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.

Patent No.:

US 10156469 B1

PDF
Full Text
Expired
Date of Patent:
Dec. 18, 2018

Filed:

Feb. 24, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Nils Kneuper, Bergkamen, DE;

Ralf Rene Cabos, Bergkamen, DE;

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01G 19/02 (2006.01); B64D 45/00 (2006.01); G01G 19/07 (2006.01); G01G 19/08 (2006.01); B64F 1/22 (2006.01);
U.S. Cl.
CPC ...
G01G 19/024 (2013.01); B64D 45/00 (2013.01); B64F 1/225 (2013.01); G01G 19/07 (2013.01); G01G 19/086 (2013.01);
Abstract

An example methods for aircraft mass determination at pushback includes determining an acceleration of a pushback vehicle while moving an aircraft, determining a pushback force applied by the pushback vehicle while moving the aircraft, and determining a total mass of the aircraft based on the pushback force, the acceleration of the pushback vehicle during pushback, and a coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves. An example system includes a pushback vehicle coupled to an acceleration sensor and a force sensor, and a computing device having one or more processors to determine a total mass of the aircraft based on the pushback force, the acceleration of the pushback vehicle during pushback, and a coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves.


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