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:
Mar. 14, 2017

Filed:

Apr. 21, 2015
Applicant:

Messier-bugatti-dowty, Velizy-Villacoublay, FR;

Inventors:

Pierre Chambard, Velizy-Villacoublay, FR;

Come Dorge, Clamart, FR;

Richard Masson, Les Loges En Josas, FR;

Jean-Baptiste Vaney, Velizy-Villacoublay, FR;

Assignee:

MESSIER-BUGATTI-DOWTY, Velizy-Villacoublay, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16D 55/42 (2006.01); B64C 25/44 (2006.01); F16D 55/24 (2006.01); F16D 55/36 (2006.01); F16D 55/00 (2006.01);
U.S. Cl.
CPC ...
F16D 55/42 (2013.01); B64C 25/44 (2013.01); F16D 55/24 (2013.01); F16D 55/36 (2013.01); F16D 2055/0058 (2013.01); F16D 2055/0095 (2013.01);
Abstract

The invention relates to a disc brake for an aircraft wheel, comprising friction discs (), including rotor discs and stator discs, a structure comprising a torsion tube () on which the discs are fitted, a rear plate () which is located at one end of the tube, and a support () for braking actuators () at another end of the tube, the actuators being able to be selectively activated in order to apply a pressing force to the discs. According to the invention, the discs are separated into two groups, including a first group () which can be used alone for taxiing braking operations, and a second group () which can be used alone or in conjunction with the first group for take-off/landing braking operations.


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