Blade outer air seal for a gas turbine engine and corresponding gas turbine engine

A blade outer air seal (12) for a gas turbine engine includes a body (22) having an outer radial surface (28), an inner radial surface (30), and a plurality of cooling air apertures (62). The body (22) extends between a forward edge (24) and an aft edge (26). The inner radial surface (30) includes a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Lutjen, Paul M, Tholen, Susan M, Knapp, James N
Format:	Patent
Sprache:	eng ; fre ; ger
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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