Method and system for starting and transient working of comprehensive fuel battery-gas turbine system

Fuel cell-gas turbine system (100) with fuel cell (102), compressor (106) and fuel processor (110) comprises a starting combustion chamber (112) producing exhaust gas with controlled feed in of fuel/air such that exhaust gas from the chamber heats the fuel processor before compressed air and fuel ar...

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Bibliographische Detailangaben
Hauptverfasser:	FERRALL JOE, CAMPBELL TONY, SOKOLOV PAVEL
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BASIC ELECTRIC ELEMENTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ELECTRICITY GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY WEAPONS
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Beschreibung
Zusammenfassung:	Fuel cell-gas turbine system (100) with fuel cell (102), compressor (106) and fuel processor (110) comprises a starting combustion chamber (112) producing exhaust gas with controlled feed in of fuel/air such that exhaust gas from the chamber heats the fuel processor before compressed air and fuel are fed into the cell and processor respectively.