Internal aluminide coating for vanes and blades and method of manufacture

A gas turbine engine component includes a substrate having first surface and a second surface disposed opposite the first surface, a plurality of holes extending through the substrate from the first surface to the second surface, the holes defined by a plurality of respective walls each extending fr...

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Bibliographische Detailangaben

Hauptverfasser:	Liu, Xuan, Jencks, Danielle E, Croft, Russell F, Perez Reisler, Rafael A, Cotnoir, Glenn A, Turko, Andy
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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