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US 12,173,893 B2Granted
Cylindrical burner apparatus and method
AssigneeGastech Engineering LLC
InventorYul E. Shaffer
Life of this patent
Estimating the term…
Abstract
A cylindrical burner apparatus and method which produce low NOx emissions and low noise levels without being dependent upon a blower, or natural draft, for providing air flow or flue gas recirculation. A flow of combustion air is induced into an initial tube pass of the burner by discharging a gas fuel from a plurality of discharge ports located in the initial tube pass. At the same time, a flow of recycled flue gas is induced through a bypass duct between a subsequent tube pass of the burner and the initial tube pass by discharging one or more jets of gas fuel through the bypass duct.
Claims4
A method of operating a cylindrical burner comprising the steps of:
- a) inducing a flow of combustion air into an interior of a straight initial tube pass of the cylindrical burner through a rearward end of the straight initial tube pass by discharging jets of a gas fuel from at least some of a plurality of fuel jet discharge ports, positioned in the interior of the straight initial tube pass forwardly of the rearward end, to provide an amount of induction and produce an amount of force which are sufficient to operate the cylindrical burner without natural daft and draw the flow of combustion air from outside of the cylindrical burner into the interior of the straight initial tube pass with no natural draft, the gas fuel discharged from the fuel jet discharge ports being combusted with the flow of combustion air in the interior of the straight initial tube pass to produce a flue gas which flows into a subsequent tube pass of the cylindrical burner, wherein the cylindrical burner does not include a blower which blows or draws air into the cylindrical burner and
- b) discharging at least a portion of the flue gas from an exhaust discharge of the cylindrical burner at or downstream of a downstream end of the subsequent tube pass,
- the fuel jet discharge ports comprising one or more first fuel jet discharge ports in the interior of the straight initial tube pass and one or more second fuel jet discharge ports in the interior of the straight initial tube pass,
- each of the one or more first fuel jet discharge ports being oriented to discharge a jet of the gas fuel in the interior of the straight initial tube pass at a first forward angle in a range of from 0° to 30° with respect to a plane extending through the first fuel jet discharge port which is perpendicular to a longitudinal axis of the straight initial tube pass, and
- each of the one or more second fuel jet discharge ports being oriented to discharge a jet of the gas fuel in the interior of the straight initial tube pass at a second forward angle, greater than the first forward angle, in a range of from 3° to 45° with respect to a plane extending through the second fuel jet discharge port which is perpendicular to the longitudinal axis.
2 more elements
A method of operating a cylindrical burner comprising:
- inducing a flow of combustion air into an interior of a straight initial tube pass of the cylindrical burner through a rearward end of the straight initial tube pass by discharging jets of a gas fuel from at least some of a plurality of fuel jet discharge ports, positioned in the interior of the straight initial tube pass forwardly of the rearward end, to provide an amount of induction and produce an amount of force which are sufficient to operate the cylindrical burner without natural draft and draw the flow of combustion air from outside of the cylindrical burner into the interior of the straight initial tube pass with no natural draft, the gas fuel discharged from the fuel jet discharge ports being combusted with the flow of combustion air in the interior of the straight initial tube pass to produce a flue gas which flows into a subsequent tube pass of the cylindrical burner, wherein the cylindrical burner does not include a blower which blows or draws air into the cylindrical burner;
- the fuel jet discharge ports comprising one or more first fuel jet discharge ports in the interior of the straight initial tube pass and one or more second fuel jet discharge ports in the interior of the straight initial tube pass;
- each of the one or more first fuel jet discharge ports being oriented to discharge a jet of the gas fuel in the interior of the straight initial tube pass at a first forward angle in a range of from 0° to 30° with respect to a plane extending through the first fuel jet discharge port which is perpendicular to a longitudinal axis of the straight initial tube pass;
- and
- each of the one or more second fuel jet discharge ports being oriented to discharge a jet of the gas fuel in the interior of the straight initial tube pass at a second forward angle, greater than the first forward angle, in a range of from 3° to 45° with respect to a plane extending through the second fuel jet discharge port which is perpendicular to the longitudinal axis.
2 more elements
Dependencies are inferred from the claim text.