Performance and Emission Characteristics of a Gas Turbine Engine Burning Soap-Derived Biokerosene/Jet A-1 Blends

被引:7
作者
Reksowardojo, Iman K. [1 ]
Duong, Long H. [2 ]
Soerawidjaja, Tatang H. [1 ]
Nguyen, Tri T. G. [3 ]
Fujita, Osamu [3 ]
Neonufa, Godlief F. [4 ]
机构
[1] Inst Teknol Bandung, Bandung, Indonesia
[2] Nguyen Tat Thanh Univ, Ho Chi Minh City, Vietnam
[3] Hokkaido Univ, Sapporo, Hokkaido, Japan
[4] Univ Atha Wacana, Kupang, East Nusa Tengg, Indonesia
关键词
Soap-derived biokerosene; Biojet fuels; Aviation alternative fuels; Gas turbine engine performance; Exhaust gas emissions; JET FUEL; ALTERNATIVE FUELS; SOOTING TENDENCY; AVIATION FUELS; VEGETABLE-OIL; GREEN DIESEL; BIOFUELS; CONVERSION; COMBUSTION; BIODIESEL;
D O I
10.4271/04-13-02-0007
中图分类号
U [交通运输];
学科分类号
08 ; 0823 ;
摘要
There has been an increased interest as regards the use of biofuels in aviation gas turbine engines due to global efforts to reduce greenhouse gas emissions along with fluctuating jet fuel prices. This work researches the use of soap-derived biokerosene (SBK) in aircraft engines. SBK is a promising biofuel option for emerging tropical countries as its production requires a relatively simple technology, and its feedstock sources are abundant in these countries. Blends of Jet A-1 with up to 20 vol.% SBK were tested on a 1S/60 Rover gas turbine engine over a range of brake powers to measure engine performance and emissions. The results were then compared to those of pure Jet A-1. It shows that the engine running on SBK/Jet A-1 blends and pure Jet A-1 have almost similar engine performance parameters including engine efficiency, specific fuel consumption (SFC), turbine inlet temperature (TIT), and exhaust gas temperature (EGT). On the other hand, increasing the volume fraction of SBK in the fuel blends with Jet A-1 leads to a slight increase in carbon monoxide (CO) and HC emissions, while insignificant differences in the nitrogen oxides (NOx) emissions were found. From this study, some valuable recommendations could be found to improve the feasibility of SBK for use as an alternative aviation fuel.
引用
收藏
页码:125 / 136
页数:12
相关论文
共 80 条
[1]   Combustion of waste trap grease oil in gas turbine generator [J].
Al-Shudeifat, M. A. ;
Donaldson, A. B. .
FUEL, 2010, 89 (03) :549-553
[2]   Performance and environmental impact of a turbojet engine fueled by blends of biodiesels [J].
Ali, A. H. H. ;
Ibrahim, M. N. .
INTERNATIONAL JOURNAL OF ENVIRONMENTAL SCIENCE AND TECHNOLOGY, 2017, 14 (06) :1253-1266
[3]  
[Anonymous], 2005, AV FUELS TECHN REV
[4]  
[Anonymous], 2010, IATA EC BRIEF AIRL F
[5]  
[Anonymous], 2014, IATA 2014 REP ALT FU
[6]  
[Anonymous], 2004, HDB AV FUEL PROP SOC
[7]  
[Anonymous], 2019, D405419 ASTM INT
[8]  
Artur K., 2018, THE J, V25, P101, DOI [10.5604/01.3001.0012.2455, DOI 10.5604/01.3001.0012.2455]
[9]  
ASTM, 2019, D165519A ASTM INT
[10]  
ASTM, 2019, D756619 ASTM