Mixing process for combustion furnaces
Abstract
A system and method for increasing combustion furnace efficiency, including the steps of providing a furnace with a plurality of secondary air injection ducts, asymmetrically positioned in an tangentially reinforcing manner; injecting fuel with substoichiometric primary air through the burners; injecting secondary air through the plurality of secondary air injection ducts; wherein the velocity of the injected air is such that the ratio of the advected air velocity to the furnace width is between about 2 sec −1 to about 150 sec −1 ; thereby increasing combustion efficiency and reactor efficiency via mixing and rotation of the combustion space.
Claims
exact text as granted — not AI-modifiedWe claim:
1 . A method for increasing combustion furnace efficiency, comprising:
providing a furnace with a plurality of secondary air injection ducts, asymmetrically positioned in an opposing manner; injecting fuel with primary air through the burners prior to injection of secondary air; injecting secondary air through the plurality of secondary air injection ducts; wherein the velocity of the injected air is such that the ratio of the velocity to the furnace width is between about 2 sec −1 to about 150 sec −1 ; thereby increasing combustion efficiency and furnace efficiency via swirl, peripheral turbulence, and rotation-induce turbulence of the combustion space.
2 . The method of claim 1 , wherein the temperature of the injected air is between about 40 and about 460 degrees centigrade (10-50% redirected combustion air).
3 . The method of claim 2 , wherein the temperature of the injected air is between about 76 and about 340 degrees centigrade (20-40% redirected combustion air).
4 . The method of claim 1 , wherein the system has at least two levels of secondary air ducts for injection of secondary air.
5 . The method of claim 4 , wherein the system has at least three levels of secondary air ducts for injection of secondary air.
6 . The method of claim 1 , wherein the velocity of the injected air is such that the ratio of the velocity to the furnace width is between about 3 sec −1 to about 60 sec −1 .
7 . A method for increasing combustion furnace efficiency, comprising:
providing a furnace with a plurality of secondary air injection ducts, asymmetrically positioned in an opposing manner; injecting fuel with primary air through the burners prior to injection secondary air; injecting secondary air through the plurality of secondary air injection ducts; wherein the velocity of the injected air is such that the penetration of the injected air is greater than the furnace width by at least about 1.5 widths; thereby increasing furnace efficiency via mixing and rotation of the combustion space.
8 . The method of claim 7 , wherein the temperature of the injected air is between about 40 and about 460 degrees centigrade (10-50% redirected combustion air).
9 . The method of claim 8 , wherein the temperature of the injected air is between about 76 and about 340 degrees centigrade (20-40% redirected combustion air).
10 . The method of claim 7 , wherein the system has at least two levels of secondary air ducts for injection of secondary air.
11 . The method of claim 10 , wherein the system has at least three levels of secondary air ducts for injection of secondary air.
12 . A method for increasing combustion furnace efficiency, comprising:
providing a furnace with a plurality of secondary air injection ducts, asymmetrically positioned in an opposing manner; injecting fuel with primary air through the burners prior to injection secondary air; injecting secondary air through the plurality of secondary air injection ducts; wherein the velocity of the injected air is such that the combustion zone rotates at least one half revolution prior to exiting the furnace; thereby increasing furnace efficiency via mixing and rotation of the combustion space.
13 . The method of claim 12 , wherein the temperature of the injected air is between about 40 and about 460 degrees centigrade (10-50% redirected combustion air).
14 . The method of claim 13 , wherein the temperature of the injected air is between about 76 and about 340 degrees centigrade (20-40% redirected combustion air).
15 . The method of claim 12 , wherein the system has at least two levels of secondary air ducts for injection of secondary air.
16 . The method of claim 15 , wherein the system has at least three levels of secondary air ducts for injection of secondary air.Join the waitlist — get patent alerts
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