An aircraft cooling system includes a first coolant stream which cools at least one first heat load and a second coolant stream which cools at least one second heat load. The aircraft cooling system is formed such that the first heat load and the second heat load are thermally coupled together. The first heat load and the second heat load can be formed by two mutually redundant aircraft components. A third coolant stream thermally couples the first heat load and the second heat load together. The third coolant stream can be cooled by a heat sink, such as the outer skin of the aircraft in a bilge region.


    Access

    Download


    Export, share and cite



    Title :

    Redundant aircraft cooling system for redundant aircraft components


    Contributors:

    Publication date :

    2015-09-29


    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 / F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS / F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION



    Redundant Transmitting System in Aircraft (RTSA)

    Chanda, Nivedita | SAE Technical Papers | 2015


    Redundant Transmitting System in Aircraft (RTSA)

    Chanda, Nivedita | British Library Conference Proceedings | 2015


    Aircraft having redundant directional control

    OLDROYD PAUL K / MCCULLOUGH JOHN RICHARD | European Patent Office | 2020

    Free access

    Aircraft having Redundant Directional Control

    OLDROYD PAUL K / MCCULLOUGH JOHN RICHARD | European Patent Office | 2018

    Free access

    AERODYNAMIC REDUNDANT ACTUATION SYSTEM FOR AIRCRAFT

    BOWERS BRET ALAN / EVOY SCOTT THOMAS | European Patent Office | 2021

    Free access