Turbine nozzle segment and method for repairing a turbine...

F - Mech Eng,Light,Heat,Weapons – 01 – D

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Details

F01D 9/04 (2006.01) F01D 5/00 (2006.01) F01D 11/00 (2006.01) F02C 7/28 (2006.01)

Patent

CA 2709932

k turbine nozzle segment (119) includes a first band (118), an airfoil (120) extending from the first band and a support attached to the first band. The support may have a plurality of circumferentially spaced apart tabs (130).

La présente invention concerne un segment de distributeur de turbine comprenant une première bande, une surface portante s'étendant à partir de la première bande et un support fixé à la première bande. Le support peut présenter une pluralité de languettes disposées à distance les unes des autres de manière circonférentielle.

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