AIRFOIL PROFILE FOR A BLADE IN A TURBINE ENGINE

An apparatus and method for an engine component having a working airflow separated into a cooling airflow and a combustion airflow, the engine component comprising a plurality of circumferentially spaced airfoils rotatable about a centerline defining an axial direction, each airfoil comprising an ou...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: Vandeputte, Thomas William
Format: Patent
Sprache:eng
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