Compressor system and method for gas liquefaction system

F - Mech Eng,Light,Heat,Weapons – 25 – B

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F25B 31/02 (2006.01) F25B 1/00 (2006.01) F25J 1/02 (2006.01)

Patent

CA 2708154

A system and method according to which a compressor having a first shaft is provided, and an aeroderivative gas turbine for driving the compressor is provided, the aeroderivative gas turbine including a gas generator and a power turbine coupled to the gas generator, the power turbine having a second shaft directly coupled to the first shaft of the compressor for directly driving the first shaft.

La présente invention concerne un système et un procédé comprenant un compresseur doté d'un premier arbre et une turbine à gaz aérodérivée pour entraîner le compresseur, la turbine à gaz aérodérivée comprenant un générateur de gaz et une turbine de puissance accouplée au générateur de gaz, la turbine de puissance comprenant un deuxième arbre accouplé directement au premier arbre du compresseur pour entraîner directement le premier arbre.

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