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:
Aug. 04, 2026

Filed:

Dec. 01, 2021
Applicant:

Safran Landing Systems, Velizy Villacoublay, FR;

Inventors:

Arnaud Gapin, Velizy, FR;

Julien Marques, Velizy, FR;

Assignee:

SAFRAN LANDING SYSTEMS, Velizy Villacoublay, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F16D 65/847 (2006.01); B60B 21/08 (2006.01); B60B 27/00 (2006.01); F16D 55/36 (2006.01); F16D 65/78 (2006.01); F16D 65/853 (2006.01);
U.S. Cl.
CPC ...
F16D 65/847 (2013.01); B60B 21/08 (2013.01); B60B 27/0052 (2013.01); F16D 65/853 (2013.01); B60B 2900/513 (2013.01); F16D 55/36 (2013.01); F16D 2065/784 (2013.01); F16D 2065/789 (2013.01);
Abstract

An aircraft wheel including a rim fitted with rotor disks driven in rotation with the rim by first splines secured to the rim and engaged in notches in the rotor disks, stator disks interposed between the rotor disks and provided with notches engaged on second splines secured to a brake torque tube arranged to be fastened to an axle carrying the aircraft wheel, one or more heatpipe extending in one or more of the first and second splines parallel to a plane containing an axis of rotation of the wheel, the heatpipe having an end projecting outside the aircraft wheel, and one or more heatsinks secured to the end of the heatpipe.


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