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:
Aug. 13, 2019

Filed:

Jan. 11, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Cedric Zaccardi, Saint Maur des Fosses, FR;

Mohamed-Lamine Boutaleb, Paris, FR;

Sebastien Christophe Chalaud, Vincennes, FR;

Eric Pierre Georges Lemarechal, Alfortville, FR;

Thierry Georges Paul Papin, Varennes-Jarcy, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/06 (2006.01); F02C 7/14 (2006.01); F02K 3/06 (2006.01); F28D 1/02 (2006.01); F28D 1/03 (2006.01); F04D 19/00 (2006.01); F04D 29/54 (2006.01); F04D 29/58 (2006.01); F28D 21/00 (2006.01); F04D 29/063 (2006.01);
U.S. Cl.
CPC ...
F04D 29/5853 (2013.01); F01D 9/065 (2013.01); F02C 7/14 (2013.01); F02K 3/06 (2013.01); F04D 19/002 (2013.01); F04D 29/063 (2013.01); F04D 29/542 (2013.01); F28D 1/0206 (2013.01); F28D 1/035 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2230/30 (2013.01); F05D 2240/12 (2013.01); F05D 2260/22141 (2013.01); F28D 2021/0021 (2013.01); F28D 2021/0089 (2013.01); F28F 2250/02 (2013.01); Y02T 50/676 (2013.01);
Abstract

A guide vane for a dual flow aircraft turbine engine includes an aerodynamic part. The aerodynamic part includes an inner duct for lubricant cooling extending in a main direction and being partly bounded by a pressure side wall and a suction side wall of the vane. The aerodynamic part is embodied as a single piece, and includes heat transfer fins arranged in the duct expanding substantially parallel to a direction of the duct. The fins are spaced from each other depending on the direction of the duct and a transversal direction of the vane, so that at least some of the fins are arranged substantially staggered.


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