Cooling system for a gas turbine compressor

摘要

The present invention provides a cooling apparatus (36) as an intercooling system according to the present invention, which is located between a plurality of compression stages (10a,10b) of a gas compressor to cool a gas that has been in the compressor, the apparatus comprising means (80) for sprinkling a desired amount or more of liquid to cool the compressed gas while restraining inflow of the liquid into the compression stages.