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Thermal strains in passivated aluminum and copper conductor lines

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Abstract

Line width and line thickness thermal strain components in passivated Al and Cu lines were observed to relax much more than the line length strain component. Although the width-to-thickness ratios were large, 3.5 and 4.4 for Al and Cu lines, respectively, the behaviors of the thermal stresses were far from the equibiaxial. Observed changes in deviatoric strains between room temperature and 190 °C for Al and 300 °C for Cu were consistent with a model in which the changes in line width and line thickness strains were simply related to changes in line length strains by the uniaxial Poisson’s ratio. Changes in line length strains were determined by the differences in metal and substrate thermal expansion coefficients and the magnitudes of temperature changes through retained elastic strain coefficients for Al of 30% for heating and for Cu of 60% for heating and 80% for cooling, with the balance accommodated by relaxation.

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Acknowledgments

We thank Dr. C.-K. Hu at the IBM T.J. Watson Research Center for useful guidance and for providing the Cu conductor line samples and Y. Ge from Rensselaer Polytechnic Institute for helpful discussions regarding the analysis. The Al samples were provided by the Intel Corporation. The XRD experiments were carried out on beamline 34-ID of the APS, Argonne National Laboratory, where Dr. W. Liu provided valuable assistance with the synchrotron x-ray microdiffraction measurements and data analysis. Use of the APS was supported by the United States Department of Energy, Office of Science, Office of Basic Energy Sciences, under Contract No. DE-AC02-06CH11357. The present research was supported at Lehigh and Rensselaer Polytechnic Institute by National Science Foundation, Grant DMR-0312189.

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Correspondence to G. Slade Cargill III.

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Zhang, H., Cargill, G.S. & Maniatty, A.M. Thermal strains in passivated aluminum and copper conductor lines. Journal of Materials Research 26, 633–639 (2011). https://doi.org/10.1557/jmr.2011.9

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