ANTI-ICING SYSTEM FOR GAS TURBINE

摘要

PROBLEM TO BE SOLVED: To provide an anti-icing system for a gas turbine.SOLUTION: A system includes a gas turbine system 10 that has a turbine 20, a combustor, and a compressor having an air intake. The air intake is configured to supply an air flow to the compressor. The system also includes a fluid injection system 12 that has a fluid wash system configured to inject a wash fluid into the gas turbine system via the air intake. The fluid wash system includes an injector 34 configured to inject the wash fluid into the gas turbine system. The fluid injection system includes an anti-icing system configured to inject an anti-icing fluid into the gas turbine system via the air intake. The anti-icing system is configured to inject the anti-icing fluid into the gas turbine system via the injector.