Gas turbine part comprising a near wall cooling arrangement
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United States of America Patent
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Apr 17, 2018
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N/A
app pub date -
Nov 27, 2013
filing date -
Nov 30, 2012
priority date (Note) -
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Abstract
A gas turbine combustor part of a gas turbine includes a wall, containing a plurality of near wall cooling channels extending essentially parallel to each other in a first direction within the wall in close vicinity to the hot side and being arranged in at least one row extending in a second direction. The near wall cooling channels are each provided at one end with an inlet for the supply of cooling air, and on the other end with an outlet for the discharge of cooling air. The inlets open into a common feeding channel for cooling air supply, and the outlets open into a common discharge channel for cooling air discharge. The feeding channel and the discharge channel extend in the second direction.
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