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Alternately swirling mains in lean premixed gas turbine combustors

机译:稀薄预混燃气轮机燃烧室中的交替旋转主电源

摘要

A gas turbine combustor for producing hot gas by burning a fuel in compressed air comprising a combustor central axis and multiple main swirlers with respective swirler axes disposed about and parallel to the combustor central axis, each main swirler delivering an air fuel mixture flowing through it and about its swirler axis, wherein each swirler imparts rotation to the air fuel mixture flowing through it in a direction opposite that of adjacent swirlers. This combustor configuration reduces shear where the outer edges of adjacent flows meet, allowing for greater tuning of the combustion chamber and reduced NOx and CO emissions.
机译:一种通过在压缩空气中燃烧燃料来产生燃气的燃气轮机燃烧器,该燃烧器包括燃烧器中心轴和多个主旋流器,多个主旋流器分别围绕并平行于燃烧器中心轴设置,每个主旋流器输送流过它的空气燃料混合物,并且绕其旋流器轴线旋转,其中每个旋流器均以与相邻旋流器相反的方向使流过它的空气燃料混合物旋转。这种燃烧器的配置减少了在相邻流的外边缘相遇处的剪切力,从而使燃烧室的调节更加出色,并减少了NOx和CO的排放。

著录项

  • 公开/公告号US9500368B2

    专利类型

  • 公开/公告日2016-11-22

    原文格式PDF

  • 申请/专利权人 WILLIAM R. RYAN;

    申请/专利号US20080235866

  • 发明设计人 WILLIAM R. RYAN;

    申请日2008-09-23

  • 分类号F23R3/14;F23R3/34;

  • 国家 US

  • 入库时间 2022-08-21 13:41:56

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