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In a method of operating a compressor, a gaseous medium is compressed in a first compressor stage. The partially compressed medium is sent from the first compressor stage into an intermediate cooler where it is cooled before being directed into the second compressor stage where it is compressed furt

In a method of operating a compressor, a gaseous medium is compressed in a first compressor stage. The partially compressed medium is sent from the first compressor stage into an intermediate cooler where it is cooled before being directed into the second compressor stage where it is compressed further. A liquid medium is sprayed into the gaseous medium in the intermediate cooler so that a two-phase mixture with a liquid phase and a gaseous phase is formed in the intermediate cooler. The liquid phase is separated again before adding it to the second compressor stage.

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What is claimed is: 1. A method of operating a compressor of a gas turbine comprising: compressing a gaseous medium in a first compressor stage of the gas turbine to create a partially compressed medium; cooling the partially compressed medium in an intermediate cooler, wherein at least about 25% o

What is claimed is: 1. A method of operating a compressor of a gas turbine comprising: compressing a gaseous medium in a first compressor stage of the gas turbine to create a partially compressed medium; cooling the partially compressed medium in an intermediate cooler, wherein at least about 25% of total cooling power occurs through uptake of sensible heat; further compressing the partially compressed medium in a second compressor stage of the gas turbine downstream of the intermediate cooler; wherein an atomized liquid medium is sprayed into the partially compressed medium in the intermediate cooler so that a two-phase flow develops therein including a liquid phase and a gaseous phase, the partially compressed medium being cooled by heat transfer from the partially compressed medium to the liquid medium and the liquid medium being separated before entering the second compressor stage; and wherein contact area developed directly by the two-phase flow provides substantially all of the cooling of the partially compressed medium in the intermediate cooler. 2. The method of claim 1, wherein the partially compressed medium is cooled by an increase in temperature of the liquid medium. 3. The method of claim 2, wherein the partially compressed medium is additionally cooled by evaporation of the liquid medium. 4. The method of claim 1, wherein the liquid medium is atomized into droplets when sprayed into the intermediate cooler. 5. The method of claim 4, wherein the liquid medium is atomized into droplets having a droplet size of less than 100 μm when sprayed into the intermediate cooler. 6. The method of claim 4, wherein the droplets are deposited by a droplet separator. 7. The method of claim 1, wherein the liquid phase separated from the intermediate cooler is cooled and then sprayed again into the intermediate cooler. 8. The method of claim 1, wherein during compression the partially compressed medium is repeatedly cooled intermediately by spraying and separating a liquid medium. 9. The method of claim 1, wherein the gaseous medium is compressed in the first compressor stage from ambient pressure to a pressure of less than 3 bar before being sent to the intermediate cooler where the liquid medium is sprayed in. 10. The method of claim 9, wherein the liquid medium is sprayed into the intermediate cooler at a temperature of less than 5째 C. 11. The method of claim 1, wherein the gaseous medium comprises air and the liquid medium comprises water. 12. A method of operating a compressor of a gas turbine comprising: compressing a gaseous medium in a first compressor stage of the gas turbine to create a partially compressed medium; cooling the partially compressed medium in an intermediate cooler by spraying liquid medium in atomized droplets in the intermediate cooler so that the partially compressed medium is cooled by heat transfer from the partially compressed medium to the liquid medium, wherein at least about 25% of total cooling power occurs through uptake of sensible heat; directing the atomized droplets of the liquid medium away from the partially compressed medium before the droplets enter the second compressor stage; further compressing the partially compressed medium in a second compressor stage of the gas turbine downstream of the intermediate cooler; wherein contact area developed directly by flow of the atomized droplets and the partially compressed medium provides substantially all of the cooling of the partially compressed medium in the intermediate cooler. 13. The method of claim 12, wherein the partially compressed medium is cooled with a corresponding increase in temperature of the liquid medium. 14. The method of claim 12, wherein the partially compressed medium is cooled by evaporation of the liquid medium. 15. The method of claim 14, wherein the atomized droplets have a droplet size of less than 100 μm when sprayed into the intermediate cooler. 16. A method of operating a compressor of a gas turbine comprising: compressing a gaseous medium in a first compressor stage of the gas turbine to create a partially compressed medium; passing the partially compressed medium through an intermediate cooler and spraying atomized droplets of a liquid medium therein so that the partially compressed medium is cooled by heat transfer to the liquid medium, wherein at least about 25% of total cooling power occurs through uptake of sensible heat; removing the atomized droplets from the intermediate cooler before the atomized droplets enter the second compressor stage; further compressing the partially compressed medium in a second compressor stage of the gas turbine downstream of the intermediate cooler; wherein a two-phase flow develops in the intermediate cooler with contact area between the atomized droplets and the partially compressed medium of the two-phase flow providing substantially all of the cooling of the partially compressed medium in the intermediate cooler. 17. The method of claim 16, wherein the partially compressed medium is cooled with a corresponding increase in temperature of the liquid medium. 18. The method of claim 16, wherein the partially compressed medium is cooled by evaporation of the liquid medium. 19. The method of claim 18, wherein the atomized droplets have a droplet size of less than 100 μm when sprayed into the intermediate cooler. 20. The method of claim 16, further comprising cooling the liquid medium removed from the intermediate cooler and recirculating the liquid medium for spraying into the intermediate cooler. 21. A method of operating a gas turbine comprising: compressing a gaseous medium in a first, low pressure compressor stage of the gas turbine to create a partially compressed medium; cooling the partially compressed medium in an intermediate cooler, wherein at least about 25% of total cooling power occurs through uptake of sensible heat; further compressing the partially compressed medium in a second compressor stage of the gas turbine downstream of the intermediate cooler; wherein an atomized liquid medium is sprayed into the partially compressed medium, at a temperature of less than 5 째 C. and a pressure of less than 3 bar, while the partially compressed medium is in the intermediate cooler so that a two-phase flow develops therein including a liquid phase and a gaseous phase; wherein the partially compressed medium is cooled by heat transfer from the partially compressed medium to the liquid medium and the liquid medium is separated before entering the second compressor stage; and wherein contact area developed directly by the two-phase flow provides substantially all of the cooling of the partially compressed medium in the intermediate cooler.