Velocity damper for a recovery boiler

Abstract

A damper for a furnace, the damper including an air port damper body engaged to an air port opening of a furnace; and at least one velocity plate in hinged engagement to the air port damper body so that an air controlling end surface of the at least one velocity plate is substantially aligned to a wall of the furnace at the air port opening when the at least one velocity plate is in a fully opened position.

Description

BACKGROUND

1. Technical Field

The present disclosure generally relates to furnace and furnace components, and more particularly to an apparatus for regulating air flow through a port introducing air to a boiler.

2. Related Art

The chemical recovery boiler is a part of the pulp production process. Specifically, the chemical recovery boiler helps recover and regenerate cooking liquors. The furnace of a chemical recovery boiler for burning black liquor has a front wall, a rear wall and sidewalls. Black liquor spraying devices are disposed on said walls on one or several levels. A plurality of air ports are arranged on several horizontal levels on said walls for introducing air into the furnace from an air supply. Flue gas generated in black liquor combustion is led into contact with various heat transfer devices, superheaters, the boiler bank and water preheaters (economizers) of the boiler, whereby the heat present in the gas is recovered in water, steam or mixture thereof flowing in the heat transfer devices.

Air is introduced into the boiler usually at three different levels: primary air into the bottom part of the furnace, secondary air above the primary air level, but below the liquor nozzles, and tertiary air above the liquor nozzles for ensuring complete combustion. Air is usually fed in via several air ports either from all four walls of the boiler or from two opposites walls only. More than three air levels for introducing air into the furnace may be arranged in the boiler.

SUMMARY

In one aspect, a velocity type damper is provided for use for controlling airflow into a furnace. As will be described herein, it has been determined that in prior damper designs, the velocity of the air being introduced to the furnace diminishes at the exit of the damper, which is the result of a change in volume for the air passage from the damper to the inlet to the furnace. The damper provided by the present disclosure avoids this reduction in air velocity by reducing the change in volume between the damper exit and the inlet to the furnace. In some embodiments, the damper designs described herein can provide for increased control of the airflow and increased control of the velocity of the air being introduced to the furnace through the damper by aligning the damper blade edges, i.e., an edge of the air control surface for the damper, to the furnace wall at the inlet. As will be described herein, the damper blades, i.e., air control surfaces, may be hinged velocity plates and/or deformable diagram plates. Without being bounded by theory, it is believed that aligning the damper blade edges to the furnace wall ensures that the air flow passage between the damper and the inlet to the furnace does not include a pronounced increase in volume relative to the air flow passage through the damper.

The velocity type damper may include at least one velocity plate that is rotated about a hinged end to provide the air control surface of the damper. In one example of this embodiment, the velocity type damper includes an air port damper body for engagement to an air port opening of a furnace. The velocity type damper may include at least one velocity plate in hinged engagement to the air port damper body so that the air controlling end surface of the velocity plate is substantially aligned to a wall of the furnace at the air port opening when the velocity plate is in a fully opened position.

The velocity type damper may also have at least one deformable diaphragm to provide the air control surface of the damper. In one example of this embodiment, the velocity type damper includes an air port damper body for engagement to an air port opening of a furnace. The velocity type damper may also include at least one diaphragm damper in engagement to the air port damper body so that when deformed, the at least one diaphragm reduces the cross sectional area of the air port damper body. The at least one diaphragm is engaged to the air port damper body so that an end of the at least one diaphragm is substantially aligned to a wall of the furnace at the air port opening.

In another aspect, a method is provided for controlling airflow into a furnace that employs a velocity type damper. In one embodiment, the method for controlling airflow may include engaging a velocity type damper to an air port opening of a furnace, in which the velocity type damper includes at least one air controlling surface that is positioned proximate to a wall of the furnace at the air port opening so that air velocity exiting the at least one air controlling surface is substantially equal to the air velocity entering the air port opening to the furnace. The method may further include adjusting a cross-sectional area through the velocity type damper to control air velocity into the furnace through the air port opening.

These and other features and advantages will become apparent from the following detailed description of illustrative embodiments thereof, which is to be read in connection with the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

The following description will provide details of embodiments with reference to the following figures wherein:

FIG. 1 is a top cross-sectional view of a velocity type damper that includes a velocity plate that is rotated about a hinged end to provide the air control surface of the damper, in accordance with one embodiment of the present disclosure.

FIG. 2 is a top cross-sectional view of a velocity type damper that includes two velocity plates that are positioned at opposing sides of the air port damper body that is connected to the air port to a furnace, in accordance with an embodiment of the present disclosure.

FIG. 3 is a side cross-sectional view of a velocity type damper that includes a velocity plate that is rotated about a hinged end to provide the air control surface of the damper, in accordance with one embodiment of the present disclosure.

FIG. 4 is a top cross-sectional view of a velocity type damper that includes a diaphragm plate that can be deformed to provide the air control surface of the damper, in accordance with one embodiment of the present disclosure.

FIG. 5 is a top cross-sectional view of a velocity type damper that includes two diaphragm plates that are positioned at opposing sides of the air port damper body that is connected to the air port to a furnace, in accordance with an embodiment of the present disclosure.

DETAILED DESCRIPTION

Reference in the specification to “one embodiment” or “an embodiment” of the present invention, as well as other variations thereof, means that a particular feature, structure, characteristic, and so forth described in connection with the embodiment is included in at least one embodiment of the present invention. Thus, the appearances of the phrase “in one embodiment” or “in an embodiment”, as well any other variations, appearing in various places throughout the specification are not necessarily all referring to the same embodiment,

Wood pulp for papermaking is usually manufactured according to the sulfate process wherein wood chips are treated with a cooking liquor including sodium sulfide and sodium hydroxide. The wood chips and the cooking liquor, called “white liquor,” are cooked in a digester under predetermined heat and temperature conditions. After cooking, the used liquor, termed “black liquor,” containing spent cooking chemicals and soluble residue from the cook, is washed out of the pulp and treated in a recovery unit where the cooking chemicals are reclaimed. Without reclamation and reuse of the cooking chemicals, the cost of the papermaking process can be prohibitive.

In the recovery process, the black liquor is first concentrated by evaporation to a low water solution, which solution is then sprayed into the firebox of a black liquor recovery boiler, a type of chemical reduction furnace. The chemical reduction furnace is a reactor wherein the processes of evaporation, gasification, pyrolysis, oxidation and reduction all occur interdependently during recovery of the cooking chemicals. The organic materials in the black liquor, lignin and other wood extracts, maintain combustion in the firebox, and the heat produced dries and melts the spent cooking chemicals as they fall to the floor of the firebox, where they build a mound of material called a char bed. The char bed is further heated to further liquefy the chemicals into a molten smelt that flows Out of the furnace through a smelt spout to a collection tank. Concurrently, combustion heat is employed to generate steam in water walls of the boiler for use as process steam and for generating electricity.

The combustion process requires the introduction of large volumes of air into the firebox. The combustion air is distributed by means of wind boxes or ducts disposed at several levels in surrounding relation to the firebox and outside the walls of the furnace. The air is forced into the firebox from the wind boxes through a plurality of passages or air ports in the walls of the furnace, viz.: primary, secondary and tertiary air ports. The primary air ports, through which about 30 to 40 percent of the air enters the furnace, are disposed on all the walls of the firebox near the bottom of the furnace and close to the char bed. The air supplied to the primary air ports is at a comparatively low pressure in order to promote a reducing atmosphere in the burning mass of char. The secondary air ports, which are fewer in number than the primary air ports and through which about 45 percent of the air enters the furnace, are disposed around the walls of the firebox, higher than the primary air ports, and usually below the level of the entry conduits through which the black liquor is sprayed into the firebox. Air supplied through the secondary air ports is at a slightly higher pressure in order to promote burning of combustible gasses rising from the glowing mass of the char bed. While the primary air ports provide a relatively large volume of air with considerable turbulence for maintaining a fireball in the char bed, the secondary air ports are intended to provide a finer control and distribution of air above the char bed and distribute the air evenly in the black liquor spray to support the combustion thereof. Air is supplied through the tertiary air ports at a still higher pressure to promote combustion of gases rising through the firebox, the tertiary air ports being higher on the wall of the furnace than the secondary air ports.

The volume and distribution of combustion air supplied to the furnace will also vary depending on the load of the furnace and the moisture content of the liquor being reduced. The distribution and volume of air entering a furnace is conveniently adjusted by regulating means such as dampers provided in supply conduits (also referred to as “air port damper bodies”) of the wind boxes. Dampers may also be provided at various locations in the wind boxes, and individual air ports may furthermore be provided with a damper, thus making possible a selective distribution of air within each wind box, or in each wind-box passage or each air port, respectively, thereby maintaining the desired air supply in all parts of the furnace.

The present disclosure provides velocity type dampers for use fur controlling airflow into a furnace through at least one of the air ports described above. The velocity type dampers 100a, 100b, 100c, 100d, 100e of the present disclosure are depicted in FIGS. 1-5. The term “velocity type” when describing the dampers of the present disclosure means that the damper can control the flow path of air to provide a jet of air through the connected air port 70 so that the velocity of air entering the furnace SO through the air port 70 is substantially equal to the velocity of the air leaving the final air control surface of the damper 100a, 100b, 100c, 100d, 100e. The air control surface of the dampers described herein may be velocity plates 50 (as depicted in FIGS. 1-3), diaphragm plates 60 (as depicted in FIGS. 4-5), or combinations thereof.

In some embodiments, the black liquor sprayed into the firebox, swirls, burns and falls toward the bottom of the firebox in the form of combustion products comprising char material and smelt. The smelt and char material contact and flow down the outer walls of the firebox and, cooled by the inflowing air, form excrescent deposits around edges of the air ports, particularly along the top edges of the air ports where the excrescent material builds up and outward under influence of air rushing through the air port. Such buildup of char material can block air flow through a port by as much as fifty percent. In addition to controlling airflow into the furnace for general operations, the velocity type dampers 100a, 100b, 100c, 100d, 100e can also adjust airflow to account for the change of air flow capacity that results from the aforementioned buildup of char material.

Air flow adjustment through the dampers 100a, 100b, 100c, 100d, 100e can be achieved by manipulating the air control surfaces of the dampers 100a, 100b, 100c, 100d, 100e to increase or decrease the cross sectional area of the pathway of the airflow through the damper. In the embodiments depicted in FIGS. 1-2, the air control surface of the damper 100a, 100b, is a side velocity plate 50 that is in hinged engagement to the body, i.e., air port damper body 55. In some embodiments, as depicted in FIG. 3, the air control surface of the damper 100c is mounted on the top of the body, i.e., air port damper body 55. In this case, the velocity plate 50 is a top velocity plate. Both side velocity plates and top velocity plates can be referred to as a velocity plate having reference number 50. The term “hinged” denotes that one end of the velocity plate 50 is in engagement through a hinge 51 so that it may be rotated relative to a fixed point. A “hinge” is a mechanical bearing that connects two solid objects, typically allowing only a limited angle of rotation between them. For example, the hinge 51 allows for the velocity plate 50 to be rotated from an entirely open position (OPEN) providing the greatest cross sectional area for the air pathway through the damper to a substantially closed position (REDUCED PORT) that reduces the cross sectional area for the air pathway through the damper. In the entirely open position for the velocity plate 50, the length L1 of the velocity plate 50 is substantially parallel to the direction of air travel through the air port damper body 55. In the substantially closed position for the velocity plate 50, the velocity plate 50 is rotated from the open position about the hinge 51 towards the center of the air port damper body 55, which reduces the cross sectional area for the air pathway through the damper. By adjusting the cross sectional area of the pathway through the damper by rotating the velocity plate 50, the damper controls 100a, 100b, 100c air flow through the air port damper body 55 into the air port 70.

In the embodiments depicted in FIGS. 4-5, the air control surface of the damper 100d, 100e is a deformable air control diaphragm 65 that is in engagement to the body, i.e., air port damper body 55, of the diaphragm damper plate 60. The diaphragm plate 60 is connected to the wall of the air port damper body 55 on at least two opposing ends of a deformable sheet metal that provides the deformable air control diaphragm 65. The diaphragm damper plate 60 may include a deformable air control diaphragm 65 that includes a pressure applied surface S1 and an air control surface S2. The deformable air control surface 65 may be deformed by applying a force to the pressure applied surface S1. Applying a force, such as compressed air, pressurized hydraulic fluid, or a mechanical force, to the pressure applied surface S1 deforms the deformable air control diaphragm 65 so that the air control surface S1 is extended towards the center of the air port damper body 55, in which the greater the deformable air control diagram 65 is extended the lesser the cross-sectional area for the air pathway through the damper. Removing the force, or applying an opposing force, such as a vacuum, to the pressure applied surface S1 can return the deformable air control diaphragm 65 back to an entirely open position for the damper, which provides the greatest cross sectional area through the air port damper body 55. By adjusting the cross sectional area of the pathway through the damper 100d, 100e by adjusting the deformable air control diaphragm 65, the damper controls air flow through the air port damper body 55 into the air port 70.

It has been determined that in prior damper designs that the decrease in the velocity of at the exit of the damper prior to the air being introduced to the furnace results from a change, i.e., increase, in volume of the air passage between the damper and the inlet to the furnace. More specifically, a high volume region is present from the end leaving the final air control surface of the damper. This means that although the adjustment of the damper can control air flow through the damper, control of the velocity of the jet of air through the damper is diminished by the presence of the high volume region, which limits the operational control of the damper.

Referring to FIGS. 1-5, the damper 100a, 100b, 100c, 100d, 100e provided by the present disclosure avoids this reduction in air velocity by reducing the change in volume between the damper exit and the inlet, e.g., air port opening 70, to the furnace 80. In some embodiments, the damper 100a, 100b, 100c, 100d, 100e designs described herein can provide for increased control of the airflow and increased control of the velocity of the air being introduced to the furnace 80 through the damper 100a, 100b, 100c, 100d, 100e by aligning the air control surfaces, e.g., damper blade edges, to the furnace wall at the inlet 70 (also referred to as air port opening 70). As described herein, the damper blade edges can be either the edge of the hinged velocity plates 50 that is closest to the inlet 70, i.e., opposite the edge of the velocity plate 50 connected to the hinge 51, and/or the edge of the deformable diagram plates 60 that are closest to the inlet 70. The term “aligning” as used to describe the positioning of the damper 100a, 100b, 100c, 100d, 100e relative to the air port opening 70 denotes that the damper blade edges for the control surfaces, such as the edge of the velocity plate 50 and/or diaphragm plate 60, are proximate to (and in some embodiments, in direct contact with) the furnace sidewall at the inlet 70. By being proximate to, it is meant that the damper 100a, 100b, 100c, 100d, 100e is positioned as close to the wall of the furnace 80 at the inlet 70 that will allow the damper 100a, 100b, 100c, 100d, 100e to function yet not extend into the furnace 80, e.g., extend past the inlet 70. By minimizing the presence of any high volume regions between the damper 100a, 100b, 100c, 100d, 100e and the inlet 70, the damper designs of the present disclosure provide that the air velocity leaving the damper 100a, 100b, 100c, 100d, 100e is substantially equal to the air velocity entering the furnace 80 through the inlet 70. Therefore, adjustment of the air control surfaces, such as the velocity plates 50 and the diaphragm plate 60, in the damper designs of the present disclosure to adjust air velocity through the damper 100a, 100b, 100c, 100d, 100e allow for accurate adjustment of the air velocity^, being introduced through to the furnace 80 through the inlet 70.

Referring to FIGS. 1-5, the air port damper body 55 of the dampers 100a, 100b, 100c, 100d, 100e is engaged to an air port opening 70 of the furnace 80, in some embodiments, the outer wall incorporates boiler tubes 81 to conduct water or steam for removing heat from the combustion process occurring within the furnace 80. The air port opening 70 is formed within the boiler outer wall. In some embodiments, the air port opening 70 defines a narrow rectangular slot which penetrates furnace wall for the admission of combustion air. As noted above, a typical boiler will have a multiplicity of air port openings 70, e.g., primary air port openings, secondary air port openings and ternary air port openings, strategically arranged around the perimeter of the boiler to admit supplemental air in desired quantities. In some embodiments, the damper designs 100a, 100b, 1100c, 100d, 100e of the present disclosure are incorporated into primary air port openings, however the dampers 100a, 100b, 100c, 100d, 100e may be incorporated in connection with any^, of the air port openings, i.e., the primary air port openings, secondary air port openings, ternary air port openings and combinations thereof

In some embodiments, the dampers 100a, 100b, 100c, 100d, 100e can be integrated into a wind box (not shown) that is also mounted to the exterior surface of the boiler outer wall. The wind box can be a sheet metal structure that is fastened to the boiler wall and can provide support for the components of the dampers 100a, 100b, 100c, 100d, 100e such as the air port damper body 55, and the air control surfaces, such as the velocity plates 50 and the diaphragm plate 60. The wind box may also have provisions for supporting a port redder that is compatible with the dampers 100a, 100b, 100c, 100d, 100e that are described herein. The wind box encloses the air ports 70 and includes an opening to allow air to enter the wind box.

The damper 100a that is depicted in FIGS. 1 and 3 is one embodiment of a velocity type damper that includes a velocity plate 50 that is rotated about a hinged end 51 to provide the air control surface of the damper 100a. The damper 100a depicted in FIG. 1 includes a single velocity plate 50 engaged to one sidewall of the air port damper body 55. The damper 100c depicted in FIG. 3 includes a single velocity plate 50 engaged to an upper surface of the air port damper body 55. In some embodiments, the at least one velocity plate 50 is in hinged engagement to the air port damper body 55 so that the air controlling end surface of the at least one velocity plate is substantially aligned to a sidewall of the furnace 80 at the air port opening 70 when the at least one velocity plate 50 is in a fully opened position (OPEN). Rotating the at least one velocity plate 50 from the fully opened position (OPEN) reduces a cross sectional area of the air passageway through the air port damper body 55. In some embodiments, the velocity plate 50 may be rotated to a substantially closed (REDUCED PORT) about the hinge so that the maximum angle α at the interface of the air port damper body 55 and the velocity plate 50 is equal to 30° or less. In another embodiment, the velocity plate 50 may be rotated to a substantially closed (REDUCED PORT) about the hinge so that the maximum angle cm at the interface of the air port damper body 55 and the velocity plate 50 is equal to 15° or less. It is noted that when the velocity plate 50 is in the substantially closed (REDUCED PORT) position, the cross sectional area through the air port damper body 55 may he reduced up to 70%. In another example, when the velocity plate 50 is in the substantially closed (REDUCED PORT) position, the cross sectional area through the air port damper body 55 may be reduced up to 50%. In an even further example, when the velocity plate 50 is in the substantially closed (REDUCED PORT) position, the cross sectional area through the air port damper body 55 may be equal to 25% or less. By controlling the cross-sectional area through the air port damper body 55, the velocity plate 50 controls the air flow through the damper 100a.

The velocity plate 50 may he formed from a metal, such as steel, stainless steel or other alloys. The velocity plate 50 may be rigid and substantially planar in geometry. In other examples, the velocity plate 50 may include at least one curvature, which can aid in the control of air through the air port damper body 55. The edge of the velocity plate 50 opposite the edge of the velocity plate 50 that is directly connected to the hinge 51 is the end of the air control surface for the damper. Adjustment, e.g., the angle α produced by rotation, of the velocity plate 50 can be provided using hydraulic actuators, electrical actuators, pneumatic actuators and combinations thereof.

The velocity plate 50 may be positioned as close as possible to the wall of the furnace 80 near the inlet 70. In the embodiment depicted in FIG. 1, the velocity plate 50 is positioned so that the edge of the velocity plate that provides the end of the air control surface is in contact with the wall of the furnace when the velocity plate 50 is in the fully open position (OPEN). In some embodiments, the design of the damper 100a conforms to the curvatures of the furnace wall. For example, the sidewall of the furnace at the air port opening 70 can include a first convex curvature at an upper portion of the air port opening 70 and a second curvature at the lower portion of the air port opening 70. The end of the air port damper body 55 can contact the second curvature and can therefore be offset from the air controlling end surface of the velocity plate 50 when the velocity plate 50 is in a fully opened position (OPEN) and engages the first curvature of the sidewall at the air port opening 70, as depicted in FIG. 1.

Although FIGS. 1 and 3 illustrate a damper 100a, 100c having a single velocity plate 50, the present disclosure is not limited to only this example, as the dampers described herein may include any number of velocity plates 50. For example, FIG. 2 illustrates one embodiment of a velocity type damper 100b that includes two velocity plates 50 that are positioned at opposing sides of the air port damper body 55 that is connected to the air port 70 to the furnace 80. It is noted that each of the velocity plates 50 that are depicted in FIG. 2 are similar to the velocity plate 50 that has been described with reference to FIG. 1. Therefore, the description of the velocity plate 50 depicted in FIG. 1 can provide at least one example of the velocity plate 50 that is depicted in FIG. 2. It is noted that by increasing the number of velocity plates 50, the greater the obstruction of the cross sectional area of the air pathway through the air port damper body 55 when the multiple velocity plates 50 are open.

FIG. 4 depicts a velocity type damper 100d that includes a diaphragm plate 60 that can be deformed to provide the air control surface of the damper 100d. In one embodiment, the damper 100d includes an air port damper body 55 engaged to an air port opening 70 of a furnace 80. In one embodiment, the damper 100d further includes at least one diaphragm plate 60 engaged to the air port damper body 55 so that an end of the at least one diaphragm 60 is proximate to a wall of the furnace at the air port opening 70. The air control surface of the damper 100d is a deformable air control diaphragm 65 that is in engagement to the body, i.e., air port damper body 55, of the diaphragm damper plate 60. The deformable air control diaphragm 65 includes a pressure applied surface S1 and an air control surface S2.

Without a force applied to the pressure applied surface S1, the deformable air control surface 65 is positioned along a sidewall of the air port damper body 55 in an open position (OPEN). Applying a force, such as compressed air, pressurized hydraulic fluid, or a mechanical force, to the pressure applied surface Si deforms the deformable air control surface 65 to extend from the sidewall of the air port damper body 55 towards the center of the air pathway through the damper 100d. The deformable air control surface 65 extended towards the center of the air pathway to a position (REDUCED PORT) that reduces the cross-sectional area for the air pathway through the damper 100d. Removing the force, or applying an opposing force, such as a vacuum, to the pressure applied surface S1 can return the deformable air control diaphragm 65 back to an entirely open position (OPEN) for the damper, which provides the greatest cross sectional area through the air port damper body 55. It is noted that when the deformable air control diaphragm 65 is in the substantially closed (REDUCED PORT) position, the cross sectional area through the air port damper body 55 may be reduced up to 70%. In another example, when the deformable air control diaphragm 65 is in the substantially closed (REDUCED PORT) position, the cross sectional area through the air port damper body 55 may be reduced up to 50% in an even further example, when the deformable air control diaphragm 65 is in the substantially closed (REDUCED PORT) position, the cross sectional area through the air port damper body 55 may be equal to 25% or less. By controlling the cross-sectional area through the air port damper body 55, the deformable air control diaphragm 65 controls the air flow through the damper 100d.

The diaphragm plate 60 may be positioned as close as possible to the sidewall of the furnace 80 near the inlet 70. The deformable air control diaphragm 65 of the diaphragm plate 60 may be formed from a deformable sheet metal, such as steel, stainless steel or an alloy. In other embodiments, the deformable air control diaphragm may be composed of a composite material. In one embodiment, the diaphragm plate 60 is connected to the sidewall of the air port damper body 55 on at least two opposing ends of the deformable sheet metal 65.

Although FIG. 4 illustrates a damper 100d having a single diaphragm plate 60, the present disclosure is not limited to only this example, as the dampers described herein may include any number of damper plates 60. For example, FIG. 5 illustrates one embodiment of a velocity type damper 100e that includes two diaphragm plates 60 that are positioned at opposing sides of the air port damper body 55 that is connected to the air port 70 to the furnace 80. It is noted that each of the diaphragm plates 60 that are depicted in FIG. 5 are similar to the diaphragm plate 60 that has been described with reference to FIG, 4. Therefore, the description of the diaphragm plate 60 depicted in FIG. 4 can provide at least one example of the diaphragm plates 60 that are depicted in FIG. 5, It is noted that by increasing the number of diaphragm plates 60, the greater the obstruction of the cross sectional area of the air pathway through the air port damper body 55 when the multiple diaphragm plates 60 are open.

The dampers 100a, 100b, 100c, 100d, 100e that are described herein may be used in a method for controlling airflow into a furnace 80. The method may include engaging a velocity type damper to an air port opening 70 of a furnace 80, as depicted in FIGS. 1-5. The velocity type dampers 100a, 100b, 100c, 100d, 100e can include at least one air controlling surface, e.g., velocity plate 50 and/or diaphragm plate 60, that is positioned proximate to a wall of the furnace at the air port opening 70 so that air velocity exiting the at least one air controlling surface is substantially equal to the air velocity entering the air port opening 70 to the furnace 80.

The method for controlling airflow into a furnace 80 further includes adjusting a cross-sectional area through the velocity type damper 100a, 100b, 100c, 100d, 100e to control air velocity into the furnace 80 through the air port opening 70.

In some embodiments, the method employs a velocity type damper 100a, 100b, 100c. that includes an air port damper body 55 is engaged to the air port opening 70 of the furnace 80, and the at least one velocity plate 50 in hinged engagement to the air port damper body 55 so that an end of the air controlling surface of the at least one velocity plate 50 is substantially aligned to the sidewall of the furnace 80 at the air port opening 70 when the at least one velocity plate 50 is in a fully opened position (OPEN), as depicted in FIGS. 1-3. Rotating the at least one velocity plate 50 from the fully opened position reduces a cross sectional area of the air passageway through the air port damper body 55. The change in the cross sectional area of the air passageway changes the velocity of the air passing through the damper 100a, 100b, 100c.

In some embodiments, the method employs a velocity type damper 100d, 100e that includes an air port damper body 55 and at least one diaphragm plate 60, as depicted in FIGS. 4 and 5. The air port damper body 55 is engaged to the air port opening 70 of the furnace 80. The at least one diaphragm plate 60 is engaged to the air port damper body 55 so that an end of the at least one diaphragm plate 60 is proximate to a sidewall of the furnace SO at the air port opening 70. The diaphragm plate 60 includes a deformable air control diaphragm 65. Deforming the deformable air control diaphragm 65 of the diaphragm plate 60 reduces the cross sectional area of the air port damper body 55. The change in the cross sectional area of the air passageway changes the velocity of the air passing through the damper 100d, 100e.

It is further noted that the damper designs 100a, 100b, 100c, 100d, 100e may be integrated with a port rodder. Port rodders are provided on recovery boilers to clean the air ports or openings, keeping them free from combustion by-products and other deposits commonly referred to as char. By frequently cleaning the port openings, air flow is uniform from all ports into the boiler thus facilitating a high rate of heat transfer and optimum operation.

A rodder generally includes a tip or cutter mounted on the end of a ram which is in turn connected to an actuator which causes the ram to be extended or retracted, e.g., into the air port 70. One such actuator would be a pneumatic cylinder. Extension and retraction of the cylinder causes the cutter to move in and out of the port, e.g., air port 70. When extended into the air port 70, the cutter contacts and dislodges the char by cutting and/or pushing it through the port and into the boiler 80.

It will also be understood that when an element is referred to as being “on” or “over” another element, it can be directly on the other element or intervening elements can also be present. In contrast, when an element is referred to as being “directly on” or “directly over” another element, there are no intervening elements present. It will also be understood that when an element is referred to as being “connected” or “coupled” to another element, it can be directly connected or coupled to the other element or intervening elements can be present. In contrast, when an element is referred to as being “directly connected” or “directly coupled” to another element, there are no intervening elements present.

It is to be appreciated that the use of any of the following “/”, “and/or”, and “at least one of”, for example, in the cases of “A/B”, “A and/or B” and “at least one of A and B”, is intended to encompass the selection of the first listed option (A) only, or the selection of the second listed option (B) only, or the selection of both options (A and B). As a further example, in the cases of “A, B, and/or C” and “at least one of A, B, and C”, such phrasing is intended to encompass the selection of the first listed option (A) only, or the selection of the second listed option (B) only, or the selection of the third listed option (C) only, or the selection of the first and the second listed options (A and B) only, or the selection of the first and third listed options (A and C) only, or the selection of the second and third listed options (B and C) only, or the selection of all three options (A and B and C). This can be extended, as readily apparent by one of ordinary skill in this and related arts, for as many items listed.

The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments. As used herein, the singular forms “a,” “an” and “the” are intended to include the plural forms as well, unless the context clearly^, indicates otherwise. It will be further understood that the terms “comprises,” “comprising,” “includes” and/or “including,” when used herein, specify the presence of stated features, integers, steps, operations, elements and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components and/or groups thereof.

Spatially relative terms, such as “beneath,” “below,” “lower,” “above,” “upper,” and the like, can be used herein for ease of description to describe one element's or feature's relationship to another element(s) or feature(s) as illustrated in the figures. It will be understood that the spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as “below” or “beneath” other elements or features would then be oriented “above” the other elements or features. Thus, the term “below” can encompass both an orientation of above and below. The device can be otherwise oriented (rotated 9( )degrees or at other orientations), and the spatially relative descriptors used herein can be interpreted accordingly. In addition, it will also be understood that when a layer is referred to as being “between” two layers, it can be the only layer between the two layers, or one or more intervening layers can also be present.

It will be understood that, although the terms first, second, etc., can be used herein to describe various elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another element. Thus, a first element discussed below could be termed a second element without departing from the scope of the present concept.

Having described preferred embodiments of a method, structures and systems for velocity dampers for a recovery boiler, it is noted that modifications and variations can be made by persons skilled in the art in light of the above teachings. It is therefore to be understood that changes may be made in the particular embodiments disclosed which are within the scope of the invention as outlined by the appended claims. Having thus described aspects of the invention, with the details and particularity required by the patent laws, what is claimed and desired protected by Letters Patent is set forth in the appended claims.

Claims

1. A damper for a furnace, the damper comprising: an air port damper body engaged to an air port opening of the furnace, the air port opening disposed at an air inlet of the furnace; andtwo velocity plates in hinged engagement to the air port damper body and configured to move symmetrically to control air flow into the furnace such that air controlling end surfaces of the two velocity plates are substantially aligned to a wall of the furnace at the air port opening such that the air controlling end surfaces are positioned at the wall of the furnace when the two velocity is plates are in a fully opened position.

2. The damper of claim 1, wherein the two velocity plates are engaged to opposing sidewalls of the air port damper body.

3. The damper of claim 1, wherein each one of the two velocity plates is engaged to sidewall portions of the air port damper body, wherein the sidewall portions are positioned at opposing sides of the air port damper body.

4. The damper of claim 1, wherein each velocity plate is planar and substantially rigid.

5. The damper of claim 1, wherein the wall of the furnace at the air port opening includes a first curvature at an upper portion of the air port opening and a second curvature at a lower portion of the air port opening, wherein an end of the air port damper body is offset from the air controlling end surface of the velocity plate when the velocity plate is in a fully opened position to engage the first and second curvature of the wall at the air port opening.

6. The damper of claim 1, wherein each velocity plate is configured to rotate from the fully opened position to reduce a cross sectional area of an air passageway through the air port damper body.

7. The damper of claim 6, wherein each velocity plate is configured to rotate to reduce the cross sectional area of the air passageway via one of a hydraulic actuator, a pneumatic actuator, or an electric actuator.

8. The damper of claim 1, wherein when substantially closed each velocity plate is configured to form an angle in a range of 15 degrees to 30 degrees at an interface of the air port damper body and the velocity plate.

9. A method for controlling airflow into a furnace comprising: engaging a velocity type damper to an air port opening disposed at an air inlet of a furnace, in which the velocity type damper includes two air controlling surfaces that are engaged to an air port damper body and configured to move symmetrically to control airflow into the furnace such that the air controlling end surfaces of the velocity type damper are positioned at a wall of the furnace at the air port opening when the two air controlling surfaces are in a fully opened position so that air velocity exiting the two air controlling surfaces is substantially equal to the air velocity entering the air port opening to the furnace; andadjusting a cross sectional area through the velocity type damper to control air velocity into the furnace through the air port opening.

10. The method of claim 9, wherein the velocity type damper comprises an air port damper body and two velocity plates, wherein the an air port damper body is engaged to the air port opening of the furnace, and the two velocity plates are in hinged engagement to the air port damper body so that ends of the two air controlling surface of the two velocity plates are substantially aligned to the wall of the furnace at the air port opening when the two velocity plates are in a fully opened position.

11. The method of claim 10, wherein the two velocity plates are engaged to sidewall portions of the air port damper body, wherein the sidewall portions are positioned at opposing sides of the air port damper body.

12. The method of claim 10, wherein rotating the two velocity plates from the fully opened position reduces a cross sectional area of an air passageway through the air port damper body.

13. The method of claim 12, wherein rotating the two velocity plates to rotate to reduce the cross sectional area of the air passageway comprises rotating the two velocity plate via one of a hydraulic actuator, a pneumatic actuator, or an electric actuator.

14. The method of claim 10, wherein rotating the two velocity plates to a substantially closed position forms an angle in a range of 15 degrees to 30 degrees at an interface of the air port damper body and each of the two velocity plates.