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. 14, 2023

Filed:

Feb. 26, 2019
Applicants:

Airbus Operations Limited, Bristol, GB;

Airbus Opérations (S.a.s.), Toulouse, FR;

Airbus (S.a.s.), Blagnac, FR;

Inventors:

Utsav Oza, Bristol, GB;

Andrew Bill, Bristol, GB;

Kurt Bruggemann, Bristol, GB;

Rodrigo Jimenez, Bristol, GB;

Brice Cheray, Bristol, GB;

Maud Consola, Bristol, GB;

Assignees:

AIRBUS OPERATIONS LIMITED, Bristol, GB;

AIRBUS OPERATIONS (SAS), Toulouse, FR;

AIRBUS (SAS), Blagnac, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B60T 17/22 (2006.01); B64F 5/60 (2017.01); F16D 66/00 (2006.01); F16D 66/02 (2006.01); B60T 8/17 (2006.01); B60T 8/58 (2006.01); B64C 25/42 (2006.01); B60T 8/171 (2006.01); B60T 8/32 (2006.01);
U.S. Cl.
CPC ...
B60T 17/221 (2013.01); B60T 8/171 (2013.01); B60T 8/1703 (2013.01); B60T 8/32 (2013.01); B60T 8/58 (2013.01); B64C 25/426 (2013.01); B64F 5/60 (2017.01); F16D 66/00 (2013.01); F16D 66/021 (2013.01); B60T 2270/406 (2013.01); B64C 25/42 (2013.01); F16D 2066/001 (2013.01); F16D 2066/006 (2013.01);
Abstract

An apparatus for an aircraft having one or more aircraft wheel brakes, and a brake wear sensor configured to measure a wear state of a brake of the one or more aircraft wheel brakes, is disclosed. The apparatus includes a processor configured to determine a wear relationship between a wear state of the brake and a number of use cycles of the brake, determine a predicted wear state of the brake based on the wear relationship; determine a number of future use cycles of the brake based on a predicted condition of the brake, the predicted condition comprising the predicted wear state of the brake; and provide an indication of the determined number of the future use cycles to ground crew and/or a pilot of the aircraft, wherein the number of future use cycles is the number of use cycles for which the brake is allowed to be used, and a use cycle comprises all uses of the brake relating to a flight undertaken by the aircraft.


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