Content area

Abstract

The invention of internal combustion engines is undoubtedly one of the greatest inventions of the modern era. There has been steady scientific research to look for alternative fuel which is economical, renewable and less harmful to nature and man compared to fossil fuels. The present project is one such experimental work to investigate the performance of a blend of diesel / N-pentanol in an appropriate combustion technique and to establish its suitability as a renewable fuel. The relative performance of diesel fuel and the blend of diesel / n-pentanol will also be analyzed. Diesel fuel blended with 30% n-pentanol is the fuel blend that is proposed to be used in the experiment. Researchers have established that the application of Homogeneously Charged Compression Ignition (HCCI) technique could result in in-cylinder reduction of NOx and PM. Higher thermal efficiency could also be attained. The project also covers studying the emission effect of the diesel/n-pentanol fuel blend for various fuel injection timing, various fuel injection pressure, different EGR rates and different inlet air temperature.

Details

Title
Experimental Investigation on Emission Characteristics of Diesel N-Pentanol Blend in Homogeneous Charged Compression Ignition Engine
Author
Mathavan, S 1 ; Mothilal, T 1 ; Andal, V 2 ; Velukumar, V 3 

 Dept. of Automobile Engg., KCG College. of Tech., Chennai, Tamilnadu, India 
 Dept. of 'Sci. and Humanities, KCG College. of Tech., Chennai, Tamilnadu, India 
 Dept. of Mech. Engg., TJS Engg. College, Chennai, Tamilnadu, India 
Volume
13
Issue
3
Pages
309-313
Publication year
2021
Publication date
2021
Publisher
MechAero Foundation for Technical Research & Education Excellence
Place of publication
Chennai
Country of publication
India
ISSN
09753060
e-ISSN
09753540
Source type
Scholarly Journal
Language of publication
English
Document type
Journal Article
ProQuest document ID
2620403805
Document URL
https://www.proquest.com/scholarly-journals/experimental-investigation-on-emission/docview/2620403805/se-2?accountid=208611
Copyright
Copyright MechAero Foundation for Technical Research & Education Excellence 2021
Last updated
2023-11-26
Database
ProQuest One Academic