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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

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.

3. 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。

4. 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。

5. 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。

6. 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。

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

US07000403B2 Primary fuel nozzle having dual fuel capability 失效
标题翻译：具有双重燃料能力的主燃料喷嘴
公开(公告)号：US07000403B2
公开(公告)日：2006-02-21
申请号：US10799970
申请日：2004-03-12
申请人： John Henriquez , Jacob McLeroy , Brian R. Mack , Vincent C. Martling
发明人： John Henriquez , Jacob McLeroy , Brian R. Mack , Vincent C. Martling
IPC分类号： F02C7/22 , F23R3/36
CPC分类号： F23R3/286 , F23R3/16 , F23R3/283 , F23R3/36 , F23R2900/00004
摘要： A fuel nozzle and gas turbine combustor capable of operating on multiple fuels with reduced carbon build-up to the fuel nozzle and adjacent combustor components is disclosed. The fuel nozzle incorporates a reconfigured gas fuel assembly and mixing tube to eliminate known areas of recirculation. Furthermore, the liquid fuel assembly includes reconfigured spray characteristics to further reduce droplet interaction with the mixing tube.
摘要翻译：公开了一种燃料喷嘴和燃气轮机燃烧器，其能够对燃料喷嘴和相邻的燃烧器部件的碳积累减少的多种燃料进行操作。燃料喷嘴包括重新配置的气体燃料组件和混合管，以消除已知的再循环区域。此外，液体燃料组件包括重新配置的喷雾特性，以进一步减少与混合管的液滴相互作用。

10. 发明授权

US06442946B1 Three degrees of freedom aft mounting system for gas turbine transition duct 有权
标题翻译：用于燃气轮机过渡管的三自由度后部安装系统
公开(公告)号：US06442946B1
公开(公告)日：2002-09-03
申请号：US09712735
申请日：2000-11-14
申请人： Robert J. Kraft , Charles Biondo , Brian R. Mack , Mark A. Minnich
发明人： Robert J. Kraft , Charles Biondo , Brian R. Mack , Mark A. Minnich
IPC分类号： F02C720
CPC分类号： F01D25/243 , F01D9/023 , F05D2250/241 , F05D2250/43 , F23R3/60
摘要： A multiple directional axes structural support system for use as the aft end mount for a gas turbine transition duct to a turbine inlet is disclosed. The mounting system is configured to withstand high temperature gradients and mechanical loads associated with gas turbine environments while allowing multiple axes adjustment and interface capability between the transition duct and the turbine inlet casing. A spherical ball joint allows for rotation about multiple (three) axes to compensate for relative thermal growth, manufacturing tolerances, and assembly tolerances between mating surfaces. The ball joint is held in place by fitted spacers, bosses, and a through-bolt, that when torqued will dampen out unwanted vibrations in the multi-axis mounting system.
摘要翻译：公开了用作用于到涡轮机入口的燃气轮机过渡管道的后端安装件的多方向轴结构支撑系统。安装系统被配置为承受与燃气轮机环境相关的高温梯度和机械负载，同时允许过渡管道和涡轮机入口套管之间的多个轴线调整和接口能力。球形球形接头允许围绕多（3）个轴线旋转，以补偿配合表面之间的相对热增长，制造公差和组装公差。球形接头通过安装的垫片，凸台和贯穿螺栓固定在适当的位置，当扭转时会抑制多轴安装系统中的不必要的振动。

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