AIRFOIL OF A TURBINE ENGINE

An airfoil (10) is provided and includes a body (20) formed to define a substantially radially extending cooling hole (30) therein, which is configured to be receptive of a supply of a coolant (11) for removing heat from the body (20), and a flag region (40) therein, which is fluidly communicative w...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Itzel, Gary Michael, Benson, Adebukola
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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