Turbine nozzle segment and assembly

Details Turbine nozzle segment and assembly Turbine nozzle segment and assembly

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/02 (2006.01) F01D 9/04 (2006.01) F01D 11/00 (2006.01) F01D 25/24 (2006.01)

Patent

CA 2709933

A turbine nozzle segment includes a band (122, 124) having a plurality of circumferentially spaced apart tabs (130) and a single airfoil (120) extending from the band.

L'invention concerne un segment de buse de turbine comprenant une bande (122, 124) composée d'une pluralité de languettes circonférentiellement espacées (130) et une surface portante unique (120) s'étendant depuis la bande.

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