Gas turbine system

摘要

The present invention is equipped with: a combustor (2) having a fuel injection nozzle (4) that injects hydrogen gas (H) and pure water (W); a water storage tank (12) that stores the pure water (W) supplied to the combustor (2); a gas compression device (10) that boosts the pressure of the hydrogen gas (H) supplied to the combustor (2); a fuel supply passage (6) that guides the pressurized hydrogen gas (H) to the combustor (2); and a pressure introduction passage (16), which connects the water storage tank (12) and the fuel supply passage (6), and pressurizes the pure water (W) by means of the pressurized hydrogen gas (H).