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

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Experimental set ups and diagnostics<br />

7<br />

6<br />

5<br />

(1) (2)<br />

(3)<br />

Pressure (bar)<br />

4<br />

3<br />

2<br />

1<br />

0<br />

Shot 1<br />

Shot 2<br />

Shot 3<br />

0 10 20 30 40 50 60 70 80 90 100<br />

Time (ms)<br />

Figure 3.8 - Pressure versus time in rectangu<strong>la</strong>r chamber<br />

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

Three <strong>combustion</strong> stages can be observed from the pressure versus time curves<br />

shown in the figures 3.7 and 3.8: (1) <strong>de</strong>velopment of a f<strong>la</strong>me kernel followed by f<strong>la</strong>me<br />

propagation at constant pressure; (2) f<strong>la</strong>me <strong>de</strong>velopment followed by rapid pressure<br />

increase and (3) f<strong>la</strong>me quenching followed by burned gases cooling.<br />

The first stage, that has a changeable duration in accordance with the initial conditions<br />

of the mixture, corresponds to the formation of the initial f<strong>la</strong>me kernel. The ignition is<br />

provoked by a spark of duration of approximately 5 ms and allows inf<strong>la</strong>ming the mixture<br />

creating a f<strong>la</strong>me kernel that <strong>de</strong>velops at sensibly constant pressure. During this phase,<br />

f<strong>la</strong>me <strong>de</strong>velopment could be difficult. In one hand, the reduced f<strong>la</strong>me radius makes the<br />

curvature effect more significant. On the other hand, the electro<strong>de</strong>s can provoke the<br />

quenching of the f<strong>la</strong>me due to heat absorption. In the second stage, a stable f<strong>la</strong>me is<br />

established. It begins when the pressure starts to increase and ends when the<br />

pressure reaches its maximum value. Fisson et al. (1994), shown that a well<br />

established f<strong>la</strong>me is obtained when the pressure reaches 1.5 times the initial pressure.<br />

At the end of this stage, the f<strong>la</strong>me approaches the wall magnifying the heat losses,<br />

which can vio<strong>la</strong>te the hypothesis of adiabatic compression. For this reason, the<br />

maximum pressure P max is lower than the adiabatic pressure P v which would be<br />

obtained if the process were adiabatic throughout all this phase. The third and <strong>la</strong>st<br />

phase represents the end of <strong>combustion</strong>, where the f<strong>la</strong>me reaches the wall nonuniformly.<br />

On the double effect of the thermal losses and the <strong>de</strong>activation of the free<br />

radicals, the f<strong>la</strong>me is quenched followed by the burned gases cooling.<br />

72

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