A six-axis femoral load cell was designed, fabricated, calibrated and tested in an ATD upper leg. It has linear characteristics with adequate output and dynamic response. Its output compared well with that of load cells mounted behind a knee bolster which was impacted by an ATD instrumented with this load cell. Although the axial load was found to be well below the present limit of FMVSS208, the bending moments were found to be high. A conservative tolerance limit for axial load should be considered and cadaver data are required.


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    Titel :

    Femoral Loads Measured by a Six-Axis Load Cell


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    King, A. I. (Autor:in) / Cheng, R. (Autor:in) / Denton, R. A. (Autor:in)

    Kongress:

    23rd Stapp Car Crash Conference ; 1979



    Erscheinungsdatum :

    1979-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Femoral Loads Measured by a Six-Axis Load Cell

    Cheng,R. / Denton,R.A. / King,A.I. et al. | Kraftfahrwesen | 1979


    Three-Axis Load-Cell Assembly

    Rewerts, G. R. | NTRS | 1986


    Analysis of Measured In-Flight Tail Loads

    Van Gelder, P. A. | British Library Online Contents | 1996


    Analysis of Measured In-Flight Tail Loads

    Van Gelder, P. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1996


    Analysis of Measured In-Flight Tail Loads

    P. A. van Gelder | NTIS | 1996