Investigation of synthethic diesel fuels and combustion characteristics using rapid compression machine (RCM)

In a compression ignition engine, the fuel/air mixing process affects the combustion process. The study mainly investigates the effects of blending ratio, injection pressure (Pinj), and ambient temperature (Ti) on ignition delay and heat recovery process during the combustion process. The fuel...

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Main Author: Abdullah, Iqbal Shahridzuan
Format: Thesis
Language:English
English
English
Published: 2022
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Online Access:http://eprints.uthm.edu.my/8266/1/24p%20IQBAL%20SHAHRIDZUAN%20ABDULLAH.pdf
http://eprints.uthm.edu.my/8266/2/IQBAL%20SHAHRIDZUAN%20ABDULLAH%20COPYRIGHT%20DECLARATION.pdf
http://eprints.uthm.edu.my/8266/3/IQBAL%20SHAHRIDZUAN%20ABDULLAH%20WATERMARK.pdf
http://eprints.uthm.edu.my/8266/
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spelling my.uthm.eprints.82662023-02-07T03:42:16Z http://eprints.uthm.edu.my/8266/ Investigation of synthethic diesel fuels and combustion characteristics using rapid compression machine (RCM) Abdullah, Iqbal Shahridzuan T Technology (General) In a compression ignition engine, the fuel/air mixing process affects the combustion process. The study mainly investigates the effects of blending ratio, injection pressure (Pinj), and ambient temperature (Ti) on ignition delay and heat recovery process during the combustion process. The fuel was blended using a fuel blending machine at three different blending ratios of 10%, 15%, and 20% using the Tire Pyrolysis Oil (TPO) and Plastic Pyrolysis Oil (PPO). Each oil was tested by using a Rapid Compression Machine (RCM). The ambient temperature was varied from 750 K until 1050 K and Pinj at 80 MPa to 130 MPa. The data obtained was compared to Euro 5 as reference. The ignition delay of TPO10 was 1.61 ms at 80 MPa compared to 0.9 ms when the pressure was 130 MPa. For Ti, the ignition delay of PPO10 at 750 K reached 1.34 ms, but at 1050 K, the ignition delay shortened to 0.64 ms. Such increment in the Pinj and Ti helps in the atomization and combustible of mixture formation by lengthening the spray tip penetration, which also produces finer fuel droplet spray and reduces ignition delay. Whereas, the increase in blending ratio is found to increase the ignition delay while the increase in Ti and Pinj decrease the ignition delay, hence improving the combustion’s performance. The increment in ignition delay increases the mixing time available, which usually results in a more uniform mixture, substantial reductions in the overall cylinder pressure, and maximum HRR. 2022-01 Thesis NonPeerReviewed text en http://eprints.uthm.edu.my/8266/1/24p%20IQBAL%20SHAHRIDZUAN%20ABDULLAH.pdf text en http://eprints.uthm.edu.my/8266/2/IQBAL%20SHAHRIDZUAN%20ABDULLAH%20COPYRIGHT%20DECLARATION.pdf text en http://eprints.uthm.edu.my/8266/3/IQBAL%20SHAHRIDZUAN%20ABDULLAH%20WATERMARK.pdf Abdullah, Iqbal Shahridzuan (2022) Investigation of synthethic diesel fuels and combustion characteristics using rapid compression machine (RCM). Masters thesis, Universiti Tun Hussein Onn Malaysia.
institution Universiti Tun Hussein Onn Malaysia
building UTHM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tun Hussein Onn Malaysia
content_source UTHM Institutional Repository
url_provider http://eprints.uthm.edu.my/
language English
English
English
topic T Technology (General)
spellingShingle T Technology (General)
Abdullah, Iqbal Shahridzuan
Investigation of synthethic diesel fuels and combustion characteristics using rapid compression machine (RCM)
description In a compression ignition engine, the fuel/air mixing process affects the combustion process. The study mainly investigates the effects of blending ratio, injection pressure (Pinj), and ambient temperature (Ti) on ignition delay and heat recovery process during the combustion process. The fuel was blended using a fuel blending machine at three different blending ratios of 10%, 15%, and 20% using the Tire Pyrolysis Oil (TPO) and Plastic Pyrolysis Oil (PPO). Each oil was tested by using a Rapid Compression Machine (RCM). The ambient temperature was varied from 750 K until 1050 K and Pinj at 80 MPa to 130 MPa. The data obtained was compared to Euro 5 as reference. The ignition delay of TPO10 was 1.61 ms at 80 MPa compared to 0.9 ms when the pressure was 130 MPa. For Ti, the ignition delay of PPO10 at 750 K reached 1.34 ms, but at 1050 K, the ignition delay shortened to 0.64 ms. Such increment in the Pinj and Ti helps in the atomization and combustible of mixture formation by lengthening the spray tip penetration, which also produces finer fuel droplet spray and reduces ignition delay. Whereas, the increase in blending ratio is found to increase the ignition delay while the increase in Ti and Pinj decrease the ignition delay, hence improving the combustion’s performance. The increment in ignition delay increases the mixing time available, which usually results in a more uniform mixture, substantial reductions in the overall cylinder pressure, and maximum HRR.
format Thesis
author Abdullah, Iqbal Shahridzuan
author_facet Abdullah, Iqbal Shahridzuan
author_sort Abdullah, Iqbal Shahridzuan
title Investigation of synthethic diesel fuels and combustion characteristics using rapid compression machine (RCM)
title_short Investigation of synthethic diesel fuels and combustion characteristics using rapid compression machine (RCM)
title_full Investigation of synthethic diesel fuels and combustion characteristics using rapid compression machine (RCM)
title_fullStr Investigation of synthethic diesel fuels and combustion characteristics using rapid compression machine (RCM)
title_full_unstemmed Investigation of synthethic diesel fuels and combustion characteristics using rapid compression machine (RCM)
title_sort investigation of synthethic diesel fuels and combustion characteristics using rapid compression machine (rcm)
publishDate 2022
url http://eprints.uthm.edu.my/8266/1/24p%20IQBAL%20SHAHRIDZUAN%20ABDULLAH.pdf
http://eprints.uthm.edu.my/8266/2/IQBAL%20SHAHRIDZUAN%20ABDULLAH%20COPYRIGHT%20DECLARATION.pdf
http://eprints.uthm.edu.my/8266/3/IQBAL%20SHAHRIDZUAN%20ABDULLAH%20WATERMARK.pdf
http://eprints.uthm.edu.my/8266/
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score 13.160551