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.
Blade for turbine engine
2004-07-20
Miscellaneous
No indication
English
Lift engine advanced turbine blade technology
Tema Archive | 1973
European Patent Office | 2019
|European Patent Office | 2016
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