Patent ID: 8437887
Filing Date: 2013-05-07
Classification: G05D,G06Q

Abstract:
1. A method for optimizing fuel consumption of an aircraft during flight, comprising steps of at a given point of a flight: determining, using an onboard computer, a fuel excess relative to a statutory loads depending on a flight profile and weather conditions forecast for rest of the flight, wherein the flight comprises an ascent phase, a cruise phase and a descent phase; if the excess is less than a given value, for at least one of the forthcoming flight phases, adjusting a speed of the aircraft so as to increase the excess; redetermining, using the onboard computer, the fuel excess; and if the excess is still less than a given value, adjusting the speed of the aircraft for another of the at least one forthcoming flight phases, wherein if the excess is less than the given value following the determining step, the aircraft speed for the cruise phase is adjusted; if the excess is still negative following the redetermining step, the speed of the aircraft for the ascent phase is adjusted, then the excess redetermined; if the excess is still negative, the speed of the aircraft for the descent phase is adjusted, then the excess redetermined.