|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/039.465 ; 60/039.281 ; 60/039.511 ; 417/044.3 ; 415/055.1|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 92 인용 특허 : 34|
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.
[ What we claim is:] [1.] A gaseous fuel compression and control system, comprising:a turbogenerator set including a turbogenerator and turbogenerator power controller, said turbogenerator including a compressor, a turbine, a combustor with a plurality of gaseous fuel nozzles and a plurality of air inlets, a recuperator, and a permanent magnet motor/generator;a helical flow compressor/turbine for supplying pressurized gaseous fuel to the gaseous fuel nozzles of said turbogenerator combustor, said turbogenerator compressor supplying compressed air to said...