TURBINE ENGINE INCLUDING A STEAM SYSTEM

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20250084789A1
SERIAL NO

18463782

Stats

ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A turbine engine for an aircraft. The turbine engine includes a combustor fluidly coupled to a fuel delivery assembly to receive fuel from the fuel delivery assembly. The fuel is injected into the combustor and combusted in the combustor to generate combustion gases. A condenser is located downstream of a turbine to receive the combustion gases and to condense water. The fuel heat exchanger is thermally coupled to the condenser to receive heat from the water condensed by the condenser. The fuel heat exchanger is located in the fuel delivery assembly to receive the fuel and to transfer the heat received from the water to the fuel. The boiler is located downstream of the fuel heat exchanger. The boiler receives the water and is fluidly connected to the combustor to receive the combustion gases and to boil the water to generate steam.

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Patent Owner(s)

Patent OwnerAddress
GENERAL ELECTRIC COMPANY1 NEUMANN WAY MAIL DROP F16 EVENDALE OH 45215-6301

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Dziech, Aaron M Crittenden, US 3 40
Miller, Brandon W Middletown, US 45 41
Rachedi, Robert R Morrow, US 5 0
Rambo, Jeffrey D Mason, US 11 0
Schimmels, Scott Alan Miamisburg, US 68 107
Sibbach, Arthur W Boxford, US 36 3

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