| 摘要 |
A gas turbine system includes a gas turbine ( 1, 2, 3 ) having a compressor ( 1 ) and a turbine ( 2 ), which via a common shaft ( 3 ) drive a generator ( 4 ), and a combustion chamber ( 6 ), the exit of which is connected to the entry to the turbine ( 2 ) of the gas turbine ( 1, 2, 3 ), has a fuel feed ( 8 ) and receives combustion air from the exit of the compressor ( 1 ) of the gas turbine ( 1, 2, 3 ) via the high-pressure side of a recuperator ( 5 ), the exit of the turbine ( 2 ) and the entry to the compressor ( 1 ) of the gas turbine ( 1, 2, 3 ) being connected via the low-pressure side of the recuperator ( 5 ), and a first exhaust-gas turbocharger (ATL 2 ) which sucks in air being connected to different locations ( 9, 10 ) of the low-pressure side of the recuperator ( 4 ) via the exit of its compressor ( 13 ) and the entry to its turbine ( 14 ).
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