| 摘要 |
FIELD: combustion of liquid or gas fuel in compressed air in gas turbine. SUBSTANCE: compressed air is fed in a flow moving along the axis. A great number of partial flows is separated at the beginning of the flow. Part of fuel is fed to each flow separately and burnt up in the pilot flame. The remaining fuel is fed to the flow in different points. It is distributed in the flow heterogeneously. Fuel formed due to heterogeneous distribution in the flow has a local maximum in each pilot flame. Then fuel is ignited on pilot flames and burnt up. EFFECT: stabilized burning and complete combustion of fuel. 5 cl, 6 dwg
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