Method for premixing air with a gaseous fuel and burner arrangement for conducting said method
AssigneeAnsaldo Energia Switzerland AG
InventorsFernando Biagioli, Madhavan Narasimhan Poyyapakkam
Life of this patent
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Abstract
A method for premixing air with a gaseous fuel for being burned in a combustion chamber includes: guiding the air in an air stream along a burner axis through a coaxial air tube into a combustion chamber arranged at an end of said air tube; and impressing a swirl on the air stream by passing it through a first swirl device concentrically arranged within the air tube and comprising a plurality of radially oriented first blades. The method further includes: injecting gaseous fuel into the air stream at the first swirl device; and mixing said air in said air stream with the injected gaseous fuel in a first mixing zone arranged just after said first swirl device.
Claims29
A method for premixing air with a gaseous fuel for being burned in a combustion chamber, said method comprising:
- guiding said air in an air stream along a burner axis through a coaxial air tube into a combustion chamber arranged at an end of said air tube;
- impressing a swirl on said air stream by passing it through a first swirl device concentrically arranged within said air tube and comprising a plurality of radially oriented first blades;
- injecting gaseous fuel into said air stream at said first swirl device;
- and
- mixing said air in said air stream with the injected gaseous fuel in a first mixing zone arranged just after said first swirl device;
- sending the mixed fuel/air stream leaving said first mixing zone through a second swirl device concentrically arranged within said air tube and
- comprising a plurality of radially oriented second blades to reduce the swirl of the mixed fuel/air stream;
- wherein the camber line of a blade of the second blades is aligned at a leading edge of the blade of the second blades with the camber line of a blade of the first blades at a trailing edge of the blade of the first blades to avoid flow separation,
- injecting gaseous fuel into said mixed fuel/air stream at said second swirl device;
- and
- further mixing said mixed fuel/air stream with the injected gaseous fuel in a second mixing zone arranged just between said second swirl device and said combustion chamber.
Dependencies are inferred from the claim text.