LEAN FUEL SUCTION GAS TURBINE

PROBLEM TO BE SOLVED: To provide a lean fuel suction gas turbine capable of slipping-out of mixed gas, by performing efficient operation, while simplifying the whole constitution. SOLUTION: This lean fuel suction gas turbine has a compressor 1 for generating compressed gas G2 by compressing mixed ga...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	KAJITA SHINICHI
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a lean fuel suction gas turbine capable of slipping-out of mixed gas, by performing efficient operation, while simplifying the whole constitution. SOLUTION: This lean fuel suction gas turbine has a compressor 1 for generating compressed gas G2 by compressing mixed gas G1 of the combustible limit concentration or less of mixing fuel and air, a first catalytic combustor 2 for burning the compressed gas G2 by catalytic reaction, a turbine 3 driven by combustion gas G3 from the first catalytic combustor 2, and a regenerator 6 for heating the compressed gas G2 introduced to the first catalytic combustor 2 by exhaust gas G4 from the turbine 3. A duct burner 7 for burning the exhaust gas G4 by a flame by first auxiliary fuel F1 is arranged between the turbine 3 and the regenerator 6. COPYRIGHT: (C)2010,JPO&INPIT