Skip to main content

Lund University Publications

LUND UNIVERSITY LIBRARIES

Investigation of engine performance for alcohol/kerosene blends as in spark-ignition aviation piston engine

Liu, Guibin ; Ruan, Can LU ; Li, Zilong ; Huang, Guan ; Zhou, Qiyan ; Qian, Yong LU and Lu, Xingcai (2020) In Applied Energy 268.
Abstract

Spark-ignition (SI) aviation piston engines are widely used on light helicopters and unmanned aerial vehicles (UAVs) because of the high-power density and ultra-high cost performance. Kerosene with high flash point is expected to improve safety of aforementioned aircrafts by replacing gasoline. However, in spark-ignition mode, kerosene is difficult to mix and is easy to knock. Short-chain alcohols have high volatility and octane number which can just make up for some defects of kerosene. In this paper, three kinds of alcohols including ethanol, n-propanol and n-butanol were blended with aviation kerosene (RP-3) by volume fraction of 30%, 50%, 70%, respectively. The combustion and emission characteristics of the blended fuels were deeply... (More)

Spark-ignition (SI) aviation piston engines are widely used on light helicopters and unmanned aerial vehicles (UAVs) because of the high-power density and ultra-high cost performance. Kerosene with high flash point is expected to improve safety of aforementioned aircrafts by replacing gasoline. However, in spark-ignition mode, kerosene is difficult to mix and is easy to knock. Short-chain alcohols have high volatility and octane number which can just make up for some defects of kerosene. In this paper, three kinds of alcohols including ethanol, n-propanol and n-butanol were blended with aviation kerosene (RP-3) by volume fraction of 30%, 50%, 70%, respectively. The combustion and emission characteristics of the blended fuels were deeply studied on a typical spark-ignition aviation piston engine. Meanwhile, engine performance fueled with commercial gasoline was also tested for comparison. Results indicated that alcohol/kerosene blends could reach higher brake thermal efficiency (BTE) (alcohol ratio ≥50%) compared to gasoline. Carbon monoxide (CO) and nitrogen oxides (NOx) emissions of blended fuels expressed dramatically descending. With the increase in alcohol ratio, the CO, hydrocarbons (HC) and soot emissions gradually decreased. The brake thermal efficiency showed an upward trend with the increase of alcohol ratios. The brake thermal efficiency of E70, P70 and B70 were increased by 2.15%, 3.52% and 6.51%, and the CO emissions of E70, P70 and B70 were reduced by 39.8%, 38.5% and 49.0%, respectively, compared to those of gasoline. Notably, n-butanol/kerosene blends exhibited the better combustion and emission characteristics, which had the higher efficiency and lower CO, HC and soot emissions.

(Less)
Please use this url to cite or link to this publication:
author
; ; ; ; ; and
publishing date
type
Contribution to journal
publication status
published
keywords
Alcohols, Brake thermal efficiency, Combustion and emission, Kerosene, Spark-ignition aviation piston engine
in
Applied Energy
volume
268
article number
114959
pages
9 pages
publisher
Elsevier
external identifiers
  • scopus:85083344387
ISSN
0306-2619
DOI
10.1016/j.apenergy.2020.114959
language
English
LU publication?
no
additional info
Publisher Copyright: © 2020 Elsevier Ltd
id
30e41385-4f9c-44d0-97ab-5455f7086c98
date added to LUP
2024-07-13 21:02:30
date last changed
2024-08-12 13:20:12
@article{30e41385-4f9c-44d0-97ab-5455f7086c98,
  abstract     = {{<p>Spark-ignition (SI) aviation piston engines are widely used on light helicopters and unmanned aerial vehicles (UAVs) because of the high-power density and ultra-high cost performance. Kerosene with high flash point is expected to improve safety of aforementioned aircrafts by replacing gasoline. However, in spark-ignition mode, kerosene is difficult to mix and is easy to knock. Short-chain alcohols have high volatility and octane number which can just make up for some defects of kerosene. In this paper, three kinds of alcohols including ethanol, n-propanol and n-butanol were blended with aviation kerosene (RP-3) by volume fraction of 30%, 50%, 70%, respectively. The combustion and emission characteristics of the blended fuels were deeply studied on a typical spark-ignition aviation piston engine. Meanwhile, engine performance fueled with commercial gasoline was also tested for comparison. Results indicated that alcohol/kerosene blends could reach higher brake thermal efficiency (BTE) (alcohol ratio ≥50%) compared to gasoline. Carbon monoxide (CO) and nitrogen oxides (NO<sub>x</sub>) emissions of blended fuels expressed dramatically descending. With the increase in alcohol ratio, the CO, hydrocarbons (HC) and soot emissions gradually decreased. The brake thermal efficiency showed an upward trend with the increase of alcohol ratios. The brake thermal efficiency of E70, P70 and B70 were increased by 2.15%, 3.52% and 6.51%, and the CO emissions of E70, P70 and B70 were reduced by 39.8%, 38.5% and 49.0%, respectively, compared to those of gasoline. Notably, n-butanol/kerosene blends exhibited the better combustion and emission characteristics, which had the higher efficiency and lower CO, HC and soot emissions.</p>}},
  author       = {{Liu, Guibin and Ruan, Can and Li, Zilong and Huang, Guan and Zhou, Qiyan and Qian, Yong and Lu, Xingcai}},
  issn         = {{0306-2619}},
  keywords     = {{Alcohols; Brake thermal efficiency; Combustion and emission; Kerosene; Spark-ignition aviation piston engine}},
  language     = {{eng}},
  month        = {{06}},
  publisher    = {{Elsevier}},
  series       = {{Applied Energy}},
  title        = {{Investigation of engine performance for alcohol/kerosene blends as in spark-ignition aviation piston engine}},
  url          = {{http://dx.doi.org/10.1016/j.apenergy.2020.114959}},
  doi          = {{10.1016/j.apenergy.2020.114959}},
  volume       = {{268}},
  year         = {{2020}},
}