Curved platform turbine blade

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

Patent

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Details

F01D 5/14 (2006.01) F01D 5/30 (2006.01)

Patent

CA 2746415

A turbine blade (10) includes an airfoil (16) and integral platform at the root thereof. The platform (18) is contoured in elevation from a ridge (36, 48) to a trough (38), and is curved axially to complement the next adjacent curved platform.

La présente invention concerne une aube (10) de turbine comprenant un profil aérodynamique (16) faisant corps avec une plate-forme au niveau de l'emplanture de l'aube. La plate-forme (18) est profilée en élévation à partir d'une saillie (36, 48) jusqu'à une goulotte (38), et est recourbée dans la direction axiale de façon à compléter la plate-forme courbe adjacente suivante.

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