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

Part of: ISABE 2017

Published online by Cambridge University Press:  21 June 2017

A. Boulanger ,
J. Hutchinson ,
W.F. Ng ,
S.V. Ekkad ,
M.J. Keefe ,
W. Xu ,
B. Barker  and
K. Hsu
A. Boulanger*
Affiliation:
Virginia Tech, College of Engineering, Department of Mechanical Engineering, Blacksburg, VirginiaUS
J. Hutchinson
Affiliation:
Virginia Tech, College of Engineering, Department of Mechanical Engineering, Blacksburg, VirginiaUS
W.F. Ng
Affiliation:
Virginia Tech, College of Engineering, Department of Mechanical Engineering, Blacksburg, VirginiaUS
S.V. Ekkad
Affiliation:
Virginia Tech, College of Engineering, Department of Mechanical Engineering, Blacksburg, VirginiaUS
M.J. Keefe
Affiliation:
Virginia Tech, College of Science, Department of Statistics Blacksburg, VirginiaUS
W. Xu
Affiliation:
Virginia Tech, College of Science, Department of Statistics Blacksburg, VirginiaUS
B. Barker
Affiliation:
Rolls Royce Corp., Indianapolis, IndianaUS
K. Hsu
Affiliation:
Rolls Royce Corp., Indianapolis, IndianaUS
*
[email protected]
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Abstract

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.

Keywords

SanddepositionturbinesArizona Road Dust
Type
Research Article
Information
The Aeronautical Journal , Volume 121 , Special Issue 1242: The International Society of Air-breathing Engines (ISABE) 2017 Conference Special Issue , August 2017 , pp. 1187 - 1199
Copyright
Copyright © Royal Aeronautical Society 2017 

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Footnotes

This paper will be presented at the ISABE 2017 Conference, 3-8 September 2017, Manchester, UK.

References

REFERENCES

1. Gabbard, C.B., LeLevier, R.E. and Parry, J.F.W. Dust-Cloud Effects on Aircraft Engines—Emerging Issues and New Damage Mechanisms, Defense Technical Information Archive, 1982, Defense Nuclear Agency, Washington, D.C., US.Google Scholar
2. Whittle, R. “Fatal Crash Prompts Marines to Change Osprey Flight Rules,” Breaking Defense, available at http://breakingdefense.com/2015/07/fatal-crash-prompts-marines-to-change- osprey-flight-rules/ (accessed 15 August 2016, 16 July 2015.Google Scholar
3. Cowherd, C. Sandblaster 2 Support of See-Through Technologies for Particulate Brownout Task 5 Final Technical Report, Report No. 110565.1.005, 2007, U.S. Army Aviation and Missile Command, Arlington, Virginia, US.Google Scholar
4. Smialek, J.L. The Chemistry of Saudi Arabian Sand—A Deposition Problem on Helicopter Turbine Airfoils, NASA TM-105234, 1991, NASA, Cleveland, Ohio, US.Google Scholar
5. Smialek, J.L., Archer, F.A. and Garlick, R.G. Turbine airfoil degradation in the Persian Gulf war, J Minerals, Metals & Materials Society, 1994, 46, (12), pp 39–41.CrossRefGoogle Scholar
6. Kim, J., Dunn, M.G. and Baran, A.J. The “Most Probable” Dust Blend and Its Response in the F-100 Hot Section Test System (HSTS), DNA-TR-91-160, 1992, Defense Nuclear Agency, Alexandria, Virginia, US.Google Scholar
7. Song, W., Hess, K.-U., Damby, D.E., Wadsworth, F.B., Lavallée, Y., Cimarelli, C. and Dingwell, D.B. Fusion characteristics of volcanic ash relevant to aviation hazards, Geophysical Research Letters, 2014, 41, (7), pp 2326–2333.CrossRefGoogle Scholar
8. Hamed, A., Tabakoff, W.C. and Wenglarz, R.A. Erosion and deposition in turbomachinery, J Propulsion Power, 2006, 22, (2), pp 350–360.CrossRefGoogle Scholar
9. Myers, R.H., Montgomery, D.C. and Anderson-Cook, C.M. Response Surface Methodology: Process and Product Optimization Using Designed Experiments, 2009, Wiley, Hoboken, New Jersey, US.Google Scholar
10. Turner, E.R., Wilson, W.D., Hylton, L.D. and Kaufman, R.M. Turbine Vane External Heat Transfer, Volume 1. Analytical and Experimental Evaluation of Surface Heat Transfer Distributions with Leading Edge Showerhead Film Cooling, NASA CR-174827, 1985, Indianapolis, Indiana, US.Google Scholar
11. Hylton, L.D., Nirmalan, V., Sultanian, B.K. and Kaufman, R.M. The Effects of Leading Edge and Downstream Turbine Vane Heat Transfer, CR-182133, 1988, NASA, Washington, D.C., US.Google Scholar
12. Nealy, D.A., Mihelc, M.S., Hylton, L.D. and Gladden, H.J. Measurements of heat transfer distribution over the surfaces of highly loaded turbine nozzle guide vanes, J Engineering for Gas Turbines and Power, 1983, 106, (January 1984), pp 149–158.CrossRefGoogle Scholar
13. Hylton, L.D., Mihelc, M.S., Turner, E.R., Nealy, D.A. and York, R.E. Analytical and Experimental Evaluation of the Heat Transfer Distribution over the Surfaces of Turbine Vanes, CR-168015, 1983, NASA, Washington, D.C., US.Google Scholar
14. Delimont, J.M., Murdock, M.K., Ng, W.F. and Ekkad, S.V. Effect of temperature on microparticle rebound characteristics at constant impact velocity—Part II, J Engineering for Gas Turbines and Power, 2015, 137, (11), p 112604.CrossRefGoogle Scholar
15. Delimont, J.M., Murdock, M.K., Ng, W.F. and Ekkad, S.V. Effect of temperature on microparticle rebound characteristics at constant impact velocity–Part I, J Engineering for Gas Turbines and Power, 2015, 137, (11), p 112603.CrossRefGoogle Scholar
16. Boulanger, A.J., Patel, H.D., Hutchinson, J., DeShong, W., Xu, W., Ng, W.F. and Ekkad, S.V. Preliminary experimental investigation of initial onset of sand deposition in the turbine section of gas turbines, ASME Turbo Expo 2016, Volume 1: Aircraft Engine; Fans and Blowers; Marine, 2016, ASME, Seoul, South Korea, p. V001T01A003.CrossRefGoogle Scholar
17. Kueppers, U., Cimarelli, C., Hess, K.-U., Taddeucci, J., Wadsworth, F.B. and Dingwell, D.B. The thermal stability of Eyjafjallajökull ash versus turbine ingestion test sands, J Applied Volcanology, 2014, 3, (1), p 4.CrossRefGoogle Scholar
18. Dunn, M.G., Padova, C., Moller, J.E. and Adams, R.M. Performance deterioration of a turbofan and a turbojet engine upon exposure to a dust environment, J Engineering for Gas Turbines and Power, 1987, 109, (3), p 336.CrossRefGoogle Scholar
19. Dunn, M.G., Padova, C. and Adams, R.M. Operation of Gas Turbine Engines in Dust-Laden Environments, ADP006197, 1987, Buffalo, New York, US.Google Scholar
20. Livingood, J.N.B. and Hrycak, P. Impingement heat transfer from turbulent air jets to flat plates: A literature survey, TM X-2778, 1973, NASA, Washington, D.C., US.Google Scholar
21. Jarvis, E.A.A. and Carter, E.A. Exploiting covalency to enhance metal-oxide and oxide-oxide adhesion at heterogeneous interfaces, J American Ceramic Society, 2003, 86, (3), pp 373–386.CrossRefGoogle Scholar