Brennstoffzuführung für Gasturbinen mit Ringbrennkammer

A central main gas supply pipe (15) and a central pilot gas supply pipe (16) are connected to a ring burner chamber (1). A main gas ring pipe (13) and pilot gas ring pipe (14) are formed inside the gas turbine housing or back wall of a known burner hood (3). The two ring pipes are connected upstream...

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Bibliographische Detailangaben
Hauptverfasser:	BEECK, ALEXANDER., ENDINGEN, CH, GUTHIER, KLAUS, 69469 WEINHEIM, DE, KOENIG, MARCEL, FREIENWIL, CH, SENIOR, PETER., STONEY STANTON, LEICESTERSHIRE, GB
Format:	Patent
Sprache:	ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING BURNERS 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:	A central main gas supply pipe (15) and a central pilot gas supply pipe (16) are connected to a ring burner chamber (1). A main gas ring pipe (13) and pilot gas ring pipe (14) are formed inside the gas turbine housing or back wall of a known burner hood (3). The two ring pipes are connected upstream to the main gas and pilot gas supply pipes (15,16) and downstream to the ring burner chamber (1). The gas ring pipes are set inside the back wall of the burner hood. With burners which can be operated selectively with liquid or gaseous fuel. A fuel lance (7) consisting only of the liquid fuel channel (9) is set in the main gas pipe.