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1. 发明授权

US06446439B1 Pre-mix nozzle and full ring fuel distribution system for a gas turbine combustor 有权
标题翻译：用于燃气轮机燃烧器的预混合喷嘴和全环燃料分配系统
公开(公告)号：US06446439B1
公开(公告)日：2002-09-10
申请号：US09706425
申请日：2000-11-03
申请人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack
发明人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack
IPC分类号： F02G100
CPC分类号： F23R3/286 , F23D2900/00008 , F23D2900/00015 , F23R3/343
摘要： A fuel nozzle system for use in a combustor utilized in a combustion turbine for reducing nitrogen oxides and other pollutants including an annular fuel distribution manifold separately mounted away from a diffusion nozzle, said annular manifold having a plurality of fuel emitting passages or holes disposed along the downstream side of the manifold, said manifold being mounted in a position away from the diffuser nozzle body to allow air to stream around the manifold on all sides allowing for a thorough mixture of fuel and air around the annular manifold for better premixing in the combustion chamber. In an alternate embodiment, the diffusion nozzle is replaced by a pilot flame nozzle that is supplied with both air and fuel through a premix air and fuel chamber to a pilot flame nozzle which is used to sustain combustion in the secondary chamber. The use of a pilot flame nozzle that has a fuel and air mixture is believed to reduced NOx emissions.
摘要翻译：一种用于燃烧器中用于还原氮氧化物和其它污染物的燃烧器的燃料喷嘴系统，所述氮氧化物和其它污染物包括分开安装在远离扩散喷嘴的环形燃料分配歧管，所述环形歧管具有多个燃料发射通道歧管的下游侧，所述歧管安装在远离扩散器喷嘴体的位置，以允许空气在所有侧面上的歧管流动，允许在环形歧管周围充分混合燃料和空气，以在燃烧室中更好地预混合。在替代实施例中，扩散喷嘴由引燃火焰喷嘴代替，该引燃火焰喷嘴通过预混合空气和燃料室供应空气和燃料两者到用于维持次级室中的燃烧的引燃火焰喷嘴。使用具有燃料和空气混合物的先导火焰喷嘴被认为减少了NOx排放。

2. 发明授权

US06430932B1 Low NOx combustion liner with cooling air plenum recesses 失效
标题翻译：低NOx燃烧衬套，带有冷却空气通风孔
公开(公告)号：US06430932B1
公开(公告)日：2002-08-13
申请号：US09909029
申请日：2001-07-19
申请人： Vincent C. Martling , Brian R. Mack , Robert J. Kraft , Mark A. Minnich
发明人： Vincent C. Martling , Brian R. Mack , Robert J. Kraft , Mark A. Minnich
IPC分类号： F02G300
CPC分类号： F23R3/002 , F05B2220/302 , F23R3/04 , F23R3/60
摘要： A combustion liner assembly for reducing nitric oxide (NOx) emissions is disclosed. This combustion liner utilizes an annular plenum outside the liner shell for the purpose of containing cooling air that has been heated and reintroducing it into the combustion process. The air plenum can be enlarged to increase the amount of cooling air contained within and still allow for installation of the liner assembly into the combustor by utilizing recesses that locally reduce the diameter of the air plenum to allow it to pass by liner mounting pegs within the combustor assembly.
摘要翻译：公开了一种用于减少一氧化氮（NOx）排放的燃烧衬套组件。该燃烧衬套在衬套外部使用环形增压室，用于容纳已被加热并将其再引入燃烧过程的冷却空气。可以扩大空气增压室以增加容纳在其中的冷却空气的量，并且还允许通过利用局部减小空气增压室的直径以允许衬套组件通过衬套安装销的内部的凹部来将衬套组件安装到燃烧器中燃烧器组件。

3. 发明授权

US06427446B1 Low NOx emission combustion liner with circumferentially angled film cooling holes 有权
标题翻译：低NOx排放燃烧衬套具有周向成角度的薄膜冷却孔
公开(公告)号：US06427446B1
公开(公告)日：2002-08-06
申请号：US09664898
申请日：2000-09-19
申请人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack , Mark A. Minnich
发明人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack , Mark A. Minnich
IPC分类号： F02C7018
CPC分类号： F23R3/14 , F23R3/06 , F23R3/286 , F23R2900/03041 , Y02T50/675
摘要： An improved dual-stage, dual-mode turbine combustor capable of reducing nitric oxide (NOx) emissions is disclosed. This can-annular combustor utilizes multiple, single wall sheet metal combustor liners, generally annular in shape, and each liner having multiple hole film cooling means, which includes at least one pattern of small, closely spaced film cooling holes angled sharply in the downstream direction and various circumferential angles for improved liner cooling and improved fuel/air mixing within the liner, resulting in lower NOx emissions.
摘要翻译：公开了一种能够减少一氧化氮（NOx）排放的改进的双级双模涡轮机燃烧器。这种罐形环形燃烧器利用多个单壁金属板燃烧器衬套，其通常为环形形状，并且每个衬套具有多个孔膜冷却装置，其包括在下游方向上急剧变化的至少一个小的紧密间隔的薄膜冷却孔的图案以及各种圆周角度，用于改进衬管冷却，并改善衬套内的燃料/空气混合，导致较低的NOx排放。

4. 发明授权

US06374594B1 Silo/can-annular low emissions combustor 失效
标题翻译：筒仓/罐环式低排放燃烧器
公开(公告)号：US06374594B1
公开(公告)日：2002-04-23
申请号：US09614577
申请日：2000-07-12
申请人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack , Mark A. Minnich , Timothy J. teRiele
发明人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack , Mark A. Minnich , Timothy J. teRiele
IPC分类号： F02C300
CPC分类号： F23R3/346 , F23C6/04 , F23R3/46
摘要： A gas turbine engine for generating electricity having low NOx emissions that includes a turbine system linearly and axially connected by a power shaft to a compressor section and having a combustion section mounted vertically relative to the turbine section and the compressor section. The combustion system includes a plurality of individual combustors mounted in a circular or annular array around the upper cap or dome of the combustion system, each of said combustors being a dual mode, two-stage, emitting low levels of NOx. Each combustor exhausts its combustion gases into a common central plenum chamber that is vertically oriented relative to the turbine engine centerline. The plenum provides the hot gases to the turbine blades through an annular chamber 360 degrees around the shaft. The gas turbine engine vertical combustion system provides for a highly efficient, low nitric oxide emissions while allowing for uniform mixing of the combusting gases powering the turbine system.
摘要翻译：一种用于产生具有低NOx排放的电力的燃气涡轮发动机，其包括通过动力轴线线性和轴向连接到压缩机部分的涡轮机系统，并且具有相对于涡轮部分和压缩机部分垂直安装的燃烧部分。燃烧系统包括围绕燃烧系统的上盖或圆顶安装成圆形或环形阵列的多个单独的燃烧器，每个燃烧器是双模式，两级发射低水平的NOx。每个燃烧器将其燃烧气体排放到相对于涡轮发动机中心线垂直定向的公共中央增压室中。气室通过围绕轴360度的环形室向涡轮机叶片提供热气体。燃气涡轮发动机垂直燃烧系统提供了高效率的低一氧化氮排放，同时允许为涡轮机系统供电的燃烧气体的均匀混合。

5. 发明授权

US06813890B2 Fully premixed pilotless secondary fuel nozzle 有权
标题翻译：完全预混的无级次级燃油喷嘴
公开(公告)号：US06813890B2
公开(公告)日：2004-11-09
申请号：US10324949
申请日：2002-12-20
申请人： Vincent C. Martling , Robert J. Kraft , Brian R. Mack
发明人： Vincent C. Martling , Robert J. Kraft , Brian R. Mack
IPC分类号： F23R330
CPC分类号： F23R3/346 , F23R3/286
摘要： A premix secondary fuel nozzle for use in transferring a flame from a first combustion chamber to a second combustion chamber is disclosed. The secondary fuel nozzle includes multiple fuel circuits, each of which are fully premixed, and neither of which are injected in a manner to directly initiate or support a pilot flame, thereby lowering emissions. Multiple embodiments are disclosed for alternate configurations of a first fuel injector, including an annular manifold and a plurality of radially extending tubes.

6. 发明授权

US06446438B1 Combustion chamber/venturi cooling for a low NOx emission combustor 有权
标题翻译：用于低NOx排放燃烧器的燃烧室/文氏管冷却
公开(公告)号：US06446438B1
公开(公告)日：2002-09-10
申请号：US09605765
申请日：2000-06-28
申请人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack , Mark A. Minnich
发明人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack , Mark A. Minnich
IPC分类号： F23R330
CPC分类号： F23R3/286 , F23R3/005 , F23R3/06
摘要： A method and apparatus for providing air cooling to the venturi and the combustion chamber in a low NOx emission combustor as used in a gas turbine engine that includes providing an annular air passage surrounding said combustion chamber and venturi where said cooling air enters the combustion chamber/venturi near the aft portion of the combustion chamber passing the air along the combustion chamber, past the venturi where the air exits near the front portion of the convergent area of the venturi. The structure prevents any channel/passage cooling air from being received into the combustion chamber at the same time introducing the outlet of the cooling air after it has passed over the combustion chamber of the venturi and been heated back into the premix chamber thereby improving the efficiency of the combustor while reducing and lowering NOx emission in the combustion process.
摘要翻译：一种用于在燃气涡轮发动机中使用的低NOx排放燃烧器中的文丘里管和燃烧室提供空气冷却的方法和装置，其包括提供围绕所述燃烧室和文丘里管的环形空气通道，其中所述冷却空气进入燃烧室/ 靠近燃烧室后部的文丘里经过燃烧室的空气，经过文丘里管，其中空气在文丘里管的会聚区域的前部附近出来。该结构防止任何通道/通道冷却空气在其通过文丘里管的燃烧室并且被加热回到预混合室中之后同时引入冷却空气的出口，从而提高效率同时减少和降低燃烧过程中的NOx排放。

7. 发明授权

US06484509B2 Combustion chamber/venturi cooling for a low NOx emission combustor 有权
标题翻译：用于低NOx排放燃烧器的燃烧室/文氏管冷却
公开(公告)号：US06484509B2
公开(公告)日：2002-11-26
申请号：US10064248
申请日：2002-06-25
申请人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack , Mark A. Minnich
发明人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack , Mark A. Minnich
IPC分类号： F23R306
CPC分类号： F23R3/005 , F23R3/06 , F23R3/286
摘要： A method for providing cooling air to the venturi and the combustion chamber in a low NOx emission combustor as used in a gas turbine engine that includes the steps of providing an annular air passage surrounding said combustion chamber and venturi where said cooling air under pressure enters the combustion chamber/venturi near the aft portion of the combustion chamber, passing the air along the combustion chamber, past the venturi where the air exits near the front portion of the convergent area of the venturi. The method prevents any channel/passage cooling air from being received into the combustion chamber, and at the same time, introduces the outlet of the cooling air, after the air has passed over the combustion chamber of the venturi and has been heated, back into the premix chamber thereby improving the efficiency of the combustor while reducing and lowering NOx emission in the combustion process.
摘要翻译：一种用于在燃气涡轮发动机中使用的低NOx排放燃烧器中的文丘里管和燃烧室的冷却空气的方法，该方法包括以下步骤：提供围绕所述燃烧室和文丘里管的环形空气通道，其中所述压力下的冷却空气进入在燃烧室的后部附近的燃烧室/文丘里管，沿着燃烧室使空气通过文丘里管，其中空气在文丘里管的会聚区域的前部附近离开。该方法防止任何通道/通道冷却空气被接收到燃烧室中，并且同时在空气已经经过文丘里管的燃烧室并且被加热之后引入冷却空气的出口从而提高了燃烧器的效率，同时降低和降低了燃烧过程中的NOx排放。

8. 发明授权

US06282904B1 Full ring fuel distribution system for a gas turbine combustor 有权
标题翻译：用于燃气轮机燃烧器的全环燃料分配系统
公开(公告)号：US06282904B1
公开(公告)日：2001-09-04
申请号：US09443916
申请日：1999-11-19
申请人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack , Mark A. Minnich , David Stephens
发明人： Robert J. Kraft , Vincent C. Martling , Brian R. Mack , Mark A. Minnich , David Stephens
IPC分类号： F02C100
CPC分类号： F23R3/286 , F23D2900/00008 , F23D2900/00015 , F23R3/343
摘要： A fuel nozzle system for use in a combustor utilized in a combustion turbine for reducing nitrogen oxides and other pollutants including an annular fuel distribution manifold separately mounted away from a diffusion nozzle, said annular manifold having a plurality of fuel emitting passages or holes disposed along the downstream side of the manifold, said manifold being mounted in a position away from the diffuser nozzle body to allow air to stream around the manifold on all sides allowing for a thorough mixture of fuel and air around the annular manifold for better premixing in the combustion chamber.
摘要翻译：一种用于燃烧器中用于还原氮氧化物和其它污染物的燃烧器的燃料喷嘴系统，所述氮氧化物和其它污染物包括分开安装在远离扩散喷嘴的环形燃料分配歧管，所述环形歧管具有多个燃料发射通道歧管的下游侧，所述歧管安装在远离扩散器喷嘴体的位置，以允许空气在所有侧面上的歧管流动，允许在环形歧管周围充分混合燃料和空气，以在燃烧室中更好地预混合。

9. 发明授权

US06675584B1 Coated seal article used in turbine engines 失效
标题翻译：用于涡轮发动机的涂层密封件
公开(公告)号：US06675584B1
公开(公告)日：2004-01-13
申请号：US10064768
申请日：2002-08-15
申请人： Terry L. Hollis , Gerry A. Sileo , Stephen W. Jorgensen , Robert J. Kraft , Vincent C. Martling
发明人： Terry L. Hollis , Gerry A. Sileo , Stephen W. Jorgensen , Robert J. Kraft , Vincent C. Martling
IPC分类号： F02C720
CPC分类号： F01D11/005 , F01D9/023 , F02C7/20 , F05D2240/55 , F16J15/0806 , F16J15/0887
摘要： An improved sealing device for use between a transition duct aft frame and turbine inlet is disclosed. The improved sealing device includes a plurality of corrugated metal seals that are secured to the transition duct aft frame along the arc-like sections of the aft frame. The corrugated seals contact both the transition duct aft frame and turbine inlet to provide a more effective seal and to control the amount of compressor discharge air introduced to cool the turbine vane platforms. In the preferred embodiment, the corrugated seals are coated to reduce wear, fretting, and galling and are used in conjunction with a transition duct thermally free aft frame and pivot bearing mounting system. An alternate embodiment of the seal is also disclosed that utilizes an alternate cooling hole pattern for providing additional cooling air to the turbine vane platform.
摘要翻译：公开了一种用于过渡管道后部框架和涡轮机入口之间的改进的密封装置。改进的密封装置包括多个波纹金属密封件，其沿着后框架的弧形部分固定到过渡管道后部框架。波纹密封件接触过渡管道后部框架和涡轮机入口以提供更有效的密封并且控制引入以冷却涡轮叶片平台的压缩机排出空气的量。在优选实施例中，波纹状密封件被涂覆以减少磨损，磨损和磨损，并且与过渡管道热释放后框架和枢转轴承安装系统结合使用。还公开了密封件的替代实施例，其利用替代的冷却孔图案来向涡轮叶片平台提供额外的冷却空气。

10. 发明授权

US06442929B1 Igniter assembly having spring biasing of a semi-hemispherical mount 失效
标题翻译：点火器组件具有半半球形安装座的弹簧偏置
公开(公告)号：US06442929B1
公开(公告)日：2002-09-03
申请号：US09873732
申请日：2001-06-04
申请人： Robert J. Kraft , Brian R. Mack , Mark A. Minnich , Peter R. Winch
发明人： Robert J. Kraft , Brian R. Mack , Mark A. Minnich , Peter R. Winch
IPC分类号： F02C7266
CPC分类号： F02C7/266 , F05D2250/241
摘要： An igniter assembly for a combustor of a gas turbine, the combustor being of a type including a case and a liner within said case, the assembly comprising an igniter including an elongate body having a first end, a second end, and a mounting feature intermediate said first and second ends, and the mounting feature includes a semi-hemispherical surface and an electrode extending through the body, and a base having an internal cavity with a first internal land, a second internal land opposite the first internal land, first seal A means in sealing contact with the first internal land, and biasing means, such as a spring, in contact with the second internal land and said mounting feature. The mounting feature is located within the cavity, the semi-hemispherical surface is proximate the first seal means, and the biasing means urges the semi-hemispherical surface into sealing contact with the first seal means to prevent the leakage of air therethrough.
摘要翻译：一种用于燃气涡轮机的燃烧器的点火器组件，该燃烧器是包括壳体和所述壳体内的衬套的类型，所述组件包括点火器，所述点火器包括具有第一端，第二端和安装特征中间件的细长主体所述第一和第二端，并且所述安装特征包括半球形表面和延伸穿过所述主体的电极，以及具有内腔的基座，所述内腔具有第一内部接地，与所述第一内部接地相对的第二内部接地，第一密封件A 与第一内部接合处密封接触的装置，以及与第二内部接地和所述安装特征接触的诸如弹簧的偏置装置。安装特征位于腔体内，半球形表面靠近第一密封装置，并且偏压装置促使半球形表面与第一密封装置密封接触，以防止空气通过其中。

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