Method of sizing and forming a cooling hole in a gas turbine engine component

The present invention relates to air-cooled components, such as airfoil components of gas turbine engines. More particularly, this invention is directed to a method for sizing and forming the cooling holes of such a component protected by a diffusion environmental coating, in which the build up of t...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Wheat, Gary Eugene, Brown, Terri Kay, Schumacher, Thomas Phillip
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!