A cooling system for removing heat generated by electrical components onboard aerospace vehicles flows coolant between an evaporator that removes heat from the component, and a condenser within the skin of the vehicle. The skin is formed from facesheets comprising multiple layers of polymer resin reinforced with meshes of single and double wall nanotubes.The nanotubes conduct the heat directionally so as to both distribute the heat over the skin and direct the heat to the outer surface of the skin where the heat can be carried away by air flowing over the skin. The skin may also include conductive carbon foam surrounding the condenser to reduce thermal resistance between the condenser and the facesheets.


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    Titel :

    COOLING SYSTEM FOR AEROSPACE VEHICLE COMPONENTS


    Weitere Titelangaben:

    KÜHLSYSTEM FÜR KOMPONENTEN VON FAHRZEUGEN FÜR LUFT- UND RAUMFAHRT
    SYSTÈME DE REFROIDISSEMENT POUR COMPOSANTS DE VÉHICULE AÉROSPATIAL


    Beteiligte:

    Erscheinungsdatum :

    17.08.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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