The experimental investigation of the operational characteristics of fuel nozzle for a heavy gas turbine was performed.
对某重型燃气轮机燃料喷嘴的工作特性进行了试验研究。
The invention relates to a gas turbine premixer with internal cooling. A system that includes a turbine fuel nozzle (144) comprising an air-fuel premixer (170).
本发明涉及具有内冷却的燃气涡轮机预混合器,具体而言,一种系统包括含有空气-燃料预混合器(170)的涡轮燃料喷嘴(144)。
The effects of nozzle structure, fuel gas injection velocity and excess air coefficient on NOx emission in high temperature air combustion were investigated.
通过两种结构烧嘴的热态燃烧试验对比,研究了烧嘴结构、燃气射流速度、过量空气系数对高温空气燃烧过程氮氧化物排放的影响特性。
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