GAS TURBINE AND OPERATING METHOD THEREOF
    1.
    发明申请
    GAS TURBINE AND OPERATING METHOD THEREOF 有权
    燃气轮机及其运行方法

    公开(公告)号:US20110138818A1

    公开(公告)日:2011-06-16

    申请号:US13056064

    申请日:2009-09-24

    摘要: Provided is a gas turbine capable of achieving high-speed startup of the gas turbine through quick operation control of an ACC system during startup of the gas turbine, improving the cooling efficiency of turbine stationary components, and quickly carrying out an operation required for cat back prevention during shutdown of the gas turbine. Included are a pressurizing device (40) connected to a branching channel (42) branching from the discharge side of a compressor (11) and capable of carrying out an operation for introducing and pressurizing air independently from the compressor (11); a temperature-control-medium supply channel (43) that guides compressed air pressurized at the pressuring device (40) to a turbine-cooling-medium channel (50) provided in stationary components of a turbine (13); and a temperature-control-medium return channel (44) that guides the compressed air that has passed through the turbine-cooling-medium channel (50) to the discharge side of the compressor (11) such that the flows are combined, and the pressurizing device (40) is operated at startup of the gas turbine and in preparation immediately before startup to carry out temperature-raising and cooling by letting the compressed air flow in the turbine-cooling-medium channel (50). The pressurizing device (40) is operated during shutdown of the gas turbine to exhaust the high-temperature gas remaining in the turbine (13).

    摘要翻译: 提供一种燃气轮机,其能够通过在燃气轮机启动期间ACC系统的快速操作控制来实现燃气轮机的高速启动,提高涡轮机固定部​​件的冷却效率,并且快速地执行回猫所需的操作 在燃气轮机停机期间的预防。 包括连接到从压缩机(11)的排出侧分支的分支通道(42)并且能够独立于压缩机(11)执行用于引入和加压空气的操作的加压装置(40)。 将压缩装置(40)加压的压缩空气引导到设置在涡轮机(13)的静止部件中的涡轮冷却介质通道(50)的温度控制介质供给通路(43)。 以及温度控制介质返回通道(44),其将已经通过所述涡轮冷却介质通道(50)的压缩空气引导到所述压缩机(11)的排出侧,使得所述流合并,并且 加压装置(40)在燃气轮机起动时运转,并且在启动之前准备进行,以通过使涡轮机冷却介质通道(50)中的压缩空气流动来进行升温和冷却。 加压装置(40)在燃气轮机关闭期间运行,以排出剩余在涡轮机(13)中的高温气体。

    Gas turbine and operating method thereof
    2.
    发明授权
    Gas turbine and operating method thereof 有权
    燃气轮机及其运行方法

    公开(公告)号:US09255490B2

    公开(公告)日:2016-02-09

    申请号:US13056064

    申请日:2009-09-24

    摘要: Provided is a gas turbine capable of achieving high-speed startup of the gas turbine through quick operation control of an ACC system during startup of the gas turbine, improving the cooling efficiency of turbine stationary components, and quickly carrying out an operation required for cat back prevention during shutdown of the gas turbine. Included are a pressurizing device (40) connected to a branching channel (42) branching from the discharge side of a compressor (11) and capable of carrying out an operation for introducing and pressurizing air independently from the compressor (11); a temperature-control-medium supply channel (43) that guides compressed air pressurized at the pressuring device (40) to a turbine-cooling-medium channel (50) provided in stationary components of a turbine (13); and a temperature-control-medium return channel (44) that guides the compressed air that has passed through the turbine-cooling-medium channel (50) to the discharge side of the compressor (11) such that the flows are combined, and the pressurizing device (40) is operated at startup of the gas turbine and in preparation immediately before startup to carry out temperature-raising and cooling by letting the compressed air flow in the turbine-cooling-medium channel (50). The pressurizing device (40) is operated during shutdown of the gas turbine to exhaust the high-temperature gas remaining in the turbine (13).

    摘要翻译: 提供一种燃气轮机,其能够通过在燃气轮机启动期间ACC系统的快速操作控制来实现燃气轮机的高速启动,提高涡轮机固定部​​件的冷却效率,并且快速地执行回猫所需的操作 在燃气轮机关闭期间的预防。 包括连接到从压缩机(11)的排出侧分支的分支通道(42)并且能够独立于压缩机(11)执行用于引入和加压空气的操作的加压装置(40)。 将压缩装置(40)加压的压缩空气引导到设置在涡轮机(13)的静止部件中的涡轮冷却介质通道(50)的温度控制介质供给通路(43)。 以及温度控制介质返回通道(44),其将已经通过所述涡轮冷却介质通道(50)的压缩空气引导到所述压缩机(11)的排出侧,使得所述流合并,并且 加压装置(40)在燃气轮机起动时运转,并且在启动之前准备进行,以通过使涡轮机冷却介质通道(50)中的压缩空气流动来进行升温和冷却。 加压装置(40)在燃气轮机关闭期间运行,以排出剩余在涡轮机(13)中的高温气体。