Gaseous fuel compression and control system and method
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United States of America Patent
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Oct 13, 1998
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N/A
app pub date -
Oct 16, 1996
filing date -
Oct 16, 1996
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Abstract
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.
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