TURBINE ENGINE AIRFOIL INSERT

An apparatus and method for improving the heat transfer coefficient for an engine component for a turbine engine such as an airfoil. The airfoil can include an outer wall defining an interior. A cooling passage can be formed in the interior defining a flow direction. An insert can be provided in the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: REDDY BHANU MAHASAMUDRAM, MANNING ROBERT FRANCIS, MARINELLI ANDREA TERESE
Format: Patent
Sprache:chi ; eng
Schlagworte:
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