Turbine engine with a blade

A blade for a turbine engine with a wall separating a cooling fluid flow and a hot gas fluid flow and having a heated surface along which the hot gas fluid flow flows and a cooled surface facing the cooling fluid flow. A plurality of cooling holes each having a passage extending between an inlet at...

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Bibliographische Detailangaben
Hauptverfasser: Feldmann, Kevin Robert, Gallier, Kirk Douglas, Rausch, Jonathan Michael, Perry, Andrew David, Osgood, Daniel Endecott, Webster, Zachary Daniel
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:A blade for a turbine engine with a wall separating a cooling fluid flow and a hot gas fluid flow and having a heated surface along which the hot gas fluid flow flows and a cooled surface facing the cooling fluid flow. A plurality of cooling holes each having a passage extending between an inlet at the cooled surface and an outlet at the heated surface. The outlet extending between an upstream end and a downstream end with respect to the hot gas fluid flow to define a distance, the passage defining a centerline forming a first angle (θ) with the heated surface.