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GAS TURBINE ENGINE COMPONENT COATING WITH SELF-HEALING BARRIER LAYER
A component for high temperature applications includes a substrate, a layer of an aluminum-containing MAX phase material and another material applied to the substrate. The layer provides a MAX phase/metal matrix composite including a first MAX phase material. The first MAX phase material has a particle size of between 1-3 microns. The metal matrix is formed from particles having a particle size of 0.02 to 0.5 microns.
GAS TURBINE ENGINE COMPONENT COATING WITH SELF-HEALING BARRIER LAYER
A component for high temperature applications includes a substrate, a layer of an aluminum-containing MAX phase material and another material applied to the substrate. The layer provides a MAX phase/metal matrix composite including a first MAX phase material. The first MAX phase material has a particle size of between 1-3 microns. The metal matrix is formed from particles having a particle size of 0.02 to 0.5 microns.
GAS TURBINE ENGINE COMPONENT COATING WITH SELF-HEALING BARRIER LAYER
GASTURBINENMOTORKOMPONENTENBESCHICHTUNG MIT SELBSTHEILENDER BARRIERESCHICHT
REVÊTEMENT DE COMPOSANT DE MOTEUR À TURBINE À GAZ AVEC COUCHE BARRIÈRE AUTORÉPARATRICE
STROCK CHRISTOPHER W (author) / AMINI SHAHRAM (author)
2024-07-24
Patent
Electronic Resource
English
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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