SEAL RUNNER WITH CONTROLLED OIL LUBRICATION

A system is provided associated with an engine (210) of an aircraft. The system includes a ring (146), a runner (104) and at least one radially-oriented hole (116) associated with the runner (104) that is configured to supply oil to an interface between the runner (104) and the ring (146). The at le...

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Bibliographische Detailangaben
Hauptverfasser:	ULLAH, M. Rifat, MILLER, Jonathan L
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CYLINDERS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PISTONS SEALINGS STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	A system is provided associated with an engine (210) of an aircraft. The system includes a ring (146), a runner (104) and at least one radially-oriented hole (116) associated with the runner (104) that is configured to supply oil to an interface between the runner (104) and the ring (146). The at least one hole (116) is contained within an axial projection of the ring (146).