Burner for gas turbine engine

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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F02C 3/00 (2006.01) F23R 3/04 (2006.01) F23R 3/06 (2006.01) F23R 3/50 (2006.01)

Patent

CA 1091455

IMPROVED BURNER FOR GAS TURBINE ENGINE Abstract of the Disclosure This invention relates to means for minimizing the smoke emitted from the exhaust of a gas turbine engine by judiciously adding air to the primary burning zone of a combustor at discrete locations. This invention contem- plates retrofitting existing burners by substituting the improvement for existing can burner components to obviate the necessity of replacing the entire combustor. -1-

298722

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