Gas turbine system based on main combustion area ammonia injection denitration and denitration method thereof
A gas turbine and main combustion zone technology, applied in gas turbine devices, turbine/propulsion fuel delivery systems, separation methods, etc., can solve problems such as high initial investment and operating costs, ammonia escape, etc., to improve the treatment effect, eliminate ammonia escape, Stable performance
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[0032] The present invention will be further described in detail below in conjunction with specific embodiments, which are explanations of the present invention rather than limitations.
[0033] The present invention is a gas turbine system based on ammonia injection and denitrification in the main combustion zone, such as figure 1 Shown, comprise compressor 2, combustor 5, turbine 14, generator 15, ammonia supply device and flue gas analyzer 16;
[0034] The combustion chamber 5 is successively a combustion chamber head 7, a main combustion zone 8, a supplementary combustion zone 9, and a mixing zone 10 from front to back; the combustion chamber head 7 is provided with a burner 6; the main combustion chamber Zone 8 is evenly provided with more than 4 ammonia injection nozzles 11 around the wall surface, the supplementary combustion zone 9 is provided with supplementary combustion air nozzles 12, and a number of mixing holes 13 are provided on the wall surface of the mixing zo...
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