An airflow exhaust system for delivering exhaust produced from a fuel cell to optimize aircraft performance. Exhaust is distributed using a conduit network and released through outlets on the aircraft skin to provide boundary layer control for the aircraft. A control system distributes exhaust for boundary layer control, actuator control, and propulsion.


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    Title :

    EXHAUST AIRFLOW SYSTEM


    Additional title:

    ABLUFTSTRÖMUNGSSYSTEM
    SYSTÈME D'ÉCOULEMENT D'AIR D'ÉCHAPPEMENT


    Contributors:
    BLA MOCAN (author)

    Publication date :

    2024-12-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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