A device for deicing a wall of an aircraft, comprising a closed circuit. The closed circuit comprises at least one condenser, positioned in the environment of the wall that is to be deiced, and in which a heat-transfer fluid condenses, generating energy in the form of latent heat which is transmitted to the wall that is to be deiced, at least one evaporator positioned in the environment of a heat source sited remotely with respect to the wall, and in which the heat-transfer fluid evaporates, absorbing energy in the form of latent heat coming from the heat source. At least part of the closed circuit is facing, in contact with, or positioned in, the wall that is to be deiced, being made of a material transparent to electromagnetic fields.


    Access

    Download


    Export, share and cite



    Title :

    SURFACE DEICING DEVICE CONFIGURED NOT TO GENERATE ELECTROMAGNETIC INTERFERENCE


    Contributors:

    Publication date :

    2019-08-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Surface deicing device configured not to generate electromagnetic interference

    CARCONE JONATHAN / ROUX PIERRE-LOUIS | European Patent Office | 2022

    Free access

    Deicing device and deicing method

    CHENG PAN / SUN QIAN / JING XIANGRONG et al. | European Patent Office | 2023

    Free access

    Airplane deicing method and deicing device

    GU XINGSHI / LIU QINGLIN / LIU SENYUN et al. | European Patent Office | 2022

    Free access

    DEICING SUPPORT DEVICE, DEICING SUPPORT METHOD, AND DEICING SUPPORT PROGRAM

    YANAGI KAZUYA | European Patent Office | 2023

    Free access

    Electromagnetic-Repulsion Systems For Deicing Aircraft

    Smith, Samuel O. / Zieve, Peter | NTRS | 1994