A cooling system (10) for cooling electronic aircraft equipment (12) comprises a primary cooling arrangement (14) configured to provide basic cooling energy for cooling the electronic aircraft equipment (12) and a supplemental cooling arrangement (16) configured to provide supplemental cooling energy for cooling the electronic aircraft equipment (12). The supplemental cooling arrangement (16) comprises a coolant supply system (26) and a coolant distribution system (32). The coolant supply system (26) is configured to supply a compressed coolant to the electronic aircraft equipment (12) to be cooled, and the coolant distribution system (32) is configured to selectively direct the compressed coolant supplied by the coolant supply system (26) to at least one of a plurality of components (18) of the electronic aircraft equipment (12).


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    Titel :

    COOLING SYSTEM AND METHOD FOR COOLING ELECTRONIC AIRCRAFT EQUIPMENT


    Weitere Titelangaben:

    KÜHLSYSTEM UND VERFAHREN ZUR KÜHLUNG VON ELEKTRONISCHER FLUGZEUGAUSRÜSTUNG
    SYSTÈME ET PROCÉDÉ POUR LE REFROIDISSEMENT DÉQUIPEMENT ÉLECTRONIQUE D'AÉRONEF


    Beteiligte:
    SCHULT JENS (Autor:in) / WHYTE STEPHEN M (Autor:in)

    Erscheinungsdatum :

    13.11.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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





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