Blade for a fan of a turbomachine, notably of the unducted fan type, corresponding fan and corresponding turbomachine

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United States of America Patent

PATENT NO 9630704
SERIAL NO

14347940

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Abstract

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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.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINES2 BOULEVARD DU GÉNÉRAL MARTIAL VALIN PARIS 75015

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Boisard, Ronan Chatillon, FR 1 6
Delattre, Gregory Clamart, FR 1 6
Falissard, Fabrice Sceaux, FR 1 6
Jacquin, Laurent Le Chesnay, FR 1 6
Ortun, Biel Paris, FR 1 6
Rodriguez, Benoit Versailles, FR 2 6
Vion, Laurence Paris, FR 1 6

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