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:
Sep. 03, 2019

Filed:

Oct. 21, 2015
Applicant:

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

Inventor:
Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/06 (2006.01); F01D 5/14 (2006.01); F01D 9/02 (2006.01); F01D 25/00 (2006.01); F04D 29/30 (2006.01); F04D 29/02 (2006.01); B22F 7/00 (2006.01); B22F 5/04 (2006.01); B22F 3/105 (2006.01); B22F 7/08 (2006.01);
U.S. Cl.
CPC ...
F01D 25/06 (2013.01); B22F 3/1055 (2013.01); B22F 5/04 (2013.01); B22F 7/004 (2013.01); B22F 7/006 (2013.01); B22F 7/08 (2013.01); F01D 5/147 (2013.01); F01D 9/02 (2013.01); F01D 25/005 (2013.01); F04D 29/023 (2013.01); F04D 29/30 (2013.01); F05D 2300/612 (2013.01); Y02P 10/295 (2015.11); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01);
Abstract

The invention relates to a blade of a low-pressure compressor of an axial turbine engine. The blade comprises a vane in which a cavity is formed. The vane has a leading edge and a trailing edge, an intrados surface and an extrados surface which extend from the leading edge to the trailing edge, an outer casing which forms the intrados surface and the extrados surface and which delimits the cavity. The blade further comprises closed foam, such as a polymethacrylic foam, which blocks the cavity in order to isolate it from the environment of the blade. The blade further has a three-dimensional lattice which is formed in the cavity and which is integral with the vane of the blade. This barrier protects from chemical attacks and the introduction of impurities. The invention also relates to a production method for a hollow turbine engine blade which is filled with foam.


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Cortequisse, Jean-Francois. (2019). Lattice type blade of an axial turbine engine compressor (U.S. Patent No. 10400625). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10400625

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