GAS TURBINE ENGINE

A gas turbine engine (10) for an aircraft comprises a unit (30) supplied with oil from a first oil circuit (43) and a second oil circuit (45). The first oil circuit (43) and the second oil circuit (45) each are fluidly coupled with at least one inlet (48, 49) and with at least one outlet (50, 60) of...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	UHKOETTER STEPHAN, EDWARDS DAVID A, HAMMOND LYNN, WILLIAMS DAVID, MENCZYKALSKI STEFAN, MASON JOHN R, DAVIES NEIL
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS 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 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING THERMAL INSULATION IN GENERAL WEAPONS
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