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:
Jul. 01, 2025

Filed:

Mar. 30, 2023
Applicant:

Airbus Operations Limited, Bristol, GB;

Inventor:

Fraser Wilson, Bristol, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/36 (2006.01); B60L 7/10 (2006.01); B60T 8/17 (2006.01); B64C 25/32 (2006.01); B64C 25/48 (2006.01); B64C 25/50 (2006.01);
U.S. Cl.
CPC ...
B64C 25/36 (2013.01); B60L 7/10 (2013.01); B60T 8/1703 (2013.01); B64C 25/405 (2013.01); B64C 25/48 (2013.01); B64C 25/50 (2013.01); B60T 2260/02 (2013.01); B60T 2270/60 (2013.01);
Abstract

An aircraft nose landing gear assembly is disclosed including two wheels, motors, brakes, and a controller. The wheels are separated by a steering axis and independently rotatable about a rotation axis in a rotation direction. The motors and brakes are each arranged to selectively engage a respective wheel. The motors and brakes supplement and resist rotation of the respective wheel in the rotation direction, respectively. On the basis of an indication to the controller of rotation of the two wheels in the rotation direction, the controller is arranged to: cause one motor to engage its respective wheel and supplement rotation, and cause the brake associated with the other wheel to engage the other wheel and resist rotation. Engagement of the motor and brake causes the wheels to pivot about the steering axis during a turning event.


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