4.4 Article

Residual stresses and thermal fatigue in CrN hard coatings characterized by high-temperature synchrotron X-ray diffraction

Journal

THIN SOLID FILMS
Volume 518, Issue 8, Pages 2090-2096

Publisher

ELSEVIER SCIENCE SA
DOI: 10.1016/j.tsf.2009.08.011

Keywords

X-ray diffraction; Chromium nitride; Stress; Physical vapor deposition; Thermal fatigue

Funding

  1. Austrian Science Fund FWF
  2. European Community-Research Infrastructure Action [R II 3-Cr-2004-506008]
  3. Christian Doppler Society
  4. PLANSEE

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The aim of this work is to analyze thermal fatigue in hard coatings/substrate composites (i) during slow heating and cooling and (ii) after local cyclic thermal laser pulse experiments. As a model system, CrN coatings with a thickness of 3 mu m deposited on steel, hard metal and Si(I 00) substrates using reactive magnetron sputtering at a temperature of 350 degrees C are used. The coatings are at first characterized by means of in-situ high-temperature X-ray diffraction (XRD) using a commercially available temperature attachment and by applying heating and cooling rates of less than 0.3 degrees C/s. The treatment results in the expected reduction of intrinsic stresses which are independent of substrate material but strongly influenced by substrate roughness. To simulate local thermal fatigue, selected coating/substrate composites are thermally cycled using a laser beam of 6 mm in diameter in a temperature range of 50-850 degrees C applying up to 10(4) cycles and using heating and cooling rates of about 10(3) degrees C/s. Subsequently, laser cycled samples are analyzed using synchrotron XRD, scanning electron microscopy and focused ion beam technique. Laser pulses cause a reduction of compressive stresses in the coatings and a development of tensile stresses in the substrates accompanied by formation of cracks and ripples. The results show that the changes of the local macro- and micro-strains/stresses in the coatings and in the underlying substrates are strongly interlinked. The stress relaxation in the coatings is caused by recovery effects, by micro-cracks formed in the tensely-stressed coating and by plastic deformation of the metallic substrates. (C) 2009 Elsevier B.V. All rights reserved.

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