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 ...

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tel-00623090, version 1 - 13 Sep 2011

Chapter 4 CHAPTER 4 EXPERIMENTAL AND NUMERICAL LAMINAR SYNGAS COMBUSTION Syngas obtained from gasification of biomass is considered to be an attractive new fuel, especially for stationary power generation. tel-00623090, version 1 - 13 Sep 2011 As reported in chapter 2 there is considerable variation in the composition of syngas due to various sources and processing methods. Continuous variation in the composition of the generated syngas from a given gasification source is another challenge in designing efficient end use applications such as burners and combustion chambers to suit changes in fuel composition. Designing such combustion appliances needs fundamental understanding of the implications of syngas composition for its combustion characteristics, such as laminar burning velocity and flammability limits. Laminar burning velocity for single component fuels such as methane (Hassan et al., 1998; Gu et al., 2000); and hydrogen (Aung et al., 1997; Bradley et al., 2007) are abundantly available in the literature for various operating conditions. Burning velocity studies on H 2 –O 2 –inert (such as N 2 , CO 2 , Ar, and He) are also available (Aung et al., 1998; Lamoureux et al., 2003). Some studies on burning velocities are also available for binary fuel mixtures such as H 2 –CH 4 (Halter et al., 2005; Coppens et al., 2007), and H 2 –CO (Vagelopoulos and Egolfopoulos, 1994; Sun et al., 2007). Vagelopoulos and Egolfopoulos, (1994) measured burning velocities of H 2 –CO mixtures using a counter flow flame technique and reported that addition of 6% or more hydrogen to H 2 –CO made the response of the H 2 –CO mixture more similar to the kinetics of hydrogen than to that of CO. McLean et al., (1994) measured unstretched laminar burning velocities for 5%H 2 – 95%CO and 50%H 2 – 50%CO mixtures using constant-pressure outwardly propagating spherical flames to evaluate the rate of the CO + OH reaction. Brown et al., (1996) reported flame stretch effects on burning velocities of H 2 –air, 50%H 2 – 50%CO–air and 5%H 2 –95%CO–air mixtures under atmospheric condition. Values of Markstein length for 50%H 2 –50%CO–air mixtures were found to be very similar to those of pure H 2 –air mixtures. It was concluded that H 2 was the dominant species and governed the Markstein length behavior for the 50% H 2 – 50% CO–air mixture. Hassan et al., (1997) reported the effects of positive stretch rate on burning velocities of H 2 –CO mixtures under different mixture conditions by varying the H 2 fraction in the fuel from 3 to 50% by volume using constant-pressure outwardly propagating spherical flames. 85

Chapter 4<br />

CHAPTER 4<br />

EXPERIMENTAL AND NUMERICAL LAMINAR SYNGAS<br />

COMBUSTION<br />

Syngas obtained from gasification of biomass is consi<strong>de</strong>red to be an attractive new<br />

fuel, especially for stationary power generation.<br />

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

As reported in chapter 2 there is consi<strong>de</strong>rable variation in the composition of syngas<br />

due to various sources and processing methods. Continuous variation in the<br />

composition of the generated syngas from a given gasification source is another<br />

challenge in <strong>de</strong>signing efficient end use applications such as burners and <strong>combustion</strong><br />

chambers to suit changes in fuel composition. Designing such <strong>combustion</strong> appliances<br />

needs fundamental un<strong>de</strong>rstanding of the implications of syngas composition for its<br />

<strong>combustion</strong> characteristics, such as <strong>la</strong>minar burning velocity and f<strong>la</strong>mmability limits.<br />

Laminar burning velocity for single component fuels such as methane (Hassan et al.,<br />

1998; Gu et al., 2000); and hydrogen (Aung et al., 1997; Bradley et al., 2007) are<br />

abundantly avai<strong>la</strong>ble in the literature for various operating conditions. Burning velocity<br />

studies on H 2 –O 2 –inert (such as N 2 , CO 2 , Ar, and He) are also avai<strong>la</strong>ble (Aung et al.,<br />

1998; Lamoureux et al., 2003). Some studies on burning velocities are also avai<strong>la</strong>ble<br />

for binary fuel mixtures such as H 2 –CH 4 (Halter et al., 2005; Coppens et al., 2007), and<br />

H 2 –CO (Vagelopoulos and Egolfopoulos, 1994; Sun et al., 2007). Vagelopoulos and<br />

Egolfopoulos, (1994) measured burning velocities of H 2 –CO mixtures using a counter<br />

flow f<strong>la</strong>me technique and reported that addition of 6% or more hydrogen to H 2 –CO<br />

ma<strong>de</strong> the response of the H 2 –CO mixture more simi<strong>la</strong>r to the kinetics of hydrogen than<br />

to that of CO. McLean et al., (1994) measured unstretched <strong>la</strong>minar burning velocities<br />

for 5%H 2 – 95%CO and 50%H 2 – 50%CO mixtures using constant-pressure outwardly<br />

propagating spherical f<strong>la</strong>mes to evaluate the rate of the CO + OH reaction. Brown et<br />

al., (1996) reported f<strong>la</strong>me stretch effects on burning velocities of H 2 –air, 50%H 2 –<br />

50%CO–air and 5%H 2 –95%CO–air mixtures un<strong>de</strong>r atmospheric condition. Values of<br />

Markstein length for 50%H 2 –50%CO–air mixtures were found to be very simi<strong>la</strong>r to<br />

those of pure H 2 –air mixtures. It was conclu<strong>de</strong>d that H 2 was the dominant species and<br />

governed the Markstein length behavior for the 50% H 2 – 50% CO–air mixture. Hassan<br />

et al., (1997) reported the effects of positive stretch rate on burning velocities of H 2 –CO<br />

mixtures un<strong>de</strong>r different mixture conditions by varying the H 2 fraction in the fuel from 3<br />

to 50% by volume using constant-pressure outwardly propagating spherical f<strong>la</strong>mes.<br />

85

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