OIL SYSTEM OF GAS-TURBINE ENGINE

FIELD: aircraft engineering. ^ SUBSTANCE: proposed oil system of gas-turbine engine has oil tank and siphon shutter installed in oil feed main line. Air bleed jet is installed in loop of siphon shutter. Siphon shutter is placed in space of oil tank so that its loop is located in upper part of space,...

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Bibliographische Detailangaben
Hauptverfasser:	MARCHUKOV EVGENIJ JUVENAL'EVICH, SEMENOV VADIM GEORGIEVICH, GOLUBOV ALEKSANDR NIKOLAEVICH, POPOV SERGEJ VLADIMIROVICH, ANDREEV ANATOLIJ VASIL'EVICH
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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Beschreibung
Zusammenfassung:	FIELD: aircraft engineering. ^ SUBSTANCE: proposed oil system of gas-turbine engine has oil tank and siphon shutter installed in oil feed main line. Air bleed jet is installed in loop of siphon shutter. Siphon shutter is placed in space of oil tank so that its loop is located in upper part of space, and jet communicates with free space of oil tank. ^ EFFECT: reduced hydraulic resistance of main line between jet and oil tank, improved reliability of oil system of gas-turbine engine. ^ 1 dwg