Combustion turbine with fuel heating system

Details Combustion turbine with fuel heating system Combustion turbine with fuel heating system

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/224 (2006.01) F01K 23/10 (2006.01)

Patent

CA 2276696

The combustion turbine system comprises a fuel line (50) connected to the combustor (30) with a portion of the fuel line being disposed in heat transfer relationship with the exhaust gas from the combustion turbine (28) so that the fuel may be heated by the exhaust gas prior to being introduced into the combustor. The sytem may also comprise a fuel by-pass (62) control system for mixing unheated fuel with the heated fuel to control the temperature (66) of the fuel being introduced into the combustor.

Le système de turbine à combustion comprend un conduit (50) de combustible relié au brûleur (30), une partie du conduit de combustible étant disposée en relation de transfert thermique avec les gaz d'échappements provenant de ladite turbine à combustion (28), de manière que le combustible puisse être chauffé par les gaz d'échappement avant d'être introduit dans le brûleur. Le système comprend également un système de commande de dérivation (62) de combustible, destiné à mélanger du combustible non chauffé au combustible chauffé afin de réguler la température (66) du combustible introduit dans le brûleur.

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