Turbine engine including a steam system
AssigneeGeneral Electric Company
InventorsArthur W. Sibbach, Robert R. Rachedi, Kirk D. Gallier
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AssigneeGeneral Electric Company
InventorsArthur W. Sibbach, Robert R. Rachedi, Kirk D. Gallier
Estimating the term…
A turbine engine for an aircraft includes a turbo-engine with a core air flow path, a fan having a fan shaft coupled to the turbo-engine to rotate the fan shaft, and a steam system. A combustor is located in the core air flow path to combust fuel and to generate combustion gases. The steam system extracts water from the combustion gases and vaporizes the water to generate steam. The steam system is fluidly coupled to the core air flow path to inject the steam into the core air flow path. The steam system includes a controller configured to determine a water content of the core air upstream of the steam injection location and to change a position of a steam flow control valve to control the flow of the steam into the core air flow path.
A turbine engine for an aircraft, the turbine engine comprising:
A turbine engine for an aircraft, the turbine engine comprising:
Dependencies are inferred from the claim text.