Gas turbine combustor

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

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F02C 3/00 (2006.01) F23C 7/02 (2006.01)

Patent

CA 1116416

47,705 GAS TURBINE COMBUSTOR ABSTRACT OF THE DISCLOSURE A stepped cylindrical combustion chamber for a gas turbine engine having secondary combustion air scoops pro- jecting thereinto wherein the first annular row of the air scoops are slanted obliquely to direct the air entering therethrough in a slightly downstream direction.

303606

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