Gradual oxidation with heat transfer
    3.
    发明授权
    Gradual oxidation with heat transfer 有权
    用热传递逐渐氧化

    公开(公告)号:US09353946B2

    公开(公告)日:2016-05-31

    申请号:US13417140

    申请日:2012-03-09

    摘要: Described herein are embodiments of systems and methods for oxidizing gases. In some embodiments, a reaction chamber is configured to receive a fuel gas and maintain the gas at a temperature within the reaction chamber that is above an autoignition temperature of the gas. The reaction chamber may also be configured to maintain a reaction temperature within the reaction chamber below a flameout temperature. In some embodiments, heat and product gases from the oxidation process can be used, for example, to drive a turbine, reciprocating engine, and injected back into the reaction chamber.

    摘要翻译: 这里描述了用于氧化气体的系统和方法的实施例。 在一些实施例中,反应室被配置为接收燃料气体并将气体保持在反应室内高于气体自燃温度的温度。 反应室也可以被配置为将反应室内的反应温度保持在熄火温度以下。 在一些实施例中,可以使用来自氧化过程的热和产物气体,例如驱动涡轮机,往复式发动机,并将其注入反应室。

    System and method to stage primary zone airflow
    6.
    发明申请
    System and method to stage primary zone airflow 审中-公开
    主要区域气流的系统和方法

    公开(公告)号:US20050144960A1

    公开(公告)日:2005-07-07

    申请号:US11074892

    申请日:2005-03-08

    摘要: A method of operating a combustion turbine engine that includes separating a flow of compressed air into a first flow stream and a second flow stream. The method also includes preheating the first flow stream to produce a preheated flow stream and premixing the second flow stream with a flow of fuel to produce a premixture. The method further includes mixing the premixture with a portion of the preheated first flow stream to produce a combustible mixture and combusting the combustible mixture to produce a flow of hot products of combustion.

    摘要翻译: 一种操作燃烧涡轮发动机的方法,包括将压缩空气流分离成第一流动流和第二流动流。 该方法还包括预热第一流动流以产生预热的流动流,并用燃料流预混合第二流动流以产生预混合物。 该方法还包括将预混合物与预热的第一流动流的一部分混合以产生可燃混合物并燃烧可燃混合物以产生热的燃烧产物流。

    System and method to stage primary zone airflow
    10.
    发明授权
    System and method to stage primary zone airflow 失效
    主要区域气流的系统和方法

    公开(公告)号:US06971227B2

    公开(公告)日:2005-12-06

    申请号:US10417016

    申请日:2003-04-16

    摘要: A combustion air delivery system comprising a compressor operable to provide a stream of compressed air and a bypass duct positioned to divide the stream of compressed air into a bypass flow stream and a primary flow stream. A recuperator is operable to preheat the primary flow to produce a flow of preheated compressed air. A premix chamber receives the bypass flow stream and mixes the bypass flow stream with a flow of fuel to produce a fuel-air flow. A can member at least partially defines a primary zone that receives the fuel-air flow and includes an aperture sized to admit a predetermined portion of the flow of preheated compressed air. The fuel-air flow and predetermined portion of the flow of preheated compressed air mix in the primary zone to produce a combustible flow. An igniter is operable to ignite the combustible flow.

    摘要翻译: 一种燃烧空气输送系统,包括可操作以提供压缩空气流的压缩机和定位成将压缩空气流分成旁路流和主流量的旁路管。 换热器可操作以预热主流以产生预热的压缩空气流。 预混室接收旁路流,并将旁路流与燃料流混合以产生燃料 - 空气流。 罐构件至少部分地限定接收燃料 - 空气流的主区,并且包括尺寸允许预热的压缩空气流的预定部分的孔。 燃料空气流和预热压缩空气流的预定部分在主区域中混合以产生可燃流。 点火器可操作地点燃可燃流。