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U.S. Department of Energy
Office of Scientific and Technical Information

Method and apparatus for in-flight combustion of carbonaceous fuels

Patent ·
OSTI ID:5720667
The method is described of combusting pulverized solid carbonaceous fuel comprising the steps of: (a) introducing such fuel into a combustion chamber near the center of one end thereof; (b) directing at least one stream of oxidizer into the chamber in a manner to provide high velocity rotational flow within the chamber; and (c) regulating the velocities and relative mass flow rates of the fuel and the oxidizer to (1) keep combustion temperatures within a range such that liquid slag is substantially continuously deposited on an inner surface of the chamber and may be removed therefrom separately from gaseous products of combustion, (2) convert most of the carbon content of the fuel particles to oxides of carbon before the particles impinge on the inner walls of the chamber, and (3) maintain a fuel-rich combustion mixture in at least a substantial portion of the combustion zone within the chamber to thereby limit the formation of oxides of nitrogen and/or sulfur.
Assignee:
TRW, Inc., Redondo Beach, CA
Patent Number(s):
US 4586443
OSTI ID:
5720667
Country of Publication:
United States
Language:
English