| 摘要 |
PURPOSE: A fuel saving gas turbine engine using water is provided to reduce the fuel consumption rate by using the minimum organic fuel, and secure flight safety by separating the organic fuel tank with passengers. CONSTITUTION: A fuel saving gas turbine engine using water is composed of a plurality of water spray nozzles installed within a discharge nozzle at the peripheral direction; a water pump connected to the water spray nozzles via pipes; a current controller connected to the water pump with electric wires; an electric heater located in the discharge nozzle and connected to the current controller; a generator connected to the current controller with the electric wires; and an engine thrust controller connected to the water pump and current controller with the wires to control the thrust of a gas turbine engine.
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