Patent ID: 7441409

Claim:
A gas turbine combustor assembly comprising: a combustor having a liner wall and a louver assembly extending circumferentially around an interior surface of the liner wall and threadingly mounted thereto, the assembly including a plurality of arcuate segments disposed end-to-end, each segment having circumferentially extending side walls, the sidewalls disposed angularly towards one another to provide each segment with a narrow closed end and a wider open end, the narrow end disposed inwardly relative to the combustor, the wider end mating with the liner wall, each segment co-operating with the liner wall to define an enclosed space therebetween, the enclosed space communicating with at least one inlet opening defined in the liner wall and a plurality of outlet openings defined in the segment, wherein each segment includes end bulkheads extending between lateral ends of the side walls, the bulkheads and sidewalls bounding therebetween the enclosed space and, wherein each bulkhead includes at least one outlet opening.