1. Field of the Disclosure
The present disclosure is related generally to refractory tiles and particularly directed to thermally conductive tiles for use in waste-to-energy systems.
2. Description of the Related Art
It has been common practice to cover furnace walls of facilities such as municipal waste incinerators with a firebrick, cements or tile sheath in order to protect the structural elements from erosive and corrosive effects of combustion. Many of these facilities now include energy recovery systems, often referred to as waste-to-energy systems (or WTE systems), which operate to retrieve the heat generated during the combustion process. In many cases, the energy recovery systems utilize a boiler that can include an array of tubes placed at the periphery of the furnace or incinerator, typically in the walls, through which a fluid such as water is circulated as a heat transfer medium. Given the harsh environment of the furnace, it is desirable to protect the heat exchanger array with a refractory material. However, unlike typical thermally insulating refractory bricks used in common furnaces, the refractory tiles that line a heat exchanger are intended to conduct heat.
In addition to the unique thermal characteristics, the attachment mechanisms of such refractory tiles are often different than standard furnace bricks in order to position the refractory tiles close to the heat exchanger. In the past, attachment mechanisms of the tiles have included hanging the bricks from metallic support shoes, or from vertical I-beams using J-shaped bolt anchors. Other mechanisms include tongue and groove mating elements utilizing a vertical metal framework. More recently, the attachment mechanisms have been made such that the refractory tiles or bricks can be attached to the wall heat exchanger array itself.
Among the many methods for hanging protective refractory brick on an array of heat exchanger tubing, one method includes hanging the refractory tiles from a bolt extending into the tile and anchoring the tile to the wall of the heat exchanger. This technique, while relatively inexpensive, subjects the brick to compressive stresses, which leads to the development of cracks and ultimately, to failure of the brick. In response to these particular problems, different anchoring mechanisms have been investigated. For example, a proprietary sunken anchor slot mechanism was designed wherein an anchoring receptacle in the shape of a “T” was formed within the body of the brick to secure the brick to a T-shaped anchor extending from the tubing wall of the heat exchanger. See, U.S. Pat. No. 5,243,801.
Despite continued improvements in refractory tile systems for WTE applications, the industry continues to demand improved designs and particularly, improved durability, efficiency, safety, and repair ease.
According to one aspect, a refractory tile system for covering a wall of a boiler is disclosed that includes a plurality of tiles adapted for assembly to cover the wall of the boiler. Each tile includes a main body having a front surface and a back surface, wherein the main body comprises a composite including silicon carbide and a metallic phase including silicon, and each tile also includes a first engagement structure extending from the back surface of the tile and having a first engagement void for receiving a complementary stud structure extending from the wall of the boiler. Each tile also includes a void plane defined by a plurality of void points, wherein the void points are points within the first engagement void that are closest to the front surface and extend along the first engagement void. Each tile also includes a hot face plane parallel to the void plane and defined by a plurality of hot face points, each hot face point being a point on the front surface closest to the void plane, wherein Ds≧0.25 Ta, Ds being shortest distance between the void plane and the hot face plane and Ta being the average thickness of the main body.
According to another aspect, a refractory tile system for covering a wall of a boiler is disclosed that includes a plurality of tiles adapted for assembly to cover the wall of the boiler, such that each tile includes a main body having a front surface and a back surface, wherein the main body is a composite material including silicon carbide and a metallic phase including silicon. The front surface of each tile has an average profile variation (Pa) of not greater than about 0.75 mm. Additionally, each tile has an engagement structure extending from the back surface of the tile and having an engagement void for receiving a complementary stud structure extending from the wall of the boiler.
According to one aspect, a refractory tile system for covering a wall of a boiler is disclosed that includes a plurality of tiles adapted for assembly to cover the wall of the boiler. Each tile includes a main body having a front surface and a back surface, wherein the main body has a thermal conductivity of not less than about 18 W/mK at 1200° C., and each tile also includes first and second engagement structures extending from the back surface of the tile and having respective first and second engagement voids for receiving complementary stud structures extending from the wall of the boiler. Each tile also includes a void plane defined by a plurality of void points, wherein the void points are points within the first and second engagement voids that are closest to the front surface and extend along the first and second engagement voids. Each tile also includes a hot face plane parallel to the void plane and defined by a plurality of hot face points, each hot face point being a point on the front surface closest to the void plane, wherein Ds≧0.25 Ta, Ds being shortest distance between the void plane and the hot face plane and Ta being the average thickness of the main body.
According to one aspect, a refractory tile system for covering a wall of a boiler is disclosed that includes a plurality of tiles adapted for assembly to cover the wall of the boiler. Each tile includes a main body having a front surface and a back surface and each tile also includes first and second engagement structures extending from the back surface of the tile and having respective first and second engagement voids for receiving complementary stud structures extending from the wall of the boiler. Each tile also includes a void plane defined by a plurality of void points, wherein the void points are points within the first and second engagement voids that are closest to the front surface and extend along the first and second engagement voids. Each tile also includes a hot face plane parallel to the void plane and defined by a plurality of hot face points, each hot face point being a point on the front surface closest to the void plane, wherein Ds≧0.25 Ta, Ds being shortest distance between the void plane and the hot face plane and Ta being the average thickness of the main body.
The present disclosure may be better understood, and its numerous features and advantages made apparent to those skilled in the art by referencing the accompanying drawings.
The use of the same reference symbols in different drawings indicates similar or identical items.
Referring to
According to the prior art refractory tile system 100, the tiles are stacked in an array. Because the voids 107 extend in a vertical direction along the entire vertical length of each tile and because the voids 107 are open at opposite ends, the tiles are restrained vertically by a secondary structure, such as a series of horizontal rails (not shown) and/or the floor of the furnace. The void/anchor arrangement only restrains the tiles horizontally (laterally).
Referring now to present embodiments, a refractory tile system for covering a wall of a boiler is disclosed that includes a plurality of tiles adapted for assembly to cover the wall of the boiler. According to one embodiment, each tile includes a main body having a front surface and a back surface, wherein the main body comprises a composite including silicon carbide and a metallic phase including silicon. Each tile also includes first and second engagement structures extending from the back surface of the tile and having respective first and second engagement voids for receiving complementary stud structures extending from the wall of the boiler. Each tile also includes a void plane defined by a plurality of void points, wherein the void points are points within the first and second engagement voids that are closest to the front surface and extend along the first and second engagement voids. Each tile also includes a hot face plane parallel to the void plane and defined by a plurality of hot face points, each hot face point being a point on the front surface closest to the void plane, wherein Ds≧0.25 Ta, Ds being shortest distance between the void plane and the hot face plane and Ta being the average thickness of the main body.
Referring to
According to one embodiment, the refractory tile 201 can be a composite material including a metallic phase, such as metal silicon, oftentimes elemental silicon. According to one embodiment, the body of the refractory tile 201 can include not greater than about 30 wt % silicon, such as not greater than about 25 wt % silicon, or not greater than about 20 wt % silicon, or still, not greater than about 15 wt % silicon. According to a particular embodiment, the body of the refractory tile 201 can include an amount of silicon within a range of between about 4.0 wt % silicon and 25 wt % silicon, such as within a range of between about 5.0 wt % to about 20 wt %, and in particular within a range of between about 6 wt % to 20 wt %.
Still, the silicon content can be reduced given the processing of the refractory tile material, including for example, in situ reaction of free silicon with free carbon in a silicon carbide-based body. As such, in one particular embodiment, the body includes a silicon reaction bonded silicon carbide composition (i.e., Si/SiC/SiC), such that the silicon content is not greater than about 3.0 wt %, or not greater than about 2.0 wt %, or even not greater than about 1.0 wt % silicon. In a particular embodiment, the body of the refractory tile 201 can have a silicon content within a range of between about 0.05 wt % and about 3.0 wt % silicon, such as within a range of between about 0.05% and about 1.0 wt % silicon.
In further reference to the material of the refractory tile 201, according to another embodiment, the body of the tile includes a material having a thermal conductivity of not less than about 18 W/mK at 1200° C., such as not less than about 20 W/mK at 1200° C., or not less than about 25 W/mK at 1200° C. Still, in another embodiment, the thermal conductivity of the tile material is greater, such as not less than about 30 W/mK at 1200° C., or not less than about 35 W/mK at 1200° C. Materials meeting certain characteristics discussed above include ADVANCER® CN-703, Nitride Bonded Silicon Carbide, CRYSTAR® RB, Reaction Bonded Silicon Carbide, SILIT® SK, Reaction Bonded Silicon Infiltrated Silicon Carbide (SiSiC).
In further reference to the characteristics of the refractory tile 201, the tile can be a dense material. According to one embodiment, the refractory tile 201 has a porosity of not greater than about 5.0 vol %, such not greater than about 3.0 vol %, or still, not greater than about 1.0 vol %. In one particular embodiment, the porosity of the refractory tile 201 is less than 1.0 vol %.
As stated above, the refractory tile 201 can be a dense material, and in addition to the porosities described above, according to one embodiment the bulk density of the material is not less than about than about 2.85 g/cm3. In another embodiment, the material comprising the main body has a bulk density of not less than about 2.90 g/cm3, such as not less than about 2.95 g/cm3, or not less than about 3.00 g/cm3. Such density provides a durable refractory tile that can have enhanced mechanical and chemical resistance, thereby improving the thermal conductivity of the tile and the operable lifetime.
The main body of the refractory tile 201 can generally be described as the material between the front surface 203 and the back surface 205. As illustrated in
In addition to the features provided above, the refractory tile 201 of
Accordingly, the engagement structures 211 and 213 can have a plurality of engagement surfaces for contacting and securing the complementary stud structures 221 and 223. Referring to
Referring again to
In further reference to the engagement structures 211 and 213, as will be appreciated, each of the engagement structures 211 and 213 can be a load bearing structure and are configured to support at least a portion of the weight of the refractory tile 201. In one particular embodiment, the engagement structures 211 and 213 are configured to support at least about half of the weight of the refractory tile 201. According to one embodiment, each of the engagement structures 211 and 213 can support at least about 75% of the weight of the tile, and still, in other embodiments, each of the engagement structures 211 and 213 can support the full weight of the refractory tile 201. It will be appreciated that while
In further reference to the engagement structures 211 and 213, according to one embodiment, the engagement structures 211 and 213 have discrete dimensions including a discrete length and width that is less than the length and width respectively of the refractory tile. For ease of reference,
The refractory tiles provided herein may have particular dimensions. Typically, the length (L) of the refractory tile is generally greater than about 10 cm. Other embodiments utilize larger refractory tiles, such that the length (L) is not less than about 15 cm, or not less than about 20 cm, or even not less than about 50 cm. Still, the length (L) of the refractory tile 601 is typically not greater than about 60 cm.
Referring again to
Referring to other aspects of the above described embodiment, a void plane 209 (Pv) and hot face plane 207 (Phf) are provided. According to the first aspect, the void plane 209 is defined by a plurality of void points 271 and 272 that are located within the engagement voids 217 and 219 and are closest to the front surface 203. Such points extend within regions 231 and 232, since points along regions 231 and 232 are equidistant from the front surface as measured through the thickness of the main body of the refractory tile 201. It will be appreciated that in light of the specification and the figures herein, the term “closest” is understood to be a measurement through the thickness of the main body of the refractory tile 201 in a direction substantially normal to the planes and surfaces defined, and such points closest to the front surface may also be outside of the plane of
As illustrated in the particular embodiment shown in
In further reference to the void plane 209 and hot face plane 207, as illustrated in
As indicated above and described in the first aspect, the shortest distance Ds between the void plane 209 and hot face plane 207 is greater than 0.25 Ta. According to other embodiments, Ds is greater than about 0.50 Ta, such as greater than about 0.75 Ta. Still, according to other embodiments, (one such illustrated and discussed below) the shortest distance between the void plane 209 and the hot face plane 207 is not less than the full measure of the average thickness of the main body, otherwise stated, Ds is not less than Ta. As such, the void plane 209 does not intersect any points on the front surface 203.
By way of comparison, referring to prior art
According to another aspect, a refractory tile system for covering a wall of a boiler is disclosed that includes a plurality of tiles adapted for assembly to cover the wall of the boiler, such that each tile includes a main body having a front surface and a back surface, wherein the main body is a composite material including silicon carbide and a metallic phase including silicon. The front surface of each tile has an average profile variation (Pa) of not greater than about 0.75 mm. Additionally, each tile has an engagement structure extending from the back surface of the tile and having an engagement void for receiving a complementary stud structure extending from the wall of the boiler.
Referring to
In addition to the Pa, a maximum change in profile (Pmax) of the front surface 307 can also be measured. Generally, the Pmax of the front surface 307 (illustrated by line 305) is the greatest measured difference between a highest or lowest point on the front surface and the mean profile line (Pmean) 303. As such, according to one embodiment, the Pmax of the front surface 307 is not greater than about 3.0 mm, such as not greater than about 2.0 mm, or still, not greater than about 1.0 mm. While in one particular embodiment, the front surface 307 is substantially planar such that the Pmax is zero mm.
By way of comparison, referring to the prior art refractory tile illustrated in
Like the front surface 307, the back surface 309 can also have an average profile variation (Pa). According to one embodiment, aside from the engagement structures, the Pa for the back surface 309 is not greater than about 1.0 mm. In another embodiment, the Pa is less, such as not greater than about 0.80 mm, or still, not greater than about 0.75 mm, or even 0.50 mm. Still, in one particular embodiment, the back surface 309 can be substantially planar. Additionally, the back surface 309 can have a maximum profile variation (Pmax). Generally, the Pmax of the back surface 309 is not greater than about 4.0 mm. However, according to other embodiments, the Pmax of the back surface 309 is not greater than about 2.0 mm, such as not greater than about 1.0 mm.
It is noted that profile values Pa, Pmax, Pmean generally are analogous ra rmax and rmean values associated with surface roughness, but that the profile values represent macroscopic surface features generally on the mm scale, rather than roughness values on a much finer scale, such as the micron scale. Like roughness values, the profile values may be measured through characterization of the tiles utilizing a profilometer having a stylus set for macroscopic analysis.
In addition to the profile variations of the front surface 307 and back surface 309, a measure of the maximum change in profile between a point on the front surface that is the greatest distance from a point on the back surface as measured through the thickness of the main body in a direction normal to the plane of the front surface (i.e., the greatest thickness) can be provided. According to one embodiment, the maximum change in profile between the front surface 307 and the back surface 309 is not greater than about 30 mm, such as not greater than about 20 mm, or even not greater than about 15 mm.
Referring to
The engagement structure 603 is an alternative engagement structure, notably including a rounded contour and includes an engagement void 605 configured to receive a complementary stud structure 607. In particular, the engagement structure 603 includes an engagement void 605 having a generally rounded contour and accessible for the complementary stud structure 607 via a channel. Accordingly, the engagement void 605 is configured to be slidably engageable with the complementary stud structure 607.
As further illustrated in
The dimensions of the engagement structure 603 are similar to those described above in accordance with other embodiments. Notably, the diameter (d) of the rounded engagement structure 603 has dimensions substantially similar to the width of previously described engagement structures. As such, generally the diameter (d) of the engagement structure 603 is not greater than about 25% of the length (L) of the refractory tile 601. Other embodiments utilize a smaller engagement structure, such that the diameter of the engagement structure 603 is not greater than about 20%, or even not greater than about 15% of the length (L) refractory tile 603. Having engagement structures of a discrete diameter (d) that is a portion of the length (L) of the tile facilitates anchoring the tile at a single point which can allow for movement of the tile about an anchoring point.
Referring to
The engagement structure 703 is adjacent to the surface of the refractory tile 701 and projects away from the surface of the tile. The engagement structure 701 has a rounded contour and includes an engagement void 705 configured to receive a complementary stud structure (not illustrated). In particular, the engagement structure 703 includes an engagement void 605 in the form of a hole, thereby creating a pocket within the engagement structure 703 for engagement of a complementary stud structure. Accordingly, the engagement void 605 is configured to be engageable with a complementary stud structure such that the stud structure is pushed through the engagement void 705 and secured within the engagement structure 703. According to one particular embodiment, the complementary stud structure can include one or more engagement flanges which may be deformed upon passage through the engagement void 703 thereby securing the stud structure within the engagement structure 703. One form of a suitable engagement flange can include for example, a washer (or alternatively a plurality of washers) placed around the stud structure which deform when passing through the engagement void 705, for example by forming conical shapes, and securing the refractory tile 701.
The dimensions of the engagement structure 703 are similar to those described above in accordance with other embodiments. As such, generally the diameter (d) of the engagement structure 703 is not greater than about 25% of the length (L) of the refractory tile 701. Other embodiments utilize a smaller engagement structure 703, such that the diameter (d) of the engagement structure 603 is not greater than about 20%, or even not greater than about 15% of the length (L) refractory tile 603. Having engagement structures of a discrete diameter (d) that is a portion of the length (L) of the tile facilitates anchoring the tile at a single point which can allow for movement of the tile about an anchoring point.
Referring to
The foregoing description has illustrated various embodiments of refractory tile assemblies including refractory tile structures coupled with engagement structures suitable for attaching the tiles to complementary stud structures. Notably, such assemblies can be monolithic or modular. That is, the combination of the refractory tile and the engagement structure can be a monolithic article such that the tile and engagement structure are a single piece. Alternatively, the tile and engagement structure can have a modular design, such that the tile and engagement structure are separate pieces that can be placed together, for example in an interlocking arrangement, and used jointly to form a refractory tile assembly. A modular design facilitates coupling of select tiles and select engagement structures for use in particular applications.
In comparison with prior refractory tile systems, such as that shown in
Still further, according to various embodiments, one or both the front and back surfaces may have reduced contour, and may indeed be generally planar. Such a structure, in combination with particular materials can notably improve performance during use, manifested by reduced build-up of slag and improved longevity though reduction of non-uniform thermal gradients along the tiles. The combination of reduced front surface contour and a material of a certain material property (e.g., density, or thermal conductivity) or composition (e.g., metal/ceramic composition) can improve gas flow along the hot face, providing a washing effect along the hot face. Still further, relative movement between the tiles and underlying cement can be improved according to embodiments, such as through use of a dense tile (low porosity), which may also have a reduced contour back surface (which contacts such cement).
Additionally, the use of particular engagement structures can improve durability by reducing crack initiation associated with prior art designs that rely on a rack or rail system to secure tiles vertically. Such engagement structures are notable in the context of certain materials as disclosed herein, as such materials, due to increased thermal transfer can exacerbate cracking.
The above-disclosed subject matter is to be considered illustrative, and not restrictive, and the appended claims are intended to cover all such modifications, enhancements, and other embodiments, which fall within the true scope of the present invention. Thus, to the maximum extent allowed by law, the scope of the present invention is to be determined by the broadest permissible interpretation of the following claims and their equivalents, and shall not be restricted or limited by the foregoing detailed description.
The following disclosure is a non-provisional application which claims priority to U.S. Provisional Application No. 60/802,093 filed May 19, 2006, entitled “Refractory Tiles for Heat Exchangers” and having named inventors Wade A. Taber and Joseph L. Ouellet, which application is incorporated by reference herein in its entirety.
Number | Date | Country | |
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60802093 | May 2006 | US |