Carbon black reactor with axial flow burner
AssigneeSid Richardson Carbon & Gasoline Co.
InventorsRobert E. Dollinger, Clinton M. Wright, Theodore A. Ruble, deceased
Life of this patent
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Abstract
An improved burner for combusting gaseous fuel and oxidant gas is provided in which the fuel and oxidant gas are premixed prior to combustion by the turbulence generated by flowing the gases through a mixing zone containing a centrally disposed flow disrupting bluff body positioned in the oxidant gas stream upstream from the point of fuel injection, and a peripheral flow disrupting bluff body disposed at the periphery of the mixing zone. The burner finds particular utility in combination with other elements of a furnace-type carbon black reactor.
Claims9
A burner comprising:
- a housing defining a generally cylindrical mixing zone having a central axis extending longitudinally therethrough;
- means for introducing oxidant gas into said mixing zone to flow axially therethrough;
- means for non-axial introduction of gaseous fuel into said mixing zone at a point downstream of said oxidant gas introduction means, whereby said fuel is released into said flowing oxidant gas;
- mixer means in said mixing zone for admixing said oxidant gas and fuel, said mixer means comprising,
- a central bluff body positioned upstream of said fuel introduction means and centered about the longitudinal axis of said mixing zone and extending radially outwardly from said axis,
- a peripheral bluff body disposed at the periphery of said mixing zone and extending radially inwardly toward said axis,
- said central and peripheral bluff bodies being spaced axially from each other;
- and
- a combustion zone downstream from said mixing zone for combusting said admixed fuel and oxidant gas,
- said combustion zone being free of turbulence generating means whereby the products of combustion thereof may flow linearly therethrough.
A method for producing hot combustion product gases in a burner having a longitudinally extending, generally cylindrical mixing zone and a combustion zone downstream thereof, said method comprising:
- introducing an oxidant gas into said mixing zone and flowing said oxidant gas axially therethrough,
- flowing said oxidant gas around a centrally disposed bluff body in said mixing zone to generate turbulence in said oxidant gas stream downstream of said central bluff body,
- introducing gaseous fuel non-axially into said oxidant gas stream in the area of turbulence generated downstream of said central bluff body to partially admix said fuel and oxidant gas,
- flowing said partially admixed fuel and oxidant gas further downstream through said mixing zone and around a peripheral bluff body disposed about the periphery of said mixing zone and spaced axially from said central bluff body,
- whereby a second area of turbulence is generally downstream of said peripheral bluff body in which second area of turbulence admixture of said fuel and oxidant gas is completed,
- flowing said admixed fuel and oxidant gas into said combustion zone, for combustion therein,
- said combustion zone being free of turbulence generating means whereby the products of combustion thereof may flow linearly therethrough.
Dependencies are inferred from the claim text.