Abstract
In a previous paper, the corrosion fronts of typical Type II corrosion pits observed on field parts were examined using the high-resolution transmission electron microscopy technique. A mixture of nanosized sulfides and oxides was observed in the pits, which suggests a solid-phase corrosion propagation process. In the present work, the corrosion products atop of the original alloy surface were characterized with an aim to understand the corrosion initiation process. A typical layered oxide structure was revealed comprising alternated NiO-rich and alumina-rich layers. Importantly, aluminum sulfate Al2(SO4)3 was found to be present in the alumina-rich layers by chemistry and diffraction analyses. The co-existence of aluminum sulfate with alumina suggests that the original protective alumina-rich layer was likely attacked by a solid reaction under the unique aeroengine operation environment. No indication of molten NiSO4-Na2SO4 mixture was identified in the corrosion pits or at the original metal/gas surface. The potential causes of lack of molten sulfate formation were discussed.
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Acknowledgments
This work was partially supported by the Office of Naval Research under Contract N00014-16-C-2002 with David A. Shifler as the program manager.
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Manuscript submitted July 17, 2020, accepted January 28, 2021.
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Zhang, WJ., Sharghi-Moshtaghin, R. Understanding the Type II Corrosion Mechanism. Metall Mater Trans A 52, 1492–1502 (2021). https://doi.org/10.1007/s11661-021-06168-x
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DOI: https://doi.org/10.1007/s11661-021-06168-x