Invention Application
US20170016350A1 SEAL RUNNER WITH CONTROLLED OIL LUBRICATION 有权
密封润滑油与受控油润滑

SEAL RUNNER WITH CONTROLLED OIL LUBRICATION
Abstract:
A system is provided associated with an engine of an aircraft. The system includes a ring, a runner and at least one radially-oriented hole associated with the runner that is configured to supply oil to an interface between the runner and the ring. The at least one hole is contained within an axial projection of the ring.
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