Aircraft passenger seat (2), wherein the aircraft passenger seat (2) has a frame (5), a seat surface group (11, 31) and a backrest element (12), wherein the seat surface group (11, 31) has a seat surface element (32), wherein the seat surface element (32) provides a seat surface on which a user of the aircraft passenger seat (2) can directly sit, wherein the seat surface group (11, 31) has a winding element (16, 34) and a first winding shaft (17, 35), wherein a first end of the winding element (16, 34) is connected to the first winding shaft (17, 35), wherein the first winding shaft (17, 35) is rotatable about a first winding axis, wherein, as the first winding shaft (17, 35) rotates around the first winding axis, the winding element (16, 34) can be wound up onto the first winding shaft (17, 35) or can be unwound from the first winding shaft (17, 35) in the region of the first end of the winding element (16, 34), wherein the seat surface element (32) is connected to the winding element (16, 34), so that the seat surface element (32) is moved as the first winding shaft (17, 35) rotates.


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    Titel :

    FLUGGASTSITZ


    Weitere Titelangaben:

    AIRCRAFT PASSENGER SEAT
    SIÈGE PASSAGER D'AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    04.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Deutsch


    Klassifikation :

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



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