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. 27, 2018

Filed:

Aug. 28, 2014
Applicant:

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

Inventor:

Rafael Perez, Boncelles, BE;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); B29D 99/00 (2010.01); B29C 45/14 (2006.01); B28B 1/00 (2006.01); B29C 70/70 (2006.01); B33Y 10/00 (2015.01); B33Y 80/00 (2015.01); B29K 79/00 (2006.01); B29K 305/00 (2006.01); B29K 309/02 (2006.01); B29L 31/08 (2006.01); B29C 67/00 (2017.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); B28B 1/001 (2013.01); B29C 45/14631 (2013.01); B29C 70/70 (2013.01); B29D 99/0025 (2013.01); B29C 67/0051 (2013.01); B29K 2079/085 (2013.01); B29K 2305/00 (2013.01); B29K 2309/02 (2013.01); B29L 2031/08 (2013.01); B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F05D 2230/30 (2013.01); F05D 2230/31 (2013.01); F05D 2300/44 (2013.01); F05D 2300/6031 (2013.01); F05D 2300/6032 (2013.01); F05D 2300/6033 (2013.01);
Abstract

The present application relates to a blade of a rectifier of a low pressure compressor of an axial turbomachine. The blade can also be a rotor and/or turbine blade. The blade includes a composite material with a matrix and a reinforcement comprising a mesh with rods. The rods of the reinforcement are connected to each other and are distributed throughout the volume between the pressure side surface and the suction side surface of the blade. The mesh forms a three-dimensional structure extending 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 present application also relates to an iterative method for manufacturing a blade composite where the reinforcement is formed by additive layer manufacturing based on titanium powder and then placed in an injection mold.


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