In an intake structure of an aircraft that takes in air from a front side of an airframe, a bump is provided on a surface of the airframe of the aircraft at a portion immediately before an intake. The bump is formed so as to smoothly protrude from the front side of the airframe while having a width that is wider than a width of the intake.


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    Titel :

    Intake structure of aircraft


    Beteiligte:
    SATO KAZUSHIGE (Autor:in) / ISO HIDEO (Autor:in) / OSUKA TAKESHI (Autor:in)

    Erscheinungsdatum :

    22.05.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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