Cooling path structure for concentrated cooling of seal area and gas turbine combustor having the same
Abstract:
A cooling path structure for concentrated cooling of a seal area in a duct assembly and a gas turbine combustor having the same are provided. The cooling path structure includes a concentrated cooling guide plate facing the seal area to introduce compressed cooling air into the seal area through a plurality of first cooling holes and a plurality of second cooling holes respectively formed in the guide plate. The first cooling holes are formed along a first inlet axis such that the introduced cooling air approaches a central axis of the seal area in a forward direction, and the second cooling holes are formed along a second inlet axis such that the introduced cooling air approaches the central axis of the seal area in a backward direction. The first and second inlet axes each are inclined at an acute angle relative to the central axis of the seal area.
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