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THERMAL BARRIER COATING FOR CMAS RESISTANCE AND LOW THERMAL CONDUCTIVITY
A thermal barrier coating for a turbine engine component contains neodymia, optionally alumina, and zirconia. The thermal barrier coating has resistance to CMAS attack and a low thermal conductivity.
THERMAL BARRIER COATING FOR CMAS RESISTANCE AND LOW THERMAL CONDUCTIVITY
A thermal barrier coating for a turbine engine component contains neodymia, optionally alumina, and zirconia. The thermal barrier coating has resistance to CMAS attack and a low thermal conductivity.
THERMAL BARRIER COATING FOR CMAS RESISTANCE AND LOW THERMAL CONDUCTIVITY
BOCHIECHIO MARIO P (Autor:in) / LITTON DAVID A (Autor:in) / MALONEY MICHAEL J (Autor:in)
04.07.2019
Patent
Elektronische Ressource
Englisch
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|THERMAL BARRIER COATING FOR CMAS RESISTANCE AND LOW THERMAL CONDUCTIVITY
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