GAS-TURBINE ENGINE

A power gas-turbine engine with two-support rotor realizing Braiton cycle and including compressor 1, combustion chamber 2, turbine 3 driving the compressor 1, and through reducer 4 û electric generator, where the drive of the electric generator is performed from the side of the compressor and the g...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SPITSYN VOLODYMYR YEVHENIIOVYCH, FILONENKO OLEKSANDR OLEKSIIOVYCH, ISAKOV BORYS VOLODYMYROVYCH, KUCHERENKO OLEH SPYRYDONOVYCH, ROMANOV VIKTOR IVANOVYCH
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
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