METHOD AND APPARATUS FOR COMBUSTOR FUEL CIRCUIT FOR ULTRA LOW CALORIFIC FUEL

PROBLEM TO BE SOLVED: To provide a diffusion combustion system (100) including a combustor (102).SOLUTION: The combustor includes at least one fuel inlet, an end cover (108), a combustion casing (110), and a combustion liner (112). The combustor is configured to: accept an ultra low calorific fuel s...

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Bibliographische Detailangaben
Hauptverfasser:	ZIMINSKY WILLY STEVE, DAVIS LEWIS BERKELY JR
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a diffusion combustion system (100) including a combustor (102).SOLUTION: The combustor includes at least one fuel inlet, an end cover (108), a combustion casing (110), and a combustion liner (112). The combustor is configured to: accept an ultra low calorific fuel supplied through a first fuel circuit (104); control supply of the ultra low calorific fuel through a second fuel circuit (126) as required to control a volumetric flow of the ultra low calorific fuel through the combustor; and combust the ultra low calorific fuel in the combustor.