Gas turbine combustor, gas turbine, and jet engine

Details Gas turbine combustor, gas turbine, and jet engine Gas turbine combustor, gas turbine, and jet engine

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/42 (2006.01) F23M 99/00 (2010.01)

Patent

CA 2364377

For the purpose of reduced NOx gas emission, a gas turbine engine comprises a cylinder (2) having a combustion region (11) inside of the cylinder (2); a resonator (16) having a cavity (15) and provided around the surface of the cylinder (2) and sound absorption holes (14) formed on the cylinder (2) and having opening ends on the cylinder (2).

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