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Evaluation of dissociated and steam-reformed methanol as automotive engine fuelsDissociated and steam reformed methanol were evaluated as automotive engine fuels. Advantages and disadvantages in using methanol in the reformed rather than liquid state were discussed. Engine dynamometer tests were conducted with a four cylinder, 2.3 liter, spark ignition automotive engine to determine performance and emission characteristics operating on simulated dissociated and steam reformed methanol (2H2 + CO and 3H2 + CO2 respectively), and liquid methanol. Results are presented for engine performance and emissions as functions of equivalence ratio, at various throttle settings and engine speeds. Operation on dissociated and steam reformed methanol was characterized by flashback (violent propagation of a flame into the intake manifold) which limited operation to lower power output than was obtainable using liquid methanol. It was concluded that: an automobile could not be operated solely on dissociated or steam reformed methanol over the entire required power range - a supplementary fuel system or power source would be necessary to attain higher powers; the use of reformed mechanol, compared to liquid methanol, may result in a small improvement in thermal efficiency in the low power range; dissociated methanol is a better fuel than steam reformed methanol for use in a spark ignition engine; and use of dissociated or steam reformed methanol may result in lower exhaust emissions compared to liquid methanol.
Document ID
19840019840
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lalk, T. R.
(Texas A&M Univ. College Station, TX, United States)
Mccall, D. M.
(Texas A&M Univ. College Station, TX, United States)
Mccanlies, J. M.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1984
Subject Category
Propellants And Fuels
Report/Patent Number
DOE/NASA/0142-1
NAS 1.26:168242
NASA-CR-168242
Report Number: DOE/NASA/0142-1
Report Number: NAS 1.26:168242
Report Number: NASA-CR-168242
Accession Number
84N27909
Funding Number(s)
CONTRACT_GRANT: NAG3-142
CONTRACT_GRANT: DE-AI01-77CS-51044
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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