Top of page. Skip to main contents. Skip to main menu. Skip to footer.
HOME > Technology > Technical ReviewVolume 45  Number 4  > Research and Development of a Combustor for an Environmentally Compatible Small Aero Engine
Mitsubishi Heavy Industries Technical Review
 Volume 48 (2011)
 Volume 47 (2010)
 Volume 46 (2009)
 Volume 45 (2008)
 Volume 44 (2007)
 Volume 43 (2006)
 Volume 42 (2005)
 Volume 41 (2004)
 Volume 40 (2003)
 Volume 39 (2002)
 Volume 38 (2001)
 Volume 37 (2000)
 Volume 36 (1999)
 Volume 35 (1998)
 Volume 34 (1997)
 Volume 33 (1996)
 Volume 32 (1995)
 Volume 31 (1994)
Mitsubishi Heavy Industries Technical Review
 Volume 45 Number 4  Aerospace Technology
 English: 1140KB/Now download pdf file
 Japanese: 974KB/Now download japanese pdf file
Research and Development of a Combustor for an Environmentally Compatible Small Aero Engine


Hideki Moriai, Tomoyoshi Nakae, Yoshiaki Miyake, Mitsuru Inada


Mitsubishi Heavy Industries, Ltd. (MHI) has proposed a rich-burn, quick-quench, lean-burn combustor for use as a simple, low NOX-emission combustor for the ECO Engine (environmentally compatible small aero engine). MHI promoted the research and development of the ECO Engine from 2004 to 2006 as a national project with a subsidy from the New Energy and Industrial Technology Development Organization (NEDO). The performance evaluation tests, conducted at the combustion test facility of the Japan Aerospace Exploration Agency (JAXA) in 2006, indicated that many requirements were satisfied, such as emissions, combustor exit temperature distribution, and combustion efficiency. The NOX emissions were less than 50% of the international regulations.