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:
Sep. 24, 2019

Filed:

Mar. 08, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

David Garrido-Lopez, Tres Cantos, ES;

Maxim Constantijn Vos, Madrid, ES;

Johan De Prins, Molenstede, BE;

Anne Jacqueline Gertruda Theodora Scholtes, Delft, NL;

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G08G 5/00 (2006.01); G06Q 10/04 (2012.01); G07C 5/08 (2006.01); G07C 5/12 (2006.01);
U.S. Cl.
CPC ...
G08G 5/0039 (2013.01); G06Q 10/047 (2013.01); G07C 5/085 (2013.01); G07C 5/12 (2013.01); G08G 5/0034 (2013.01); G08G 5/0091 (2013.01);
Abstract

A method and electronic device for providing an optimal quantity of aircraft fuel. The method comprises collecting recorded flight data from past flights of an aircraft; determining aircraft specific performance correction parameters per flight phase, using the recorded flight data; collecting a flight plan of the aircraft; determining the total fuel required for the given flight plan, using the aircraft specific performance correction parameters; determining a single synthetic drag factor (ϵ) and a single synthetic fuel factor (ϵ) that, when used by the aircraft FMS, yield the said total fuel required for the given flight plan; receiving an estimated total fuel required determined by the aircraft FMS based on the flight plan, the single synthetic drag factor (ϵ) and the single synthetic fuel factor (ϵ). The method allows reducing the fuel weight and total flight cost, and is particularly advantageous for FMS which only admit one single drag factor and one single fuel factor.


Find Patent Forward Citations

Loading…