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:
Jul. 04, 2023

Filed:

Apr. 07, 2020
Applicant:

Safran Landing Systems, Velizy Villacoublay, FR;

Inventors:

Olivier Frey, Moissy-Cramayel, FR;

Frédéric Pithoud, Moissy-Cramayel, FR;

Serge Barthelemy, Moissy-Cramayel, FR;

Assignee:

SAFRAN LANDING SYSTEMS, Velizy Villacoublay, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B60T 13/74 (2006.01); H02P 29/40 (2016.01); B60T 8/17 (2006.01);
U.S. Cl.
CPC ...
B60T 13/746 (2013.01); B60T 8/1703 (2013.01); H02P 29/40 (2016.02); B60T 2250/00 (2013.01);
Abstract

The invention provides a method of electrically powering an electromechanical braking actuator () fitted to an aircraft wheel brake, in which the power supply current (I) delivered to the electromechanical braking actuator is saturated to a saturation value (Isat) in order to limit the current consumed by the electromechanical braking actuator and thereby limit the forces developed by the actuator. The method includes the step of determining the saturation value (Isat) as a function of an internal temperature (T) of the electromechanical braking actuator while it is in operation.


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