A composite sandwich structure for heating an environment includes a first core layer made from a first cellular material and having a first thickness, and a second core layer made from a second cellular material and having a second thickness less than the first thickness. The structure further includes a heating layer having a thermoelectric heating element and disposed between the first and second core layers. The first core layer is positioned between the heating layer and the environment.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ASYMMETRIC CORE SANDWICH STRUCTURE FOR HEATED FLOOR PANELS


    Beteiligte:
    HU JIN (Autor:in) / CHING NATHANIEL (Autor:in) / OWENS GEORGE F (Autor:in) / SLANE CASEY (Autor:in) / BOTURA GALDEMIR CEZAR (Autor:in) / HEIN BRANDON (Autor:in) / MULLEN JAMES A (Autor:in)

    Erscheinungsdatum :

    13.06.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung



    HEATED FLOOR PANELS

    HU JIN / CHING NATHANIEL / SLANE CASEY et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    HEATED FLOOR PANELS

    HU JIN / CHING NATHANIEL / SLANE CASEY et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    HEATED FLOOR PANELS

    CHING NATHANIEL / HU JIN / SLANE CASEY | Europäisches Patentamt | 2020

    Freier Zugriff

    HEATED FLOOR PANELS

    HU JIN / CHING NATHANIEL / SLANE CASEY et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    HEATED AIRCRAFT FLOOR PANELS

    OWENS GEORGE / ROACH KEVIN E / MULLEN JAMES et al. | Europäisches Patentamt | 2019

    Freier Zugriff