TURBINE ENGINE HAVING FOLDED ANNULAR JET COMBUSTOR

摘要

A combustor (28) for a turbine engine (10) is disclosed. The combustor may have a can-like dilution zone (34), a primary combustion zone (32), and a secondary combustion zone (36). The primary combustion zone may be disposed radially about the can-like dilution zone. The secondary combustion zone may be disposed at an end of the can-like dilution zone to fluidly communicate the primary combustion zone and the can-like dilution zone.