Due to the increasing demands for environment protection, the regulation of NOx emissions from aircraft engines specified by ICAO have become more stringent year by year. A combustor with lean staged fuel injectors is one of the effective methods to reduce NOx emissions. Kawasaki heavy industries Ltd GTBC and Japan Aerospace Exploration Agency (JAXA) have been conducting joint research on a lean staged concentric fuel nozzle for a high pressure ratio aero engine. High pressure combustion tests were performed to clarify the effect of the contour of the air flow passage of the main premix duct, the arrangement of the swilers and the fuel injection position on the NOx emission especially at high power. Visualization of the fuel spray at elevated pressure inside of the premix duct using a model with transparent walls and a laser diagnostics technique showed clear relationship between the distribution of the fuel spray and the NOx emission.
Skip Nav Destination
ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition
June 6–10, 2011
Vancouver, British Columbia, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5462-4
PROCEEDINGS PAPER
Suppression of NOx Emission of a Lean Staged Combustor for an Aircraft Engine
H. Fujiwara,
H. Fujiwara
Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
Search for other works by this author on:
K. Matsuura,
K. Matsuura
Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
Search for other works by this author on:
K. Shimodaira,
K. Shimodaira
Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
Search for other works by this author on:
S. Hayashi,
S. Hayashi
Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
Search for other works by this author on:
M. Kobayashi,
M. Kobayashi
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
Search for other works by this author on:
T. Oda,
T. Oda
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
Search for other works by this author on:
A. Horikawa,
A. Horikawa
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
Search for other works by this author on:
R. Matsuyama,
R. Matsuyama
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
Search for other works by this author on:
H. Ogata,
H. Ogata
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
Search for other works by this author on:
Y. Kinoshita
Y. Kinoshita
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
Search for other works by this author on:
H. Fujiwara
Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
K. Matsuura
Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
K. Shimodaira
Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
S. Hayashi
Japan Aerospace Exploration Agency, Chofu, Tokyo, Japan
M. Kobayashi
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
T. Oda
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
A. Horikawa
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
R. Matsuyama
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
H. Ogata
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
Y. Kinoshita
Kawasaki Heavy Industries Ltd. GTBC, Akashi, Hyogo, Japan
Paper No:
GT2011-46256, pp. 1027-1034; 8 pages
Published Online:
May 3, 2012
Citation
Fujiwara, H, Matsuura, K, Shimodaira, K, Hayashi, S, Kobayashi, M, Oda, T, Horikawa, A, Matsuyama, R, Ogata, H, & Kinoshita, Y. "Suppression of NOx Emission of a Lean Staged Combustor for an Aircraft Engine." Proceedings of the ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. Volume 2: Combustion, Fuels and Emissions, Parts A and B. Vancouver, British Columbia, Canada. June 6–10, 2011. pp. 1027-1034. ASME. https://doi.org/10.1115/GT2011-46256
Download citation file:
46
Views
Related Proceedings Papers
Related Articles
Emissions Reduction by Varying the Swirler Airflow Split in Advanced Gas Turbine Combustors
J. Eng. Gas Turbines Power (July,1993)
FLOX ® Combustion at High Power Density and High Flame Temperatures
J. Eng. Gas Turbines Power (December,2010)
Emission and Performance of a Lean-Premixed Gas Fuel Injection System for Aeroderivative Gas Turbine Engines
J. Eng. Gas Turbines Power (January,1996)
Related Chapters
A Simple Carburetor
Case Studies in Fluid Mechanics with Sensitivities to Governing Variables
Combined Cycle Power Plant
Energy and Power Generation Handbook: Established and Emerging Technologies
Fuel Nozzle Geometry Effects on Cavitation and Spray Behavior at Diesel Engine Conditions
Proceedings of the 10th International Symposium on Cavitation (CAV2018)