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    • 2. 发明授权
    • Gas turbine pilot burner water injection and method of operation
    • 燃气轮机燃油喷射器及其运行方法
    • US06715295B2
    • 2004-04-06
    • US10152518
    • 2002-05-22
    • Satish GaddeThomas J. Gordon
    • Satish GaddeThomas J. Gordon
    • F02C330
    • F02C3/30F02C9/28
    • A gas turbine engine (12) including a water injection system (56) for providing a flow of water (60) to only a pilot diffusion combustion zone (20) of a dual-mode combustor (10) and not to a pre-mixed combustion zone (18) of the combustor. The selective reduction of peak flame temperature in the pilot flame zone provides a maximum reduction in the production of oxides of nitrogen with a minimum consumption of water. The pilot fuel fraction of the combustor may be increased prior to the initiation of the pilot water injection flow. The flow rate of the pilot injection water may be varied as a function of the power level of the gas turbine, and further as a function of the humidity of the ambient air (36).
    • 一种燃气涡轮发动机(12),包括用于仅向双模式燃烧器(10)的先导扩散燃烧区(20)提供水(60)的水流注入系统(56),而不是预混合 燃烧器的燃烧区(18)。 在引燃火焰区域中选择性降低峰值火焰温度可以最大限度地减少氮氧化物的产生,同时减少水的消耗。 在先导注水流动开始之前,可以增加燃烧器的引燃燃料部分。 先导注入水的流量可以根据燃气轮机的功率水平而变化,并且还可以作为环境空气(36)的湿度的函数而变化。