Gas turbine engine reverse-flow combustor

Details Gas turbine engine reverse-flow combustor Gas turbine engine reverse-flow combustor

2011-08-23

2011-08-23

Kim, Ted (Department: 3741)

Power plants

Combustion products used as motive fluid

Coaxial combustion products generator and turbine

C060S754000, C060S756000, C060S752000

Reexamination Certificate

active

08001793

ABSTRACT:
A gas turbine engine reverse-flow sheet metal combustor for an aero gas turbine engine has a louverless single-piece liner design which includes a plurality of effusion patches, containing multiple rows of effusion cooling holes, bounded by cooled effusionless bands to aid in repairability of the combustor. The cooling of the bands improves the durability of the combustor and provides a method of repair for the combustor.

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