Engine Component

Abstract: An engine component (80) for a gas turbine engine (10) includes a film-cooled substrate (82) having a hot surface (84) facing hot combustion gas flow and a cooling surface (86) facing a cooling fluid flow. A film hole (90) extends through the substrate (82) to an outlet (94) on the hot surface (84). A flow conditioning structure (112, 162) is provided upstream of the outlet (94).

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