Turbomachine airfoil having a variable thickness thermal barrier coating

An airfoil includes a root and a tip, which define a span of the airfoil therebetween. The airfoil also includes a leading edge and a trailing edge downstream of the leading edge along a flow direction. The leading edge and the trailing edge each extend across the span of the airfoil from the root t...

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Bibliographische Detailangaben

Hauptverfasser:	Jasper, Martin James, Pilson, Richard Ryan, Kester, Christopher W, Agudo, Jan, Myers, Melbourne James
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL 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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