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. 02, 2019

Filed:

Jan. 25, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Sina S. Golshany, Lynnwood, WA (US);

Gnanulan Canagaratna, Everett, WA (US);

Matthew W. Orr, Kirkland, WA (US);

Andrew W. Fassmann, O'Fallon, MO (US);

Daniel Wajerski, Bellevue, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01G 19/07 (2006.01); G08G 5/00 (2006.01); G06Q 10/08 (2012.01); G06Q 10/04 (2012.01); G05D 1/00 (2006.01); G07C 5/08 (2006.01); B64F 5/60 (2017.01); G06Q 50/30 (2012.01); G06Q 10/06 (2012.01);
U.S. Cl.
CPC ...
G01G 19/07 (2013.01); B64F 5/60 (2017.01); G05D 1/0055 (2013.01); G06Q 10/04 (2013.01); G06Q 10/083 (2013.01); G07C 5/0841 (2013.01); G08G 5/0034 (2013.01); G08G 5/0039 (2013.01); G06Q 10/06312 (2013.01); G06Q 50/30 (2013.01);
Abstract

In a particular implementation, a method includes generating an initial weight estimate associated with an aircraft based on a reference operational empty weight (OEW) and at least one of a latitude or an altitude of the aircraft at a first location. The reference OEW is predetermined at a second location that is distinct from the first location. The method includes determining an additional load capability of the aircraft based on a difference between the initial weight estimate and the reference OEW. The method further includes generating an output that indicates the additional load capability.


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