FIELD: gas turbines with induced catalytic combustion. SUBSTANCE: provision is made for escape of fuel of catalytic guide burner for stabilization of main burner at catalytic burning of flow of pilot fuel. Catalytic guide burner is located in center relative to cross section of straightway passage and main burner is placed in the coronal position. Flow of pilot fuel is directed catalytic guide burner through preliminary forming cascade. EFFECT: burning fuel at minimum content of nitric oxides. 6 cl, 4 dwg
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