METHOD OF BURNING FUEL AND DEVICE FOR REALIZATION OF THIS METHOD Russian patent published in 2002 - IPC

Abstract RU 2193139 C1

FIELD: heat engineering; ignition and maintenance of combustion in combustion chambers of various power systems of gas- turbine plants, gas-turbine engines, furnaces, boilers, etc. SUBSTANCE: method consists in forming two zones of fuel-and-air mixture at shortage and excess of air by supplying fuel and air, twisting flow of fuel- and-air mixture in first zone; air and fuel are fed to first zone; part of fuel is fed before swirler; then, fuel-and-air mixture is transferred to second zone by enclosing it in limited space of gas duct; twisting the flow of fuel-and-air mixture in first zone is effected at intensity S found from the following formula: S = (ω2•Dfl)/2g≥104, where ω - is angular velocity of flow twisting; Dfl - is diameter of flow of fuel-and-air mixture; g is free fall acceleration; excess air coefficient α in first zone is selected within the following range: α = Gair/(Gm•L0) = 0,6÷1,5, where Gair - is flow rate of air through fuel burning unit; Gm - is total flow rate of fuel through fuel burning unit; L0 - is stoichiometric coefficient. Relationship of fraction of fuel fed before swirler G1 to total flow rate of fuel Gm is G1/Gm = 1-0. EFFECT: low thermal factor due to effective twisting of fuel-and-air mixture, transporting it through considerable distance from fuel burning unit inlet and forming cone at outlet of this unit. 5 cl, 4 dwg

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RU 2 193 139 C1

Authors

Sverdlov E.D.

Markov F.G.

Loshenkova N.S.

Dates

2002-11-20Published

2001-06-15Filed