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:
Jun. 18, 2019

Filed:

Mar. 20, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Oliver C. Meier, Mill Creek, WA (US);

Roy A. Eggink, Mukilteo, WA (US);

Kristoffer R. Jonson, Seattle, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 43/02 (2006.01); G08G 5/00 (2006.01); G07C 5/08 (2006.01); B64D 45/00 (2006.01); B64D 43/00 (2006.01); G01C 21/20 (2006.01); G01C 23/00 (2006.01); G05D 1/00 (2006.01);
U.S. Cl.
CPC ...
G08G 5/0047 (2013.01); B64D 43/00 (2013.01); B64D 43/02 (2013.01); B64D 45/0005 (2013.01); G01C 21/20 (2013.01); G01C 23/00 (2013.01); G05D 1/0005 (2013.01); G07C 5/0816 (2013.01);
Abstract

A system and method for the real-time optimization of aircraft fuel economy includes sensors to monitor in-flight performance characteristics, to monitor the status of aircraft control elements during flight, to monitor fuel consumption, and to identify aircraft position information during flight. A processor is coupled to receive information from the sensors. During flight, the processor calculates a current performance level by entering the received information into a predetermined flight model. The processor then determines, based on a comparison of the calculated current performance level with a predetermined expected performance level, a current level of fuel efficiency. Next, the processor determines any parameter changes for improving fuel efficiency. Finally, the processor causes the determined parameter changes to be displayed on a flight deck display. The flight crew may then selectively implement one or more of the determined parameter changes via the flight deck display.


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