Turbine blade and corresponding manufacturing method

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

Patent

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Details

F01D 5/20 (2006.01)

Patent

CA 2762413

A turbine blade includes an airfoil having first and second tip ribs extending along the opposite pressure and suction sides thereof. A tip baffle bifurcates the airfoil tip into two pockets, with a first pocket being laterally open at its aft end to recover leakage flow, and a second pocket being laterally closed.

Une aube de turbine comprend un profil aérodynamique comportant des première et seconde nervures de pointe s'étendant le long des côtés de pression et d'aspiration opposés de celui-ci. Un déflecteur de pointe fait bifurquer la pointe de profil aérodynamique dans deux poches, une première poche étant latéralement ouverte au niveau de son extrémité arrière pour récupérer un courant de fuite, et une seconde poche latéralement fermée.

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