Gas turbine systems and methods employing a vaporizable...

F - Mech Eng,Light,Heat,Weapons – 01 – K

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F01K 21/04 (2006.01)

Patent

CA 2710280

Systems and methods utilizing turbines, including a compressor turbine with a vaporizable liquid delivery device, are presented. A compressor turbine uses the evaporation of a vaporizable liquid at or near thermal equilibrium from the vaporizable liquid delivery device during the compression. The vapor created thereby typically carries the thermal energy discharged after the gas turbine cycle. The amount of liquid vaporized during compression, the length of time vaporization takes, the proximity to thermal equilibrium at which vaporization occurs, the amount of thermal energy recovered by recuperation, and the temperature at the inlet of the combustion chamber are generally interrelated parameters that can be controlled to increase efficiency.

L'invention concerne des systèmes et des procédés faisant appel à des turbines, contamment une turbine de compresseur présentant un dispositif de distribution de liquide vaporisable. Une turbine de compresseur utilise l'évaporation d'un liquide vaporisable en équilibre thermique ou proche de celui-ci à partir du dispositif de distribution de liquide vaporisable pendant la compression. La vapeur ainsi créée transporte généralement l'énergie thermique évacué après le cycle de la turbine à gaz. La quantité de liquide vaporisé pendant la compression, la durée nécessaire pour la vaporisation, la proximité par rapport à l'équilibre thermique auquel se produit la vaporisation, la quantité d'énergie thermique recyclée par récupération et la température à l'entrée de la chambre de combustion sont des paramètres généralement interreliés qui peuvent être contrôlés afin d'augmenter l'efficacité.

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