This invention relates generally to secondary air injection to combustion systems and, particularly, to dampers for secondary air tubes in fossil fuel fired boilers.
Combustion systems are used in numerous industrial environments to generate heat and hot gases. For example, boilers and furnaces burn hydrocarbon fuels, e.g., oil and coal, in stationary combustors to produce heat to raise the temperature of a fluid, e.g., water. Industrial combustors typically employ various burner elements to combust the fuel and air injectors to provide combustion air to ensure complete combustion of the fuel. A typical industrial furnace, whether gas or fossil fired and hereafter referred to as a boiler, typically includes a lower combustion zone and a generally vertically extending flue gas passage.
The air introduced into a combustion system may be staged. Primary air is mixed with the fuel as both are injected into a combustion zone. Secondary air (also known as overfire air) may be injected into a combustion chamber downstream (in the direction of flue gas flow) of the primary combustion zone. The secondary air may be used to burnout any unburned hydrocarbons remaining from the primary combustion zone.
Overfire air is typically injected into the flue gas at a location in the flue gas passage downstream of the combustion zone. The combustion air provided to the combustion zone may be reduced to suppress flame temperature in the combustion zone and NOx formation. Suppressing combustion temperature creates excessive unburned hydrocarbons in the flue gas. The overfire air, introduced above the primary combustion zone, completes combustion of the unburned hydrocarbons which are then converted to carbon dioxide and water.
In conventional boilers, the overfire air is introduced to the flue passage through injection ports in the front or side walls or both of the boiler. The amount of secondary air (overfire air) needed for effective burnout may vary depending on the operating condition of the combustion system. To adjust the amount of secondary air, dampers are closed or opened to vary the amount of secondary air flowing from the secondary air tubes into the flue passage. However, conventional dampers tend to either shut off secondary air flow or allow substantial amounts of air flow. Conventional dampers tend not to effectively allow for adjustable amounts of secondary air. There is a long felt need for an improved damper for a secondary (overfire) air system.
A damper and overfire air duct has been developed for a combustion system having a combustion structure defining a flue gas passage, the damper and overfire air duct including: an inlet to the overfire air duct and an outlet to the duct discharging overfire air into the flue gas passage, and the damper aligned with an axis of the overfire air duct, and having an open position axially distal to the inlet and a closed position at least partially in the inlet and duct, wherein the damper is movable axially between the open and closed positions.
An overfire air duct has been developed for a combustion system having a combustion structure defining a flue gas passage, the damper and overfire air duct comprising: an inlet to the overfire air duct and an outlet to the duct discharging overfire air into the flue gas passage, and the damper aligned with an axis of the overfire air duct, and having an open position axially distal to the inlet and a closed position at least partially in the inlet and duct, wherein the damper is movable axially between the open and closed positions.
A method has been developed to regulate overfire air passing through an overfire air duct and entering a flue gas stream in a combustion system, the method comprising: directing overfire air into an inlet of the overfire air duct, passing the overfire air through the duct and discharging the overfire air into the flue gas stream in the combustion system; adjusting a flow rate of overfire air entering the inlet using a damper adjacent the inlet; moving the damper parallel to an axis of the overfire air duct to increase and decrease the overfire air entering the inlet, wherein the damper having an open position at which the damper is extended out of the inlet and a closed position in which the damper is substantially in the inlet and blocking air entering the inlet.
The fuel/air mixture 18 injected by the combustion devices 16 burns primarily in the combustion zone 12 and generates hot combustion gases that flow upward through the flue gas passage 14. From the combustion zone 12, the hot combustion gases flow into an optional reburn zone 20 into which additional (reburn) fuel 22 is supplied to the hot combustion gases to promote additional combustion.
Downstream of combustion and reburn zones, overfire air (OFA) 24 is injected through an overfire air nozzle(s) 26 into the OFA burnout zone 28 in the flue gas stream. A reducing agent, e.g., nitrogen (N-agent), may be injected into the flue gases with one or more of the streams of overfire air. Downstream of the OFA burnout zone, the combustion flue gas 24 passes through a series of heat exchangers 30 and a particulate control device (not shown), such as an electrostatic precipitator (ESP) or baghouse, that removes solid particles from the flue gas, such as fly ash.
Turning vanes 36, in the inlet port 34 of a hollow elbow conduit 42, turn the overfire air to a direction, e.g., horizontal, that is preferably substantially perpendicular to the flow of flue gases moving up through the structure 11 of the combustion system 10. An annular flange 44 on the elbow conduit provides a coupling for a hollow frustoconical air duct 46 that extends towards a hollow cylindrical end section 48 of the overfire air injector assembly 32. The cylindrical end section includes a flange 50 that provides a coupling mount for the assembly 32 to the wall of the structure 11 of the combustion system 10. For example, the cylindrical end section 48 fits into a circular aperture in the structure wall and the flange 50 is bolted to a mounting ring on the wall and at the circumference of the wall aperture.
The distal end 52 of overfire air injector assembly 32 is hollow and extends a short distance, e.g., one-half to three meters, beyond the wall of the structure and into the flue gas stream. Overfire air is discharged from the distal end 52 and into the flue gas stream at the burnout zone 28, as is shown in
An inner cylindrical air duct 54 extends through the frustoconical duct 46 and cylindrical end section 48. The cylindrical air duct has an air outlet aligned with the distal end 52 of the cylindrical end section. The cylindrical air duct 54 has an inner overfire air passage 56 that extends through the duct from an inlet 58 to the duct. The duct inlet 58 may extend into the interior of a hollow elbow conduit 42. An axially movable damper 60 for the air duct 54 is positioned at the inlet 58.
An annular outer overfire air duct 62 extends between the air duct 54 and an inner wall of the cylindrical end section 48 and an inner wall of the frustoconical duct 46. A swirler 64, e.g., radial array of vanes, may be positioned in the outer overfire air duct 62 to impart a rotation to the overfire air flowing through the outer duct 62. While not shown, a swirler may be positioned in the inner overfire air passage 56. An annular damper 66 may be near the inlet (aligned with flange 44) to the outer overfire air duct 62 to regulate the volumetric rate of overfire air through the duct 62. The damper 66 may be adjusted, e.g., between closing offer overfire air flow to duct 62 and fully open to such air flow, by an actuator 40. The actuator 40 may include a separate actuation arm and hydraulic servo for each damper/louver system controlled by the actuator 40.
The damper 60 is axially mounted on a damper control rod 68. The control rod and damper may slide in and out of the inlet 58 of the inner cylindrical duct 54. The damper 60 is shown fully open in
Even with the damper 60 at the fully closed (see damper in position 60a, a cooling gap 70 may be formed between the outer periphery of the damper 60 and the inner wall of inlet 58 to the duct 54. Air passes through the cooling gap while the damper is in a closed position 60a to cool the end of the duct 54 which is exposed to the radiant heat energy of the combustion in the combustion system.
The rod 68 is supported by a U-shaped mounting bracket 72 having legs 74 that attach to a quarl ring 76. The quarl is a furstoconical metal collar that guides the overfire into the inlet 58 from the elbow conduit 42 (
An actuator 82 (See
The position of the damper 60 with respect to the inlet 58 may be adjusted to account for changes in the operation of the combustion system 10. For example, as the load on the boiler changes, the damper may be adjusted axially in or out to reduce or increase the amount of overfire air entering the flue gases in the combustion system. Further, the damper may be adjusted to provide enhanced emission controls, e.g., nitrous oxide (NOx) control, which may be achieved by increasing or reducing the amount of overfire air entering the flue gases.
The shape of the damper 60 may be such that the outer perimeter of the damper has a diameter that is slightly, e.g., within one quarter inch, smaller than an inside diameter of the duct 54. The damper may be circular in front view and preferably has a front view shape substantially similar to the interior cross-sectional shape of duct 54. The damper may have a simple, convex polygon shape as shown in
The conventional disc damper 160 tends not to provide proportional flow control for the overfire air flowing through the passage 156. In particular, the disc damper tends to rapidly allow substantially a full air flow through the passage as the disc is rotated away from the fully closed position 160a.
There is a long felt need for an inlet damper that provides proportional flow control of overfire air entering an inner overfire air passage. This need is believed to be satisfied by the damper 60 shown in
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
Number | Name | Date | Kind |
---|---|---|---|
823836 | Wiemann | Jun 1906 | A |
1976208 | Agthe et al. | Oct 1934 | A |
4381718 | Carver et al. | May 1983 | A |
5199355 | Larue | Apr 1993 | A |
5205226 | Kitto et al. | Apr 1993 | A |
5724897 | Breen et al. | Mar 1998 | A |
5944506 | Kamal et al. | Aug 1999 | A |
7047891 | Vatsky | May 2006 | B2 |
20030145768 | Vatsky | Aug 2003 | A1 |
20040244367 | Swanson et al. | Dec 2004 | A1 |
Number | Date | Country | |
---|---|---|---|
20080283039 A1 | Nov 2008 | US |