ePrints@IIScePrints@IISc Home | About | Browse | Latest Additions | Advanced Search | Contact | Help

Combustion studies on concentrated distillery effluents

Patel, NM and Paul, PJ and Mukunda, HS and Dasappa, S (1996) Combustion studies on concentrated distillery effluents. In: 26th International Symposium on Combustion, JUL 28-AUG 02, 1996, NAPLES, ITALY.

[img] PDF
COMBUSTION_STUDIES_ON.pdf - Published Version
Restricted to Registered users only

Download (297kB) | Request a copy
Official URL: http://dx.doi.org/10.1016/S0082-0784(96)80079-8

Abstract

Studies on ignition and combustion of distillery effluent containing solids consisting of 38 +/- 2% inorganics and 62 +/- 2% of organics (cane sugar derivatives) have been carried out in order to investigate the role of droplet size and ambient temperature in the process of combustion. Experiments were conducted on in liquid droplets of effluent having solids concentration 65% and (2) spheres of died (100% solids) effluent of diameters ranging from 0.5 to 25 mm. These spheres were introduced into a furnace where air temperature ranged from 500 to 1000 degrees C, and they burned with two distinct regimes of combustion-flaming and glowing. The ignition delay of the 65% concentration effluent increases with diameter as in the case of nonvolatile droplets, while that of dried spheres appears to be independent of size. The ignition delay shows Arrhenius dependence on temperature. The flaming combustion involves a weight loss of 50-80%, depending on ambient temperature, and the flaming time is given by t(f) similar to d(0)(2), as in the case of liquid fuel droplets and wood spheres. Char glowing involves weight loss of an additional 10-20%, with glowing time behaving as t(c) similar to d(0)(2) as in the case of wood char, even though the inert content of effluent char is as large as 50% compared to 2-3% in wood char Char combustion has been modeled, and the results of this model compare well with the experimental results.

Item Type: Conference Paper
Publisher: Combustion institute
Additional Information: Copyright of this article belongs to Combustion institute.
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering)
Date Deposited: 21 Apr 2011 07:46
Last Modified: 21 Apr 2011 07:46
URI: http://eprints.iisc.ac.in/id/eprint/37080

Actions (login required)

View Item View Item