A blade for a fan of a turbomachine, for example of unducted fan type, a corresponding fan, and a corresponding turbomachine. The blade includes a mechanism arranged, at a single location, to locally, as the fan rotates, disturb a distribution of flow around the blade so as to form two independent main vortices downstream.
PALE POUR UNE HELICE DE TURBOMACHINE, NOTAMMENT A SOUFFLANTE NON CARENEE, HELICE ET TURBOMACHINE CORRESPONDANTES
PROPELLER BLADE FOR UNDUCTED FAN ENGINE, PROPELLER COMPRISING SUCH A BLADE AND CORRESPONDING ENGINE
PROPELLERBLATT FÜR MANTELLOSE GEBLÄSETRIEBWERKE, PROPELLER MIT EINEM DERARTIGEN PROPELLERBLATT SOWIE GEBLÄSETRIEBWERK
2017-04-19
Patent
Electronic Resource
French
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