Innovative wall-integrated multipass cooling system for gas turbine blades (Innolink: 101.821 IP-EE)

Forschungsstelle

INNOSUISSE

Projektnummer

61756.1 IP-EE

Projekttitel

Innovative wall-integrated multipass cooling system for gas turbine blades (Innolink: 101.821 IP-EE)

Projekttitel Englisch

Innovative wall-integrated multipass cooling system for gas turbine blades (Innolink: 101.821 IP-EE)

Texte zu diesem Projekt

	Deutsch	Französisch	Italienisch	Englisch
Kurzbeschreibung		-	-
Abstract		-	-	-

Kategorie	Text
Kurzbeschreibung (Deutsch)	Innovative wall-integrated multipass cooling system for gas turbine blades (Innolink: 101.821 IP-EE)
Kurzbeschreibung (Englisch)	Innovative wall-integrated multipass cooling system for gas turbine blades
Abstract (Deutsch)	The aim is to increase the efficiency of gas turbines by developing a near wall multipass cooling system. The cooling channels will be studied with experiments and simulations. The mechanical and thermal integrity, as well as the manufacturability of the resulting blades will be assessed.