Turbine engine blade with improved cooling

A turbine blade, including a root, a vane including a leading edge and a trailing edge and a pressure-side wall and a suction-side wall, and including cooling vents at the trailing edge, this vane also including first and second serpentine circuits; each serpentine circuit including several ducts ex...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Garles, Kevin Yannick, Botrel, Erwan Daniel, Coudert, Laurent Patrick Robert
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:A turbine blade, including a root, a vane including a leading edge and a trailing edge and a pressure-side wall and a suction-side wall, and including cooling vents at the trailing edge, this vane also including first and second serpentine circuits; each serpentine circuit including several ducts extending in the span direction, being connected to each other by angled portions; each serpentine circuit being supplied with air by its duct that is closest to the leading edge; and wherein the vents are supplied by the first and by the second serpentine circuit.