Experimental investigation of the onset of sand deposits on Hastelloy-X between 1,000°C and 1,100°C

Deposit formation on turbine hardware in propulsion turbine engines can occur in many arid regions globally. Characterising crystalline deposits on metallic substrates can aid in component resilience and health monitor algorithms during particle ingestion. This study has developed two statistical em...

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Veröffentlicht in:Aeronautical journal 2017-08, Vol.121 (1242), p.1187-1199
Hauptverfasser: Boulanger, A., Hutchinson, J., Ng, W.F., Ekkad, S.V., Keefe, M.J., Xu, W., Barker, B., Hsu, K.
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Sprache:eng
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Zusammenfassung:Deposit formation on turbine hardware in propulsion turbine engines can occur in many arid regions globally. Characterising crystalline deposits on metallic substrates can aid in component resilience and health monitor algorithms during particle ingestion. This study has developed two statistical empirical models for prediction from acquired experimental data for the onset of deposits. The prediction models are for crystalline particulate (Arizona Road Test Dust) deposits on a flat rectangular Hastelloy-X test coupon. Particle impingement angles varied between 20° and 80° in experimental flow temperatures of 1,000–1,100°C. Averaged deposits are methodically quantified through normalised particle deposit tallies per area and percent coverage of the surface using microscopic imaging and image processing programs. Deposit accumulation is a quadratic function of both near-surface coupon temperature and coupon angle.
ISSN:0001-9240
2059-6464
DOI:10.1017/aer.2017.48