METHOD OF OPERATION OF TURBOJET REHEATED ENGINE WITH SWIVEL PROPULSIVE JET NOZZLE (VERSIONS)

FIELD: aeronautical engineering; gas-turbine engines with heat addition in afterburner which are provided with propulsive jet nozzles with thrust vector changeable in direction. SUBSTANCE: method consists in delivery of air and fuel to afterburner. On the command for turning the nozzle, flow rates o...

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Bibliographische Detailangaben

Hauptverfasser:	GOJKHENBERG M.M, ANDREEV A.V, KOSTJUCHENKO M.M, MARCHUKOV E.JU, CHEPKIN V.M
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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