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. 02, 2023

Filed:

Feb. 06, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Cédric Zaccardi, Moissy-Cramayel, FR;

Christophe Marcel Lucien Perdrigeon, Moissy-Cramayel, FR;

Catherine Pikovsky, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/18 (2006.01); F01D 9/06 (2006.01); F02C 7/18 (2006.01); F02C 6/08 (2006.01); B33Y 80/00 (2015.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 5/187 (2013.01); F01D 9/065 (2013.01); F02C 6/08 (2013.01); F02C 7/185 (2013.01); B33Y 80/00 (2014.12); F05D 2240/121 (2013.01); F05D 2250/61 (2013.01); F05D 2250/712 (2013.01); F05D 2260/213 (2013.01); F05D 2260/2214 (2013.01); F05D 2260/232 (2013.01); F05D 2260/606 (2013.01);
Abstract

A turbomachine blade including a body that extends mainly in a plane defined by a main axis and a longitudinal direction, which is defined by a lower surface wall, an upper surface wall, a leading edge located at a first longitudinal end of the body and a trailing edge located at a second longitudinal end of the body, wherein the body of the blade includes a plurality of first pipes that extend mainly along the direction of the main axis, for circulation of a gas flow, and a plurality of second pipes that extend mainly along the longitudinal direction, for circulation of a second gas flow.


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