27.12.2013 Views

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

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

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

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Chapter 5<br />

TDC 1.25 ms 2.5 ms 3.75 ms 5.0 ms<br />

6.25 ms 7.5 ms 8.75 ms 10.0 ms 11.25 ms<br />

12.5 ms 13.75 ms 15.0 ms 16.25 ms 17.5 ms<br />

(a)<br />

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

-12.5 ms -11.25 ms -10.0 ms -8.75 ms -7.5 ms<br />

-6.25 ms -5.0 ms -3.75 ms -2.5 ms -1.25 ms<br />

TDC 1.25 ms 2.5 ms 3.75 ms 5.0 ms<br />

6.25 ms 7.5 ms 8.25 ms 10.0 ms<br />

(b)<br />

Figure 5.12 –Direct visualization of stoichiometric updraft syngas-air mixtures <strong>combustion</strong> in a<br />

RCM. (a) Ignition at TDC; (b) ignition at 12.5 ms BTDC.<br />

When the ignition is ma<strong>de</strong> at TDC the <strong>combustion</strong> occurs at constant volume, in the<br />

clearance volume. Direct visualizations show an explosion with fast and turbulent f<strong>la</strong>me<br />

propagation with <strong>combustion</strong> duration of about 17.5 ms. In opposite, the initial phase of<br />

<strong>combustion</strong> shows a quasi-spherical re<strong>la</strong>tively smooth f<strong>la</strong>me kernel specially for ignition<br />

timing of 12.5 ms BTDC. The f<strong>la</strong>me kernel propagation is <strong>la</strong>minar and at some point<br />

experience f<strong>la</strong>ttening due to piston movement reaching the TDC. After that, a change<br />

to constant volume <strong>combustion</strong> occurs. The whole <strong>combustion</strong> duration is around 22.5<br />

ms, a remarkable increase compared with the full constant volume <strong>combustion</strong>. This is<br />

due to the <strong>de</strong>viation from TDC ignition that allows lower initial pressure and<br />

temperature for <strong>combustion</strong> in the compression stroke, lower turbulence intensity as<br />

seen in 3.2.5 and higher heat transfer areas.<br />

149

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!