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Title Technology transfer completed at KARI (turbine disc on gas turbine engine) Date 2020.03.09 08:56
Name administrator Count 1172
This technology improves the robustness of the turbine disk structure of the gas turbine engine. 
This technology is related to turbine disks that minimize stress other than centrifugal force by blocking heat transfer of turbine blades, 
and minimize cooling and temperature gradient through introduction of cooling channel inside disc.
Used primarily for aviation/industrial purposes.

웹사이트 업로드용 2.jpg      웹사이트 업로드용 1.jpg     웹사이트 업로드 1.jpg
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