METHOD AND ELECTRONIC DEVICE FOR DETERMINING AT LEAST ONE FUEL CONSUMPTION DOMAIN FOR AN AIRCRAFT, RELATED COMPUTER PROGRAM AND ELECTRONIC DISPLAY SYSTEM

It comprises, for at least one flight phase, calculating a consumption limit curve as a function of the altitude and the propulsion variable, corresponding to a forecasted average consumption for said flight phase; and determining-from the flight envelope and the limit curve-the consumption domain a...

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Bibliographische Detailangaben
Hauptverfasser:	HAURET, Daniel, MENNECHET, Florent, SERVANTIE, Xavier
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS MEASURING MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUIDLEVEL METERING BY VOLUME PARACHUTES PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	It comprises, for at least one flight phase, calculating a consumption limit curve as a function of the altitude and the propulsion variable, corresponding to a forecasted average consumption for said flight phase; and determining-from the flight envelope and the limit curve-the consumption domain as a function of the altitude and the propulsion variable and including a first consumption subdomain lower than the forecasted consumption for said flight phase and a second consumption subdomain greater than said forecasted consumption, the first and second subdomains being separated by the limit curve.