Airfoil with cooling circuit

An airfoil for a turbine engine having an engine component including an air supply circuit coupled to a plurality of passages within the outer wall of the engine component where cooling air moves from the air supply circuit to an outer surface of the engine component through the passages.

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Bibliographische Detailangaben
1. Verfasser: Bunker, Ronald Scott
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:An airfoil for a turbine engine having an engine component including an air supply circuit coupled to a plurality of passages within the outer wall of the engine component where cooling air moves from the air supply circuit to an outer surface of the engine component through the passages.