Gas turbine

摘要

The turbine has a combustion chamber (10) with inner and outer walls (12, 13) comprising respective downstream end parts (12a, 13a). The end parts are arranged against respective inner and outer platforms of vanes (21) of a high pressure turbine nozzle (20). Connection screws (25,27) are radially installed in vanes by passing through holes formed in the end parts, where the screws connect the nozzle to the end parts.