An aircraft cushion includes a lower portion, upper portion, and forward portion of foam. The lower portion is configured to be located by a forward frame element (e.g., tube) and to be supported by the forward frame element and a seat diaphragm (e.g., stretched fabric). The upper portion and forward portion are softer for user comfort. The lower portion, using a shape of the foam (e.g., structural foam), may removably snap onto the forward frame element, and rotate down into place for ease of installation.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HYBRID BOTTOM SEAT CUSHION


    Beteiligte:

    Erscheinungsdatum :

    2023-12-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    CUSHION SKIN, SEAT CUSHION, AND VEHICLE SEAT

    TAKAZAWA SYUNJI / HASUMI HIDEKI / KAGEYAMA ATSUSHI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    SEAT CUSHION AND VEHICULAR SEAT COMPRISING THE SEAT CUSHION

    TAKAHASHI TOSHIHIKO | Europäisches Patentamt | 2023

    Freier Zugriff

    SEAT CUSHION

    BAN MOMOKO | Europäisches Patentamt | 2023

    Freier Zugriff

    SEAT CUSHION

    TABATA TSUYOSHI / KAMATA HIDEKI | Europäisches Patentamt | 2018

    Freier Zugriff

    SEAT CUSHION

    SUGIURA TAKESHI | Europäisches Patentamt | 2017

    Freier Zugriff