System and method of operating a gas turbine engine with an...

Details System and method of operating a gas turbine engine with an... System and method of operating a gas turbine engine with an...

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 3/20 (2006.01) F02C 3/34 (2006.01)

Patent

CA 2732125

A gas turbine engine system is provided. The gas turbine engine system includes a gas turbine engine and an exhaust gas conditioning system. The gas turbine engine includes at least one combustion chamber and at least one turbine down-stream from the combustion chamber. The combustion chamber is coupled in flow communication to a source of hydrocarbonaceous fuel and to a source of oxygen. The gas turbine engine is operable with a working fluid that is substantially nitrogen- free. The exhaust gas conditioning system is coupled between a discharge outlet of the gas turbine engine and an inlet of the gas turbine engine.

L'invention concerne un système de moteur à turbine à gaz. Le système de moteur à turbine à gaz inclut un moteur à turbine à gaz et un système de conditionnement du gaz d'échappement. Le moteur à turbine à gaz inclut au moins une chambre de combustion et au moins une turbine en aval de la chambre de combustion. La chambre de combustion est couplée en communication fluidique à une source de combustible hydrocarboné et à une source d'oxygène. Le moteur à turbine à gaz peut fonctionner avec un fluide de travail qui est pratiquement sans azote. Le système de conditionnement du gaz d'échappement est couplé entre une sortie de refoulement du moteur à turbine à gaz et une entrée du moteur à turbine à gaz.

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