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    Method and apparatus for reducing gas turbine engine emissions
    2.
    发明授权
    Method and apparatus for reducing gas turbine engine emissions 失效
    减少燃气轮机发动机排放的方法和装置

    公开(公告)号：US07260935B2

    公开(公告)日：2007-08-28

    申请号：US11143266

    申请日：2005-06-02

    申请人： Andrei Colibaba-Evulet ,  Michael John Bowman ,  Simon Ralph Sanderson ,  Anthony John Dean

    发明人： Andrei Colibaba-Evulet ,  Michael John Bowman ,  Simon Ralph Sanderson ,  Anthony John Dean

    IPC分类号： F02C1/00

    CPC分类号： F23R3/54 ,  F23R3/002 ,  F23R3/14 ,  F23R3/34 ,  F23R2900/03044 ,  Y02T50/675

    摘要： A low emission turbine includes a reverse flow can-type combustor that generally includes a primary and secondary fuel delivery system that can be independently controlled to produce low CO, UHC, and NOx emissions at design set point and at conditions other than design set point. The reverse flow can-type combustor generally includes an annularly arranged array of swirler and mixer assemblies within the combustor, wherein each swirler and mixer in the array includes a primary and secondary fuel delivery system that can be independently controlled. Also disclosed herein is a can-type combustor that includes fluid passageways that perpendicularly impinge the outer surface of a heat shield. Processes for operating the can-type combustors are also disclosed.

    摘要翻译： 低排放涡轮机包括逆流罐式燃烧器，其通常包括主燃料输送系统和辅助燃料输送系统，其可独立控制以在设计设定点和设计设定点以外的条件下产生低CO，UHC和NOx排放。 反向流动罐式燃烧器通常包括在燃烧器内的环形排列的旋流器和混合器组件，其中阵列中的每个旋流器和混合器包括可以独立控制的主要和次要燃料输送系统。 本文还公开了一种罐型燃烧器，其包括垂直地撞击隔热罩的外表面的流体通道。 还公开了用于操作罐式燃烧器的方法。

    Systems and methods of reducing NOx emissions in gas turbine systems and internal combustion engines
    6.
    发明授权
    Systems and methods of reducing NOx emissions in gas turbine systems and internal combustion engines 失效
    减少燃气轮机系统和内燃机NOx排放的系统和方法

    公开(公告)号：US07650744B2

    公开(公告)日：2010-01-26

    申请号：US11388466

    申请日：2006-03-24

    申请人： Balachandar Varatharajan ,  Chellappa Balan ,  Michael John Bowman

    发明人： Balachandar Varatharajan ,  Chellappa Balan ,  Michael John Bowman

    IPC分类号： F02B43/00

    CPC分类号： F02C1/002 ,  F02C3/20 ,  F05D2270/082 ,  Y02T50/677

    摘要： A gas turbine systems of reducing NOX emissions and enhancing operability comprises a compressor; a combustor disposed downstream of and in fluid communication with the compressor; a turbine assembly disposed down stream of and in fluid communication with the combustor; an oxygen-enriched gas source disposed in selective fluid communication with the compressor, the combustor, or a combination of the foregoing, wherein the oxygen-enriched gas source is a pressure swing absorption system, an electrolyzer, or a membrane reactor.

    摘要翻译： 一种减少NOx排放并提高可操作性的燃气轮机系统包括：压缩机; 设置在压缩机下游并与压缩机流体连通的燃烧器; 涡轮组件，其布置在燃烧器的下游并与燃烧器流体连通; 设置成与压缩机，燃烧器或前述的组合选择性流体连通的富氧气体源，其中富氧气体源是变压吸收系统，电解器或膜反应器。

    Systems and methods for power generation with carbon dioxide isolation
    7.
    发明授权
    Systems and methods for power generation with carbon dioxide isolation 有权

    公开(公告)号：US07266940B2

    公开(公告)日：2007-09-11

    申请号：US11178165

    申请日：2005-07-08

    申请人： Chellappa Balan ,  Michael John Bowman ,  Joell Randolph Hibshman, II ,  Andrei Tristan Evulet ,  Jennifer Lynn Molaison

    发明人： Chellappa Balan ,  Michael John Bowman ,  Joell Randolph Hibshman, II ,  Andrei Tristan Evulet ,  Jennifer Lynn Molaison

    IPC分类号： F02C6/00

    CPC分类号： F02C9/40 ,  F02C3/22 ,  F02C3/34 ,  Y02E20/16

    摘要： A power generation system and method includes a first gas turbine system comprising a first combustion chamber configured to combust a first fuel stream of primarily hydrogen that is substantially free of carbon-based fuels. The first gas turbine system also includes a first compressor configured to supply a first portion of compressed oxidant to the first combustion chamber and a first turbine configured to receive a first discharge from the first combustion chamber and generate a first exhaust and electrical energy. The power generation system further includes a second gas turbine system comprising a second combustion chamber configured to combust a second fuel stream to generate a second discharge. The first compressor of the first gas turbine system is configured to supply a second portion of compressed oxidant to the second combustion chamber. The second turbine system also includes a second turbine configured to receive the second discharge from the second combustion chamber to generate a second exhaust and electrical energy and a second compressor configured to receive the second discharge comprising carbon dioxide. The second compressor is also configured to discharge a recycle stream to the second combustion chamber and a split stream to a separator system adapted to recover carbon dioxide.