Innovative wall-integrated multipass cooling system for gas turbine blades - Texts

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Research unit

INNOSUISSE

Project number

61756.1 IP-EE

Project title

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

Texts for this project

	German	French	Italian	English
Short description		-	-
Abstract		-	-	-

Inserted texts

Category	Text
Short description (German)	Innovative wall-integrated multipass cooling system for gas turbine blades (Innolink: 101.821 IP-EE)
Short description (English)	Innovative wall-integrated multipass cooling system for gas turbine blades
Abstract (German)	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.