Khandelwal, B. (2014) Reforming technologies to improve the performance of combustion systems. Aerospace, 1 (2). 67 - 96. ISSN 2226-4310
Abstract
A large number of theoretical and experimental studies have shown that the performance of kerosene combustion increases significantly if combustion is being assisted by the addition of hydrogen to the fuel/air mixture during the combustion process. It reduces the amount of CO, CO2 and NOx emissions, while increasing the flame stability limits. It also helps in bruning fuel/air mixtures at much leaner equivalence ratios. The same principle could be applied to gain benefits in gas turbine combustors. Hydrogen for this purpose could be produced by the reforming of hydrocarbon fuels using a reformer module. This paper presents key hydrogen reforming technologies which, by implementation in gas turbine combustors, hold potential for improving both their performance and service life.
Metadata
Item Type: | Article |
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Authors/Creators: |
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Copyright, Publisher and Additional Information: | This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. |
Keywords: | kerosene reforming; gas turbine combustor; novel combustion technologies; hydrogen assisted combustion |
Dates: |
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Institution: | The University of Sheffield |
Academic Units: | The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Mechanical Engineering (Sheffield) |
Depositing User: | Symplectic Sheffield |
Date Deposited: | 29 Sep 2014 10:32 |
Last Modified: | 29 Sep 2014 10:40 |
Published Version: | http://dx.doi.org/10.3390/aerospace1020067 |
Status: | Published |
Publisher: | MDPI |
Refereed: | Yes |
Identification Number: | 10.3390/aerospace1020067 |
Open Archives Initiative ID (OAI ID): | oai:eprints.whiterose.ac.uk:80721 |