a comparative study on theoretical and experimental strengths of padeyes under in-plane loads

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A comparative study on theoretical and experimental strengths of padeyes under in-plane loads

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  • Proceedings of the Fourth (1994) Internationai Offshore and Polar Engineering ConferenceOsaka, Japan, April 10-15, 1994Copyright 1994 by The International Society of Offshore and Polar EngineersISBN 1-880653-10-9 (Set); ISBN 1-880653-11-7 (VoL I)

    A Comparative Study on Theoretical and Experimental Strengthsof Padeyes Under In-Plane Loads

    Y.S. Choo, K.C. Choi and K.B. LeeNational University of Singapore

    Singapore

    Padeyes and pin-eonnections are commonly used as lifting

    components in onshore and offshore installation. Despite of their apparent

    geometric simplicity, the nonlinear elasto-plastic behaviour of padeyes under

    increasing loading is complex. Present design approaches normally limit the

    maximum elastic stresses calculated from simplified equations to within

    allowable stress limits and are very stringent on the pin-hole tolerance.

    This paper presents parametric results for padeyes subjected to in-plane

    quasi-static loads using nonlinear finite element analyses and a simple

    graphical plot which facilitates the evaluation of padeye strength in relation

    to its geometric ratios. The current results are shown to correlate closely

    with published experimental results and provide better correlation than some

    standard design equations. The effect of different padeye shapes, for the

    parametric range investigated, is found to have marginal influence on

    strength. The reduction in ultimate strength of padeyes with large pinlhole

    tolerance is significantly lower than predicted by elastic theory due to stress

    redistribution within the padeye plate.

    KEYWORDs: Padeyes, pin-eonnections, strength comparison, nonlinear

    behaviour, finite element analysis, design codes

    NOMENCLATUREa "Loaded-edge" distance along the line of load P referenced from the

    hole centre-line = L (see Fig. 1)a' "Loaded-edge" distance along the line of load P, measured from

    edge of hole (see Fig 1)be "Unloaded-edge" distance, measured from the side of hole to the

    edge of padeye (see Fig. 1)C, Strength reduction ratio = p / P'"