Innovative wall-integrated multipass cooling system for gas turbine blades

Research unit

INNOSUISSE

Project number

101.821 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
Key words	-	-	-
Abstract	-	-	-

Category	Text
Key words (English)	Energy & environment, Energy efficiency
Abstract (English)	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.