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:
Jun. 30, 2020

Filed:

Mar. 07, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Mohamed-Lamine Boutaleb, Paris, FR;

Fabien Roger Gaston Caty, Alfortville, FR;

Sebastien Vincent Francois Dreano, Longjumeau, FR;

Thierry Georges Paul Papin, Varennes-Jarcy, FR;

Christophe Marcel Lucien Perdrigeon, Ballainvilliers, FR;

Cedric Zaccardi, Saint-Maur-des-Fosses, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/06 (2006.01); F01D 9/04 (2006.01); F01D 25/12 (2006.01); F01D 25/18 (2006.01); F02C 7/14 (2006.01); F28D 21/00 (2006.01); F01D 5/18 (2006.01); F28F 1/40 (2006.01); F28D 1/02 (2006.01); F28D 1/053 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 9/065 (2013.01); F01D 25/12 (2013.01); F01D 25/18 (2013.01); F02C 7/14 (2013.01); F01D 5/188 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2230/22 (2013.01); F05D 2250/183 (2013.01); F05D 2260/22141 (2013.01); F28D 1/0233 (2013.01); F28D 1/0535 (2013.01); F28D 2021/0021 (2013.01); F28D 2021/0049 (2013.01); F28D 2021/0089 (2013.01); F28F 1/40 (2013.01); F28F 2250/02 (2013.01); F28F 2255/18 (2013.01); Y02T 50/675 (2013.01);
Abstract

A guide vane for a twin-spool aircraft turbomachine has an aerodynamic part that includes an internal lubricant cooling passage extending along a principal lubricant flow direction. The aerodynamic part is made in a single piece and also includes heat transfer fins arranged in the passage connecting the intrados and extrados walls and extending approximately parallel to the direction, these fins being distributed in successive rows along the principal direction and made such that for two rows of staggered directly consecutive fins, a first row includes fins forming a positive acute angle A1 with a dummy reference plane, while a second row includes fins forming a negative acute angle A2 with this plane.


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