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Gas turbine engine component coating with self-healing barrier layer
A component for high temperature applications includes a substrate and a layer of an aluminum-containing MAX phase material and another material applied to the substrate.
Gas turbine engine component coating with self-healing barrier layer
A component for high temperature applications includes a substrate and a layer of an aluminum-containing MAX phase material and another material applied to the substrate.
Gas turbine engine component coating with self-healing barrier layer
STROCK CHRISTOPHER W (Autor:in) / AMINI SHAHRAM (Autor:in)
30.04.2019
Patent
Elektronische Ressource
Englisch
IPC:
C23C
Beschichten metallischer Werkstoffe
,
COATING METALLIC MATERIAL
/
C04B
Kalk
,
LIME
/
F01D
Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen
,
NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
/
F02C
Gasturbinenanlagen
,
GAS-TURBINE PLANTS
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