METHOD AND SYSTEM TO ENSURE FULL OIL TUBES AFTER GAS TURBINE ENGINE SHUTDOWN

A gas turbine engine (20) includes a bearing compartment (62) that has an inlet (86). A supply line (72) splits into a supply conduit (78) and a reservoir conduit (80) that are fluidly parallel to one another for a length. The reservoir conduit (80) fluidly rejoins the supply conduit (78) at a junct...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	AVIS, Thomas Bruce, PARNIN, Francis
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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