THERMAL BARRIER COATING, LAYERED COMPONENT COMPRISING A THERMAL BARRIER COATING AND GAS TURBINE ENGINE COMPRISING A LAYERED COMPONENT

A gas turbine engine includes a compressor section, a combustor section, a turbine section, a hot gas path and a layered component (600) including a substrate (502) and a thermal barrier coating (TBC) (602) having: a single layer of 6-15% wt.% yttria-stabilized zirconia in a tetragonal phase arrange...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KHATTAR, Rohit, SUBRAMANIAN, Ramesh, SHARMA, Atin
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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