Synthesis gas expander located immediately upstream of...

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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F02C 3/28 (2006.01) F02C 3/22 (2006.01)

Patent

CA 2271660

The invention improves the reliability of burning a synthesis gas as fuel for a combustion turbine (12) to produce power by incorporating a synthesis gas expander (48) immediately upstream of the combustion turbine. Increased efficiency occurs from additional power output from the expander and by reduction or elimination of nitrogen compression from an air separation unit for the control of oxides of nitrogen.

L'invention permet d'améliorer la fiabilité de la combustion d'un gaz de synthèse utilisé comme combustible dans une turbine à gaz (12) en vue de produire de l'énergie, en incorporant une chambre d'expansion (48) de gaz de synthèse immédiatement en amont de la turbine à gaz. On améliore l'efficacité grâce à une sortie de puissance supplémentaire dans la chambre d'expansion et grâce à la réduction ou à l'élimination de la compression d'azote dans l'unité de séparation d'air en vue de limiter l'émission d'oxydes d'azote.

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