LUBRICATION SYSTEM FOR GAS TURBINE ENGINES

A lubrication system (70) for a gas turbine engine (20) may include a pump (86) for moving a lubricant through a conduit from a lubricant tank (82) to an engine component (80). Further, a scheduling valve (94) positioned in the conduit (90) between the lubricant tank (82) and the engine component (8...

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Bibliographische Detailangaben
Hauptverfasser:	KNAPP CARNEY, Katherine A, PARNIN, Francis, TEICHOLZ, Matthew D, WEINER, Richard Alan
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS CRANKCASE VENTILATING ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GAS-TURBINE PLANTS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING LUBRICATING INTERNAL COMBUSTION ENGINES LUBRICATING OF MACHINES OR ENGINES IN GENERAL MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	A lubrication system (70) for a gas turbine engine (20) may include a pump (86) for moving a lubricant through a conduit from a lubricant tank (82) to an engine component (80). Further, a scheduling valve (94) positioned in the conduit (90) between the lubricant tank (82) and the engine component (80) may vary a flow of the lubricant (74) to the engine component (78) based on a condition.