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:
May. 15, 2018

Filed:

Oct. 15, 2014
Applicant:

Snecma, Paris, FR;

Inventors:

Gabrijel Radeljak, Torcy, FR;

Pascal Couhier, Saint Fargeau Ponthierry, FR;

Benedicte Leleu, Paris, FR;

Frederic Raymond Jean Miroudot, Bry sur Marne, FR;

Sebastien Hameau, Lieusaint, FR;

Antoine Jean Jausovec, Tournan en Brie, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 17/08 (2006.01); F01D 21/00 (2006.01); F01D 25/28 (2006.01); F01D 9/02 (2006.01); F04D 27/00 (2006.01); F01D 17/02 (2006.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); F01D 9/02 (2013.01); F01D 17/02 (2013.01); F01D 17/085 (2013.01); F01D 25/285 (2013.01); F04D 27/001 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2260/12 (2013.01); F05D 2260/83 (2013.01); Y02T 50/671 (2013.01); Y10T 29/49323 (2015.01);
Abstract

The invention relates to an instrumented airfoil for mounting in a flow passage through a turbine, compressor, or module of a turbine engine. An instrumentation member is attached to an airfoil and includes information-obtaining means received in a cutout formed in the airfoil and projecting relative to the leading edge or the trailing edge. According to the invention, the instrumentation member also comprises a holder portion that is united with the information-obtaining means and that is attached to the cutout in such a manner that its surface is in alignment respectively with the suction side wall, the pressure side wall, and the leading edge or the trailing edge of the airfoil, the transitions between these respective surfaces not presenting any setbacks.


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