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A symmetric device for stabilization of a flame includes a primary oxidant pipe and a fuel pipe. The fuel pipe is internal to the primary oxidant pipe creating a primary oxidant conduit. A secondary oxidant pipe is internal to the fuel pipe creating a fuel conduit. A primary oxidant source supplies

A symmetric device for stabilization of a flame includes a primary oxidant pipe and a fuel pipe. The fuel pipe is internal to the primary oxidant pipe creating a primary oxidant conduit. A secondary oxidant pipe is internal to the fuel pipe creating a fuel conduit. A primary oxidant source supplies oxidant to the primary oxidant conduit. A fuel source supplies fuel to the fuel conduit. A secondary oxidant source supplies oxidant to the secondary oxidant pipe. The first oxidant velocity is greater than the second oxidant velocity and the fuel velocity is less than the second oxidant velocity. The primary oxidant pipe end extends past the fuel pipe forward end and the fuel pipe forward end extends past the secondary oxidant pipe end. A mismatch in velocity between fuel and oxidant generates a large scale vortex. An asymmetric embodiment is also provided.

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1. A device for stabilization of a flame in a combustion apparatus, comprising:(a) a primary oxidant pipe having a primary oxidant pipe internal surface and a primary oxidant pipe forward end;(b) a fuel pipe having a fuel pipe internal surface, a fuel pipe external surface, and a fuel pipe forward e

1. A device for stabilization of a flame in a combustion apparatus, comprising:(a) a primary oxidant pipe having a primary oxidant pipe internal surface and a primary oxidant pipe forward end;(b) a fuel pipe having a fuel pipe internal surface, a fuel pipe external surface, and a fuel pipe forward end, said fuel pipe disposed at least partially internal to said primary oxidant pipe, wherein a hollow primary oxidant flow conduit is formed between said fuel pipe external surface and said primary oxidant pipe internal surface;(c) a secondary oxidant pipe having a secondary oxidant pipe external surface and a secondary oxidant pipe forward end, said secondary oxidant pipe disposed at least partially internal to said fuel pipe, wherein a hollow fuel flow conduit is formed between said secondary oxidant pipe external surface and said fuel pipe internal surface, and wherein said secondary oxidant pipe has an internal, secondary oxidant conduit;(d) a primary oxidant flow source for supplying oxidant at a first oxidant flow velocity to said primary oxidant conduit;(e) a fuel flow source for supplying a fuel at a fuel flow velocity to said fuel flow conduit;(f) a secondary oxidant flow source for supplying oxidant at a second oxidant flow velocity to said secondary oxidant conduit;(g) wherein said first oxidant flow velocity is greater than said second oxidant flow velocity and said fuel flow velocity is less than said second oxidant flow velocity; and(h) wherein said primary oxidant pipe end extends past said fuel pipe forward end and said fuel pipe forward end extends past said secondary oxidant pipe end;whereby a mismatch in velocity between flowing fuel and flowing oxidant generates a large scale vortex of the oxidant and fuel as they mix. 2. The device for stabilization of a flame of claim 1, wherein the first oxidant velocity is in a range from about 30 feet per second to about 90 feet per second. 3. The device for stabilization of a flame of claim 1, wherein the fuel flow velocity is in a range from about 2 feet per second to about 6 feet per second. 4. The device for stabilization of a flame of claim 1, wherein the second oxidant flow velocity is in a range from about 15 feet per second to about 45 feet per second. 5. The device for stabilization of a flame of claim 1, wherein the first oxidant flow velocity is greater than 30 ft./sec., the fuel flow velocity is less than 20 ft./sec. and the second oxidant flow velocity is between the first oxidant velocity and the fuel flow velocity. 6. A device for stabilization of a flame in a combustion apparatus, comprising:(a) a primary oxidant pipe having a primary oxidant pipe internal surface, a circular cross-sectional shape of a primary oxidant pipe diameter, and a primary oxidant pipe forward end;(b) a fuel pipe having a fuel pipe internal surface, a fuel pipe external surface, a circular cross-sectional shape of a fuel pipe diameter, and a fuel pipe forward end, said fuel pipe disposed coaxial to said primary oxidant pipe, and at least a portion of said fuel pipe disposed internal to said primary oxidant pipe, wherein a hollow cylindrical primary oxidant flow conduit is formed between said fuel pipe external surface and said primary oxidant pipe internal surface;(c) a secondary oxidant pipe having a secondary oxidant pipe external surface, a circular cross-sectional shape of a secondary oxidant pipe diameter, and a secondary oxidant pipe forward end, said secondary oxidant pipe disposed coaxial to said primary oxidant pipe, and at least a portion of said secondary oxidant pipe disposed internal to said fuel pipe, wherein a hollow cylindrical fuel flow conduit is formed between said secondary oxidant pipe external surface and said fuel pipe internal surface, and wherein said secondary oxidant pipe has an internal secondary oxidant flow conduit;(d) a primary oxidant flow source for supplying oxidant at a first oxidant flow velocity to said primary oxidant conduit;(e) a fuel flow sour ce for supplying a fuel at a fuel flow velocity to said fuel flow conduit;(f) a secondary oxidant flow source for supplying oxidant at a second oxidant flow velocity to said secondary oxidant conduit;(g) wherein said first oxidant flow velocity is greater than said second oxidant flow velocity and said fuel flow velocity is less than said second oxidant flow velocity; and(h) wherein said primary oxidant pipe end extends past said fuel pipe forward end by a first length and said fuel pipe forward end extends past said secondary oxidant pipe end by a second length;whereby a mismatch in velocity between flowing fuel and flowing oxidant generates a large scale vortex of the oxidant and fuel as they mix. 7. The device for stabilization of a flame of claim 6, wherein the first oxidant velocity is in a range from about 30 feet per second to about 90 feet per second. 8. The device for stabilization of a flame of claim 6, wherein the fuel flow velocity is in a range from about 2 feet per second to about 6 feet per second. 9. The device for stabilization of a flame of claim 6, wherein the second oxidant flow velocity is in a range from about 15 feet per second to about 45 feet per second. 10. The device for stabilization of a flame of claim 6, wherein a ratio of said first length to said fuel pipe diameter is approximately 1 to 3. 11. The device for stabilization of a flame of claim 6, wherein a ratio of said first length to said primary oxidant pipe diameter is approximately 1 to 3. 12. The device for stabilization of a flame of claim 6, wherein a ratio of said second length to said secondary oxidant pipe diameter is approximately 1 to 3. 13. The device for stabilization of a flame of claim 6, wherein the first oxidant velocity is in a range from about 30 feet per second to about 90 feet per second, the fuel flow velocity is in a range from about 2 feet per second to about 6 feet per second, the second oxidant flow velocity is in a range from about 15 feet per second to about 45 feet per second, a ratio of said first length to said fuel pipe diameter is approximately 1 to 3, a ratio of said first length to said primary oxidant pipe diameter is approximately 1 to 3, and a ratio of said second length to said secondary oxidant pipe diameter is approximately 1 to 3. 14. The device for stabilization of a flame of claim 6, wherein the first oxidant flow velocity is greater than 30 ft./sec., the fuel flow velocity is less than 20 ft./sec. and the second oxidant flow velocity is between the first oxidant velocity and the fuel flow velocity. 15. A device for stabilization of a flame in a combustion apparatus, comprising:(a) an oxidant pipe having an oxidant pipe internal surface and an oxidant pipe forward end;(b) a fuel pipe having a fuel pipe internal surface, a fuel pipe external surface, and a fuel pipe forward end, said fuel pipe disposed at least partially internal to said oxidant pipe, wherein a hollow oxidant flow conduit is formed between said fuel pipe external surface and said oxidant pipe internal surface;(c) an oxidant feed pipe connected to said oxidant pipe, said oxidant feed pipe connected at an angle to said oxidant pipe such that an oxidant flowing through said oxidant feed pipe is adapted to travel through said oxidant feed pipe and impinge on said fuel pipe external surface and then travel through said oxidant flow conduit to said fuel pipe forward end;(d) an oxidant flow source for supplying the oxidant at an oxidant flow velocity to said oxidant feed pipe;(e) a fuel flow source for supplying a fuel at a fuel flow velocity to said fuel pipe;(f) wherein said oxidant flow velocity is greater than said fuel flow velocity; and(g) wherein said oxidant pipe forward end extends past said fuel pipe forward end;whereby a mismatch in velocity between flowing fuel and flowing oxidant generates a large scale vortex of the oxidant and fuel as they mix. 16. The device for stabilization of a flame of claim 15, wherein the oxidant flow vel ocity is in a range from about 10 feet per second to about 50 feet per second. 17. The device for stabilization of a flame of claim 15, wherein the fuel flow velocity is in a range from about 2 feet per second to about 10 feet per second. 18. The device for stabilization of a flame of claim 15, wherein said oxidant feed pipe is connected at an angle of about ninety degrees to said oxidant pipe. 19. A device for stabilization of a flame in a combustion apparatus, comprising:(a) an oxidant pipe having an oxidant pipe internal surface, a circular cross-sectional shape of an oxidant pipe diameter and an oxidant pipe forward end;(b) a fuel pipe having a fuel pipe internal surface, a fuel pipe external surface, a circular cross-sectional shape of a fuel pipe diameter, and a fuel pipe forward end, said fuel pipe disposed coaxial to said oxidant pipe, and at least a portion of said fuel pipe disposed internal to said oxidant pipe, wherein a hollow cylindrical oxidant flow conduit is formed between said fuel pipe external surface and said oxidant pipe internal surface;(c) an oxidant feed pipe connected to said oxidant pipe, said oxidant feed pipe having an oxidant feed pipe diameter and connected at an angle to said oxidant pipe such that an oxidant flowing through said oxidant feed pipe is adapted to travel through said oxidant feed pipe and impinge on said fuel pipe external surface and then travel through said oxidant flow conduit to said fuel pipe forward end;(d) an oxidant flow source for supplying the oxidant at an oxidant flow velocity to said oxidant feed pipe;(e) a fuel flow source for supplying a fuel at a fuel flow velocity to said fuel pipe;(f) wherein said oxidant flow velocity is greater than said fuel flow velocity; and(g) wherein said oxidant pipe forward end extends past said fuel pipe forward end by a first length and said fuel pipe extends past an uppermost point of an internal surface of said oxidant feed pipe by a second length;whereby a mismatch in velocity between flowing fuel and flowing oxidant generates a large scale vortex of the oxidant and fuel as they mix. 20. The device for stabilization of a flame of claim 19, wherein the oxidant flow velocity is in a range from about 10 feet per second to about 50 feet per second. 21. The device for stabilization of a flame of claim 19, wherein the fuel flow velocity is in a range from about 2 feet per second to about 10 feet per second. 22. The device for stabilization of a flame of claim 19, wherein said oxidant feed pipe is connected at an angle of about ninety degrees to said oxidant pipe. 23. The device for stabilization of a flame of claim 19, wherein a ratio of said first length to said oxidant feed pipe diameter is approximately 0.5 to 2. 24. The device for stabilization of a flame of claim 19, wherein a ratio of said second length to said fuel pipe diameter is approximately 1 greater than or equal to about 1. 25. The device for stabilization of a flame of claim 19, wherein a ratio of said oxidant pipe diameter to said fuel pipe diameter is approximately 1.2 to 1.8. 26. The device for stabilization of a flame of claim 19, wherein the oxidant flow velocity is in a range from about 10 feet per second to about 50 feet per second, the fuel flow velocity is in a range from about 2 feet per second to about 10 feet per second, said oxidant feed pipe is connected at an angle of about ninety degrees to said oxidant pipe, a ratio of said first length to said oxidant feed pipe diameter is approximately 0.5 to 2, a ratio of said second length to said fuel pipe diameter is greater than or equal to 1, and a ratio of said oxidant pipe diameter to said fuel pipe diameter is approximately 1.2 to 1.8.