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:
Nov. 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:

Andrew Bill, Bristol, GB;

Utsav Oza, Bristol, GB;

Esther Ramirez-Paya, Bristol, GB;

David Joel Clarke, Bristol, GB;

Assignees:

AIRBUS OPERATIONS LIMITED, Bristol, GB;

AIRBUS OPÉRATIONS (S.A.S.), Toulouse, FR;

AIRBUS (S.A.S.), Blagnac, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60T 8/00 (2006.01); 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

A braking system and a method for applying one or more aircraft wheel brakes according to at least one of a plurality of wheel brake control functions are disclosed. The method includes receiving an indication of an aircraft speed from an aircraft speed indicator, controlling a wheel braking operation of the aircraft according to at least a first wheel brake control function if the aircraft speed indicated by the aircraft speed indicator exceeds a speed threshold, and controlling the wheel braking operation of the aircraft according to at least a second wheel brake control function if the aircraft speed does not exceed the speed threshold. Also disclosed is an aircraft including one or more aircraft wheel brakes and the disclosed braking system.


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