Emissions assessment of alternative aviation fuel at simulated altitudes

DOIResolve DOI: http://doi.org/10.1115/GT2011-45133
AuthorSearch for: ; Search for: ; Search for: ; Search for: ; Search for: ; Search for: ; Search for: ; Search for: ; Search for:
Proceedings titleProceedings of the ASME Turbo Expo
ConferenceASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011, 6 June 2011 through 10 June 2011, Vancouver, BC
Pages5161; # of pages: 11
SubjectAviation 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
AbstractTo 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.
Publication date
AffiliationNational Research Council Canada (NRC-CNRC)
Peer reviewedYes
NPARC number21271678
Export citationExport as RIS
Report a correctionReport a correction
Record identifier96741b92-77a1-43da-ae86-09c66a253c12
Record created2014-03-24
Record modified2016-05-09
Bookmark and share
  • Share this page with Facebook (Opens in a new window)
  • Share this page with Twitter (Opens in a new window)
  • Share this page with Google+ (Opens in a new window)
  • Share this page with Delicious (Opens in a new window)
Date modified: