Turbine blade having a cooling air deflector

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

Patent

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Details

F01D 5/08 (2006.01) F01D 5/18 (2006.01) F01D 5/30 (2006.01)

Patent

CA 2444862

The invention relates to a blade (11) for a turbine, comprising a foot (13) enabling it to be protracted into a honeycomb element (14) of a disk (12) of said turbine, provided with an internal air cooling circuit comprising means for admitting air (15) disposed on the foot of the blade opposite the honeycomb element, and means for discharging air. The foot (13) of the blade is provided with means (20) for homogenizing the pressure and temperature of the cooling air entering the means for admitting air.

L'invention concerne une aube (11) pour turbine, l'aube présentant un pied (13) permettant de la rapporter dans une alvéole (14) d'un disque (12) de la turbine, l'aube possédant un circuit interne de refroidissement par air comprenant des moyens d'entrée d'air (15) situés sur le pied de l'aube et en regard de l'alvéole, et des moyens de sortie d'air. Le pied (13) de l'aube est pourvu de moyens (20) d'homogénéisation de la pression et de la température de l'air de refroidissement pénétrant dans les moyens d'entrée d'air.

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