Skip to main content
U.S. Department of Energy
Office of Scientific and Technical Information

Combustor liner cooling system

Patent ·
OSTI ID:1089422
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.
Research Organization:
General Electric Company (Schenectady, NY)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
8,499,566
Application Number:
12/855,156
OSTI ID:
1089422
Country of Publication:
United States
Language:
English

Similar Records

Annular combustor with outer transition liner cooling
Patent · Tue Aug 24 00:00:00 EDT 1993 · OSTI ID:6271270

Hot gas path component cooling system
Patent · Mon Feb 17 23:00:00 EST 2014 · OSTI ID:1125003

Combustor liner cooling arrangement
Patent · Mon Jan 29 23:00:00 EST 1990 · OSTI ID:6911976

Related Subjects