Airfoil having porous metal filled cavities

A turbine airfoil used in a gas turbine engine includes a plurality of cavities opening in a direction facing the airfoil surface, each cavity having cooling holes communicating with an internal cooling fluid passage of the airfoil, and the airfoil surface above the cavity being a thermal barrier co...

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Bibliographische Detailangaben
1. Verfasser: Landis, Kenneth K
Format: Patent
Sprache:eng
Online-Zugang:Volltext bestellen
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