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

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Chapter 4<br />

4.2.3.4 Quenching distance and heat flux estimations<br />

After validating the numerical co<strong>de</strong> for updraft and downdraft syngas compositions,<br />

un<strong>de</strong>r various conditions of pressure and equivalence ratios, one can then use it to<br />

predict the quenching distance and heat flux of syngas-air mixtures.<br />

As f<strong>la</strong>me propagates from the centre of the chamber, pressure increases, and<br />

consequently the temperature also increases. This is the compression phase (1) in the<br />

figure 4.50. The heat transfer from the unburned gases to the wall, manly by<br />

conduction, but also marginally by radiation. The heat flux through the wall increases<br />

up to the f<strong>la</strong>me quenching.<br />

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

During wall-f<strong>la</strong>me interaction, the f<strong>la</strong>me transfer in average one third of its thermal<br />

power to the wall (Boust, 2006), which makes a heat flux peak to appear. The f<strong>la</strong>me is<br />

quenched at a finite distance to the wall, the quenching distance. It remains, therefore,<br />

a thin <strong>la</strong>yer of unburned gases between the burned gases and the wall. The instant of<br />

the heat flux peak is less reproducible than its amplitu<strong>de</strong>. In fact, such instant is<br />

somewhere between the inflexion point of the pressure curve and the instant of<br />

maximum pressure. During this phase (2), the wall-f<strong>la</strong>me interaction is gradually<br />

dispersed throughout the chamber, which exp<strong>la</strong>ins the inflexion point in the pressure<br />

curve. The existence of the phase (2) indicates that <strong>combustion</strong> is not strictly spherical.<br />

After the peak of pressure, the <strong>combustion</strong> phase gives p<strong>la</strong>ce to the cooling phase (3).<br />

The wall heat losses are now only due to the burned gases heat source. The heat<br />

transfer is ma<strong>de</strong> through the thin <strong>la</strong>yer of unburned gases between the burned gases<br />

and wall.<br />

1.0<br />

P<br />

(1)<br />

(2)<br />

(3)<br />

P (MPa) ; Qw (MW/m 2 )<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

Qw<br />

--------- d2P/dt2<br />

0.0<br />

0 50 100 150 200 250 300<br />

Time (ms)<br />

Figure 4.50 – Combustion <strong>de</strong>velopment in spherical chamber fluidized bed syngas.<br />

135

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