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Impact of Flowfield on Pollutants’ Emission from a Swirl-Assisted Distributed Combustor Read chapter Read first chapter

2021 | OriginalPaper | Chapter

Emission Characteristics on Combustion of HEFA Alternative-Aviation Fuel Under In-Flight Conditions

Authors : Hitoshi Fujiwara, Keiichi Okai

Published in: Advances in IC Engines and Combustion Technology

Publisher: Springer Singapore

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Abstract

Global climate change, due to the rapid increase in CO2 emissions, especially caused by aviation, is one of the critical issues to be solved through international collaborations.

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Literature
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National Academies of Sciences, Engineering, and Medicine (2016) Commercial aircraft propulsion and energy systems research: reducing global carbon emissions. The National Academies Press, Washington DC. https://​doi.​org/​10.​17226/​23490
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ASTM D7566-18 (2018) Standard specification for aviation turbine fuels containing synthesized hydrocarbons, ASTM International, West Conshohocken, PA
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Fukuyama Y, Fujiwara H, Okai K, Alternative fuels and their impact on the turbofan engine design and performance under the realistic flight conditions, ACGT paper No. 51, Asian Joint Congress on Gas Turbines 2009 (ACGT 2009), Tokyo, Japan 2009 (ACGT2009-051)
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Okai K, Fujiwara H, Hongoh M, Shimodaira K (2012) Application of a Bio-fuel to a single sector combustor for an experimental small aero-engine, Asian Joint Congress on Gas Turbines 2012 (ACGT 2012), Shanghai, China (ACGT 2012-2121)
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Lefebvre AH, Ballal DR (2010) Gas turbine combustion: alternative fuels and emissions, 3rd edn. CRC press, Taylor & Francis
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Initiatives for next-generation aviation fuels, report of the initiatives for next-generation aviation fuels (English translation of the original Japanese version) (2015) https://​urldefense.​proofpoint.​com/​v2/​url?​u=​http-3A_​_​aviation.​u-2Dtokyo.​ac.​jp_​inaf_​roadmap-5Fen.​pdf&​d=​DwIFJg&​c=​vh6FgFnduejNhPPD​0fl_​yRaSfZy8CWbWnIf4​XJhSqx8&​r=​eX-g8gqe3d-GoWycz_​7rrFqNjbM5XPbKrf​S6HBeL60XuS2oval​zEMTtidqJEphSc&​m=​QAcgkidUX2FbqCIF​XX90FcMspD02ZtK_​ljfACAXNeK0&​s=​v6HBureYBA0U46R9​_​UzLyTP5EuPsdo-CYZOzv-D6e08&​e=​. Accessed 18 June 2020
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Makida M, Yamada H, Shimodaira K (2014) Detailed research on rich-lean type single sector and full annular combustor for small air-craft engine. In: 29th congress of the international council of the aero-nautical sciences (ICAS 2014), St. Petersburg, Russia (ICAS2014-0628)
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Hottel HC, Broughton FP (1932) Ind Eng Chem 4(2):166–174
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Döpelheuer A (2001) Quantities, characteristics and reduction potential of aircraft engine emissions. SAE 2001-01-3008
Metadata
Title
Emission Characteristics on Combustion of HEFA Alternative-Aviation Fuel Under In-Flight Conditions
Authors
Hitoshi Fujiwara
Keiichi Okai
Copyright Year
2021
Publisher
Springer Singapore
Book
Advances in IC Engines and Combustion Technology

Print ISBN: 978-981-15-5995-2

Electronic ISBN: 978-981-15-5996-9

Copyright Year: 2021

DOI
https://doi.org/10.1007/978-981-15-5996-9_4

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