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:
Feb. 01, 2022

Filed:

May. 28, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Sébastien Vincent François Dreano, Moissy-Cramayel, FR;

Mohammed-Lamine Boutaleb, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/06 (2006.01); F02C 7/14 (2006.01); B33Y 80/00 (2015.01);
U.S. Cl.
CPC ...
F02C 7/14 (2013.01); F01D 9/065 (2013.01); B33Y 80/00 (2014.12); F05D 2220/36 (2013.01); F05D 2230/31 (2013.01); F05D 2230/53 (2013.01); F05D 2240/12 (2013.01); F05D 2260/213 (2013.01); F05D 2260/221 (2013.01);
Abstract

An aircraft turbomachine blade includes an aerodynamic part manufactured in one piece by additive manufacturing, this aerodynamic part including a pressure-side wall, a suction-side wall and an internal fluid passage, this internal fluid passage being crossed by a plurality of disruptive elements that each connect the pressure-side wall to the suction-side wall, being irregularly spaced apart according to varied parameters in a chosen and optimized range, the junction of the disruptive elements with the pressure-side and suction-side walls not following a particular arrangement along the internal passage so as to form a disorderly arrangement.


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