FLOW DIRECTING COVER FOR ENGINE COMPONENT

摘要

An assembly 60 for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, an airfoil 62 including a radial end, a first passageway having an outlet at the radial end, and a second passageway having an inlet at the radial end. The assembly 60 further includes a cover 64 having at least one turning cavity configured to direct fluid expelled from the outlet of the first passageway into the inlet of the second passageway.