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Research unit
INNOSUISSE
Project number
36919.1 IP-ENG
Project title
Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts

Texts for this project
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Short description
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Abstract
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Inserted texts


CategoryText
Short description
(German)
Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts
Short description
(English)
Design of additive manufactured low cost advanced cooled gas turbine hot gas path parts
Abstract
(German)
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.