A rotorcraft seating assembly includes a seat base supporting a seat bucket (102), the seat base having left- and right- side panel portions. Each side panel portion has a linear bucket guide channel set into its inside face (including an upper portion for adjusting the seat bucket (102) relative to the seat base for pilots of varying heights, and a lower portion for energy attenuation (EA) stroking in response to a crash event) and a bucket guide slot set into its outside face (including a linear upper portion corresponding to the range of adjustment of the seat bucket (102) and a curved lower portion allowing the seat bucket (102) to translate forward and away from the seat base during EA stroking). The curved outer bucket guide slot allows for the required EA stroking distance within a minimal vertical space between the seat bucket (102) and the flight deck floor.


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    Titel :

    COMPACT ROTORCRAFT SEATING ASSEMBLY WITH NON-LINEAR BUCKET GUIDE CHANNELS


    Weitere Titelangaben:

    KOMPAKTE DREHFLÜGLERSITZANORDNUNG MIT NICHTLINEAREN SCHALENFÜHRUNGSKANÄLEN
    ENSEMBLE DE SIÈGE DE GIRAVION COMPACT À CANAUX DE GUIDAGE DE COQUE NON LINÉAIRES


    Beteiligte:
    PACHECO CHAD R (Autor:in) / PEREZ MOISES (Autor:in) / HOOVER DOUGLAS E (Autor:in)

    Erscheinungsdatum :

    10.05.2023


    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



    COMPACT ROTORCRAFT SEATING ASSEMBLY WITH NON-LINEAR BUCKET GUIDE CHANNELS

    PACHECO CHAD / PEREZ MOISES / HOOVER DOUGLAS E | Europäisches Patentamt | 2023

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