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특허 상세정보

Gaseous fuel compression and control method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/30   
미국특허분류(USC) 60/039.02 ; 60/039.465 ; 60/039.281 ; 60/039.282
출원번호 US-0086615 (1998-05-27)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Miller
인용정보 피인용 횟수 : 53  인용 특허 : 12
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 method of gaseous fuel compression and control for a turbogenerator having a combustor supplied with gaseous fuel by a helical flow compressor/turbine driven by a permanent magnet motor/generator separate from the turbogenerator the method comprising the steps of:establishing the turbogenerator speed required based upon the power load requirements of the turbogenerator;establishing the turbogenerator combustion temperature or turbine exhaust gas temperature based on the power load requirements of the turbogenerator;establishin...

이 특허를 인용한 특허 피인용횟수: 53

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