Large amounts of tiny microparticles are ingested into gas turbines over their operating life, resulting in unexpected wear and tear. Knowledge of such microparticle behavior at gas turbine operating temperatures is limited in published literature. In this study, Arizona Road Dust (ARD) is injected into a hot flow field to measure the effects of high temperature and velocity on particle rebound from a polished 304 Stainless Steel (SS) coupon. The results are compared with baseline (27m/s) measurements at ambient (300°K) temperature made in the Virginia Tech Aerothermal Rig, as well as previously published literature. Mean Coefficient of Restitution (COR) was shown to decrease with the increased temperature/velocity conditions in the VT Aerothermal Rig. The effects of increasing temperature and velocity led to a 12% average reduction in COR at 533°K (47m/s), 15% average reduction in COR at 866°K (77m/s), and 16% average reduction in COR at 1073°K (102m/s) compared with ambient results. The decrease in COR appeared to be almost entirely a result of increased velocity that resulted from heating the flow. Trends show that temperature plays a minor role in energy transfer between particle and impact surface below a critical temperature.
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ASME Turbo Expo 2013: Turbine Technical Conference and Exposition
June 3–7, 2013
San Antonio, Texas, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5513-3
PROCEEDINGS PAPER
Study of Microparticle Rebound Characteristics Under High Temperature Conditions
J. M. Delimont,
J. M. Delimont
Virginia Tech, Blacksburg, VA
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S. V. Ekkad
S. V. Ekkad
Virginia Tech, Blacksburg, VA
Search for other works by this author on:
C. J. Reagle
Virginia Tech, Blacksburg, VA
J. M. Delimont
Virginia Tech, Blacksburg, VA
W. F. Ng
Virginia Tech, Blacksburg, VA
S. V. Ekkad
Virginia Tech, Blacksburg, VA
Paper No:
GT2013-95083, V002T03A011; 9 pages
Published Online:
November 14, 2013
Citation
Reagle, CJ, Delimont, JM, Ng, WF, & Ekkad, SV. "Study of Microparticle Rebound Characteristics Under High Temperature Conditions." Proceedings of the ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. Volume 2: Aircraft Engine; Coal, Biomass and Alternative Fuels; Cycle Innovations. San Antonio, Texas, USA. June 3–7, 2013. V002T03A011. ASME. https://doi.org/10.1115/GT2013-95083
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