System for providing fuel to a combustor
AssigneeGeneral Electric Company
InventorJonathan Dwight Berry
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AssigneeGeneral Electric Company
InventorJonathan Dwight Berry
Estimating the term…
A fuel supply system for a gas turbine combustor includes an annular duct that at least partially defines a hot gas path within the combustor. An orifice is at least partially defined by the annular duct and defines a flow path through the annular duct into the hot gas path. A plurality of fuel injectors are arranged circumferentially around the annular duct to provide for fluid communication through the annular duct into the hot gas path. A fuel distribution manifold is disposed adjacent to an outer side of the annular duct. The fuel distribution manifold includes a main body that at least partially defines an inlet for receiving fuel, an outlet that is in fluid communication with the fuel injectors, and a fuel purge passage that provides for fluid communication between the inlet and the orifice.
A fuel supply system for a gas turbine combustor, comprising:
A combustor, comprising:
A gas turbine, comprising:
Dependencies are inferred from the claim text.