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:
Oct. 06, 2020

Filed:

Nov. 07, 2018
Applicant:

Safran Landing Systems, Velizy-Villacoublay, FR;

Inventors:

Brian Goyez, Velizy-Villacoublay, FR;

François Bonigen, Velizy-Villacoublay, FR;

Olivier Frey, Velizy-Villacoublay, FR;

Assignee:

SAFRAN LANDING SYSTEMS, Vélizy-Villacoublay, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/44 (2006.01); B60T 8/17 (2006.01); B60T 13/74 (2006.01); F16D 65/16 (2006.01);
U.S. Cl.
CPC ...
B60T 8/1703 (2013.01); B60T 13/746 (2013.01); B64C 25/44 (2013.01); F16D 65/16 (2013.01);
Abstract

Generally described, an architecture for an aircraft braking system is provided. The architecture includes a brake having friction members and electromechanical actuators, each electromechanical actuator having an electric motor and a power module; a computer arranged to produce digital control signals; a power unit arranged to produce an electrical power supply for powering the electric motors; and a junction box disposed on the undercarriage. The junction box may be configured to receive and to distribute the electrical power supply. The junction box generally includes an electrical motor control module that produces digital motor command signals from the digital control signals, and an electrical converter module that converts the digital motor command signals into analog motor command signals for the power modules of the electromechanical actuators.


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