Combustor system with main fuel injector for reduced combustion dynamics
AssigneeGeneral Electric Company
InventorsEric John Stevens, Mark David Durbin, Randall Charles Boehm
Life of this patent
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AssigneeGeneral Electric Company
InventorsEric John Stevens, Mark David Durbin, Randall Charles Boehm
Estimating the term…
The present disclosure is directed to a combustor system including a fuel nozzle comprising a main fuel injector defining an angled main injection port. Each angled main injection port defines an inlet end and an outlet end. The outlet end is oriented downstream relative to the inlet end at an angle relative to a centerline axis of the fuel nozzle. The angled main injection port permits egress of fuel from a main fuel circuit to the combustion chamber. The fuel nozzle further defines a radial main injection port. The outlet end is oriented along an axial direction approximately equal relative to the inlet end and radially outward thereof relative to the centerline axis. The radial main injection port is extended perpendicular relative to the centerline axis.
A combustor system, comprising:
A gas turbine engine, comprising:
Dependencies are inferred from the claim text.