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.
Blade for a fan of a turbomachine, notably of the unducted fan type, corresponding fan and corresponding turbomachine
2017-04-25
Patent
Electronic Resource
English
UNDUCTED RECTIFIER FOR A TURBOMACHINE, TURBOMACHINE MODULE AND AIRCRAFT TURBOMACHINE
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