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公开(公告)号：US07272933B2
公开(公告)日：2007-09-25
申请号：US10766437
申请日：2004-01-28
CPC分类号： A63B71/0605 , A63B63/00 , A63B2024/0043 , A63B2243/0025 , F01D25/32 , F02C3/305 , F02C7/143 , F02C7/1435 , F05D2260/211 , Y02T50/675
摘要： A method for operating a gas turbine engine, including a first compressor, a second compressor, and a turbine, coupled together in serial flow arrangement. The method includes channeling compressed airflow discharged from the first compressor through an intercooler having a cooling medium flowing therethrough, operating the intercooler such that condensate is formed in the intercooler from the compressed airflow, and channeling the condensate to an inlet of the first or second compressor to facilitate reducing an operating temperature of the gas turbine engine.
摘要翻译： 一种用于操作包括第一压缩机，第二压缩机和涡轮机的燃气涡轮发动机的方法，其以串联流动布置耦合在一起。 该方法包括将从第一压缩机排出的压缩气流引导通过具有流过其中的冷却介质的中间冷却器，操作中间冷却器，使冷凝物从压缩空气流形成在中间冷却器中，并将冷凝物引导至第一或第二压缩机的入口 以便于降低燃气轮机的工作温度。
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公开(公告)号：US07685827B2
公开(公告)日：2010-03-30
申请号：US11852802
申请日：2007-09-10
CPC分类号： A63B71/0605 , A63B63/00 , A63B2024/0043 , A63B2243/0025 , F01D25/32 , F02C3/305 , F02C7/143 , F02C7/1435 , F05D2260/211 , Y02T50/675
摘要： A method for operating a gas turbine engine, including a first compressor, a second compressor, and a turbine, coupled together in serial flow arrangement. The method includes channeling compressed airflow discharged from the first compressor through an intercooler having a cooling medium flowing therethrough, operating the intercooler such that condensate is formed in the intercooler from the compressed airflow, and channeling the condensate to an inlet of the first or second compressor to facilitate reducing an operating temperature of the gas turbine engine.
摘要翻译： 一种用于操作包括第一压缩机，第二压缩机和涡轮机的燃气涡轮发动机的方法，其以串联流动布置耦合在一起。 该方法包括将从第一压缩机排出的压缩气流引导通过具有流过其中的冷却介质的中间冷却器，操作中间冷却器，使冷凝物从压缩空气流形成在中间冷却器中，并将冷凝物引导至第一或第二压缩机的入口 以便于降低燃气轮机的工作温度。
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3.发明授权Method and apparatus for operating an intercooler for a gas turbine engine 有权用于操作燃气涡轮发动机的中间冷却器的方法和装置公开(公告)号：US07284377B2
公开(公告)日：2007-10-23
申请号：US10856640
申请日：2004-05-28
CPC分类号： F02C7/224 , F02C3/305 , F02C7/143 , Y02T50/675
摘要： A method for operating a gas turbine engine includes channeling compressed airflow discharged from a first compressor through an intercooler having a cooling medium flowing therethrough, channeling a working fluid through the intercooler to facilitate increasing an operating temperature of the working fluid, and channeling the discharged working fluid to a combustor to facilitate increasing an operating efficiency of the gas turbine engine.
摘要翻译： 一种用于操作燃气涡轮发动机的方法包括将从第一压缩机排出的压缩气流引导通过具有流过其中的冷却介质的中间冷却器，将工作流体引导通过中间冷却器，以便于增加工作流体的工作温度，并引导排出的工作 流体到燃烧器以便于提高燃气涡轮发动机的运行效率。
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公开(公告)号：US07487642B2
公开(公告)日：2009-02-10
申请号：US11264234
申请日：2005-11-01
CPC分类号： F02C7/224 , F02C3/305 , F05D2270/082 , Y02E20/16
摘要： A method for operating a gas turbine engine including a compressor, a combustor, and a turbine, coupled together in serial flow arrangement, and a fuel heating system including a heat exchanger and an economizer. The method includes channeling fuel through the heat exchanger, channeling a working fluid through the heat exchanger to facilitate regulating the operating temperature of the fuel and the operating temperature of the working fluid, and channeling the fuel and the working fluid into the gas turbine engine combustor to facilitate increasing a fuel efficiency of the gas turbine engine.
摘要翻译： 一种用于操作燃气涡轮发动机的方法，所述燃气涡轮发动机包括以串联流动方式联接在一起的压缩机，燃烧器和涡轮，以及包括热交换器和节能器的燃料加热系统。 该方法包括将燃料引导通过热交换器，将工作流体引导通过热交换器，以便于调节燃料的工作温度和工作流体的工作温度，以及将燃料和工作流体引入燃气轮机发动机燃烧器 以便于提高燃气涡轮发动机的燃料效率。
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