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 loadsTRANSCRIPT
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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'"