Airfoil platform impingement cooling

Details Airfoil platform impingement cooling Airfoil platform impingement cooling

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/18 (2006.01) F01D 9/02 (2006.01) F01D 25/12 (2006.01)

Patent

CA 2528049

A gas turbine engine airfoil has a platform cooling scheme including an impingement hole for directing cooling air against an undersurface of the airfoil platform.

Profil aérodynamique de turbine à gaz avec une méthode de refroidissement de la plate-forme dudit profil, muni d'un trou de contact pour diriger l'air de refroidissement contre une surface inférieure de la plate-forme du profil aérodynamique.

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