Characterization and failure analysis of a polymeric clamp hanger component
Contents |
Abstract
This paper characterizes the failure of a polymeric clamp hanger component using finite element analysis coupled with experimental methods such as scanning electron microscopy, x-ray computed tomography, and mechanical testing. Using Fourier transform infrared spectroscopy, the material was identified as a polypropylene. Internal porosity that arose from the manufacturing procedure was determined using three dimensional x-ray computed tomography. From static mechanical experiments, the forces applied on the component were determined and used in a finite element simulation, which clearly showed the process of fracture arising from the pre-existing processing pores. The fracture surfaces were observed under a scanning electron microscope confirming the finite element simulation results illustrating that low-cycle fatigue fracture occurred in which the fatigue cracks nucleated from the manufacturing porosity.
Figures
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| Picture of product and fractured component: (a) clamp hanger and (b) fractured polymer grip. | |
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| ESEM image of fractured surface: (a) magnification of the central pore; (b) overall fracture surface; and (c) and discolored edge. | ||
The FTIR spectrum of the specimen used in this study with the characteristic transmittance bands matching those of isotactic polypropylene (iso-PP)
Estimated normal load at various rod positions during closure.
Compressive stress–strain response of the polypropylene clasp.
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| Solid models for finite element analysis: (a) without pores, whole model and (b) with pores, cross-section of model to show pores. | |
Cross-section of the coarse mesh containing pores. The stress is applied at Area #1 while Area #3 is fixed in the x- and y-directions. The Area #2 denotes the artificially created pores to mimic the micro CT findings.
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| High fidelity meshes in the curved region of the model for both non-pore and pore cases: (a) without pores and (b) with pores. | |
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| Clipped models showing: (a) stress triaxiality without pores; (b) stress triaxiality with pores; (c) von Mises stress without pores; and (d) von Mises stress with pores. | |||
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| An isosurface of triaxiality for meshes (a) without pores and (b) with pores. The isosurface is shown in green and represents a triaxiality value of 0.6 | |
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The figures of this page was reproduced with permission from Elsevier/Rights Link Order No. 501116679.

