|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/039.02 ; 60/039.465 ; 60/039.281 ; 60/039.282|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 53 인용 특허 : 12|
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 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...