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. 05, 2015

Filed:

Nov. 21, 2011
Applicants:

Neal Gilleran, Long Beach, CA (US);

Robert Sweet, Beaver, UT (US);

Jonathan Edelson, Portland, OR (US);

Isaiah Watas Cox, Baltimore, MD (US);

Inventors:

Neal Gilleran, Long Beach, CA (US);

Robert Sweet, Beaver, UT (US);

Jonathan Edelson, Portland, OR (US);

Isaiah Watas Cox, Baltimore, MD (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/00 (2006.01); B64C 25/40 (2006.01);
U.S. Cl.
CPC ...
B64C 25/405 (2013.01); Y02T 50/823 (2013.01);
Abstract

A failsafe system and method for ensuring the safe operation of an aircraft with a ground movement system to drive the aircraft independently on the ground is provided. The system includes at least one aircraft nose or main drive wheel powered by an onboard wheel driver responsive to sensed aircraft and ground movement system operating parameters to continue operation in response to parameters within normal limits or to prevent continued operation if sensed parameters are outside normal limits and indicate continued operation to be unsafe. The onboard wheel driver includes a locking assembly responsive automatically or manually to signals indicating sensed parameters to lock the onboard wheel driver in an activated or an inactivated condition, depending on whether operation of the ground movement system can be continued safely.


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