ANTI-ICING SYSTEM FOR A GAS TURBINE

摘要

A system includes a gas turbine system that has a turbine, 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 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 configured to inject the wash fluid into the gas turbine system and 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.

主权项

1. A system, comprising:
a gas turbine system, comprising:
a turbine;a combustor; anda compressor having an air intake, wherein the air intake is configured to supply an air flow to the compressor; and a fluid injection system, comprising:
a fluid wash system configured to inject a wash fluid into the gas turbine system via the air intake, wherein the fluid wash system comprises an injector configured to inject the wash fluid into the gas turbine system; andan anti-icing system configured to inject an anti-icing fluid into the gas turbine system via the air intake, wherein the anti-icing system is configured to inject the anti-icing fluid into the gas turbine system via the injector.