SE7502987L

1477062 Gas turbine plant TURBINE INDUSTRIE 19 March 1975 [20 March 1974] 11523/75 Heading F1G A gas turbine plant comprises a first turbine rotor 14 and a supersonic compressor rotor 4 mounted on a shaft 6 supported by oil bearings 15 upstream of the rotors, and a second turbine rotor 18 on a secon...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	RIBETON J, FRIBERG J, MERIGOUX J-M, MAGINOT P
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS 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:	1477062 Gas turbine plant TURBINE INDUSTRIE 19 March 1975 [20 March 1974] 11523/75 Heading F1G A gas turbine plant comprises a first turbine rotor 14 and a supersonic compressor rotor 4 mounted on a shaft 6 supported by oil bearings 15 upstream of the rotors, and a second turbine rotor 18 on a second shaft 20 supported downstream of the second rotor on oil bearings 21, 22, the radius of the first turbine rotor being 2 to 10% less than that of the compressor rotor. One or more combustion chambers 8 are arranged eccentrically at the shaft axis.