Title:
Turbo machinery element
Document Type and Number:
Japanese Patent JP6034860
Kind Code:
B2
Abstract:
A turbomachine element including an airfoil set including a plurality of airfoils that are offset from one another in a lateral direction, and upstream from at least one end of each airfoil, a group of a plurality of vortex generator devices that are mutually offset both laterally and axially.
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Inventors:
Pesteille, Agnes
Perot, Bangsan
Bonifuas, Jiyan-Christophe Theleral Rozier
Perot, Bangsan
Bonifuas, Jiyan-Christophe Theleral Rozier
Application Number:
JP2014515256A
Publication Date:
November 30, 2016
Filing Date:
June 11, 2012
Export Citation:
Assignee:
SNECMA
International Classes:
F04D29/54; F01D5/14; F01D9/02; F04D29/32; F04D29/68
Domestic Patent References:
| JP57073805A |
Foreign References:
| US20100143140 | ||||
| WO2006080386A1 |
Attorney, Agent or Firm:
Kawaguchi International Patent Office