The invention relates mainly to a seat (10) intended for being installed in an aircraft, comprising: a backrest (13); a seat portion (12) rotatably mounted about an axis (X) relative to said backrest (13) between an extended position and a folded position; a return system (16) capable of automatically moving the seat portion (12) from the extended position to the folded position; and a mechanical system (17) for reducing the speed of the seat portion (12), comprising: a cam-shaped plate (22) and a roller (21) capable of moving along an edge (23) of said cam-shaped plate (22) during a movement of said seat portion (12) from said extended position to said folded position generated by said return system (16), at least one of the two elements, among said roller (21) and said cam-shaped plate (22), being capable of compressing during the movement of the roller (21) so as to absorb kinetic energy of said seat portion (12) in order to reduce the movement speed thereof.


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    Titel :

    SIEGE D'AERONEF MUNI D'UN SYSTEME MECANIQUE DE REDUCTION DE VITESSE D'ASSISE


    Weitere Titelangaben:

    AIRCRAFT FOLDING SEAT WITH MECHANICAL SYSTEM FOR DAMPER THE SEAT RETRACTION
    FLUGZEUGKLAPPSITZ MIT MECHANISCHER VORRICHTUNG ZUR DÄMPFUNG DER KLAPPBEWEGUNG


    Beteiligte:
    MESAROS ALEXANDRE (Autor:in) / LEBEGUE BRICE (Autor:in) / LAVAL JORDI (Autor:in)

    Erscheinungsdatum :

    2019-07-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60N SEATS SPECIALLY ADAPTED FOR VEHICLES , Sitze besonders für Fahrzeuge ausgebildet / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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