Turbine nozzle segment

A turbine nozzle segment includes a band (124) having a plurality of tabs (152), an airfoil extending from the band and a support structure (166) attached to the tabs. The support structure has a plurality of biasing structures (168).

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Bibliographische Detailangaben
Hauptverfasser:	TODD STEPHEN HEFFRON, SANJEEWA THUSITHA FONSEKA, CLIVE ANDREW MORGAN
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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Beschreibung
Zusammenfassung:	A turbine nozzle segment includes a band (124) having a plurality of tabs (152), an airfoil extending from the band and a support structure (166) attached to the tabs. The support structure has a plurality of biasing structures (168).