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:
Sep. 20, 2022

Filed:

May. 05, 2020
Applicant:

Safran Landing Systems, Velizy-Villacoublay, FR;

Inventor:

Olivier Frey, Velizy-Villacoublay, FR;

Assignee:

SAFRAN LANDING SYSTEMS, Velizy-Villacoublay, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60T 7/10 (2006.01); B60T 8/17 (2006.01); B64C 25/44 (2006.01); F16D 55/36 (2006.01); F16D 65/18 (2006.01); H02P 3/02 (2006.01); F16D 121/24 (2012.01);
U.S. Cl.
CPC ...
B60T 8/1703 (2013.01); B64C 25/44 (2013.01); F16D 55/36 (2013.01); F16D 65/186 (2013.01); H02P 3/025 (2013.01); F16D 2121/24 (2013.01);
Abstract

A control method of an electrical braking system for aircraft includes a plurality of electromechanical actuators capable of applying a braking force on friction members. Each electromechanical actuator includes an electric motor equipped with one or more windings. The braking system further includes at least one power module configured to send to each electric motor winding a phase current and at least one control module configured to control, in response to a braking setpoint, the sending by the power module of a setpoint phase current determined depending on the braking force to be applied. The method further includes the variation of the phase current transmitted to each winding of the electric motor so as to cause the phase current to oscillate around the setpoint phase current.


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