| 摘要 |
A gas turbine unit which has a fuel gas compressor system for increasing the pressure of a fuel gas before entering a fuel system of the gas turbine unit is disclosed. The fuel gas compressor system comprises at least one compressor, gas inlet means for supplying the fuel gas to each compressor, and supply means for supplying the compressed fuel gas to the fuel system of the gas turbine unit. The fuel gas compressor system is placed inside a housing for the gas turbine unit.
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