The difficulties in making spatially-resolved measurements of soot concentration inside practical combustors, which do not rely on sample extraction techniques, are highlighted. Restricted optical access presents the principal constraint to the adoption of established tomographic techniques. A novel hybrid approach, which combines a traversable laser shielding tube and conventional integrated absorption measurement, is demonstrated in two tubular combustors operating at a range of AFRs, inlet air temperatures and pressures. Measurements are reported which have been taken through existing primary and dilution ports and through additional line-of-sight holes drilled in the liner specifically for that purpose. Distinctive radial profiles of soot volume fraction emerge, reflecting the annular development of richer mixtures, which favour soot formation, downstream of the fuel injector.
Skip Nav Destination
ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition
June 5–8, 1995
Houston, Texas, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7880-4
PROCEEDINGS PAPER
Spatially-Resolved Soot Measurements in Gas Turbine Combustors
Q.-P. Zheng,
Q.-P. Zheng
Cranfield University, Bedford, England
Search for other works by this author on:
C. D. Stewart,
C. D. Stewart
Cranfield University, Bedford, England
Search for other works by this author on:
J. B. Moss
J. B. Moss
Cranfield University, Bedford, England
Search for other works by this author on:
Q.-P. Zheng
Cranfield University, Bedford, England
C. D. Stewart
Cranfield University, Bedford, England
J. B. Moss
Cranfield University, Bedford, England
Paper No:
95-GT-337, V003T06A060; 7 pages
Published Online:
February 16, 2015
Citation
Zheng, Q, Stewart, CD, & Moss, JB. "Spatially-Resolved Soot Measurements in Gas Turbine Combustors." Proceedings of the ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations. Houston, Texas, USA. June 5–8, 1995. V003T06A060. ASME. https://doi.org/10.1115/95-GT-337
Download citation file:
107
Views
Related Proceedings Papers
Related Articles
Experimental Analysis of Soot Formation and Oxidation in a Gas Turbine Model Combustor Using Laser Diagnostics
J. Eng. Gas Turbines Power (December,2011)
Soot Formation and Flame Characterization of an Aero-Engine Model Combustor Burning Ethylene at Elevated Pressure
J. Eng. Gas Turbines Power (February,2014)
The Influence of Fuel Hydrogen Content Upon Soot Formation in a Model Gas Turbine Combustor
J. Eng. Gas Turbines Power (October,1984)
Related Chapters
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Combined Cycle Power Plant
Energy and Power Generation Handbook: Established and Emerging Technologies
Augmentation of Turbulence and Mixing in Gas Turbine Combustors by Introducing Unsteady Effects
Proceedings of the 2010 International Conference on Mechanical, Industrial, and Manufacturing Technologies (MIMT 2010)