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


    Access

    Download


    Export, share and cite



    Title :

    Cooling system for cooling electronic aircraft equipment, aircraft equipped with a cooling system for cooling electronic aircraft equipment and method for cooling electronic aircraft equipment


    Contributors:

    Publication date :

    2018-01-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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




    COOLING SYSTEM AND METHOD FOR COOLING ELECTRONIC AIRCRAFT EQUIPMENT

    SCHULT JENS / WHYTE STEPHEN M | European Patent Office | 2019

    Free access

    Aircraft equipment cooling

    ISHIDA TOSHIYUKI / UEFUJI YOICHI / MORISHITA MASATOSHI et al. | European Patent Office | 2017

    Free access

    Aircraft cooling system and aircraft with aircraft cooling system

    KLIMPEL FRANK | European Patent Office | 2022

    Free access

    AIRCRAFT COOLING SYSTEM AND AIRCRAFT WITH AIRCRAFT COOLING SYSTEM

    KLIMPEL FRANK | European Patent Office | 2019

    Free access