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:
Feb. 13, 2018

Filed:

Jul. 08, 2016
Applicants:

Airbus Operations Limited, Bristol, GB;

Airbus Operations Sas, Toulouse, FR;

Inventors:

Louis-Emmanuel Romana, Bristol, GB;

Miguel Angel Gama, Bristol, GB;

Assignees:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G07C 5/08 (2006.01); B64C 25/50 (2006.01); B64C 25/48 (2006.01); B64C 25/10 (2006.01); B60T 8/17 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
G07C 5/0808 (2013.01); B60T 8/1703 (2013.01); B64C 25/10 (2013.01); B64C 25/48 (2013.01); B64C 25/50 (2013.01); G07C 5/0816 (2013.01); B60T 2270/406 (2013.01); B64D 2045/0085 (2013.01);
Abstract

A data processing unit for monitoring the performance of at least one undercarriage which is used for braking and/or steering an aircraft, wherein the data processing unit is configured to: receive data representative of operating characteristics of the undercarriage(s) and use that data to calculate a maximum achievable braking force and/or yaw moment to be generated by the undercarriage(s). Also a method for monitoring the performance of at least one aircraft undercarriage which is used for braking and/or steering an aircraft, the method including: receiving data representative of operating characteristics of the undercarriage(s); and using that data to calculate a maximum achievable braking force and/or yaw moment to be generated by the undercarriage(s).


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