A light aircraft cabin containing a seat and anthropometric dummy was subjected to a vertical deceleration to simulate a minor crash. Several alternatives seats were used, all typical of those in light aircraft. The tests showed that with most seats a moderate rate of desert (5 m/s) could produce potentially injurious forces in the spine, but one seat limited the forces to a safe value. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Simulated Crash Decelerations in a Light Aircraft Cabin


    Beteiligte:

    Erscheinungsdatum :

    1983


    Format / Umfang :

    42 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    Aircraft cabin light systems

    TIMM BIRGER / ANTONCZYK VOLKER / HEINE HENRIK | Europäisches Patentamt | 2016

    Freier Zugriff

    AIRCRAFT CABIN LIGHT SYSTEM

    TIMM BIRGER / ANTONCZYK VOLKER / HEINE HENRIK | Europäisches Patentamt | 2015

    Freier Zugriff