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.
Patent No.:
Date of Patent:
Jul. 29, 2025
Filed:
Jun. 12, 2020
Applicant:
Safran Landing Systems, Velizy Villacoublay, FR;
Inventors:
Aurélie Soula, Moissy-Cramayel, FR;
Patrice Palazzoli, Moissy-Cramayel, FR;
Alexandre Daulny, Moissy-Cramayel, FR;
Arnaud Caraty, Moissy-Cramayel, FR;
Assignee:
SAFRAN LANDING SYSTEMS, Velizy Villacoublay, FR;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16D 65/12 (2006.01); B33Y 80/00 (2015.01); B64C 25/44 (2006.01); F16D 55/36 (2006.01); B23K 26/342 (2014.01); B33Y 10/00 (2015.01); F16D 65/02 (2006.01);
U.S. Cl.
CPC ...
F16D 65/12 (2013.01); B33Y 80/00 (2014.12); B64C 25/44 (2013.01); F16D 55/36 (2013.01); B23K 26/342 (2015.10); B33Y 10/00 (2014.12); F16D 2065/1364 (2013.01); F16D 2065/138 (2013.01); F16D 2065/1392 (2013.01); F16D 2250/00 (2013.01);
Abstract
The invention relates to a bar () for a braked aircraft wheel (), the bar being for fitting to a rim () of the wheel in order to drive rotor brake disks () in rotation. The bar comprises a substantially rectilinear body () having at least one segment () including two wings () connected together by a core () and intended to co-operate with the rotor disks. At least one brace element () connects a free edge of each of the wings to a central portion of the core.