GAS TURBINE ENGINE WITH A COOLED NOZZLE SEGMENT

An apparatus and method of cooling a hot portion of a gas turbine engine within a nozzle segment (100) comprising an outer and inner band (116) and at least one vane (72) extending between the outer and inner band (116). The outer band (118) includes a forward and aft cavity (136). The apparatus com...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DEMERS, Daniel Edward, CORREIA, Victor Hugo Silva, HOOPER, Tyler Frederick, HERNANDEZ, Wilhelm R. Ramon
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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