发明名称 Gaseous fuel compression and control system
摘要 A gaseous fuel compression and control system is disclosed which utilizes a helical flow compressor/turbine integrated with a permanent magnet motor/generator and driven by a torque controlling inverter to compress or expand gaseous fuels, precisely control fuel pressure and flow, and precisely control the operations (speed, combustion temperature and output power) of a gaseous fuel fired turbogenerator. <IMAGE>
申请公布号 IL121531(A) 申请公布日期 2000.02.17
申请号 IL19970121531 申请日期 1997.08.12
申请人 CAPSTONE TURBINE CORPORATION 发明人
分类号 F01D5/14;F01D5/04;F01D15/10;F01D25/00;F02C3/22;F02C7/22;F02C7/236;F02C9/28;F02C9/30;F02C9/40;F04D23/00;F04D25/06;F04D27/00;H02K21/12;H02P9/04;(IPC1-7):F02C9/30 主分类号 F01D5/14
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