Patent · US Active

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

US9630704B2 · kind B2 · utility

4Cited by
5References
5Claims
0Family size

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Key dates

Filing dateSep 28, 2012
Grant dateApr 25, 2017
Priority date
Expiry dateJan 9, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.