Combustion chamber assembly having removable center liner

Abstract From the Canadian patent

The combustion section of the gas turbine in comprised of an engine casing receiving compressor discharge air and housing a plurality of combustion chamber assemblies having removable inner center liners. The combustion chamber assemblies are comprised of an outer liner having an end wall in which fuel injectors are mounted and the removable inner center liner extending within the outer liner from the end wall to define an annular combustion chamber space adjacent the end wall.