The patent relates to a novel and improved system for restraining the pilot or occupant in a seat during an emergency situation. The improved system includes a lever assembly which, when operated, draws opposite ends of a lap belt downwardly and forwardly so as to minimize the tendency of the pilot to submarine under the belt.


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    Titel :

    Aircraft Seat Restraint Tensioning Mechanism


    Beteiligte:
    H. Noble (Autor:in) / E. H. Hartel (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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