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The pilot burner for a high MN inlet burner is folded to substantially reduce the overall length of the combustor. The annular burner includes a splitter design where a diffuser surrounds the burner and connects to an outer shroud which contains the inlet of the pilot burner. Flow reverses into the

The pilot burner for a high MN inlet burner is folded to substantially reduce the overall length of the combustor. The annular burner includes a splitter design where a diffuser surrounds the burner and connects to an outer shroud which contains the inlet of the pilot burner. Flow reverses into the pilot burner where it is directed to the primary burning zone of the combustion chamber.

대표청구항 ▼

An annular burner for high Mach number airflow for a turbine type power plant including an inner generally axially extending wall defining an inner wall liner section, an outer generally axially extending wall spaced from said inner wall defining an outer wall liner section and together therewith de

An annular burner for high Mach number airflow for a turbine type power plant including an inner generally axially extending wall defining an inner wall liner section, an outer generally axially extending wall spaced from said inner wall defining an outer wall liner section and together therewith defining a main combustion zone, an inner and outer casing coaxially mounted relative to each other and defining a space for receiving said inner and outer wall liner sections, each being spaced therefrom for defining an inner shroud passageway and an outer shroud passageway, the inner and outer wall liner sections being substantially closer at its fore end relative to its rear end and having an inlet passage for receiving compressor discharge air and being in substantially axial alignment, splitter means at the inlet forming a portion of said inlet passage for proportioning some of said compressor discharge air into the inner and outer shroud passageways, a pilot burner disposed in said outer shroud passageway having an inner wall and an outer wall spaced from each other defining an annular passageway surrounding and being common to a portion of said outer wall liner section, said inner and outer wall of said pilot burner terminating intermediate the ends of said main combustion zone and defining an annular inlet for receiving compressor discharge air from said outer shroud passageway flowing in a reverse relationship to the normal flow of the main combustor working medium, at least one fuel nozzle at the inlet of said pilot burner, an exit end substantially at the forward end of said pilot burner and means for reversing the flow of pilot burner exhaust into said main combustion zone for flowing axially with said working medium.