Turbine blade with improved cooling characteristics and...

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

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F01D 5/18 (2006.01)

Patent

CA 2569563

La présente invention concerne le domaine des aubes de turbine de turbomachine, notamment une aube de turbine (1), comportant une paroi intrados (2), une paroi extrados (3), au moins une première cavité radiale de bord de fuite (4), au moins une seconde cavité radiale (5) en amont de la cavité de bord de fuite (4), une paroi interne (6) séparant les cavités radiales (4 et 5) et comprenant au moins un canal (7) reliant les cavités (4 et 5) entre elles, ledit canal (7) étant orienté selon un axe (71) coupant la surface interne (42) de la paroi intrados (2).

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