An electronics cooling system (100) for an aircraft includes a heat exchanger (101) comprising a coolant circuit (103), an air circuit (105) and a fuel circuit (107) such that each of the circuits is in thermal communication with the other circuit. The coolant circuit (103) is in thermal communication with one or more aircraft electronics. The air circuit (105) is fluidly connectable with at least one air source,.The fuel circuit (107) is fluidly connectable with a fuel tank (111) between the fuel tank (111) and an engine of the aircraft and/or fluidly connectable with a fuel loop that returns to the fuel tank (111).


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT ELECTRONICS THERMAL REGULATION SYSTEM


    Additional title:

    THERMISCHES REGELUNGSSYSTEM FÜR DIE ELEKTRONIK EINES FLUGZEUGS
    SYSTÈME DE RÉGULATION THERMIQUE DE L'ÉLECTRONIQUE D'UN AÉRONEF


    Contributors:

    Publication date :

    2020-02-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F28D Wärmetauscher, soweit in keiner anderen Unterklasse vorgesehen, in denen die Wärmetauschmittel nicht in direkte Berührung miteinander kommen , HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT



    Aircraft electronics thermal regulation systems

    PAL DEBABRATA | European Patent Office | 2022

    Free access

    AIRCRAFT ELECTRONICS THERMAL REGULATION SYSTEMS

    PAL DEBABRATA | European Patent Office | 2020

    Free access

    Aircraft electronics thermal regulation systems

    PAL DEBABRATA | European Patent Office | 2019

    Free access

    AIRCRAFT ELECTRONICS THERMAL REGULATION SYSTEMS

    PAL DEBABRATA | European Patent Office | 2018

    Free access

    Light-aircraft electronics

    Engineering Index Backfile | 1967