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. 31, 2020

Filed:

Dec. 22, 2017
Applicants:

Brian Goyez, Velizy-Villacoublay, FR;

Dominique Onfroy, Velizy-Villacoublay, FR;

Olivier Frey, Velizy-Villacoublay, FR;

Inventors:

Brian Goyez, Velizy-Villacoublay, FR;

Dominique Onfroy, Velizy-Villacoublay, FR;

Olivier Frey, Velizy-Villacoublay, FR;

Assignee:

SAFRAN LANDING SYSTEMS, Vélizy-Villacoublay, FR;

Attorney:
Int. Cl.
CPC ...
B64C 25/44 (2006.01); B60T 8/17 (2006.01); B60T 13/74 (2006.01); B60T 8/172 (2006.01); B60T 8/32 (2006.01); F16D 65/18 (2006.01); F16D 121/24 (2012.01);
U.S. Cl.
CPC ...
B64C 25/44 (2013.01); B60T 8/172 (2013.01); B60T 8/1703 (2013.01); B60T 8/325 (2013.01); B60T 13/741 (2013.01); F16D 65/18 (2013.01); F16D 2121/24 (2013.01);
Abstract

A braking system architecture for aircraft, the architecture comprising: a brake including friction members and electromechanical actuators for exerting a braking torque on the wheel; a computer situated in the fuselage of the aircraft and arranged to produce first control signals; and a junction box situated on the undercarriage, the junction box being connected to the computer and to the electromechanical actuators, the junction box being configured to receive the first control signals and to use the first control signals to produce second control signals for application to the electromechanical actuators in order to control the electromechanical actuators.


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