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

• Unité de recherche: INNOSUISSE
• Numéro de projet: 61756.1 IP-EE
• Titre du projet anglais: Innovative wall-integrated multipass cooling system for gas turbine blades (Innolink: 101.821 IP-EE)

Description succincte (Allemand)

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

Description succincte (Anglais)

Innovative wall-integrated multipass cooling system for gas turbine blades

Résumé des résultats (Abstract) (Allemand)

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.