Recuperated gas turbine engine system and method employing...

Details Recuperated gas turbine engine system and method employing... Recuperated gas turbine engine system and method employing...

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/40 (2006.01) F23C 9/00 (2006.01) F23N 5/00 (2006.01) F23N 5/02 (2006.01) F23N 5/18 (2006.01)

Patent

CA 2534429

A recuperated gas turbine engine system and associated method employing catalytic combustion, wherein the combustor inlet temperature can be controlled to remain above the minimum required catalyst operating temperature at a wide range of operating conditions from full-load to part-load and from hot-day to cold-day conditions. The fuel is passed through the compressor along with the air and a portion of the exhaust gases from the turbine. The recirculated exhaust gas flow rate is controlled to control combustor inlet temperature.

L'invention concerne un système de turbine à gaz à récupération et un procédé associé faisant appel à la combustion catalytique, permettant de réguler la température d'entrée de la chambre de combustion de manière à la maintenir au-dessus de la température minimale requise pour la catalyse dans une large variété de conditions de fonctionnement, allant des conditions de fonctionnement à pleine charge aux conditions de fonctionnement à charge partielle, et des conditions de temps chaud aux conditions de temps froid. Le combustible est conduit à travers le compresseur conjointement à l'air, et à une partie des gaz d'échappement de la turbine. Le débit du gaz d'échappement recyclé est réglé de manière à réguler la température à l'entrée de la chambre de combustion.

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