A platform for research: civil engineering, architecture and urbanism
A platform for research: civil engineering, architecture and urbanism
QUINARY, LOW-CONDUCTIVITY THERMAL BARRIER COATINGS FOR TURBINE ENGINE COMPONENTS
Thermal barrier coatings, which may be used in gas turbine engines, comprise or consist of a tantala-niobia-zirconia mixture that is stabilized with two or more stabilizers. An exemplary thermal barrier coating comprises or consists of, by mole percent: about 2% to about 30% YO; about 8% to about 30% YbOor GdOor combination thereof; about 6% to about 30% TaO; about 0.1% to about 10% NbO; about 0% to about 10% HfO; and a balance of ZrO.
QUINARY, LOW-CONDUCTIVITY THERMAL BARRIER COATINGS FOR TURBINE ENGINE COMPONENTS
Thermal barrier coatings, which may be used in gas turbine engines, comprise or consist of a tantala-niobia-zirconia mixture that is stabilized with two or more stabilizers. An exemplary thermal barrier coating comprises or consists of, by mole percent: about 2% to about 30% YO; about 8% to about 30% YbOor GdOor combination thereof; about 6% to about 30% TaO; about 0.1% to about 10% NbO; about 0% to about 10% HfO; and a balance of ZrO.
QUINARY, LOW-CONDUCTIVITY THERMAL BARRIER COATINGS FOR TURBINE ENGINE COMPONENTS
QUINÄRE WÄRMEDÄMMSCHICHTEN MIT GERINGER LEITFÄHIGKEIT FÜR TURBINENMOTORKOMPONENTEN
REVÊTEMENTS DE BARRIÈRE THERMIQUE QUINAIRES À FAIBLE CONDUCTIVITÉ POUR COMPOSANTS DE MOTEUR À TURBINE
JORGENSEN DAVID JOHN (author) / BAKER WIL (author) / TOLPYGO VLADIMIR K (author)
2021-08-11
Patent
Electronic Resource
English
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