Gas turbine

A gas turbine is provided that includes combustor configured to burn a low-heating-value fuel and further configured to receive steam that is injected into the gas turbine. A method of modifying a gas turbine and for operating a gas turbine are presented.

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Bibliographische Detailangaben
Hauptverfasser:	O'BECK JOHN TIMOTHY, TENDICK REX CARL
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIR SUPPLY BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS DRAUGHT-INDUCING FLUES 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 REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTIONRESIDUES SUPPLYING NON-COMBUSTIBLE LIQUID OR GAS WEAPONS
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Beschreibung
Zusammenfassung:	A gas turbine is provided that includes combustor configured to burn a low-heating-value fuel and further configured to receive steam that is injected into the gas turbine. A method of modifying a gas turbine and for operating a gas turbine are presented.