The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 10, 2019

Filed:

Nov. 09, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Stephane Roger Mahias, Montrouge, FR;

Baptiste Batonnet, Sezanne, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F01D 5/14 (2006.01); F01D 5/16 (2006.01); F01D 25/04 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); F01D 5/141 (2013.01); F01D 5/16 (2013.01); F01D 25/04 (2013.01); F05D 2220/30 (2013.01); F05D 2250/183 (2013.01); F05D 2250/184 (2013.01); F05D 2250/185 (2013.01); F05D 2250/71 (2013.01); F05D 2250/711 (2013.01); F05D 2250/712 (2013.01); F05D 2250/74 (2013.01); F05D 2260/96 (2013.01);
Abstract

The present invention relates to a turbine engine guide () vane (), with a height (H) extending between a vane root () and a vane tip () along a radial direction (Z), said vane () comprising a succession of five bulge portions along a tangential direction (Y) perpendicular to the radial direction (Z), this succession of bulge portions extending over the whole height (H) of the vane (), and the convexity of the successive bulge portions being alternately in one direction and in the other. The vane () has the advantage of having an eigenfrequency for the first striped vibration mode which is different from the urging frequencies of said vane (), during the operation of the turbine engine.


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