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Thermal barrier coatings for turbine engine components
Thermal barrier coatings consist of a tantala-zirconia mixture that is stabilized with two or more stabilizers. An exemplary thermal barrier coating consists of, by mole percent: about 8% to about 30% YO 1.5 ; about 8% to about 30% YbO 1.5 or GdO 1.5 or combination thereof; about 8% to about 30% TaO 2.5 ; about 0% to about 10% HfO 2 ; and a balance of ZrO 2 .
Thermal barrier coatings for turbine engine components
Thermal barrier coatings consist of a tantala-zirconia mixture that is stabilized with two or more stabilizers. An exemplary thermal barrier coating consists of, by mole percent: about 8% to about 30% YO 1.5 ; about 8% to about 30% YbO 1.5 or GdO 1.5 or combination thereof; about 8% to about 30% TaO 2.5 ; about 0% to about 10% HfO 2 ; and a balance of ZrO 2 .
Thermal barrier coatings for turbine engine components
Wärmedämmschichten für Turbinenmotorbauteile
Revêtements de barrière thermique pour composants de moteur à turbine
TOLPYGO VLADIMIR K (Autor:in) / BAKER WIL (Autor:in)
06.06.2018
Patent
Elektronische Ressource
Englisch
IPC:
C23C
Beschichten metallischer Werkstoffe
,
COATING METALLIC MATERIAL
/
C04B
Kalk
,
LIME
/
C09D
Überzugsmittel, z.B. Anstrichstoffe, Firnisse oder Lacke
,
COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS
/
F01D
Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen
,
NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
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