Claims
- 1. A method of combustion, comprising providing a feed stream of pulverulent solid hydrocarbonaceous fuel in a gaseous carrier,
obtaining from said feed stream at least one obtained stream comprising said fuel and said carrier and having a ratio of fuel to carrier that is higher than the ratio of fuel to carrier of said feed stream, feeding said obtained stream and air from a burner to a combustion chamber, injecting oxygen into said obtained stream at or near said burner, and combusting the coal in said obtained stream in said combustion chamber with said air and oxygen in a flame that has a fuel-rich flame zone, wherein the amount of said oxygen is less than 25% of the stoichiometric amount required for complete combustion of said fuel and keeps the zone fuel-rich, while reducing the amount of air fed through said burner by an amount containing sufficient oxygen that the overall combustion zone stoichiometric ratio varies by not more than 10% compared to the stoichiometric ratio without said addition of oxygen.
- 2. A method according to claim 1 wherein the fuel rich flame zone stoichiometric ratio is between 0.6 and 1.0.
- 3. A method according to claim 1 wherein the fuel rich flame zone stoichiometric ratio is between 0.7 and 0.85.
- 4. A method according to claim 1 further comprising adding air from a source other than said burner into a region within said combustion chamber outside said fuel-rich flame zone to establish a fuel rich primary combustion zone, in an amount containing at least sufficient oxygen that the total amount of oxygen fed into said combustion chamber is at least the stoichiometric amount needed for complete combustion of said fuel.
- 5. A method according to claim 4 wherein the primary combustion zone stoichiometric ratio is between 0.6 and 1.0.
- 6. A method according to claim 4 wherein the primary combustion zone stoichiometric ratio is between 0.7 and 0.85.
- 7. A method according to claim 1 wherein said fuel is coal.
- 8. A method according to claim 7 wherein the fuel rich flame zone stoichiometric ratio is between 0.6 and 1.0.
- 9. A method according to claim 7 wherein the fuel rich flame zone stoichiometric ratio is between 0.7 and 0.85.
- 10. A method according to claim 7 further comprising adding air from a source other than said burner into a region within said combustion chamber outside said fuel-rich flame zone to establish a fuel rich primary combustion zone, in an amount containing at least sufficient oxygen that the total amount of oxygen fed into said combustion chamber is at least the stoichiometric amount needed for complete combustion of said fuel.
- 11. A method according to claim 10 wherein the primary combustion zone stoichiometric ratio is between 0.6 and 1.0.
- 12. A method according to claim 10 wherein the primary combustion zone stoichiometric ratio is between 0.7 and 0.85.
- 13. A method according to claim 7 wherein said gaseous carrier is air.
- 14. A method according to claim 13 wherein the fuel rich flame zone stoichiometric ratio is between 0.6 and 1.0.
- 15. A method according to claim 13 wherein the fuel rich flame zone stoichiometric ratio is between 0.7 and 0.85.
- 16. A method according to claim 13 further comprising adding air from a source other than said burner into a region within said combustion chamber outside said fuel-rich flame zone to establish a fuel rich primary combustion zone, in an amount containing at least sufficient oxygen that the total amount of oxygen fed into said combustion chamber is at least the stoichiometric amount needed for complete combustion of said fuel.
- 17. A method according to claim 16 wherein the primary combustion zone stoichiometric ratio is between 0.6 and 1.0.
- 18. A method according to claim 16 wherein the primary combustion zone stoichiometric ratio is between 0.7 and 0.85.
- 19. A method according to claim 1 wherein said obtained stream is obtained by passing said feed stream through a venturi.
- 20. A method according to claim 1 wherein said obtained stream is obtained by passing said feed stream through apparatus that imparts a swirling motion to said feed stream.
Parent Case Info
[0001] This application is a continuation-in-part of U.S. patent application Ser. No. 09/757,611, filed Jan. 11, 2001, and claims priority from U.S. Provisional Application No. 60/380,817 filed May 15, 2002 and U.S. Provisional Application No. 60/380,818 filed May 15, 2002. The contents of said three applications are hereby incorporated herein by reference.
Government Interests
[0002] This invention was made with United States Government support under Cooperative Agreement No. DE-FC26-00NT40756 awarded by the Department of Energy. The United States Government has certain rights in the invention.
Provisional Applications (2)
|
Number |
Date |
Country |
|
60380817 |
May 2002 |
US |
|
60380818 |
May 2002 |
US |
Continuation in Parts (1)
|
Number |
Date |
Country |
Parent |
09757611 |
Jan 2001 |
US |
Child |
10194828 |
Jul 2002 |
US |