26th Congress of International Council of the Aeronautical Sciences
including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
14 - 19 September 2008, Anchorage, Alaska, USA
Paper ICAS 2008-4.3.2

DEVELOPMENT OF FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT JET ENGINE IN JAXA TECHCLEAN PROJECT

M. Makida, H. Yamada, T. Yamamoto
JAXA, Japan

Keywords: Full annular combustor, Practical conditions, NOx reduction, Rich-Lean

JAXA APG has conducted a series of research experiments to develop a combustor for a small aircraft engine (OPR about 20). Based on the selected design, a full annular combustor was designed and tested under practical conditions using an experimental facility newly developed in 2007.

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