GAS TURBINE ENGINE LOW PRESSURE ROTOR CONNECTION UNIT

FIELD: engines and pumps.SUBSTANCE: invention relates to gas turbine engines (GTE) of aircraft application, namely to design of compressor and turbine rotor connection unit. Technical result is achieved by the fact that the known unit for connection of the low-pressure rotor shafts of the gas turbin...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Dontsov Sergej Nikolaevich, Uzbekov Andrej Valerevich, Kikot Nikolaj Vladimirovich
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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