Blade for turbine engine

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

Patent

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Details

F01D 5/14 (2006.01) F01D 5/02 (2006.01) F01D 5/30 (2006.01) F02C 3/04 (2006.01) F04D 29/34 (2006.01) F04D 29/38 (2006.01)

Patent

CA 2409382

A blade for a turbine engine having a centerline. The blade comprises: a root section extending at an angle relative to the centerline; and an airfoil section extending from the root section. The root section is directly adjacent said airfoil section. In other words, the blade is neckless. The blade is part of a rotor assembly, and is preferably a fan blade.

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