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Etude de la combustion de gaz de synthèse issus d'un processus de ...

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Conclusions<br />

conditions, therefore single compression tests were also performed in the RCM<br />

operating with and without <strong>combustion</strong> in or<strong>de</strong>r to i<strong>de</strong>ntify different parameters re<strong>la</strong>ted<br />

with its operation, namely the heat transfer to the walls.<br />

tel-00623090, version 1 - 13 Sep 2011<br />

Higher pressures are obtained with methane-air mixture followed by downdraft-syngas<br />

and <strong>la</strong>stly by updraft-syngas. These results could be endorsed to the heat of reaction of<br />

the fuels and air to fuel ratio un<strong>de</strong>r stoichiometric conditions, but also to burning<br />

velocities. Updraft and downdraft syngas compositions have simi<strong>la</strong>r burning velocities<br />

in <strong>la</strong>minar conditions but the same is not found in turbulent conditions, where the<br />

difference in peak pressure is higher by about 25%. As the turbulent burning velocity is<br />

proportional to the <strong>la</strong>minar burning velocity, analysing the corre<strong>la</strong>tions for <strong>la</strong>minar<br />

burning velocity of the typical syngas compositions <strong>de</strong>veloped on this work show that<br />

the effect of pressure is very significant (coefficient β for updraft is 40% higher in<br />

re<strong>la</strong>tion to downdraft syngas coefficient). The higher pressure used on RCM also<br />

makes temperature to increase due to compression but the effect of temperature on<br />

burning velocity for typical syngas compositions is irrelevant since the coefficient α is of<br />

the or<strong>de</strong>r. Another major finding is that syngas typical compositions are characterized<br />

by high ignition timings due to their low burning velocities.<br />

A simu<strong>la</strong>tion co<strong>de</strong> for the power cycle of syngas-fuelled engines has been <strong>de</strong>veloped,<br />

using a quasi-dimensional mo<strong>de</strong>l with ‘standard’ mo<strong>de</strong>ling assumptions. Mo<strong>de</strong>l testing<br />

has been carried on over <strong>de</strong>tailed experimental data avai<strong>la</strong>ble in literature for hydrogen<br />

and methane, two of the main constituents of syngas. The very good agreement found<br />

allows validating the <strong>de</strong>veloped mo<strong>de</strong>l and applied it to typical syngas compositions. An<br />

attempt to adapt the mo<strong>de</strong>l to the RCM is ma<strong>de</strong> by changing several aspects of the<br />

mo<strong>de</strong>l namely the in-cylin<strong>de</strong>r volume function and burning rate mo<strong>de</strong>l. The comparison<br />

with experimental results obtained in this work in the RCM shows that the adapted<br />

co<strong>de</strong> is able to reproduce fairly well the in-cylin<strong>de</strong>r pressure and that the Woschni<br />

mo<strong>de</strong>l works well in its original formu<strong>la</strong>tion and represent the heat transfer of the RCM<br />

compression stroke.<br />

The validated mo<strong>de</strong>l is then applied to a syngas-fuelled engine in or<strong>de</strong>r <strong>de</strong>termine its<br />

performance. Conclusions can be drawn that typical syngas compositions besi<strong>de</strong>s its<br />

lower heat value and burning velocities can be used on SI engines even at elevated<br />

rotation speeds.<br />

198

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