An energy recovery device (D, D1 to Dn) for an aircraft includes: a turbine (d1) that is provided between a cabin of the aircraft (A1 to A3) and an opening (V) for discharging cabin discharge air from the cabin to the outside of the aircraft and is operated by only the cabin discharge air; and a power generator (d2) that is driven by the turbine (d1).


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    Title :

    ENERGY RECOVERY DEVICE FOR AIRCRAFT


    Additional title:

    ENERGIERÜCKGEWINNUNGSVORRICHTUNG FÜR FLUGZEUG
    DISPOSITIF DE RÉCUPÉRATION D'ÉNERGIE POUR AVION


    Contributors:

    Publication date :

    2022-06-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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