Disclosed examples include a structurally integrated thermal management system that uses the structure of an aerospace vehicle as part of the heat dissipation system. In this system, structural elements of the aerospace vehicle function as a thermal bus, and are thermally connected with heat-generating electrical components, so that heat from those components is directed away from the component by the structure of the vehicle itself, into lower temperature surfaces of the vehicle.


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    Titel :

    STRUCTURALLY INTEGRATED THERMAL MANAGEMENT SYSTEM FOR AEROSPACE VEHICLES


    Weitere Titelangaben:

    STRUKTURINTEGRIERTES THERMOMANAGEMENTSYSTEM FÜR LUFT- UND RAUMFAHRZEUGE
    GESTION THERMIQUE POUR VÉHICULES AÉROSPATIAUX


    Beteiligte:
    BLANDING DAVID E (Autor:in) / MULEY ARUN (Autor:in) / COFFMAN JEFFREY C (Autor:in) / VAN AFFELEN DOUG (Autor:in)

    Erscheinungsdatum :

    2019-09-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64G Raumfahrt , COSMONAUTICS



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