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1. 发明授权

US09127844B2 Fuel nozzle 有权
标题翻译：燃油喷嘴
公开(公告)号：US09127844B2
公开(公告)日：2015-09-08
申请号：US13196611
申请日：2011-08-02
申请人： Ilya Aleksandrovich Slobodyanskiy , William Francis Carnell, Jr.
发明人： Ilya Aleksandrovich Slobodyanskiy , William Francis Carnell, Jr.
IPC分类号： F23R3/14 , B21D53/00 , F23R3/26 , F23R3/36
CPC分类号： F23R3/36 , Y10T29/49323
摘要： A fuel nozzle is provided and includes a nozzle body defining first and second interior regions for providing a supply of first and second fluids, a collar defining a third interior region and radial slots permitting radial ingress of a third fluid to the third interior region and a nozzle tip interposed between the nozzle body and the collar. The nozzle tip defines an annular slot, first discrete passageways by which the first fluid is communicated from the first interior region to the annular slot, second discrete passageways by which the first fluid is communicated from the annular slot to the radial slots, and third discrete passageways by which the second fluid is communicated from the second interior region to the radial slots.
摘要翻译：提供燃料喷嘴并且包括限定用于提供第一和第二流体的第一和第二内部区域的喷嘴体，限定第三内部区域的轴环和允许第三流体径向进入第三内部区域的径向槽，以及喷嘴头插在喷嘴主体和轴环之间。喷嘴尖端限定一个环形槽，第一离散通道，第一流体通过该第一离散通道从第一内部区域连通到环形槽，第二离散通道使第一流体从环形槽连通到径向狭槽，第三离散通道第二流体通过该通道从第二内部区域连通到径向槽。

2. 发明授权

US09181876B2 Method and apparatus for operating a gas turbine engine 有权
标题翻译：用于操作燃气涡轮发动机的方法和装置
公开(公告)号：US09181876B2
公开(公告)日：2015-11-10
申请号：US13343286
申请日：2012-01-04
申请人： Predrag Popovic , William Francis Carnell, Jr. , Andrew Mitchell Rodwell
发明人： Predrag Popovic , William Francis Carnell, Jr. , Andrew Mitchell Rodwell
IPC分类号： F02C7/16 , F02C6/08 , F02C7/224
CPC分类号： F02C7/16 , F02C6/08 , F02C7/143 , F02C7/224 , F05D2260/20
摘要： A gas turbine includes a compressor, a combustor downstream from the compressor and a heat transfer system, wherein the heat transfer system receives a compressed working fluid from the compressor. A fluid coupling between the heat transfer system and the combustor, wherein the fluid coupling receives the compressed working fluid from the heat transfer system. A conditioner in fluid communication with the compressor and a fluid coupling between the heat transfer system and the conditioner, wherein the fluid coupling receives a cooling media from the heat transfer system. A method for operating the gas turbine includes flowing a compressed working fluid from the compressor to the heat transfer system, transferring heat energy from the compressed working fluid to the heat transfer system, flowing the compressed working fluid from the heat transfer system to a combustor, and flowing a cooling media from the heat transfer system to a compressor inlet.
摘要翻译：燃气轮机包括压缩机，压缩机下游的燃烧器和传热系统，其中传热系统从压缩机接收压缩的工作流体。传热系统和燃烧器之间的流体耦合，其中流体联接器从传热系统接收压缩的工作流体。与压缩机流体连通的调节器和传热系统和调节器之间的流体联接，其中流体联接器从热传递系统接收冷却介质。用于操作燃气轮机的方法包括将压缩的工作流体从压缩机流动到传热系统，将热能从压缩的工作流体传递到传热系统，将压缩的工作流体从传热系统流到燃烧器，并将冷却介质从传热系统流动到压缩机入口。

3. 发明授权

US09121613B2 Combustor with brief quench zone with slots 有权
标题翻译：燃烧器与狭缝的短暂淬火区域
公开(公告)号：US09121613B2
公开(公告)日：2015-09-01
申请号：US13488466
申请日：2012-06-05
申请人： William Francis Carnell, Jr. , Gregory Allen Boardman
发明人： William Francis Carnell, Jr. , Gregory Allen Boardman
IPC分类号： F02C3/20 , F23R3/14 , F23R3/42 , F23R3/12 , F23R3/30 , F23R3/58
CPC分类号： F23R3/42 , F23R2900/00015
摘要： The present application provides a combustor for combusting a number of flows of air and a number of flows of fuel. The combustor may include a central swirler for producing a high swirl quench air flow, a number of trapped vortex cavities surrounding the central swirler for producing a flow of combustion gases, a brief severe quench zone downstream of the trapped vortex cavities to quench the flow of combustion gases between an outer quench air flow and the high swirl quench air flow, and an expansion zone downstream of the brief severe quench zone.
摘要翻译：本申请提供了一种用于燃烧多个空气流和多个燃料流的燃烧器。燃烧器可以包括用于产生高漩涡骤冷空气流的中心旋流器，围绕中心旋流器的多个被捕获的涡流腔，用于产生燃烧气体流，在被捕获的涡流腔下游的短暂的严酷淬火区域以淬灭在外部骤冷空气流与高旋涡骤冷空气流之间的燃烧气体以及在短暂的严酷骤冷区下游的膨胀区。

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