发明名称 System and method for modifying rotor thrust
摘要 A gas turbine includes a compressor, a turbine downstream of the compressor having stators, and a rotor connecting the compressor to the turbine. The rotor includes rotor cavities. A supply plenum containing a process by-product gas and a control valve is connected to at least one of the rotor cavities to supply the process by-product gas to at least one of the rotor cavities. A process for operating a gas turbine having a compressor and a turbine includes connecting the compressor to the turbine by a rotor, creating cavities in the rotor, and injecting a process by-product gas into at least one of the cavities. The process further includes regulating the flow of the process by-product gas into at least one of the cavities according to a pre-programmed parameter.
申请公布号 US8434994(B2) 申请公布日期 2013.05.07
申请号 US20090534584 申请日期 2009.08.03
申请人 PAL DIPANKAR;GARCIA-CRESPO ANDRES JOSE;GENERAL ELECTRIC COMPANY 发明人 PAL DIPANKAR;GARCIA-CRESPO ANDRES JOSE
分类号 F01D3/00 主分类号 F01D3/00
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