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公开(公告)号:US10941667B2
公开(公告)日:2021-03-09
申请号:US16174553
申请日:2018-10-30
Applicant: SAFRAN AIRCRAFT ENGINES
Inventor: Claire Marie Figeureu , Eric Pierre Georges Lemarechal , Benjamin Bulot , Mathieu Simon Paul Gruber , Raphael Barrier , Cyril Polacsek
Abstract: A stator vane including a vane root, a vane tip, a leading edge extending between the root and the tip, the leading edge having a serrated profile having a succession of teeth and of troughs each having an amplitude and a thickness, wherein a series of at least three teeth and three consecutive troughs starting from the vane root and/or from the vane tip have a growing amplitude and/or thickness.