NOZZLE SEGMENT FOR USE WITH MULTIPLE DIFFERENT TURBINE ENGINES

To provide a nozzle segment that can be used with multiple different types of turbine engines.SOLUTION: A nozzle segment includes an inner band, an outer band, and at least one nozzle vane extending between the inner and outer bands. The outer band includes a hook that extends radially outwardly fro...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	JOE T BROWN, NORMAN ANDREW BARRETT II
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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