Improved flame tube or "liner" for a combustion chamber of a...

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

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F23R 3/50 (2006.01) F23R 3/08 (2006.01)

Patent

CA 2413655

An improved flame tube or "liner" (112) for a combustion chamber (110) of a gas turbine with low emission of pollutants, of the type; comprising a cylindrical structure connected to the outlet of a premixing chamber (114) by means of a truncated conical end (120), in which the premixing chamber (114) is supplied with air which is guided by a cavity (116) which is located between the flame tube (112) and outer walls (118) of the combustion chamber (110), this air circulating in the opposite direction to the flow of combustion products; a first cylindrical region (122) of the flame tube (112) is surrounded by a cylindrical casing (136) which creates an annular chamber (138).

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