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:
Nov. 14, 2017

Filed:

Aug. 28, 2014
Applicant:

Techspace Aero S.a., Herstal (Milmort), BE;

Inventor:
Assignee:

SAFRAN AERO BOOSTERS SA, Herstal (Milmort), BE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); B22F 5/04 (2006.01); F01D 5/28 (2006.01); B22F 7/08 (2006.01); B29C 67/00 (2017.01); B22F 3/105 (2006.01); B29K 79/00 (2006.01); B29K 105/00 (2006.01); B29K 505/08 (2006.01); B29L 31/08 (2006.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); B22F 3/1055 (2013.01); B22F 5/04 (2013.01); B22F 7/08 (2013.01); B29C 67/0077 (2013.01); F01D 5/147 (2013.01); B29K 2079/085 (2013.01); B29K 2105/251 (2013.01); B29K 2505/08 (2013.01); B29L 2031/08 (2013.01); F05D 2230/31 (2013.01); F05D 2300/603 (2013.01); Y02P 10/295 (2015.11);
Abstract

The present application relates to a blade of low pressure rectifier axial turbomachine. The blade can also be a rotor blade and/or a turbine blade. The blade includes a composite material with a matrix and a reinforcement that includes a mesh forming a three dimensional structure with a plurality of rods that describe a three-dimensional mesh based on polyhedrons. The three-dimensional structure extends over the majority of the thickness of the blade between the pressure side surface and the suction side surface and/or the majority of the length of the blade between the leading edge and the trailing edge. The rods of the reinforcement are bonded to each other and are distributed throughout the volume between the pressure side surface and the suction side surface of the blade. The rods form a three-dimensional mesh occupying the entire blade. The present application also relates to an iterative method for manufacturing a blade by additional layer manufacturing.


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