METHOD FOR ADJUSTING A NATURAL GAS TEMPERATURE FOR A FUEL SUPPLY LINE OF A GAS TURBINE ENGINE
    1.
    发明申请
    METHOD FOR ADJUSTING A NATURAL GAS TEMPERATURE FOR A FUEL SUPPLY LINE OF A GAS TURBINE ENGINE 有权
    用于调节燃气涡轮发动机燃油供应天然气温度的方法

    公开(公告)号:US20140238035A1

    公开(公告)日:2014-08-28

    申请号:US14189206

    申请日:2014-02-25

    Abstract: The method for adjusting a natural gas temperature for a fuel supply line of a gas turbine engine includes measuring by infrared analysis the natural gas percentage content of methane (CH4), ethane (C2H6), propane (C3H8), butane (C4H10), carbon dioxide (CO2), calculating the nitrogen (N2) percentage content as the complement to 100 of the measured percentage content of methane (CH4), ethane (C2H6), propane (C3H8), butane (C4H10), carbon dioxide (CO2), calculating an index indicative of the natural gas energy content and adjusting the natural gas temperature on the basis of the index.

    Abstract translation: 用于调节燃气轮机的燃料供给管线的天然气温度的方法包括通过红外分析来测量甲烷(CH 4),乙烷(C 2 H 6),丙烷(C​​ 3 H 8),丁烷(C 4 H 10),碳 二氧化碳(CO2),计算氮(N2)百分含量,作为测量甲烷(CH4),乙烷(C2H6),丙烷(C​​3H8),丁烷(C4H10),二氧化碳(CO2), 计算指示天然气能量含量的指标,并根据指标调整天然气温度。

    GAS TURBINE WITH COOLING AIR COOLING SYSTEM AND METHOD FOR OPERATION OF A GAS TURBINE AT LOW PART LOAD
    2.
    发明申请
    GAS TURBINE WITH COOLING AIR COOLING SYSTEM AND METHOD FOR OPERATION OF A GAS TURBINE AT LOW PART LOAD 审中-公开
    具有冷却空气冷却系统的气体涡轮机和低部分负载下的气体涡轮机操作方法

    公开(公告)号:US20150089955A1

    公开(公告)日:2015-04-02

    申请号:US14501465

    申请日:2014-09-30

    CPC classification number: F02C9/18 F02C6/08 F02C7/143 F02C7/18 F02C9/52

    Abstract: A gas turbine and method for operating a gas turbine, includes a compressor, a combustor, a turbine and a cooling air cooling system having at least a first cooling air line going from a first bleed of the compressor to the turbine, and at least one second cooling air line at a downstream position of the compressor relative to the first cooling air line. A heat exchanger is arranged in the second cooling air line for cooling the extracted air of higher pressure. The heat exchanger is connected with an air inlet side of the compressor such that heat is transferred in order to heat up the inlet air of the compressor.

    Abstract translation: 一种用于操作燃气轮机的燃气轮机和方法,包括压缩机,燃烧器,涡轮机和冷却空气冷却系统,其具有至少第一冷却空气管线从压缩机的第一次泄放到涡轮机,以及至少一个 第二冷却空气管线在压缩机的下游位置相对于第一冷却空气管路。 在第二冷却空气管路中布置有热交换器,用于冷却抽出的较高压力的空气。 热交换器与压缩机的空气入口侧连接,以便传递热量以加热压缩机的入口空气。

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