An aircraft includes a fuselage, an aircraft propulsion system including an open rotor, and a pylon mounting the propulsion system to the fuselage. The fuselage includes an acoustic panel configured to attenuate noise generated by the open rotor.


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    Title :

    Noise attenuation for an open rotor aircraft propulsion system


    Contributors:

    Publication date :

    2017-04-25


    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



    NOISE ATTENUATION FOR AN OPEN ROTOR AIRCRAFT PROPULSION SYSTEM

    ALONSO-MIRALLES JOSE S / YU JIA | European Patent Office | 2017

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    KINGAN MICHAEL | European Patent Office | 2017

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