An aircraft seat includes infinitely adjustable, lateral tilt control within a specified range. The aircraft seat includes a stationary support, a tilting frame rotatably or translatably attached to the stationary base, and a tilt control mechanism to adjust the tilt within the defined range and positively lock the frame without back-driving. The tilt control mechanism may include a plurality of linkages connected to the stationary support and the tilting frame, and to each other via a threaded block; a threaded shaft adjusts the linkages and thereby adjust the tilt. Alternatively, the tilt control mechanism comprises a curved rack and a pinion. The threaded block and threaded shaft, or the rack and pinion define ACME threads to prevent back-driving.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Side to side tilting aircraft seat mechanism


    Beteiligte:

    Erscheinungsdatum :

    14.02.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    SIDE TO SIDE TILTING AIRCRAFT SEAT MECHANISM

    HOOVER DOUGLAS E | Europäisches Patentamt | 2022

    Freier Zugriff

    SIDE TO SIDE TILTING AIRCRAFT SEAT MECHANISM

    HOOVER DOUGLAS | Europäisches Patentamt | 2022

    Freier Zugriff

    Side cushion tilting system of vehicle seat cushion

    SONG JAE-YEOL / CHOI HAE-TAE / SONG CHAE-SEONG et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Side bolster tilting system of vehicle seat cushion

    SONG JAE YEOL / CHOI HAE TAE / SONG CHAE SUNG et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    SIDE BOLSTER TILTING SYSTEM OF VEHICULAR SEAT CUSHION

    SONG JAE-YEL / CHOI HAI-TAI / SONG CHAE-SUNG et al. | Europäisches Patentamt | 2020

    Freier Zugriff