GAS TURBINE PLANT

The invention relates to gas turbine plants. The oil systems of a gas turbine engine and of actuating units are designed in the form of individual adjustable flow circuits each of which comprises fuel-oil heat exchangers, the cooling medium of which is in the form of a cryogenic gas fuel, a delivery...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	FEDORCHENKO DMITRIY GENNADIYEVICH, GRISHANOV OLEG ALEKSEJEVICH, IGNACHKOV STANISLAV MIKHAYLOVICH, BONDARENKO LEONID MARKOVICH, NESTEROV EDUARD IVANOVICH, KOSSOV VALERIY SEMYENOVICH
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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Beschreibung
Zusammenfassung:	The invention relates to gas turbine plants. The oil systems of a gas turbine engine and of actuating units are designed in the form of individual adjustable flow circuits each of which comprises fuel-oil heat exchangers, the cooling medium of which is in the form of a cryogenic gas fuel, a delivery pump and an oil tank. The cooling cavities of the fuel-oil heat exchangers are connected, at the inputs thereof, to a fuel supply and adjusting device and, at the outputs thereof, to a fuel heater which is arranged in the sleeve of the gas turbine engine. Said invention makes it possible to design a low-consumption gas turbine plant provided with a small-sized oil-cooling and fuel-heating system.