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Forschungsstelle
INNOSUISSE
Projektnummer
36919.1 IP-ENG
Projekttitel
Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts
Projekttitel Englisch
Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts

Texte zu diesem Projekt
 DeutschFranzösischItalienischEnglisch
Kurzbeschreibung
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Abstract
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Erfasste Texte


KategorieText
Kurzbeschreibung
(Deutsch)
Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts
Kurzbeschreibung
(Englisch)
Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts
Abstract
(Deutsch)
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.