OIL SYSTEM OF A GAS TURBINE ENGINE, COMPRISING A FIRST OIL CIRCUIT AND AT LEAST ONE SECOND OIL CIRCUIT, AND GAS TURBINE ENGINE

An oil system of a gas turbine engine, includes a first oil circuit and a second oil circuit. Via of the oil circuits, oil is supplied to a hydraulic load of a transmission of the engine. Downstream of the load, in the region of a return of the transmission, oil is introduced into the oil circuits f...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KURZ-HARDJOSOEKATMO, Wolfram, KRACHT, Uwe, UHKÖTTER, Stephan, MENCZYKALSKI, Stefan, WILLIAMS, David
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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