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    • 2. 发明授权
    • System and method for thermal control in a gas turbine engine
    • 燃气轮机的热控制系统和方法
    • US09003764B2
    • 2015-04-14
    • US13329203
    • 2011-12-16
    • Pradeep Stanley ThackerAaron John Avagliano
    • Pradeep Stanley ThackerAaron John Avagliano
    • F02C7/08F02C6/00F02C3/30F22B1/18F02C1/00F02C1/06F02C6/04
    • F02C1/06F02C1/007F02C6/00F02C6/003F02C6/04Y02E20/16
    • A system includes a gas turbine engine that includes a compressor section configured to generate compressed air and a combustor coupled to the compressor section. The combustor is configured to combust a first mixture comprising the compressed air and a first fuel to generate a first combustion gas. The gas turbine engine also includes a turbine section coupled to the combustor. The turbine section is configured to expand the first combustion gas to generate an exhaust gas. The gas turbine engine also includes a boiler coupled to the turbine section. The boiler is configured to combust a second mixture comprising a portion of the first combustion gas and a second fuel to generate a second combustion gas that is routed to the turbine section. In addition, the boiler generates a first steam from heat exchange with the second combustion gas.
    • 一种系统包括燃气涡轮发动机,其包括构造成产生压缩空气的压缩机部分和连接到压缩机部分的燃烧器。 燃烧器构造成燃烧包括压缩空气和第一燃料的第一混合物以产生第一燃烧气体。 燃气涡轮发动机还包括联接到燃烧器的涡轮部分。 涡轮部分构造成膨胀第一燃烧气体以产生废气。 燃气涡轮发动机还包括联接到涡轮部分的锅炉。 锅炉构造成燃烧包括第一燃烧气体的一部分和第二燃料的第二混合物,以产生路由到涡轮部分的第二燃烧气体。 此外,锅炉产生与第二燃烧气体进行热交换的第一蒸汽。