A method for controlling an inerting system designed to inject a flow of inert gas into a fuel tank of an aircraft during a mission. The method includes: determining a value of a parameter of the mission of the aircraft at a given moment; determining the ratio between the determined value of the mission parameter and a value at the given moment of an equivalent parameter of a standard mission profile, and deducing a weight coefficient therefrom; using the weight coefficient to weight a value of the inert gas flow rate recommended by the standard mission profile for the value of the equivalent parameter at the given moment so that an appropriate inert gas flow rate to be injected is determined for the needs of the mission at the given moment; and commanding the inerting system to inject the inert gas flow rate determined at the given moment.
PROCEDE DE COMMANDE D'UN SYSTEME D'INERTAGE D'UN RESERVOIR DE CARBURANT, ET SYSTEME D'INERTAGE POUR LA MISE EN OEUVRE DU PROCEDE
2018-07-27
Patent
Electronic Resource
French
European Patent Office | 2018
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