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

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

Experimental and numerical <strong>la</strong>minar syngas <strong>combustion</strong><br />

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

They stated that as the H 2 concentration in the H 2 –CO mixture increased, the mixture<br />

started behaving simi<strong>la</strong>rly to the H 2 –air mixture and the effect of f<strong>la</strong>me stretch on<br />

burning velocity also became more pronounced. Sun et al., (2007) measured stretchfree<br />

burning velocities for CO–H 2 –air mixtures at different mixing ratios (the values of<br />

the CO/H 2 ratio used were 50:50, 75:25, 95:5, and 99:1), equivalence ratios and<br />

pressures using expanding spherical f<strong>la</strong>mes at constant pressure. They used artificial<br />

air with helium instead of nitrogen to have stable f<strong>la</strong>mes at higher pressures. Burke et<br />

al., (2007) studied the effects of CO 2 on the burning velocity of a 25% H 2 –75% CO<br />

mixture with 12.5%O 2 –87.5%He oxidizer un<strong>de</strong>r stoichiometric conditions and they<br />

varied the CO 2 concentration in the fuel from 0 to 25% using spherically expanding<br />

f<strong>la</strong>mes. They stated that the <strong>la</strong>rgest f<strong>la</strong>me radius for calcu<strong>la</strong>tion of unstretched burning<br />

velocity should be less than 30% of the radius wall in a cylindrical chamber. Natarajan<br />

et al., (2007) investigated the effects of CO 2 on burning velocities of H 2 –CO mixtures<br />

for different H 2 /CO ratios, varying the CO 2 mole fraction in the fuel (0% and 20%), the<br />

equivalence ratio (0.5–1.0), the initial temperature (300–700K), and pressure (1–5<br />

atm). Two measurement techniques were used: one using f<strong>la</strong>me area images of a<br />

conical Bunsen f<strong>la</strong>me and the other based on velocity profile measurements in a onedimensional<br />

stagnation f<strong>la</strong>me.<br />

No extensive <strong>combustion</strong> study is avai<strong>la</strong>ble in the literature for typical syngas<br />

compositions like the ones expressed in chapter 2. This motivated the present work to<br />

choose three typical compositions of syngas and to study the <strong>la</strong>minar burning velocity<br />

and f<strong>la</strong>me stability. These typical syngas compositions were selected from Bridgwater,<br />

(1995) and are shown in the Table 4.1.<br />

Table 4.1 – Syngas compositions (% by volume)<br />

Gasifier<br />

Gas composition<br />

(% by volume) HHV<br />

(MJ/m 3 )<br />

H 2 CO CO 2 CH 4 N 2<br />

Updraft 11 24 9 3 53 5.5<br />

Downdraft 17 21 13 1 48 5.7<br />

Fluidized bed 9 14 20 7 50 5.4<br />

There are also gaps in the fundamental un<strong>de</strong>rstanding of syngas <strong>combustion</strong><br />

characteristics, especially at elevated pressures that are relevant to practical<br />

combustors. In this chapter, constant volume spherically expanding f<strong>la</strong>mes are used to<br />

<strong>de</strong>termine a burning velocity corre<strong>la</strong>tion valid for engine conditions.<br />

86

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

Saved successfully!

Ooh no, something went wrong!