GAS TURBINE AND METHOD OF CONTROLLING A GAS TURBINE AT PART-LOAD CONDITION
    23.
    发明申请
    GAS TURBINE AND METHOD OF CONTROLLING A GAS TURBINE AT PART-LOAD CONDITION 审中-公开
    气体涡轮机和控制部分负荷条件下的气体涡轮机的方法

    公开(公告)号:US20140182297A1

    公开(公告)日:2014-07-03

    申请号:US13733313

    申请日:2013-01-03

    CPC classification number: F02C9/00 F02C9/48

    Abstract: A gas turbine includes a compressor section, a combustion section downstream from the compressor section, a turbine section downstream from the combustion section, and a controller. The controller controls the operation of the gas turbine at a reduced load, and is capable of querying a database including multiple sets of operational parameters for the gas turbine correlated with at least one measured output response at each set of operational parameters. One of the sets of operational parameters provides a desired gas turbine load that meets a target level for the output response. Related methods are also disclosed.

    Abstract translation: 燃气轮机包括压缩机部分,压缩机部分下游的燃烧部分,燃烧部分下游的涡轮部分和控制器。 控制器以减小的负载控制燃气轮机的操作,并且能够查询数据库,其包括与在每组操作参数下的至少一个测量的输出响应相关的燃气轮机的多组操作参数。 一组操作参数提供满足输出响应的目标水平的期望的燃气轮机负载。 还公开了相关方法。

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