The invention relates to an air system for an aircraft, that includes air consumers; air sources and a network of ducts and associated control valves controlled by a control unit. The air system is characterized in that: the network of ducts and associated valves includes at least one isolation valve, arranged between an air bleed device and an air duct connecting an air conditioning pack and an auxiliary power unit; the control unit is configured to be able to determine an ideal configuration of the control valves according to the identified requirements of each consumer and a degraded configuration that makes it possible to supply air to predetermined air consumers from the available air sources when the ideal configuration is not attainable.


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    Title :

    SYSTEME D'ALIMENTATION PNEUMATIQUE DISTRIBUÉ D'UN AERONEF


    Additional title:

    DISTRIBUTED PNEUMATIC POWER SUPPLY SYSTEM FOR AN AIRCRAFT
    VERTEILTES PNEUMATISCHES VERSORGUNGSSYSTEM EINES LUFTFAHRZEUGS


    Contributors:

    Publication date :

    2025-06-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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