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Yýu who have problems to bring you a company of our online media site may get the problems from another countries where their payment card can’t be accepted.1. Field of the Invention
The present invention relates to a structure of a fuel pump for a gas turbine, which is driven by a combustion gas from a burner and has a disk rotor, which is rotatably supported in a pump chamber to be driven by a gas turbine engine, and a vane rotor, which is coaxial with the disk rotor, and which includes vanes, and a construction of the rotor, the pump chamber, and a blade space between the rotor and the rotor.
2. Description of the Prior Art
A turbine engine is an axial type engine in which a turbine shaft is disposed substantially coaxially with a compressor shaft. A rotating blade is mounted to the periphery of the turbine shaft, and this rotating blade sucks a combustion gas from an air compressor and drives a turbine rotor which rotates at high speed, thereby generating a power.
The air compressor is driven by an electric motor or the like to charge air into the compressor chamber. The combustion gas, which is sucked from an air intake port is combusted in a combustion chamber. The combustion gas is then supplied to a turbine, and drives the turbine rotor to rotate at high speed. The rotating blade is rotatably mounted to a peripheral wall of the turbine chamber and is driven by this high speed rotation. The turbine is composed of a turbine wheel which is coaxial with the turbine rotor and is driven by the rotor to rotate at high speed and a blade which is attached to the turbine wheel and is rotated by this high speed rotation of the turbine wheel. The turbine wheel is provided with a plurality of blades, a turbine stator or the like.
A control valve is disposed between the combustion chamber and the turbine chamber for controlling the supply of the combustion gas to the turbine chamber,