A combustor, a gas turbine, and a jet engine

F - Mech Eng,Light,Heat,Weapons – 23 – R

Patent

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Details

F23R 3/10 (2006.01) F02C 3/04 (2006.01) F23R 3/14 (2006.01) F23R 3/54 (2006.01)

Patent

CA 2353514

This invention relates to a combustor which can simultaneously reduce an amount of NOx exhaust and combustion oscillation. The combustor comprises an internal cylinder which accommodates a premixing nozzle, and an external cylinder which accommodates the internal cylinder and includes an air flow passage which supplies air from a compressor to the premixing nozzle. The air flow passage is provided with a punched metal plate near the maximum velocity fluctuation position wherein the velocity fluctuation of the air flow is increased to the maximum.

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