GAS TURBINE CONTROL SYSTEM HAVING OPTIMIZED IGNITION AIR FLOW CONTROL

Method and apparatus for generating an ignition enabling signal for use with a combustion turbine (104), wherein a sensor for generating an ambient air temperature and/or pressure signal, a reference member for generating a reference signal representative of the turbine speed at which optimum air fl...

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Bibliographische Detailangaben

Hauptverfasser:	STEPHEN EUGENE MUMFORD, WILLIAM LAWRENCE MCCARTY
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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