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:
Aug. 01, 2023

Filed:

Mar. 11, 2020
Applicant:

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

Inventors:

Stuart Mark Ferrell, Burnsville, MN (US);

William T. Reed, New York, NY (US);

Jan Vana, Prague, CZ;

Isaiah W. Cox, London, GB;

Assignee:

Borealis Technical Limited, Isle of Man, IM;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 45/00 (2006.01); B64D 43/00 (2006.01); G08G 5/06 (2006.01); G08G 5/00 (2006.01); B64D 47/08 (2006.01);
U.S. Cl.
CPC ...
B64D 45/0005 (2013.01); B64D 43/00 (2013.01); B64D 47/08 (2013.01); G08G 5/0095 (2013.01); G08G 5/06 (2013.01); B64D 2045/0075 (2013.01);
Abstract

A monitoring system and method are provided for real time monitoring of flaps, landing gears, or tail skids to determine safe taxi, takeoff, and flight readiness. Monitoring units, including scanning LiDAR devices combined with cameras or sensors, mounted in aircraft exterior locations produce a stream of meshed data that is securely transmitted to a processing system to generate a real time visual display of the flaps, landing gears, or tail skid for communication to aircraft pilots to ensure safe aircraft taxi, takeoff, and flight readiness. Actual flap position alignment with optimal flap setting, proper retraction and extension positions of landing gears, and tail skid condition is ensured. Safety of aircraft taxi, takeoff and flight and airport operations are improved when the present system and method are used to prevent incidents related to misaligned flaps and improperly positioned landing gears or tail skids.


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