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특허 상세정보

Gaseous fuel compression and control system and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/30    F04D-009/04   
미국특허분류(USC) 60/039.465 ; 60/039.281 ; 60/039.511 ; 417/044.3 ; 415/055.1
출원번호 US-0730945 (1996-10-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Miller
인용정보 피인용 횟수 : 92  인용 특허 : 34
초록

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.

대표
청구항

[ 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...

이 특허에 인용된 특허 (34)

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