Turbine nozzles

Turbine nozzle including a plurality of airfoil vanes (120,122,124,126) extending between an inner band (56) and an outer band (54), wherein the outer band includes at least one mounting system (70) that extends radially outwardly therefrom and includes a rail (92,94) and at least one hook (96). The...

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Bibliographische Detailangaben
Hauptverfasser:	LENAHAN, DEAN, BRAINCH, GULCHARAN S
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CYLINDERS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PISTONS SEALINGS STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	Turbine nozzle including a plurality of airfoil vanes (120,122,124,126) extending between an inner band (56) and an outer band (54), wherein the outer band includes at least one mounting system (70) that extends radially outwardly therefrom and includes a rail (92,94) and at least one hook (96). The turbine nozzle is coupled into the gas turbine engine using the mounting system such that the turbine nozzle is at least partially supported by the at least one hook. A seal assembly is positioned between the at least one hook and the outer band to facilitate reducing radial leakage through the turbine nozzle.