , F23R2900/00012 , F23R2900/00017 , Y10T29/49229
摘要： An assembly for a gas turbine is presented. The assembly includes a gas supply pipe passing through a bore in a flange of the gas turbine for supplying gas to a combustion chamber of the gas turbine and a sleeve surrounding the gas supply pipe, having a first end and a second end, wherein the first end is sealingly coupled to the gas supply pipe, and wherein the sleeve is adapted to be sealingly coupled to the flange at the second end such that the sleeve extends along a thickness of the flange.
摘要翻译：提出了一种燃气轮机组件。组件包括通过燃气轮机的凸缘中的孔的气体供应管，用于将气体供应到燃气轮机的燃烧室，以及围绕气体供应管的套管，其具有第一端和第二端，其中第一端部密封地联接到气体供应管，并且其中套筒适于在第二端处密封地联接到凸缘，使得套筒沿着凸缘的厚度延伸。

6. 发明申请

US20140130502A1 GAS TURBINE ASSEMBLY AND METHOD THEREFOR 有权
标题翻译：气体涡轮组件及其方法
公开(公告)号：US20140130502A1
公开(公告)日：2014-05-15
申请号：US13885710
申请日：2011-11-30
申请人： Andreas Böttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
发明人： Andreas Böttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
IPC分类号： F23R3/28 , F02C7/20
CPC分类号： F02C7/20 , F23R3/283 , F23R3/286 , F23R2900/00005 , F23R2900/00012 , F23R2900/00017 , Y10T29/49229
摘要： An assembly for a gas turbine is presented. The assembly includes a gas supply pipe passing through a bore in a flange of the gas turbine for supplying gas to a combustion chamber of the gas turbine and a sleeve surrounding the gas supply pipe, having a first end and a second end, wherein the first end is sealingly coupled to the gas supply pipe, and wherein the sleeve is adapted to be sealingly coupled to the flange at the second end such that the sleeve extends along a thickness of the flange.
摘要翻译：提出了一种燃气轮机组件。组件包括通过燃气轮机的凸缘中的孔的气体供应管，用于将气体供应到燃气轮机的燃烧室，以及围绕气体供应管的套管，其具有第一端和第二端，其中第一端部密封地联接到气体供应管，并且其中套筒适于在第二端处密封地联接到凸缘，使得套筒沿着凸缘的厚度延伸。

7. 发明授权

US08091364B2 Combustion chamber wall, gas turbine installation and process for starting or shutting down a gas turbine installation 有权
标题翻译：燃烧室壁，燃气轮机安装和启动或关闭燃气轮机装置的过程
公开(公告)号：US08091364B2
公开(公告)日：2012-01-10
申请号：US11920397
申请日：2006-05-10
申请人： Andreas Böttcher , Jens Kleinfeld , Claus Krusch
发明人： Andreas Böttcher , Jens Kleinfeld , Claus Krusch
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/002 , F23M5/085 , F23R3/50 , F23R3/60
摘要： In a combustion chamber wall for a combustion chamber having a combustion chamber outlet through which a hot combustion exhaust gas can exit the combustion chamber, the combustion chamber wall comprises an outlet end which surrounds the combustion chamber outlet, and the outlet end is provided with a tempering device.
摘要翻译：在具有燃烧室出口的燃烧室的燃烧室壁中，热燃烧废气可以通过燃烧室出口离开燃烧室，燃烧室壁包括围绕燃烧室出口的出口端，并且出口端设有一个回火装置

8. 发明授权

US08266352B2 Key-operated memory-programmable control coupled to a personal computer 有权
标题翻译：键盘操作的存储器可编程控制耦合到个人计算机
公开(公告)号：US08266352B2
公开(公告)日：2012-09-11
申请号：US10583645
申请日：2004-10-12
申请人： Jens Kleinfeld
发明人： Jens Kleinfeld
IPC分类号： G06F13/38
CPC分类号： G05B19/108 , G05B19/05 , G05B2219/15115
摘要： The keys which are used to activate the machine functions are embodied as keys (T1 Tn) which are directly connected to one of the SPS inputs (9). One of the several key planes can be selected by the user interface (13) of the PC coupled to the SPS. A control unit (4), which is connected to the SPS inputs (9) and which processes data in the SPS, is provided. Said control unit contains information about the keyboard layout of the keys (T1 Tn) on the respectively selected key plane by the PC by means of the data interface (8) and comprises a key signal which is arranged on the SPS entry (9).
摘要翻译：用于激活机器功能的键被实现为直接连接到SPS输入（9）之一的键（T1 Tn）。可以通过耦合到SPS的PC的用户界面（13）来选择几个关键平面中的一个。提供了连接到SPS输入（9）并且处理SPS中的数据的控制单元（4）。所述控制单元通过数据接口（8）包含由PC通过分别选择的键平面上的键（T1 Tn）的键盘布局的信息，并且包括布置在SPS条目（9）上的键信号。

9. 发明申请

US20120137691A1 Gas turbine assembly and method therefor 审中-公开
标题翻译：燃气轮机组件及其方法
公开(公告)号：US20120137691A1
公开(公告)日：2012-06-07
申请号：US12957476
申请日：2010-12-01
申请人： Andreas Bõttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
发明人： Andreas Bõttcher , Timothy A. Fox , Daniel W. Garan , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Stephen A. Ramier , David M. Ritland , Marcus Zurhorst
IPC分类号： F02C7/22 , B23P11/00
CPC分类号： F02C7/20 , F05D2260/94 , F05D2260/941 , F23R3/283 , F23R3/286 , F23R2900/00005 , F23R2900/00012 , Y10T29/49229
摘要： An assembly for a gas turbine is presented. The assembly includes a gas supply pipe passing through a bore in a flange of the gas turbine for supplying gas to a combustion chamber of the gas turbine and a sleeve surrounding the gas supply pipe, having a first end and a second end, wherein the first end is sealingly coupled to the gas supply pipe, and wherein the sleeve is adapted to be sealingly coupled to the flange at the second end such that the sleeve extends along a thickness of the flange.
摘要翻译：提出了一种燃气轮机组件。组件包括通过燃气轮机的凸缘中的孔的气体供应管，用于将气体供应到燃气轮机的燃烧室，以及围绕气体供应管的套管，其具有第一端和第二端，其中第一端部密封地联接到气体供应管，并且其中套筒适于在第二端处密封地联接到凸缘，使得套筒沿着凸缘的厚度延伸。

10. 发明申请

US20100170267A1 BURNER FOR A GAS TURBINE 有权
标题翻译：燃气轮机
公开(公告)号：US20100170267A1
公开(公告)日：2010-07-08
申请号：US12520134
申请日：2007-12-20
申请人： Andreas Böettcher , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Sabine Tüschen , Ulrich Wörz
发明人： Andreas Böettcher , Thomas Grieb , Jens Kleinfeld , Tobias Krieger , Sabine Tüschen , Ulrich Wörz
IPC分类号： F02C7/20 , F23D11/36 , F23R3/00
CPC分类号： F23R3/283 , F23D11/36
摘要： A burner for a gas turbine including a main burner and a pilot burner is provided. The main burner has a supporting structure, a heat shield and a holder for the heat shield, and wherein the holder is at least partially located within the supporting structure and the heat shield is at least partially located within the holder. The heat shield is fastened to the holder by a force-fit and/or a frictional connection.
摘要翻译：提供一种用于包括主燃烧器和引燃燃烧器的燃气轮机的燃烧器。主燃烧器具有支撑结构，隔热罩和用于隔热罩的保持器，并且其中保持器至少部分地位于支撑结构内，并且隔热罩至少部分地位于支架内。隔热罩通过压配合和/或摩擦连接固定在支架上。

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