A thermal management system is provided. The thermal management system includes a housing extending between a leading end and a trailing end. The housing includes a cooling structure defining at least one inlet, at least one outlet, and a duct coupled in flow communication between the at least one inlet and the at least one outlet. The cooling structure is configured to generate a fluid flow from the at least one inlet to the at least one outlet through the duct in response to the housing moving through a fluid. The thermal management system further includes an electronics assembly disposed in contact with the cooling structure. The cooling structure is configured to transfer heat generated by the electronics assembly to the fluid moving through the duct to cool the electronics assembly.


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    Title :

    SYSTEMS AND METHODS FOR THERMAL MANAGEMENT OF EXTERNALLY MOUNTED ELECTRONIC EQUIPMENT FOR AN AIRCRAFT


    Additional title:

    SYSTEME UND VERFAHREN ZUR WÄRMEVERWALTUNG EINER EXTERN MONTIERTEN ELEKTRONISCHEN AUSRÜSTUNG FÜR EIN FLUGZEUG
    SYSTÈMES ET PROCÉDÉS DE GESTION THERMIQUE D'ÉQUIPEMENT ÉLECTRONIQUE MONTÉ À L'EXTÉRIEUR POUR UN AÉRONEF


    Contributors:

    Publication date :

    2024-08-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H05K PRINTED CIRCUITS , Gedruckte Schaltungen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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