DOE OSTI · 1089422
Combustor liner cooling system
Abstract
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.
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Lacy, Benjamin Paul, Berkman, Mert Enis. 2013-08-06. Combustor liner cooling system. https://www.osti.gov/biblio/1089422
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