GAS TURBINE ENGINE

FIELD: engines and pumps. ^ SUBSTANCE: proposed engine comprises turbine second stage cooled nozzle vane with inner cavity. Vane inner cavity inlet communicates with compressor intermediate stage via cooling air flow rate control shutter while its outlet is communicated with turbine flow section ups...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KUZNETSOV VALERIJ ALEKSEEVICH, LATYSHEV VJACHESLAV GEORGIEVICH, BALOSHKO VLADISLAV LEONIDOVICH
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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