Catalytic flame stabilization encompasses the use of a porous catalytic surface to initiate, stabilize, and provide a continuous pilot for flame propagation. A preliminary assessment of the feasibility of employing catalytic flame stabilization to the design of flameholders for aircraft afterburners has been completed. Initial testing has demonstrsted that catalytic flame stabilization in aircraft afterburners can be achieved. For the non-optimal catalytic flameholders evaluated, smooth light-off and stable operation were obtained; higher combustion efficiencies were measured and higher pressure losses were observed. During the course of the experiment a significant number of design aspects were determined to require further investigation. These design aspects along with other results of this study are discussed in this paper.
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ASME 1980 International Gas Turbine Conference and Products Show
March 10–13, 1980
New Orleans, Louisiana, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7965-8
PROCEEDINGS PAPER
Experimental Evaluation of Catalytic Flame Stabilization for Aircraft Afterburners
L. C. Angello,
L. C. Angello
Electric Power Research Institute, Palo Alto, CA
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E. N. Coppola
E. N. Coppola
Air Force Aero Propulsion Laboratory, Wright-Patterson Air Force Base, OH
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L. C. Angello
Electric Power Research Institute, Palo Alto, CA
E. N. Coppola
Air Force Aero Propulsion Laboratory, Wright-Patterson Air Force Base, OH
Paper No:
80-GT-56, V01AT01A056; 10 pages
Published Online:
April 17, 2015
Citation
Angello, LC, & Coppola, EN. "Experimental Evaluation of Catalytic Flame Stabilization for Aircraft Afterburners." Proceedings of the ASME 1980 International Gas Turbine Conference and Products Show. Volume 1A: General. New Orleans, Louisiana, USA. March 10–13, 1980. V01AT01A056. ASME. https://doi.org/10.1115/80-GT-56
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