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1. 发明授权

US06418726B1 Method and apparatus for controlling combustor emissions 失效
标题翻译：用于控制燃烧器排放的方法和装置
公开(公告)号：US06418726B1
公开(公告)日：2002-07-16
申请号：US09871262
申请日：2001-05-31
申请人： Michael Jerome Foust , Hukam Chand Mongia
发明人： Michael Jerome Foust , Hukam Chand Mongia
IPC分类号： F23R360
CPC分类号： F23R3/286 , F23R3/14 , F23R3/343
摘要： A combustor for a gas turbine engine operates with high combustion efficiency and low carbon monoxide, nitrous oxide, and smoke emissions during low, intermediate, and high engine power operations is described. The combustor includes a mixer assembly including a pilot mixer, a main mixer, and a mid-power and cruise mixer. The pilot mixer includes a pilot fuel injector, at least one swirler, and an air splitter. The main mixer extends circumferentially around the pilot mixer. The mid-power and cruise mixer extends between the main and pilot mixers and includes a plurality of fuel injection ports which inject fuel radially inwardly to facilitate radial and circumferential fuel-air mixing to provide a substantially uniform fuel and air distribution for combustion.
摘要翻译：描述了用于燃气涡轮发动机的燃烧器，其具有高燃烧效率，并且在低，中，高发动机功率运行期间以低一氧化碳，一氧化二氮和烟雾排放进行操作。该燃烧器包括一个混合器组件，该混合器组件包括一个先导式混合器，一个主混合器和一个中等功率和巡航混合器。先导式混合器包括一个先导燃料喷射器，至少一个旋流器和一个空气分离器。主混合器围绕导向混合器周向延伸。中功率和巡航混合器在主混合器和先导式混合器之间延伸并且包括多个燃料喷射口，其向内径向向内喷射燃料，以便于径向和周向的燃料 - 空气混合，以提供用于燃烧的基本均匀的燃料和空气分布。

2. 发明授权

US06484489B1 Method and apparatus for mixing fuel to decrease combustor emissions 有权
标题翻译：用于混合燃料以减少燃烧器排放物的方法和装置
公开(公告)号：US06484489B1
公开(公告)日：2002-11-26
申请号：US09871343
申请日：2001-05-31
申请人： Michael Jerome Foust , Hukam Chand Mongia
发明人： Michael Jerome Foust , Hukam Chand Mongia
IPC分类号： F02C726
CPC分类号： F23R3/14 , F23R3/286 , F23R3/343
摘要： A combustor for a gas turbine engine operates with high combustion efficiency and low carbon monoxide, nitrous oxide, and smoke emissions during low, intermediate, and high engine power operations is described. The combustor includes a mixer assembly including a pilot mixer and a main mixer. The pilot mixer includes a pilot fuel injector, at least one swirler, and an air splitter. The main mixer extends circumferentially around the pilot mixer and includes a plurality of fuel injection ports and a conical air swirler upstream from the fuel injection ports. During idle engine power operation, the pilot mixer is aerodynamically isolated from the main mixer, and only air is supplied to the main mixer. During increased power operations, fuel is also supplied to the main mixer, and the main mixer conical swirler facilitates radial and circumferential fuel-air mixing to provide a substantially uniform fuel and air distribution for combustion.
摘要翻译：描述了用于燃气涡轮发动机的燃烧器，其具有高燃烧效率，并且在低，中，高发动机功率运行期间以低一氧化碳，一氧化二氮和烟雾排放进行操作。燃烧器包括一个包括先导式混合器和主混合器的混合器组件。先导式混合器包括一个先导燃料喷射器，至少一个旋流器和一个空气分离器。主混合器围绕先导混合器周向延伸，并且包括多个燃料喷射端口和在燃料喷射端口上游的锥形空气旋流器。在怠速发动机动力运行期间，先导式混合器与主混合器在空气动力学上隔离，只有空气供应到主混合器。在增加动力作业期间，燃料也被供应到主混合器，并且主混合器锥形旋流器有助于径向和周向的燃料 - 空气混合，以提供用于燃烧的基本均匀的燃料和空气分布。

3. 发明授权

US06405523B1 Method and apparatus for decreasing combustor emissions 失效
标题翻译：减少燃烧器排放的方法和装置
公开(公告)号：US06405523B1
公开(公告)日：2002-06-18
申请号：US09675667
申请日：2000-09-29
申请人： Michael Jerome Foust , Hukam Chand Mongia
发明人： Michael Jerome Foust , Hukam Chand Mongia
IPC分类号： F02C726
CPC分类号： F23R3/286 , F23R3/14 , F23R3/343
摘要： A combustor for a gas turbine engine operates with low nitrous oxide emissions during engine operations. The combustor includes a center mixer assembly and a second mixer assembly radially outward from the center mixer assembly. The center mixer assembly includes a pilot fuel injector, a swirler, and an air splitter, and the second mixer assembly includes a plurality of mixers that include a swirler, an atomizer, and a venturi. A combustor fuel delivery system includes a pilot fuel circuit to supply fuel to the center mixer assembly and a main fuel circuit to supply fuel to the second mixer assembly.
摘要翻译：用于燃气涡轮发动机的燃烧器在发动机操作期间以低的一氧化二氮排放进行操作。燃烧器包括中心混合器组件和从中心混合器组件径向向外的第二混合器组件。中心混合器组件包括引燃燃料喷射器，旋流器和空气分离器，并且第二混合器组件包括多个混合器，其包括旋流器，雾化器和文丘里管。燃烧器燃料输送系统包括用于向中心混合器组件供应燃料的先导燃料回路和向第二混合器组件供应燃料的主燃料回路。

4. 发明授权

US06381964B1 Multiple annular combustion chamber swirler having atomizing pilot 有权
标题翻译：具有雾化飞行员的多环形燃烧室旋流器
公开(公告)号：US06381964B1
公开(公告)日：2002-05-07
申请号：US09675664
申请日：2000-09-29
申请人： Byron Andrew Pritchard, Jr. , Allen Michael Danis , Michael Jerome Foust , Mark David Durbin , Hukam Chand Mongia
发明人： Byron Andrew Pritchard, Jr. , Allen Michael Danis , Michael Jerome Foust , Mark David Durbin , Hukam Chand Mongia
IPC分类号： F02G300
CPC分类号： F23R3/14 , F23R3/286 , F23R3/343
摘要： A mixer assembly for use in a combustion chamber of a gas turbine engine. The assembly includes a pilot mixer and a main mixer. The pilot mixer includes an annular pilot housing having a hollow interior, a pilot fuel nozzle mounted in the housing adapted for dispensing droplets of fuel to the hollow interior of the pilot housing, and a plurality of concentrically mounted axial swirlers positioned upstream from the pilot fuel nozzle. Each of the swirlers has a plurality of vanes for swirling air traveling through the respective swirler to mix air and the droplets of fuel dispensed by the pilot fuel nozzle. The main mixer includes a main housing surrounding the pilot housing defining an annular cavity, a plurality of fuel injection ports for introducing fuel into the cavity, and a swirler positioned upstream from the plurality of fuel injection ports having a plurality of vanes for swirling air traveling through the swirler to mix air and the droplets of fuel dispensed by the fuel injection ports.
摘要翻译：一种用于燃气涡轮发动机的燃烧室的混合器组件。该组件包括一个先导式混合器和一个主混合器。先导式混合器包括具有中空内部的环形导向壳体，安装在壳体中的引燃燃料喷嘴，其适于将燃料液滴分配到先导壳体的中空内部;以及多个同心安装的轴向旋流器，其位于导向燃料喷嘴。每个旋流器具有多个叶片，用于旋转通过相应的旋流器的旋转空气以混合空气和由引燃燃料喷嘴分配的燃料的液滴。主混合器包括围绕引导壳体的主壳体，其限定环形空腔，用于将燃料引入空腔中的多个燃料喷射端口和位于多个燃料喷射端口的上游的旋流器，其具有用于旋转空气行进的多个叶片通过旋流器来混合空气和由燃料喷射口分配的燃料的液滴。

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