Combustion system with precombustor
A precombustor having a chamber having a first end and a second end, and an inlet configured to deliver a substantially parallel flow of solid fuel surrounded by oxygen at the first end. The first end further includes a recirculation step and the second end fluidly communicates with a furnace. The inlet and the recirculation step are arranged to form a recirculation zone of at least a portion of the solid fuel and the oxygen. A combustion system and method for operating a combustion system are also disclosed.
1. A precombustor comprising:
a chamber bounded by a first end, outer walls, and a second end; and
an inlet configured to deliver a substantially parallel flow of solid fuel surrounded by oxygen through the first end of the chamber,
wherein the first end of the chamber includes a recirculation step immediately downstream of the inlet and the second end of the chamber fluidly communicates with a furnace;
wherein the inlet and the recirculation step are arranged to form a recirculation zone within the chamber of at least a portion of the solid fuel and the oxygen exiting the inlet, the recirculation step having a step height h from an edge of the inlet to an edge of the chamber defined by the outer walls;
wherein the inlet is further configured to provide recycled flue gas; and
wherein the inlet is further configured to provide recycled flue gas downstream of the recirculation step.
2. The precombustor of claim 1 , wherein the inlet includes an inlet port configured to provide the solid fuel.
3. The precombustor of claim 1 , wherein the precombustor is configured such that:
1.2
≤
D
p
d
≤
2.4
wherein D p is the chamber diameter and d is the inlet diameter.
4. The precombustor of claim 1 , wherein the chamber has length (L) and that is greater than or equal to about 5 times the recirculation step height (h).
5. The precombustor of claim 1 , wherein the precombustor is configured such that:
L
≤
7.4
*
d
+
15.7
*
h
-
9.7
*
h
2
d
wherein L is precombustor length and d is the inlet diameter.
6. The precombustor of claim 1 , wherein the precombustor is configured such that:
0.1 *d≦h≦ 0.7 *d
wherein d is the inlet diameter.
7. The precombustor of claim 1 , wherein the precombustor includes a circular cross-sectional geometry.
8. The precombustor of claim 1 , wherein the precombustor includes a non-circular cross-sectional geometry.
9. The precombustor of claim 1 , wherein the inlet is configured to deliver a second oxygen stream which is at least partially surrounded by fuel.
10. A combustion system comprising:
a furnace; and
at least one precombustor, the at least one precombustor having a chamber bounded by a first end, outer walls, and a second end, and an inlet configured to deliver a substantially parallel flow of solid fuel surrounded by oxygen through the first end of the chamber, the first end further including a recirculation step immediately downstream of the inlet, the second end fluidly communicating with the furnace;
wherein the inlet and the recirculation step are arranged to form a recirculation zone within the chamber of at least a portion of the solid fuel and the oxygen exiting the inlet, the recirculation step having a step height from an edge of the inlet to an edge of the chamber defined by the outer walls;
wherein the inlet is further configured to provide recycled flue gas; and
wherein the inlet is further configured to provide recycled flue gas downstream of the recirculation step.
11. The system of claim 10 , wherein the inlet includes a inlet port configured to provide the solid fuel.
12. The system of claim 10 , wherein the precombustor is configured such that:
1.2
≤
D
p
d
≤
2.4
wherein Dp is the chamber diameter and d is the inlet diameter.
13. The system of claim 10 , wherein the chamber has length (L) and that is greater than or equal to about 5 times the recirculation step height (h).
14. The system of claim 10 , wherein the precombustor is configured such that:
L
≤
7.4
*
d
+
15.7
*
h
-
9.7
*
h
2
d
wherein L is precombustor length and d is the inlet diameter.
15. The system of claim 10 , wherein the precombustor is configured such that:
0.1 *d<=h<= 0.7 *d
wherein d is the inlet diameter.
16. The system of claim 10 , wherein the precombustor includes a circular cross-sectional geometry.
17. The system of claim 10 , wherein the precombustor includes a non-circular cross-sectional geometry.
18. The system of claim 10 , wherein the inlet is configured to deliver a second oxygen stream which is at least partially surrounded by fuel.
19. A method for operating a combustion system comprising:
providing a furnace;
providing at least one precombustor, the precombustor having a chamber bounded by a first end, outer walls, and a second end, and an inlet configured to deliver a substantially parallel flow of solid fuel surrounded by oxygen through the first end of the chamber, wherein the concentration of O 2 is at least 35%, the first end further including a recirculation step immediately downstream of the inlet, the second end fluidly communicating with the furnace; and
delivering the solid fuel and the oxygen to the inlet to form a recirculation zone within the chamber of at least a portion of the solid fuel and the oxygen exiting the inlet, the recirculation step having a step height h from an edge of the inlet to an edge of the chamber defined by the outer walls; wherein the length of the precombustor is sufficient to prevent a flame generated by the system from contacting the precombustor;
wherein the inlet provides recycled flue gas; and
wherein the inlet provides recycled flue gas downstream of the recirculation step.
20. The method of claim 19 , further comprising delivering a second oxygen stream which is at least partially surrounded by fuel.
21. The method of claim 19 wherein the recirculation zone is located within the chamber of the precombustor.