Turbine cooling system
AssigneeGeneral Electric Company
InventorJason Nathaniel Cook
Life of this patent
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AssigneeGeneral Electric Company
InventorJason Nathaniel Cook
Estimating the term…
A turbine cooling system is provided, having a compressor for supplying cooling air, a forward turbine rotor wheel space, a high-pressure packing seal (HPPS) bypass cavity, and a metering device. The forward turbine rotor wheel space is cooled by the cooling air supplied by the compressor. The HPPS bypass cavity is in fluid communication with and receives a portion of the cooling air from the compressor, and is in fluid communication with and supplies the cooling air to the forward turbine rotor wheel space. The metering device is in operable communication with the forward turbine rotor wheel space and the HPPS bypass cavity to modulate the cooling air supplied to the forward turbine rotor wheel space from the HPPS bypass cavity. The metering device modulates the cooling air based on at least one operating condition of the turbine.
A turbine cooling system for a turbine, comprising:
A turbine cooling system for a turbine, comprising:
A turbine having a turbine cooling system, comprising:
Dependencies are inferred from the claim text.