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Title: Combustor liner cooling system

A combustor liner is disclosed. The combustor liner includes an upstream portion, a downstream end portion extending from the upstream portion along a generally longitudinal axis, and a cover layer associated with an inner surface of the downstream end portion. The downstream end portion includes the inner surface and an outer surface, the inner surface defining a plurality of microchannels. The downstream end portion further defines a plurality of passages extending between the inner surface and the outer surface. The plurality of microchannels are fluidly connected to the plurality of passages, and are configured to flow a cooling medium therethrough, cooling the combustor liner.
Authors:
;
Publication Date:
OSTI Identifier:
1089422
Report Number(s):
8,499,566
12/855,156
DOE Contract Number:
FC26-05NT42643
Resource Type:
Patent
Research Org:
General Electric Company (Schenectady, NY)
Sponsoring Org:
USDOE
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING