Gas turbine and method for reconditioning such a gas turbine

摘要

An annular combustor (24) has inner and outer side walls (26,25) that are attached to an annular front plate along axial direction. The burners (21,22) are connected to the front plate that covers the flat front segments (23) for protecting against heat. A cooling plate is arranged behind a front plate. A seal portion is extended radially between the front segments that are detachably attached to the front plate. An outer sealing strip is arranged in the middle portion that is provided between the front segments, for sealing the outer edge of cooling plate. An independent claim is included for reconditioning method of gas turbine.