High-temperature gas exhausted to outside of an aircraft including exhaust air from an air conditioner is prevented from thermally influencing an airframe. An aircraft includes, in an airframe, an exhaust port configured to exhaust, to outside of the aircraft, high-temperature gas that flows through an exhaust duct provided in an air conditioner and has temperature higher than allowable temperature of GFRP used as a material of a fairing, and a partition as a turning reduction portion configured to reduce a turning component contained in flow of the high-temperature gas before the high-temperature gas is exhausted to the outside of the aircraft.


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    Title :

    AIRCRAFT, AND AIRCRAFT MAINTENANCE METHOD


    Contributors:

    Publication date :

    2020-01-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



    AIRCRAFT AND AIRCRAFT MAINTENANCE METHOD

    HARA NOBUHIDE | European Patent Office | 2020

    Free access

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