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公开(公告)号：US08973367B2
公开(公告)日：2015-03-10
申请号：US13133741
申请日：2009-11-05
申请人： Andreas Böttcher , Tobias Krieger , Jürgen Meisl
发明人： Andreas Böttcher , Tobias Krieger , Jürgen Meisl
CPC分类号： F23R3/283 , F23D11/12 , F23D11/38 , F23D2214/00
摘要： Disclosed is a fuel lance for a burner, in particular a gas turbine burner, including a tip that has a nozzle surface including at least two fuel nozzles. The nozzle surface is provided with slots between the fuel nozzles. As a rule, the lance is provided for operation with a liquid fuel.
摘要翻译： 公开了一种用于燃烧器，特别是燃气涡轮燃烧器的燃料喷枪，其包括具有包括至少两个燃料喷嘴的喷嘴表面的末端。 喷嘴表面在燃料喷嘴之间设有槽。 通常，喷枪用于液体燃料的操作。
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2.发明授权公开(公告)号：US09074771B2
公开(公告)日：2015-07-07
申请号：US13126239
申请日：2009-09-14
CPC分类号： F23R3/002 , F23R3/10 , F23R2900/03042
摘要： A burner insert for a gas turbine combustion chamber is provided. The burner insert includes a burner insert wall including a cold side and a hot side, an edge delimiting the burner insert wall. The edge includes an edge bar extending at least partially circumferentially and projecting beyond the cold side. A burner opening for inserting a burner is formed in the burner insert wall.
摘要翻译： 提供了一种用于燃气轮机燃烧室的燃烧器插入件。 燃烧器插入件包括包括冷侧和热侧的燃烧器插入壁，界定燃烧器插入壁的边缘。 边缘包括至少部分地周向延伸并突出超过冷侧的边缘条。 用于插入燃烧器的燃烧器开口形成在燃烧器插入壁中。
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3.发明申请公开(公告)号：US20110197590A1
公开(公告)日：2011-08-18
申请号：US13126239
申请日：2009-09-14
CPC分类号： F23R3/002 , F23R3/10 , F23R2900/03042
摘要： A burner insert for a gas turbine combustion chamber is provided. The burner insert includes a burner insert wall including a cold side and a hot side, an edge delimiting the burner insert wall. The edge includes an edge bar extending at least partially circumferentially and projecting beyond the cold side. A burner opening for inserting a burner is formed in the burner insert wall.
摘要翻译： 提供了一种用于燃气轮机燃烧室的燃烧器插入件。 燃烧器插入件包括包括冷侧和热侧的燃烧器插入壁，界定燃烧器插入壁的边缘。 边缘包括至少部分地周向延伸并突出超过冷侧的边缘条。 用于插入燃烧器的燃烧器开口形成在燃烧器插入壁中。
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公开(公告)号：US20110247338A1
公开(公告)日：2011-10-13
申请号：US13133741
申请日：2009-11-05
申请人： Andreas Böttcher , Tobias Krieger , Jürgen Meisl
发明人： Andreas Böttcher , Tobias Krieger , Jürgen Meisl
CPC分类号： F23R3/283 , F23D11/12 , F23D11/38 , F23D2214/00
摘要： Disclosed is a fuel lance for a burner, in particular a gas turbine burner, including a tip that has a nozzle surface including at least two fuel nozzles. The nozzle surface is provided with slots between the fuel nozzles. As a rule, the lance is provided for operation with a liquid fuel.
摘要翻译： 公开了一种用于燃烧器，特别是燃气涡轮燃烧器的燃料喷枪，其包括具有包括至少两个燃料喷嘴的喷嘴表面的末端。 喷嘴表面在燃料喷嘴之间设有槽。 通常，喷枪用于液体燃料的操作。
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公开(公告)号：US08955328B2
公开(公告)日：2015-02-17
申请号：US13029246
申请日：2011-02-17
CPC分类号： F23R3/283 , F23C2900/07021 , F23D23/00 , F23R2900/00018
摘要： A burner arrangement is provided. The burner arrangement includes a support and at least two fuel nozzles attached to the support in the direction of flow, with each fuel nozzle including a support-side section which includes a contact surface on the support side with which it rests on a supporting surface of the support, with at least two fuel nozzle tips embodied in one piece extending out from the support-side section in the direction of flow and the support-side contact surface including at least two extension parts projecting in the direction of the support, with the extension parts each embodying a channel through which fuel is fed in each case to the fuel nozzle tips through passages which are arranged in the support-side contact surface of the support-side section.
摘要翻译： 提供燃烧器装置。 燃烧器装置包括支撑件和沿流动方向附接到支撑件的至少两个燃料喷嘴，每个燃料喷嘴包括支撑侧部分，该支撑侧部分包括在支撑侧上的接触表面，支撑侧支撑在支撑面的支撑表面上 所述支撑件具有至少两个燃料喷嘴尖端，所述至少两个燃料喷嘴尖端沿着流动方向从所述支撑侧部分延伸出一体，并且所述支撑侧接触表面包括至少两个在所述支撑件的方向上突出的延伸部分， 延伸部分各自包括通道，通过该通道将燃料在每种情况下通过布置在支撑侧部分的支撑侧接触表面中的通道供应到燃料喷嘴尖端。
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6.发明申请Burner arrangement for a combustion system for combusting liquid fuels and method for operating such a burner arrangement 审中-公开用于燃烧液体燃料的燃烧系统的燃烧器装置和用于操作这种燃烧器装置的方法公开(公告)号：US20100316966A1
公开(公告)日：2010-12-16
申请号：US12814707
申请日：2010-06-14
申请人： Andreas Böttcher , Tobias Krieger , Ulrich Wörz
发明人： Andreas Böttcher , Tobias Krieger , Ulrich Wörz
摘要： A burner arrangement for a combustion system for combusting liquid fuels including a burner hub, at least one air supply channel and at least one fuel supply channel for each fuel type is provided. The at least one fuel supply channel is embodied at least partially in the burner hub, with a flow divider arranged in at least one fuel supply channel, which is distanced from the wall of the fuel supply channel so that an interspace associated with the flow path of the fuel flowing through the fuel supply channel is formed between the wall of the fuel supply channel and the flow divider. A method for operating such a burner arrangement is also provided.
摘要翻译： 一种用于燃烧液体燃料的燃烧系统的燃烧器装置，包括燃烧器轮毂，至少一个空气供应通道和至少一个用于每种燃料类型的燃料供应通道。 至少一个燃料供应通道至少部分地被实施在燃烧器毂中，其中分流器布置在至少一个燃料供应通道中，该燃料供应通道与燃料供应通道的壁分开，使得与流动路径相关联的空间 在燃料供给通道的壁和分流器之间形成流过燃料供给通道的燃料。 还提供了一种用于操作这种燃烧器装置的方法。
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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
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。
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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
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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公开(公告)号：US20130213122A1
公开(公告)日：2013-08-22
申请号：US13882802
申请日：2010-11-02
申请人： Andreas Böttcher , Tobias Krieger
发明人： Andreas Böttcher , Tobias Krieger
IPC分类号： G01M15/14
CPC分类号： G01M15/14 , F01D5/005 , F05D2230/80 , F05D2260/80 , Y02T50/67
摘要： A method for testing a component for determining a maximum period of use for renewed use of the component is proposed. The component was in use and is subjected to a refurbishment for reuse. Core drilling of the used component enables a simultaneous refurbishment of the component. The state of the component is analyzed.
摘要翻译： 提出了一种用于测试用于确定组件的更新使用的最大使用时间的组件的方法。 该组件正在使用中，并进行翻新以便重新使用。 使用的部件的核心钻孔能够同时翻新部件。 分析组件的状态。
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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
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。
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