Abstract
Helicopter turbine engines used in the Desert Shield and Desert Storm operations experienced excessive sand ingestion. Fine particles were able to bypass filters and proceed through the combustor or cooling gaspaths. The first-stage turbine vanes were impacted with viscous silicate particles, forming a deposit on the leading-edge root platform and resulting in overheating and oxidation. The chemistry of the raw sand determines that of the ingested powders, the deposits, and the material reactions.
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Smialek, J.L., Archer, F.A. & Garlick, R.G. Turbine airfoil degradation in the persian gulf war. JOM 46, 39–41 (1994). https://doi.org/10.1007/BF03222663
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DOI: https://doi.org/10.1007/BF03222663