Burner for gas turbine engine

Details Burner for gas turbine engine Burner for gas turbine engine

F - Mech Eng,Light,Heat,Weapons

02

C

60/113, 60/165

F02C 7/00 (2006.01) F23R 3/34 (2006.01) F23R 3/42 (2006.01) F23R 3/54 (2006.01)

Patent

CA 1108873

BURNER FOR GAS TURBINE ENGINE Abstract of the Disclosure 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. -1-

316988

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