METHOD OF FORMING COOLING PASSAGE FOR TURBINE COMPONENT WITH CAP ELEMENT

Methods of forming a cooling passage on a turbine component 200 having a component wall with an internal surface 212 and an external surface 214, are disclosed. An opening 220 is formed passing through the component wall and fluidly connecting the internal and external surfaces. The opening includes...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	GREGG, Jason Ray, DYSON, Thomas Earl, RATHAY, Nicholas William
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	Methods of forming a cooling passage on a turbine component 200 having a component wall with an internal surface 212 and an external surface 214, are disclosed. An opening 220 is formed passing through the component wall and fluidly connecting the internal and external surfaces. The opening includes a metering section 222 extending from the internal surface to a metering end, and a diffuser area 226 extending from the metering end to the external surface. A preformed cap element is added to close a portion of the diffuser area to form the cooling passage with a diffusion section 242 extending from the metering end to the external surface. The preformed metal cap element includes a projection 244 extending internally of the external surface and into the diffusion area to define an internally facing section of the diffusion section. The cooling passage extends through the component wall and fluidly connects the internal surface and the external surface.