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:
Jun. 16, 2026

Filed:

Oct. 25, 2021
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Mathieu Julien Charlas, Moissy-Cramayel, FR;

Adrien Francis Paixao, Moissy-Cramayel, FR;

Simon Talibart, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23P 6/00 (2006.01); B22F 5/00 (2006.01); B22F 10/28 (2021.01); B22F 10/30 (2021.01); B22F 10/85 (2021.01); B29C 64/118 (2017.01); B29C 64/393 (2017.01); B33Y 10/00 (2015.01); B33Y 50/02 (2015.01); F02C 7/045 (2006.01); F02K 1/82 (2006.01); B29K 23/00 (2006.01); B29K 63/00 (2006.01); B29K 77/00 (2006.01); B29K 307/04 (2006.01); B29L 31/60 (2006.01);
U.S. Cl.
CPC ...
B23P 6/007 (2013.01); B22F 5/009 (2013.01); B22F 10/28 (2021.01); B22F 10/30 (2021.01); B22F 10/85 (2021.01); B29C 64/118 (2017.08); B29C 64/393 (2017.08); B33Y 10/00 (2014.12); B33Y 50/02 (2014.12); F02C 7/045 (2013.01); F02K 1/827 (2013.01); B22F 2301/052 (2013.01); B22F 2998/10 (2013.01); B29K 2023/12 (2013.01); B29K 2063/00 (2013.01); B29K 2077/10 (2013.01); B29K 2307/04 (2013.01); B29L 2031/608 (2013.01); F05D 2220/323 (2013.01); F05D 2230/80 (2013.01); F05D 2260/96 (2013.01);
Abstract

A method for repairing a part for an aircraft turbine engine, the part including a lower panel, an upper panel and a core having a honeycomb structure arranged between the lower panel and the upper panel, the part having an unimpaired portion and an at least partially impaired portion, the repair method including the following steps: (a) removing at least one portion of the lower panel or the upper panel from an area to be repaired; (b) removing at least one portion of the core from the area to be repaired; (c) reforming the core in the area to be repaired directly on the part by additive manufacturing; (d) reforming the lower panel or the upper panel in the area to be repaired, directly on the part.


Find Patent Forward Citations

Quick Actions:

Charlas, Mathieu. (2026). Method for repairing a part for an aircraft turbine engine (U.S. Patent No. 12654262). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12654262

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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