Gas turbine system comprises turbine or compressor stage, whose driven side is connected with another compressor or turbine stage, and engine or generator upstream former turbine or compressor stage, with which working medium is air

摘要

The gas turbine system comprises a turbine or compressor stage, whose driven side is connected with another compressor or turbine stage, and an engine or generator (2) upstream the former turbine or compressor stage, with which the working medium is air. The former compressor (4) is supplied with a temperature of minus 36 degree Celsius. An independent claim is included for a method for operating a gas turbine system.