SEAL RUNNER WITH CONTROLLED OIL LUBRICATION

摘要

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).