Conversion of a Spark-Ignited Aircraft Engine to JP-8 Heavy Fuel for Use in Unmanned Aerial Vehicles

被引:41
作者
Duddy, Brian J. [1 ]
Lee, James [1 ]
Walluk, Mark [1 ]
Hallbach, David [1 ]
机构
[1] Rochester Inst Technol, Rochester, NY 14623 USA
关键词
D O I
10.4271/2011-01-0145
中图分类号
U [交通运输];
学科分类号
08 ; 0823 ;
摘要
In order to satisfy a single-fuel mandate, the U.S. Department of Defense has a need for engines in the 20 to 50 hp range to power midsized Unmanned Aerial Vehicles (UAVs) and the ability to operate on JP-8 also known as "heavy"fuel. It is possible to convert two-stroke aircraft engines designed to operate on a gasoline-oil mixture to run on JP-8/oil using the Sonex Combustion System (SCS) developed by Sonex Research, Inc. Conversion of the engine involves replacing the cylinder heads with new components designed to accept a steel combustion ring insert. Also required are glow-plugs to preheat the cylinder head prior to engine start. The converted engine produces the same power output as the stock engine operating on gasoline. Conversion of both a 20 hp and 40 hp engine was successfully achieved using the SCS.
引用
收藏
页码:82 / 93
页数:12
相关论文
共 17 条
[1]  
[Anonymous], 2004, DEF SCI BOARD STUD U
[2]  
[Anonymous], 2005, DAT SEEK 2 UAV FLIGH, P64
[3]  
[Anonymous], 1999, F34JP8 NATO US DEP D
[4]  
Brown R.B., 2001, COMBUSTION DATA ACQU
[5]  
Cordon D., 2008, 2008320023 SAE, DOI [10.4271/2008-32-0023, DOI 10.4271/2008-32-0023]
[6]  
EDWARDS T, 2001, 20010498 AIAA
[7]  
Edwards T, 2004, 20043885 AIAA
[8]  
Ernst J., 2003, 20036534 AIAA
[9]  
Heywood J.B., 1988, INTERNAL COMBUSTION
[10]  
Kalkstein James, 2006, 2006010278 SAE, DOI [10.4271/2006-01-0278, DOI 10.4271/2006-01-0278]