The patent application describes a lightweight, low cost, collapsible, side-facing seat construction for troop carrying aircraft designed to attenuate crash load forces in an improved manner. A fabric seat sling depending from a support strap assembly is suspended via energy absorbing devices from an aircraft overhead frame structure and is supported by a simple pivoted strut assembly secured to the aircraft floor structure. Shoulder and lap safety belts are secured through the seat by tie-down straps angled outwardly from both sides of the seat directly to the aircraft floor for increased occupant safety and anti-sway resistance. A minimum of rigid, heavy, relatively expensive compression-carrying structural members is thus utilized in this unique seat while providing maximum comfort and safety to its occupant.


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    Titel :

    Crash Load Attenuating Troop Seat


    Beteiligte:
    M. J. Reilly (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Crash Load Attenuating Troop Seat

    M. J. Reilly | NTIS | 1975


    Cash Load Attenuating Troop Seat

    M. J. Reilly | NTIS | 1973


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