Herein provided are methods and systems for assessing a fuel burn level of an aircraft for a planned mission. Flight information relating to the planned mission is obtained via a graphical user interface, the flight information comprising configurable number of passengers for the aircraft. A requisite engine bleed level for the planned mission is determined based on the flight information. The fuel burn level is assessed based on the requisite engine bleed level.
METHODS AND SYSTEMS FOR ASSESSING FUEL BURN LEVELS IN AIRCRAFT
2020-10-22
Patent
Electronic Resource
English
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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