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:
Oct. 24, 2017

Filed:

Mar. 16, 2012
Applicants:

Laura Collett, Cheltenham, GB;

Kyle R. Schmidt, Charlton Kings, GB;

Pia Sartor, Cheltenham, GB;

Inventors:

Laura Collett, Cheltenham, GB;

Kyle R. Schmidt, Charlton Kings, GB;

Pia Sartor, Cheltenham, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 17/50 (2006.01); B64C 25/00 (2006.01); G05B 17/02 (2006.01); G05B 23/02 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
G06F 17/5009 (2013.01); B64C 25/00 (2013.01); G05B 17/02 (2013.01); G05B 23/0243 (2013.01); B64D 2045/008 (2013.01);
Abstract

Method and system of determining ground-to-tire friction coefficient for an aircraft landing event. The method uses an aircraft computational model to repeatedly model the landing event, varying one or more initial conditions of the aircraft model until a best match between a modelled value and a provided value of aircraft vertical acceleration is determined. The method uses initial conditions associated with the best match of modelled and provided vertical acceleration values and a strain value from a sensor on the aircraft landing gear, with the ground-to-tire friction coefficient is a variable. The method models the landing gear to generate a modelled strain value and compares this with the measured strain value, and repeats the landing gear modelling step with a different value for the ground-to-tire friction coefficient until a best match between the modelled strain value and the measured strain value is determined and outputting the respective friction coefficient value.


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Collett, Laura. (2017). Method and system for determining friction coefficient μ for an aircraft landing event (U.S. Patent No. 9798838). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9798838

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