Turbine nozzle segment

Details Turbine nozzle segment Turbine nozzle segment

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 11/00 (2006.01)

Patent

CA 2709962

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).

L'invention concerne un segment de buse de turbine qui comprend une bande (124) pourvue d'une pluralité de pattes (152), un profil aérodynamique s'étendant à partir de la bande et une structure de support (166) reliée aux pattes. La structure de support présente une pluralité de structures de sollicitation (168).

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