Claims
- 1. A combustion system for the production of carbon nanomaterials which comprises:
a) one or more inlets for introducing an oxygen-containing gas and a hydrocarbon fuel gas in the combustion system such that a flame can be established from the gases; b) an optional reaction zone downstream of the flame; c) a droplet delivery apparatus for introducing droplets of a liquid hydrocarbon feedstock into the flame, the reaction zone, or both; and d) an apparatus for collecting condensable products generated in the combustion system.
- 2. The combustion system of claim 1 wherein the droplet delivery apparatus comprises one or more spray nozzles for generating a spray of liquid droplets of hydrocarbon feedstock into the flame or the reaction zone.
- 3. The combustion system of claim 2 wherein the liquid hydrocarbon is mixed with a gas in the spray nozzle or nozzles.
- 4. The combustion system of claim 3 wherein the gas in the spray nozzle is an oxygen-containing gas.
- 5. The combustion system of claim 1 wherein the pressure in the combustion system downstream of the burner surface is maintained at sub-atmospheric pressure.
- 6. The combustion system of claim 1 wherein the pressure in the combustion system downstream of the burner surface is maintained above about 20 torr.
- 7. The combustion system of claim 1 wherein the pressure in the combustion system is maintained between about 200 torr and 20 torr.
- 8. The combustion system of claim 2 wherein the sprayed droplets have a Sauter mean diameter of 40 microns or less.
- 9. The combustion system of claim 2 wherein the spray nozzle used to inject the hydrocarbon feedstock has a spray angle of at least 90 degrees.
- 10. The combustion system of claim 1 wherein the liquid hydrocarbon feedstock comprises 30% or more by weight of polynuclear aromatic hydrocarbons.
- 11. The combustion system of claim 1 wherein the hydrocarbon fuel gas is methane or natural gas.
- 12. The combustion system of claim 1 wherein the flame established from the mixed gases is non-sooting until the introduction of liquid hydrocarbon droplets.
- 13. The combustion system of claim 1 which contains a reaction zone.
- 14. The combustion system of claim 13 wherein the reaction zone is insulated.
- 15. The combustion system of claim 1 which is employed to produce fullerenes, fullerenic soot or both.
- 16. The combustion system of claim 1 which is maintained at sub-atmospheric pressure and which further comprising a burner having a burner surface wherein the one or more inlets for introducing an oxygen-containing gas and a hydrocarbon fuel gas into the combustion system are introduced through the burner and the flame is established at the burner surface.
- 17. The combustion system of claim 16 wherein the burner surface comprises a porous refractory material.
- 18. The combustion system of claim 17 wherein the porous refractory material is a porous refractory plate.
- 19. The combustion system of claim 17 wherein the porous refractory material comprises refractory particles.
- 20. The combustion system of claim 16 wherein the burner further comprises a plenum.
- 21. The combustion system of claim 20 wherein the burner plenum is in thermal contact with a liquid to provide temperature control of the plenum.
- 22. The combustion system of claim 20 further comprising a porous refractory material between the plenum and the burner surface.
- 23. The combustion system of claim 22 wherein the burner plenum is separated from the porous refractory by a porous metal frit.
- 24. The combustion system of claim 16 wherein the flame from the burner is non-sooting until the addition of the liquid hydrocarbon from the nozzle.
- 25. The combustion system of claim 16 wherein the droplet delivery apparatus is a single spray nozzle that is axially aligned with the burner.
- 26. The combustion system of claim 16 wherein the droplet delivery apparatus comprises a plurality of spray nozzles arranged radially around the burner for injecting droplets into the flame or the reaction zone.
- 27. The combustion system of claim 16 which comprises a reaction zone.
- 28. The combustion system of claim 27 wherein the reaction zone is insulated.
- 29. The combustion system of claim 16 wherein the liquid hydrocarbon feedstock is introduced into the flame or the reaction zone through one or more spray nozzles and mixed with a gas in the spray nozzle or nozzles.
- 30. The combustion system of claim 29 wherein the gas in the spray nozzle is an oxygen-containing gas.
- 31. The combustion system of claim 16 wherein the pressure in the combustion system is maintained between about 200 torr and 20 torr.
- 32. The combustion system of claim 16 wherein the liquid hydrocarbon feedstock droplets have a Sauter mean diameter of 40 microns or less.
- 33. The combustion system of claim 16 wherein the liquid hydrocarbon droplets are introduced into the flame or the reaction zone through one or more spray nozzles having a spray angle of at least 90 degrees.
- 34. The combustion system of claim 16 wherein the hydrocarbon fuel gas is methane or natural gas.
- 35. The combustion system of claim 16 wherein the liquid hydrocarbon feedstock comprises 30% or more by weight of polynuclear aromatic hydrocarbons.
- 36. The combustion system of claim 35 wherein the liquid hydrocarbon feedstock is a coal tar distillate or a petroleum distillate.
- 37. The combustion system of claim 35 wherein the hydrocarbon fuel gas is methane or natural gas.
- 38. The combustion system of claim 16 which is employed to produce fullerenes, fullerenic soot or both.
- 39. A method for making carbon nanomaterials which comprises the steps of:
a) establishing a flame from a flow of oxygen-containing gas and a hydrocarbon fuel; and b) introducing droplets of hydrocarbon feedstock into the flame to thereby generate carbon nanomaterials; and c) collecting the carbon nanomaterials formed.
- 40. The method of claim 39 wherein the flame is established at a burner surface.
- 41. The method of claim 39 herein the method is conducted in a combustion system maintained at sub-atmospheric pressure.
- 42. The method of claim 41 wherein the pressure in the combustion system is maintained between about 200 torr and about 20 torr.
- 43. The method of claim 40 wherein the burner surface comprises a porous refractory material.
- 44. The method of claim 43 wherein the porous refractory material is a porous refractory plate.
- 45. The method of claim 43 wherein the porous refractory material comprises refractory particles.
- 46. The method of claim 40 wherein the burner further comprises a plenum.
- 47. The method of claim 46 wherein the burner plenum is in thermal contact with a liquid to provide temperature control of the plenum.
- 48. The combustion system of claim 46 further comprising a porous refractory material between the plenum and the burner surface.
- 49. The combustion system of claim 48 wherein the burner plenum is separated from the porous refractory by a porous metal frit.
- 50. The method of claim 39 further comprising the step of providing a reaction zone upstream of the flame which is thermally insulated to retain heat from the flame and such that liquid hydrocarbon feedstock or products generated from the feedstock are held at or above about 1000° C. for a residence time of at least about 1 millisecond.
- 51. The method of claim 50 wherein droplets are introduced into the flame or the reaction zone employing a droplet delivery apparatus comprising one or more spray nozzles.
- 52. The method of claim 51 wherein the liquid hydrocarbon is mixed with a gas in the spray nozzle.
- 53. The method of claim 52 wherein the gas is oxygen.
- 54. The method of claim 51 wherein the sprayed droplets have a Sauter mean diameter of 40 microns or less.
- 55. The method of claim 51 wherein the spray nozzle used to inject the hydrocarbon feedstock has a spray angle of 90 degrees or more.
- 56. The method of claim 39 wherein the liquid hydrocarbon feedstock comprises 30% by weight or more of polynuclear aromatic hydrocarbon.
- 57. The method of claim 39 wherein the hydrocarbon fuel gas is methane or natural gas.
- 58. The method of claim 39 wherein the flame is non-sooting until the addition of the liquid hydrocarbon droplets.
- 59. The method of claim 39 for producing fullerenes, fullerenic soot or both.
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This application takes priority under 35 U.S.C. 119(e) from U.S. provisional application No. 60/337,750, filed Dec. 5, 2002.
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
[0002] This invention was made with government support from the U.S. Department of Energy under SBIR grant number DE-FG03-98ER82692. The United States government has certain rights in this invention.
Provisional Applications (1)
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Number |
Date |
Country |
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60337750 |
Dec 2001 |
US |