发明名称 Turbine cooling system
摘要 <p>A turbine cooling system is provided, having a compressor (20) for supplying cooling air, a forward turbine rotor wheel space (50), a high-pressure packing seal (HPPS) bypass cavity (60), and a metering device (46). The forward turbine rotor wheel space (50) is cooled by the cooling air supplied by the compressor. The HPPS bypass cavity (60) 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 (46) is in operable communication with the forward turbine rotor wheel space (50) and the HPPS bypass cavity (60) 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.</p>
申请公布号 EP2623714(A3) 申请公布日期 2013.12.18
申请号 EP20120198418 申请日期 2012.12.20
申请人 GENERAL ELECTRIC COMPANY 发明人 COOK, JASON NATHANIEL
分类号 F01D11/00;F01D5/08;F01D25/12 主分类号 F01D11/00
代理机构 代理人
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