Turbine blade cooling system with lower turning vane bank

A turbine blade having a base and an airfoil, the base including cooling air inlets and an internal cooling air passageway, and the airfoil including an internal multi-bend heat exchange path beginning at the base and ending at a cooling air outlet at the trailing edge of the airfoil. The airfoil al...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Pointon, Stephen Edward, Hamm, Hans D, Okpara, Nnawuihe, Hirako, Kevin, Meier, Andrew T
Format: Patent
Sprache:eng
Schlagworte:
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