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1. 发明授权

US08973369B2 Gas-turbine burner having inflow guide means 有权
标题翻译：具有流入引导装置的燃气轮机燃烧器
公开(公告)号：US08973369B2
公开(公告)日：2015-03-10
申请号：US13715233
申请日：2012-12-14
申请人： Robert Angel , Drew Ehlert , Matthias Hase , Michael Huth , James Marshall , Yevgeniy Shteyman
发明人： Robert Angel , Drew Ehlert , Matthias Hase , Michael Huth , James Marshall , Yevgeniy Shteyman
IPC分类号： F02C1/00 , F02G3/00 , F23R3/14 , F23R3/28 , F23R3/34
CPC分类号： F23R3/14 , F23D2900/00008 , F23D2900/14701 , F23R3/286 , F23R3/343
摘要： A gas-turbine burner having a plurality of main swirl generators which each have an inlet flow opening formed by the main swirl generator edge is provided. In order to achieve a uniform flow of combustion air through the main swirl generator, the gas-turbine burner has an inlet-flow guide means with a flow guide surface which runs from one of the inlet-flow openings to an adjacent inlet-flow opening, to which the main swirl generator edges which form the inlet-flow openings are connected, and the flow guide surface widens from there radially upwards. The main swirl generators are central-symmetrically arranged around a pilot burner and the flow guide surface runs radially outside the main swirl generators.
摘要翻译：本发明提供一种燃气轮机燃烧器，其具有多个主漩涡发生器，每个主漩涡发生器具有由主漩涡发生器边缘形成的入口流动开口。为了实现燃烧空气通过主漩涡发生器的均匀流动，燃气轮机燃烧器具有入口流动引导装置，其具有从一个入口流动开口延伸到相邻入口流动开口的流动引导表面形成入口流动开口的主漩涡发生器边缘连接到其上，并且流动引导表面从那里径向向上变宽。主涡旋发生器围绕引燃燃烧器中心对称地布置，并且流动引导表面径向地在主漩涡发生器外部延伸。

2. 发明申请

US20130269352A1 GAS-TURBINE BURNER 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US20130269352A1
公开(公告)日：2013-10-17
申请号：US13715233
申请日：2012-12-14
申请人： Robert Angel , Drew Ehlert , Matthias Hase , Michael Huth , James Marshall , Yevgeniy Shteyman
发明人： Robert Angel , Drew Ehlert , Matthias Hase , Michael Huth , James Marshall , Yevgeniy Shteyman
IPC分类号： F23R3/14
CPC分类号： F23R3/14 , F23D2900/00008 , F23D2900/14701 , F23R3/286 , F23R3/343
摘要： A gas-turbine burner having a plurality of main swirl generators which each have an inlet flow opening formed by the main swirl generator edge is provided. In order to achieve a uniform flow of combustion air through the main swirl generator, the gas-turbine burner has an inlet-flow guide means with a flow guide surface which runs from one of the inlet-flow openings to an adjacent inlet-flow opening, to which the main swirl generator edges which form the inlet-flow openings are connected, and the flow guide surface widens from there radially upwards. The main swirl generators are central-symmetrically arranged around a pilot burner and the flow guide surface runs radially outside the main swirl generators.
摘要翻译：本发明提供一种燃气轮机燃烧器，其具有多个主漩涡发生器，每个主漩涡发生器具有由主漩涡发生器边缘形成的入口流动开口。为了实现燃烧空气通过主漩涡发生器的均匀流动，燃气轮机燃烧器具有入口流动引导装置，其具有从一个入口流动开口延伸到相邻入口流动开口的流动引导表面形成入口流动开口的主漩涡发生器边缘连接到其上，并且流动引导表面从那里径向向上变宽。主涡旋发生器围绕引燃燃烧器中心对称地布置，并且流动引导表面径向地在主漩涡发生器外部延伸。

3. 发明申请

US20100275605A1 Gas-Turbine Burner 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US20100275605A1
公开(公告)日：2010-11-04
申请号：US12668121
申请日：2008-07-02
申请人： Matthias Hase , Michael Huth , Robert Angel , Drew Ehlert , James Marshall , Yevgeniy Shteyman
发明人： Matthias Hase , Michael Huth , Robert Angel , Drew Ehlert , James Marshall , Yevgeniy Shteyman
IPC分类号： F02C7/22
CPC分类号： F23R3/14 , F23D2900/00008 , F23D2900/14701 , F23R3/286 , F23R3/343
摘要： A gas-turbine burner having a plurality of main swirl generators, each having an inlet flow opening formed by the main swirl generator edge, is provided. In order to achieve a uniform flow of combustion air through the main swirl generator, the gas-turbine burner has an inlet-flow guide means with a flow guide surface which runs from one of the inlet-flow openings to an adjacent inlet-flow opening, to which the main swirl generator edges which form the inlet-flow openings are connected, and the flow guide surface widens from there radially upwards. The main swirl generators are central-symmetrically arranged around a pilot burner and the flow guide surface runs radially outside the main swirl generators.
摘要翻译：一种具有多个主旋流发生器的燃气轮机燃烧器，其具有由主涡流发生器边缘形成的入口流动开口。为了实现燃烧空气通过主漩涡发生器的均匀流动，燃气轮机燃烧器具有入口流动引导装置，其具有从一个入口流动开口延伸到相邻入口流动开口的流动引导表面形成入口流动开口的主漩涡发生器边缘连接到其上，并且流动引导表面从那里径向向上变宽。主涡旋发生器围绕引燃燃烧器中心对称地布置，并且流动引导表面径向地在主漩涡发生器外部延伸。

4. 发明授权

US08387394B2 Gas-turbine burner 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US08387394B2
公开(公告)日：2013-03-05
申请号：US12668121
申请日：2008-07-02
申请人： Matthias Hase , Michael Huth , Robert Angel , Drew Ehlert , James Marshall , Yevgeniy Shteyman
发明人： Matthias Hase , Michael Huth , Robert Angel , Drew Ehlert , James Marshall , Yevgeniy Shteyman
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/14 , F23D2900/00008 , F23D2900/14701 , F23R3/286 , F23R3/343
摘要： A gas-turbine burner having a plurality of main swirl generators, each having an inlet flow opening formed by the main swirl generator edge, is provided. In order to achieve a uniform flow of combustion air through the main swirl generator, the gas-turbine burner has an inlet-flow guide means with a flow guide surface which runs from one of the inlet-flow openings to an adjacent inlet-flow opening, to which the main swirl generator edges which form the inlet-flow openings are connected, and the flow guide surface widens from there radially upwards. The main swirl generators are central-symmetrically arranged around a pilot burner and the flow guide surface runs radially outside the main swirl generators.
摘要翻译：一种具有多个主旋流发生器的燃气轮机燃烧器，其具有由主涡流发生器边缘形成的入口流动开口。为了实现燃烧空气通过主漩涡发生器的均匀流动，燃气轮机燃烧器具有入口流动引导装置，其具有从一个入口流动开口延伸到相邻入口流动开口的流动引导表面形成入口流动开口的主漩涡发生器边缘连接到其上，并且流动引导表面从那里径向向上变宽。主涡旋发生器围绕引燃燃烧器中心对称地布置，并且流动引导表面径向地在主漩涡发生器外部延伸。

5. 发明授权

US09127842B2 Burner, operating method and assembly method 有权
标题翻译：燃烧器，操作方法和装配方法
公开(公告)号：US09127842B2
公开(公告)日：2015-09-08
申请号：US12472729
申请日：2009-05-27
申请人： Andreas Böttcher , Thomas Grieb , Matthias Hase , Peter Kaufmann , Werner Krebs , Tobias Krieger , Patrick Lapp , Mark F. Rubio , Udo Schmitz , Daniel Vogtmann , Ulrich Wörz
发明人： Andreas Böttcher , Thomas Grieb , Matthias Hase , Peter Kaufmann , Werner Krebs , Tobias Krieger , Patrick Lapp , Mark F. Rubio , Udo Schmitz , Daniel Vogtmann , Ulrich Wörz
IPC分类号： F23R3/28 , F23R3/34
CPC分类号： F23R3/283 , F23R3/286 , F23R3/343 , F23R2900/00005 , F23R2900/00012 , F23R2900/00017 , F23R2900/03282 , Y10T29/4932 , Y10T29/49323 , Y10T29/49826
摘要： A burner incorporating a pilot cone and a mounting insert is provided. The pilot cone is constructed as a pilot cone assembly which is decoupled from the mounting insert. Further, an operating method for increasing the service life of a burner which incorporates a pilot cone assembly and a mounting insert is provided. The pilot cone assembly has a cone side and incorporates at least one further side where the further side is arranged to be essentially parallel to one of the sides of the mounting insert and spaced apart from it, so that between the further side and the side of the mounting insert there is a defined gap. In an operation of the burner, the gap is significantly reduced by the thermal expansion in at least at one point of contact between the further side and the side of the mounting insert. Finally, an assembly method is provided.
摘要翻译：提供了一种结合了先导锥体和安装插件的燃烧器。先导锥体构造为与安装插入件分离的先导锥体组件。此外，提供了一种用于增加包括先导锥组件和安装插入件的燃烧器的使用寿命的操作方法。导向锥组件具有锥形侧面并且包括至少一个另外的侧面，其中另一侧被布置成基本上平行于安装插入件的一个侧面并与之隔开，使得在另一侧和侧面之间安装插件有一个限定的间隙。在燃烧器的操作中，通过在安装插入件的另一侧和侧面之间的至少一个接触点处的热膨胀，间隙显着减小。最后，提供一种装配方法。

6. 发明授权

US09074762B2 Stabilizing the flame of a burner 有权
标题翻译：稳定燃烧器的火焰
公开(公告)号：US09074762B2
公开(公告)日：2015-07-07
申请号：US13388304
申请日：2010-08-02
申请人： Matthias Hase , Werner Krebs , Bernd Prade
发明人： Matthias Hase , Werner Krebs , Bernd Prade
IPC分类号： F23C9/06 , F23C9/00 , F23D11/38 , F23D14/48 , F23R3/34
CPC分类号： F23C9/06 , F23C9/006 , F23C2202/10 , F23C2202/20 , F23D11/38 , F23D14/48 , F23R3/343 , F23R2900/03282
摘要： A burner of a gas turbine including a reaction chamber and a plurality of jet nozzles opening into the reaction chamber is provided. Fluid is injected through an outlet into the reaction chamber by the jet nozzles using of a fluid stream wherein the fluid is burned into hot gas in the reaction chamber. An annular gap is disposed about the fluid stream for at least one jet nozzle so that a part of the hot gas is drawn out of the reaction chamber and flows opposite the fluid flow direction into the annular gap and is mixed with the fluid stream within the jet nozzle. The ring gap is formed by means of an insert tube, and wherein the insert rube includes a thickening at the upstream end. A method for stabilizing the flame of such a burner of a gas turbine is also provided.
摘要翻译：提供一种燃气轮机的燃烧器，其包括反应室和通向反应室的多个喷嘴。流体通过流体流通过喷嘴通过出口注入反应室，其中流体在反应室中被燃烧成热气体。围绕用于至少一个喷嘴的流体流布置有环形间隙，使得一部分热气体从反应室中抽出并且与流体流动方向相反地流动到环形间隙中，并与流体流内部混合喷嘴。环形间隙通过插入管形成，并且其中插入式立管在上游端包括增厚。还提供了一种用于稳定燃气轮机燃烧器的火焰的方法。

7. 发明授权

US09032736B2 Method for operating a burner and burner, in particular for a gas turbine 有权
标题翻译：用于操作燃烧器和燃烧器的方法，特别是用于燃气轮机
公开(公告)号：US09032736B2
公开(公告)日：2015-05-19
申请号：US13256293
申请日：2010-03-16
申请人： Matthias Hase
发明人： Matthias Hase
IPC分类号： F23R3/02 , F23R3/04 , F23R3/28 , F23R3/34
CPC分类号： F23R3/286 , F23R3/02 , F23R3/04 , F23R3/34
摘要： A method for operating a burner comprising a burner axis and at least one jet nozzle is provided. The nozzle or nozzles include a central axis, a jet nozzle outlet, a wall that runs in a radial direction starting from the central axis and that faces the burner axis and a volumetric fluid flow that includes a fuel and flows through the jet nozzle or nozzles to the jet nozzle outlet. An air film is formed at the jet nozzle outlet between the volumetric fluid flow including the fuel and the wall that faces the burner axis by means of air that is injected into the jet nozzle or nozzles along the wall that faces the burner axis.
摘要翻译：提供了一种用于操作包括燃烧器轴线和至少一个喷嘴的燃烧器的方法。喷嘴或喷嘴包括中心轴线，喷嘴喷嘴出口，从中心轴线开始并面向燃烧器轴线的径向延伸的壁和包含燃料并流过喷嘴或喷嘴的体积流体流到喷嘴出口。通过喷射到喷嘴中的空气或者沿着面向燃烧器轴线的壁的喷嘴，在喷嘴出口处形成包括燃料和面向燃烧器轴线的壁的容积流体流之间的空气膜。

8. 发明申请

US20130008168A1 BURNER FOR STABILIZING THE COMBUSTION OF A GAS TURBINE 审中-公开
标题翻译：燃烧器用于稳定燃气涡轮机的燃烧
公开(公告)号：US20130008168A1
公开(公告)日：2013-01-10
申请号：US13637046
申请日：2011-02-25
申请人： Matthias Hase
发明人： Matthias Hase
IPC分类号： F23R3/34 , F02C7/224 , F02C7/08
CPC分类号： F23R3/005 , F23L15/00 , F23R3/10 , F23R3/54 , F23R2900/00014 , Y02E20/348
摘要： A burner for stabilizing the combustion of a gas turbine is provided. The burner includes a combustion chamber and a plurality of nozzles opening out into the combustion chamber wherein fluid is introduced into the combustion chamber by the nozzles in the form of a fluid jet, wherein the fluid is burned in the combustion chamber to fatal a hot gas, wherein an annular gap is provided in the case of at least one nozzle for feeding the fluid to the nozzle at a nozzle inlet, wherein a preheater is provided for heating the fluid before entering the nozzle, wherein the preheater is a pre-burner with or without a combustion chamber, and wherein the pre-burner with or without a combustion chamber is arranged in the annular gap.
摘要翻译：提供了一种用于稳定燃气轮机燃烧的燃烧器。该燃烧器包括燃烧室和多个喷嘴，该喷嘴通向燃烧室，其中流体以流体射流的形式通过喷嘴引入燃烧室，其中流体在燃烧室中燃烧以致死热气体，其中在至少一个喷嘴的情况下设置环形间隙，用于在喷嘴入口处将流体供给到喷嘴，其中提供预热器用于在进入喷嘴之前加热流体，其中预热器是具有或没有燃烧室，并且其中具有或不具有燃烧室的预燃烧器布置在环形间隙中。

9. 发明申请

US20120186265A1 Stabilizing the flame of a burner 有权
标题翻译：稳定燃烧器的火焰
公开(公告)号：US20120186265A1
公开(公告)日：2012-07-26
申请号：US13388304
申请日：2010-08-02
申请人： Matthias Hase , Werner Krebs , Bernd Prade
发明人： Matthias Hase , Werner Krebs , Bernd Prade
IPC分类号： F23R3/36 , F02C7/224
CPC分类号： F23C9/06 , F23C9/006 , F23C2202/10 , F23C2202/20 , F23D11/38 , F23D14/48 , F23R3/343 , F23R2900/03282
摘要： A burner of a gas turbine including a reaction chamber and a plurality of jet nozzles opening into the reaction chamber is provided. Fluid is injected through an outlet into the reaction chamber by the jet nozzles using of a fluid stream wherein the fluid is burned into hot gas in the reaction chamber. An annular gap is disposed about the fluid stream for at least one jet nozzle so that a part of the hot gas is drawn out of the reaction chamber and flows opposite the fluid flow direction into the annular gap and is mixed with the fluid stream within the jet nozzle. The ring gap is formed by means of an insert tube, and wherein the insert rube includes a thickening at the upstream end. A method for stabilizing the flame of such a burner of a gas turbine is also provided.
摘要翻译：提供一种燃气轮机的燃烧器，其包括反应室和通向反应室的多个喷嘴。流体通过流体流通过喷嘴通过出口注入反应室，其中流体在反应室中被燃烧成热气体。围绕用于至少一个喷嘴的流体流布置有环形间隙，使得一部分热气体从反应室中抽出并且与流体流动方向相反地流动到环形间隙中，并与该流体流内的流体流混合喷嘴。环形间隙通过插入管形成，并且其中插入式立管在上游端包括增厚。还提供了一种用于稳定燃气轮机燃烧器的火焰的方法。

10. 发明申请

US20120174591A1 Fuel Line System, Method for Operating of a Gas Turbine, and a Method for Purging the Fuel Line System of a Gas Turbine 审中-公开
标题翻译：燃油管路系统，燃气轮机的运行方法以及燃气轮机燃油管路系统的清除方法
公开(公告)号：US20120174591A1
公开(公告)日：2012-07-12
申请号：US13496222
申请日：2010-09-23
申请人： Matthias Hase , Axel Mayr , Jürgen Meisl
发明人： Matthias Hase , Axel Mayr , Jürgen Meisl
IPC分类号： F02C7/22
CPC分类号： F02C7/228 , F02C7/232
摘要： A fuel line system for a gas turbine and a method for purging the same is provided. Parts of the line system may be purged using a comparatively low quantity of purging medium. To this end, a control valve is provided in each of the fuel line segments located immediately upstream of the fuel injection nozzles, the control characteristics of the control valve being adjustable by means of a fluid or gaseous control medium
摘要翻译：提供了一种用于燃气轮机的燃油管路系统及其清洗方法。可以使用相对较少量的清洗介质来清除管线系统的部分。为此，在位于燃料喷嘴的紧邻上游的每个燃料管线段中设置有控制阀，控制阀的控制特性可通过流体或气体控制介质

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