An aircraft with a motor bay is described; a motor system with a discharge duct; a heat exchanger arranged outside said motor system; a first air intake; a first duct along which the heat exchanger is arranged; a first converging nozzle having a downstream section fluidically connected with the discharge duct and with the first duct so as to create a first flow rate of air adapted to cool the heat exchanger; and a second air intake that is open in the motor bay and distinct from the first air intake; a second converging nozzle having a second downstream section fluidically connected with the discharge duct and with the motor bay, so as to create a second flow rate of cooling air of the motor bay directed from the second air intake towards the discharge duct and by-passing the motor system.


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    Title :

    AIRCRAFT CAPABLE OF HOVERING


    Contributors:

    Publication date :

    2023-05-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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