Development of Can-Type Low NO sub(x) Combustor for Micro Gas Turbine (Fundamental Characteristics in a Primary Combustion Zone with Upward Swirl)

Development of Can-Type Low NO sub(x) Combustor for Micro Gas Turbine (Fundamental Characteristics in a Primary Combustion Zone with Upward Swirl)

Can-type low NO sub(x) combustor for micro gas turbine was developed. The distributions of temperature and gas compositions in the primary zone were measured and the behavior of the burned gas recirculation by the upward swirl flow was discussed on the basis of the measured results. When the length...

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Veröffentlicht in:Fuel (Guildford) 2007-10, Vol.86 (15), p.2463-2463
Hauptverfasser: Furuhata, Tomohiko, Amano, Shunsuke, Yotoriyama, Kousaku, Arai, Masataka
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container_issue 15
container_start_page 2463
container_title Fuel (Guildford)
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creator Furuhata, Tomohiko
Amano, Shunsuke
Yotoriyama, Kousaku
Arai, Masataka
description Can-type low NO sub(x) combustor for micro gas turbine was developed. The distributions of temperature and gas compositions in the primary zone were measured and the behavior of the burned gas recirculation by the upward swirl flow was discussed on the basis of the measured results. When the length of primary zone was 109 mm, the lean combustion limit was higher and CO and NO sub(x) concentrations at the combustor exit were lower than those in the other lengths. In the case of 175 mm, the flame in the primary zone changed to luminous flame, and the CO and NO sub(x) concentrations in exhaust gas were increased. The effect of guide vane height strongly affected the lean combustion limit. The limit greatly fell when the height was 8 mm.
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title Development of Can-Type Low NO sub(x) Combustor for Micro Gas Turbine (Fundamental Characteristics in a Primary Combustion Zone with Upward Swirl)
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