24.08.2013 Views

MODELING CHAR OXIDATION AS A FUNCTION OF PRESSURE ...

MODELING CHAR OXIDATION AS A FUNCTION OF PRESSURE ...

MODELING CHAR OXIDATION AS A FUNCTION OF PRESSURE ...

SHOW MORE
SHOW LESS

Create successful ePaper yourself

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

Langmuir rate equation, the reaction order should increase with temperature. However,<br />

some experiments showed that the reaction order of the char-oxygen reaction decreased<br />

with increased particle temperature at constant oxygen concentration (Ranish and Walker,<br />

1993; Banin et al., 1997a). These observations indicated that either the adsorption-<br />

desorption interpretation of the Langmuir rate equation or the belief that E a is less than E d<br />

is not true.<br />

The understanding from this project is: 1) the mechanism of the Langmuir rate<br />

equation is not well understood, and the adsorption-desorption interpretation may not be<br />

true; 2) impurities can affect the activation energies of different processes to different<br />

extents. Keeping these two points in mind, it is no surprise that E 1 (E a is not used since<br />

the mechanism is not known) can be less than, equal to, or greater than E 0.<br />

Observed Activation Energy in Zone I<br />

An expression (Eq. 7.22) was developed to relate the observed activation energy<br />

to the activation energies of k 1p and K p under Zone I conditions, provided that the oxygen<br />

partial pressure at the external surface of the particle (P os) is constant.<br />

HP-CBK Model<br />

The High Pressure Carbon Burnout Kinetics model (HP-CBK) was developed in<br />

this project. This new model was based on the CBK model developed by Hurt et al.<br />

(1998b). The HP-CBK was shown to be satisfactory in modeling char oxidation at both<br />

atmospheric and elevated pressures. The HP-CBK model used: 1) intrinsic Langmuir<br />

kinetics rather than global n-th order kinetics; 2) the analytical solution of the<br />

125

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

Saved successfully!

Ooh no, something went wrong!