Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts

• Unité de recherche: INNOSUISSE
• Numéro de projet: 36919.1 IP-ENG
• Titre du projet anglais: Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts

Description succincte (Allemand)

Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts

Description succincte (Anglais)

Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts

Résumé des résultats (Abstract) (Allemand)

The main goal of the project is to design and manufacture lower cost gas turbine hot gas path parts with advanced high efficiency cooling. An optimised SLM process is to be developed for the additive manufacture of nickel based superalloy parts with improved performance and efficiency.