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.
Patent No.:
Date of Patent:
Apr. 04, 2017
Filed:
Nov. 26, 2014
Applicant:
Airbus Operations Limited, Bristol, GB;
Inventors:
George Iordanidis, Bristol, GB;
John Rees, Bristol, GB;
Assignee:
Airbus Operations Limited, Bristol, GB;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60T 8/86 (2006.01); B64C 25/44 (2006.01); B60T 8/17 (2006.01); B60T 8/88 (2006.01); B64C 25/46 (2006.01); F16D 65/14 (2006.01); B60T 13/74 (2006.01); F16D 121/24 (2012.01);
U.S. Cl.
CPC ...
B64C 25/44 (2013.01); B60T 8/1703 (2013.01); B60T 8/885 (2013.01); B60T 13/741 (2013.01); B64C 25/46 (2013.01); F16D 65/14 (2013.01); B60T 2270/402 (2013.01); F16D 2121/24 (2013.01);
Abstract
An electrically actuated braking system for an aircraft, including: an electro-mechanical brake actuator (EMAbrake) proximate a wheel of the aircraft, the EMAbrake including a motor; an electro-mechanical actuator controller (EMAC) including a first motor controller for generating a first drive signal for the EMAbrake, and a second motor controller for generating a second drive signal for the EMAbrake, wherein the first motor controller and the second motor controller are dissimilar so as to provide protection against common mode failure of the first and second motor controllers.