| DOI | Resolve DOI: https://doi.org/10.1115/GT2011-45133 |
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| Author | Search for: Chishty, W.A.1; Search for: Davison, C.R.1; Search for: Bird, J.1; Search for: Chan, T.; Search for: Cuddihy, K.; Search for: McCurdy, M.; Search for: Barton, P.; Search for: Krasteva, A.; Search for: Poitras, P. |
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| Affiliation | - National Research Council of Canada
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| Format | Text, Article |
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| Conference | ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011, 6 June 2011 through 10 June 2011, Vancouver, BC |
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| Subject | Aviation fuel; Aviation industry; Camelina; Economic sustainability; Emission data; Energy security; Engine performance; Engine speed; Flight testing; Jet A-1; Life cycle impact assessment; Particulate Matter; Power settings; Aircraft engines; Aviation; Carbon dioxide; Carbon monoxide; Climate change; Exhibitions; Jet engines; Machine design; Nitrogen oxides; Standards; Alternative fuels |
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| Abstract | To address the global fuel challenges of energy security, economic sustainability and climate change the stakeholders of aviation industry are actively pursuing the development and qualification of alternative 'drop-in' fuels. New standards will be required to regulate the use of these new fuels, which requires not only fuel specification and rig/engine and flight testing but also an emission life cycle impact assessment of these fuels. This paper reports on emission data measured at various simulated altitudes and engine speeds from a jet engine operated on conventional and alternative aviation fuels. The work was conducted as part of on-going efforts by departments within the Government of Canada to systematically assess regulated as well as non-regulated emissions from the use of alternative aviation fuels. The measurements were performed on an instrumented 1000 N-thrust turbojet engine using a baseline conventional Jet A-1 fuel and a semisynthetic (50/50) blend with Camelina based Hydroprocessed Renewable Jet (JP8-HRJ8) fuel. Emission results reported here include carbon dioxide, carbon monoxide, nitrogen oxides and particulate matter measured at several simulated altitudes and power settings. In order to ensure that the assessments have a common baseline, relevant engine performance and operability data were also recorded. Copyright © 2011 by ASME. |
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| Publication date | 2011 |
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| In | |
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| Language | English |
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| Peer reviewed | Yes |
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| NPARC number | 21271678 |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | 96741b92-77a1-43da-ae86-09c66a253c12 |
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| Record created | 2014-03-24 |
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| Record modified | 2020-04-21 |
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