GAS-TURBINE UNIT

thermal engineering. SUBSTANCE: gas- turbine unit gas has turbine and compressor mounted on common shaft and combustion chamber with fuel injectors. Combustion chamber communicates at its outlet directly with turbine inlet and at its inlet, with compressor outlet through jet apparatus. Fuel injector...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GURA A.N, IVANOV V.A, VITOSHKIN A.A, VORONIN V.N, SUKHOV A.I, JAKOVLEV A.JA, BELOGUBETS F.A, TROFIMOV V.I, TURTUSHOV V.A, RACHUK V.S
Format:	Patent
Sprache:	eng ; rus
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
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