GAS TURBINE INTAKE ANTI-ICING DEVICE
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United States of America Patent
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Issued Date -
Sep 26, 2013
app pub date -
Dec 10, 2012
filing date -
Mar 21, 2012
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
The gas turbine intake anti-icing device is used for a gas turbine electric power generation system (1) having a gas turbine (2) and a power generator (20) coupled to the gas turbine (2) and rotationally driven to generate electrical power. The gas turbine intake anti-icing device includes a power generator cooling mechanism (21, 22, 23, 25), which takes air from the outside and introduces air into the power generator (20) to cool the power generator (20), and exhaust air supply path (31) that connects intake path (9) of the gas turbine (2) to exhaust path (30) for air that is discharged from power generator cooling mechanism (21, 22, 23, 25) after the power generator (20) is cooled. The air discharged from the power generator cooling mechanism (21, 22, 23, 25) is supplied to the intake path (9) of the gas turbine (2) through the exhaust air supply path (31).
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