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.


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    Title :

    ASYMMETRIC CORE SANDWICH STRUCTURE FOR HEATED FLOOR PANELS


    Contributors:

    Publication date :

    2019-06-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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    HU JIN / CHING NATHANIEL / SLANE CASEY et al. | European Patent Office | 2020

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    HEATED AIRCRAFT FLOOR PANELS

    OWENS GEORGE F / ROACH KEVIN E / MULLEN JAMES et al. | European Patent Office | 2017

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