An electronics cooling system for an aircraft includes a heat exchanger comprising a coolant circuit, an air circuit, and a fuel circuit such that each of the circuits is in thermal communication with at least one of the other circuits. The coolant circuit is in thermal communication with one or more aircraft electronics. The air circuit is in fluid communication with at least one air source. The fuel circuit is in fluid communication with a fuel tank between the fuel tank and an engine of the aircraft.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft electronics thermal regulation systems


    Contributors:

    Publication date :

    2022-03-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION



    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

    AIRCRAFT ELECTRONICS THERMAL REGULATION SYSTEM

    PAL DEBABRATA | European Patent Office | 2020

    Free access

    Light-aircraft electronics

    Engineering Index Backfile | 1967