An aircraft seat assembly including first and second stanchions (202) forming interior spaces (204) open through forward slots (208). A seat pan (206) is pivotally attached to the stanchions (202) and includes rearward extensions (212) that extend through the forward slots (208) and are received in the interior spaces (204). First and second spring mechanisms (218) reside in the respective first and second interior spaces (204) and are attached at opposing ends to their respective stanchion (202) and to the seat pan (206). In use, rotating the seat pan (206) toward a deployed position elongates the first and second elongation springs (220) thereby energizing a return force of the spring mechanisms.


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    Titel :

    AIRCRAFT SEAT WITH INTERNAL SEAT PAN RETURN SPRING MECHANISM


    Weitere Titelangaben:

    FLUGZEUGSITZ MIT INNEREM SITZSCHALENRÜCKSTELLFEDERMECHANISMUS
    SIÈGE D'AÉRONEF AVEC MÉCANISME DE RAPPEL DE DOSSIER DE SIÈGE INTERNE


    Beteiligte:
    DAY MARTIN SHAWN (Autor:in) / PACHECO CHAD R (Autor:in) / FOISIE DOUGLAS A (Autor:in)

    Erscheinungsdatum :

    2024-04-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60N SEATS SPECIALLY ADAPTED FOR VEHICLES , Sitze besonders für Fahrzeuge ausgebildet



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