An aircraft cooling system includes: a rotor capable of generating thrust in a vertical direction; a heat generating member disposed below the rotor; a support member (a boom) that supports the heat generating member; a structure (a second fairing) protruding from the support member toward the rotor; and a heat exchanger (a surface heat exchanger) provided in the structure. A refrigerant heated by the heat generating member is introduced to an inlet (a fairing inlet) provided in the heat exchanger, and the refrigerant cooled by the heat exchanger is supplied to the heat generating member from an outlet (a fairing outlet) provided in the heat exchanger.


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    Title :

    AIRCRAFT COOLING SYSTEM AND AIRCRAFT


    Contributors:

    Publication date :

    2024-09-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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