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. 16, 2017

Filed:

Dec. 19, 2013
Applicant:

Borealis Technical Limited, North Plains, OR (US);

Inventors:

Rodney T. Cox, North Plains, OR (US);

Isaiah W. Cox, London, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/50 (2006.01); B64C 25/40 (2006.01); B64C 25/34 (2006.01);
U.S. Cl.
CPC ...
B64C 25/405 (2013.01); B64C 25/50 (2013.01); B64C 2025/345 (2013.01); Y02T 50/823 (2013.01);
Abstract

A controllable aircraft taxi system is provided that enables the simultaneous control of aircraft autonomous ground movement and direction of aircraft autonomous ground movement. Independently controlled non-engine drive means capable of driving an aircraft landing gear wheel to move an aircraft autonomously on the ground without reliance on the aircraft's main engines are mounted to provide driving torque to aircraft a selected number of main landing gear wheels. The aircraft nose landing gear steering system is provided with steering angle detection and measurement means adapted to communicate with main landing gear wheel non-engine drive means, enabling simultaneous control over both autonomous aircraft ground travel and direction of autonomous aircraft ground travel. The present invention overcomes steering challenges presented by using non-engine drive means on main landing gear wheels to drive aircraft autonomously during taxi.


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