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US07246002B2 Method for controlling fuel splits to gas turbine combustor 失效
用于控制燃气分流到燃气轮机燃烧器的方法

Method for controlling fuel splits to gas turbine combustor
Abstract:
A method for determining a target exhaust temperature for a gas turbine including: determining a target exhaust temperature based on a compressor pressure condition; determining a temperature adjustment to the target exhaust temperature based on at least one parameter of a group of parameters consisting of specific humidity, compressor inlet pressure loss and turbine exhaust back pressure; and adjusting the target exhaust temperature by applying the temperature adjustment.
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