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:
May. 24, 2016

Filed:

Nov. 15, 2013
Applicants:

Airbus Operations Limited, Bristol, GB;

Airbus Operations Sas, Toulouse, FR;

Inventors:

Miguel Angel Gama-Valdez, Bristol, GB;

Louis-Emmanuel Romana, Toulouse, FR;

Andrea Damiani, Bristol, GB;

Michael Richard Whincup, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/00 (2006.01); B64C 25/44 (2006.01); G05D 1/00 (2006.01); B60T 8/17 (2006.01); B60T 8/1766 (2006.01); B64C 25/40 (2006.01); B64C 25/48 (2006.01); B64C 25/34 (2006.01); G05D 1/02 (2006.01); B64C 25/10 (2006.01); B64C 25/18 (2006.01); B64C 25/26 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0083 (2013.01); B60T 8/1703 (2013.01); B60T 8/1766 (2013.01); B64C 25/34 (2013.01); B64C 25/405 (2013.01); B64C 25/48 (2013.01); G05D 1/0202 (2013.01); B64C 25/00 (2013.01); B64C 25/10 (2013.01); B64C 25/18 (2013.01); B64C 25/26 (2013.01); B64C 2025/008 (2013.01); Y02T 50/823 (2013.01);
Abstract

A landing gear force and moment distributor system for an aircraft having a longitudinal axis aligned in a forward-aft direction, a vertical axis perpendicular to the longitudinal axis, and a landing gear including a pair of bogies arranged symmetrically about the longitudinal axis, each bogie having an actuator arranged to brake and/or drive one or more wheels. The force distribution system includes a distribution module arranged to: receive an input demand including a longitudinal force input demand corresponding to a desired braking or driving force along the longitudinal axis for the landing gear and a moment input demand corresponding to a desired moment about the vertical axis for the landing gear; and to use the received input demand to calculate an output command including, for each bogie, a longitudinal force output command corresponding to a braking or driving force along the longitudinal axis to be applied to the bogie.


Find Patent Forward Citations

Gama-Valdez, Miguel. (2016). Landing gear force and moment distributor (U.S. Patent No. 9348335). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9348335

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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