Refractory materials formed from mats or blankets of ceramic fibers are routinely used to line the interior of high temperature furnaces and other devices involving exposure to high temperature conditions. The insulating materials are typically formed from layers of fibrous refractory material that are often assembled into modules, which may have a cube-shape. The cube-shape is commonly utilized to facilitate post manufacturing shipping, handling and installation. The layers of fibrous material may be held together by a variety of methods and each layer is commonly composed of the same material throughout. As illustrated in
When a furnace is designed to operate at very high temperature, e.g., such that the furnace walls must be capable of withstanding temperatures in the range of 2000° F. up to 3000° F., the ceramic materials capable of withstanding such conditions can be quite expensive. In general, only the outer portion on the hot face of the module is actually exposed to these very high temperatures, since the insulating effect of the ceramic fiber material will allow a substantially lower temperature to be maintained on the cold face of the module against the furnace interior wall. In furnaces insulated on the interior with such insulating modules, it is quite common for the temperature on the furnace casing next to the cold face of the module to be maintained at a temperature that is substantially cooler, e.g., about 1,000° F. or more, cooler than the hot face of the module. If the module is composed of insulating layers of a single material that extend all the way from the hot face to the cold face of the module, this means that the expensive insulating fibrous refractory material necessary to withstand the very high temperatures on the hot face must be used throughout the module, a solution which is not cost effective.
Efforts have been made to design insulating modules that employ two types of ceramic materials, with an expensive ceramic material rated for very high temperatures on the hot face and a less expensive material with a lower temperature rating on the cold face. The approaches reported to date suffer from various disadvantages. For example, U.S. Pat. No. 4,379,382 describes a high temperature insulation module having one type of ceramic fiber mat on the hot face and a second fiber mat on its cold face. The two ceramic mats are held together by a planar support member positioned between the mats. The two ceramic mats are either bonded to the support member by layers of cement applied to the outer periphery of the support member or by means of pins or clips attaching a mat to the support member. Either method of attachment can be subject to failure under certain conditions as well as the support member, which is commonly formed from metal, being potentially subject to deterioration due to corrosion.
The present application relates to refractory modules, insulating modules for lining an interior surface of a furnace wall and other compositions, which may be used to provide insulation in devices designed for use under high temperature conditions, e.g., temperatures in the range of 2,000 to 3000° F. The present modules may be comprised of at least two insulating module layers or elements and typically include a plurality of such layers/elements positioned in a side-by-side orientation. The insulating module layers may include a fibrous refractory material, such as a fibrous refractory blanket or mat. Each module layer or element may include hot face and cold face sections having joint edges held in juxtaposition along a section juncture(s) by the interlocking engagement of one or more tabs extending from a joint edge of a section with correspondingly positioned and dimensioned slots in a joint edge of another section. The inner contour of the slot commonly substantially corresponds in shape to the outer contour of its paired tab. Commonly, at least some portion of each tab's outer contour extends laterally in an outward direction from the base of the tab.
In some embodiments, each module layer may include first and second sections having joint edges held in juxtaposition along a section juncture by a single tab in one section inserted into a slot in the other section. The inner contour of the slot commonly substantially corresponds in shape to the outer contour of the tab. Where at least some portion of the tab's outer contour extends laterally in an outward direction from a perpendicular to the base of the tab, the interlocking engagement of the tab and the correspondingly shaped slot are said to form a “puzzle joint.” For example, the first section may have a slot extending into a joint edge thereof and the second section may have a correspondingly shaped tab extending outwardly from a joint edge. The tab typically may have an enlarging profile outer contour and the inner contour of the slot has a shape which substantially corresponds to the tab's outer contour. The first and second sections may be positioned to form an insulating module layer, e.g., as shown in
In one embodiment of an insulating module, each insulating module layer includes a first section having a slot extending thereinto from a first joint edge; and a second section having a tab extending from a second joint edge; wherein the tab has an enlarging profile outer contour and the slot has an inner contour which substantially corresponds to the tab outer contour; and the first and second sections are secured together by the tab being inserted into the slot to form a puzzle joint, such that the first and second joint edges are positioned with respect to each other to form a section juncture. The first and second sections are commonly each formed from a fibrous refractory material, e.g., fibrous refractory blanket or mat. A plurality of the insulating module layers may be held together with their major surfaces positioned in a side-by-side orientation. The adjacent layers may have been compressingly engaged, e.g., by application of a compression force in a direction substantially perpendicular to the major surfaces of the layers. As used herein, the term “adjacent layers” refers to any two layers which are positioned such that the two layers have major surfaces positioned immediately adjacent each other (i.e., with no other layers interposed therebetween). In some instances, the compressing engagement of adjacent layers may be the only feature holding the insulating module layers positioned in a side-by-side alignment, i.e., no high temperature cement or other adhesive and no clips and/or elongated plastic fasteners is used to hold the layers in position.
In some embodiments of the insulating module, adjacent insulating module layers have section junctures located in a manner such that the section junctures are offset with respect to each other, i.e., the section junctures in adjacent insulating module layers do not “cross” or overlap. In such embodiments, it is very common to have the extension length of each tab be less than the offset distance between the section juncture in that layer and the section juncture in the immediately adjacent layer(s). The offset distance between the section junctures in adjacent insulating module layers is typically somewhat greater than the extension length of the tab(s) in each layer. In certain of these embodiments, each tab may have an extension length, which is substantially the same as a preset tab extension length; and the section juncture in each layer is offset from the section junctures in adjacent layers by a distance which is greater the tab extension length. In many embodiments, the offset distance between the section junctures in adjacent insulating module layers may be at least about 120% and, more commonly, at least about 130% of the tab extension length. In some embodiments, the offset distance between the section junctures in adjacent insulating module layers is about 120% to 150% of the tab extension length.
In other embodiments, the present application provides an insulating module which includes a plurality of insulating module elements, where each insulating module element may include one or two hot face pieces, which may be formed from fibrous refractory blanket, and one or two cold face pieces, which may also be formed from fibrous refractory blanket (typically a different fibrous refractory blanket material from that used to form the hot face piece(s)). For example, an insulating module element may be formed by folding a “hot face” fibrous refractory blanket in a “U-shape” and joining the ends (“joint edges”) of the U-shaped piece to the joint edges of two straight pieces of “cold face” fibrous refractory blanket. Each of the “cold face” fibrous refractory blanket sections may have one or more tabs extending from the tab joint edge thereof. The U-shaped folded hot face fibrous refractory blanket may have one or more slots extending into its two joint edges. The slots may be configured to be aligned with paired tabs extending from the tab joint edges of the two cold face sections where for each tab/slot pair, the slot has an inner contour which substantially corresponds in shape to the outer contour of the paired tab. This allows the tab/slot pairs to be interlocking engaged and hold the tab joint edges of the two cold face pieces in juxtaposition with the joint edges of the U-shaped piece along respective section junctures. The “hot face” fibrous refractory blanket U-shaped piece is often folded such that the two joint edges are offset, typically such that the offset distance is greater than the tab extension lengths of the tabs extending from the two cold face sections. In other embodiments in which the insulating module elements include a U-shaped folded piece of fibrous refractory blanket, the cold face portion of the element may be formed from the U-shaped piece. In such embodiments, the “hot face” of the element may be formed from two “hot face” fibrous refractory blanket pieces. In still other embodiments, both the cold face and hot face portions of the element may both be formed from U-shaped folded fibrous refractory blanket. In each of these embodiments, the joint edges of the hot face piece(s) typically have slots positioned and shaped to receive correspondingly shaped paired tabs in interlocking engagement.
In some embodiments, the insulating module may include a support member having at least one elongated anchor rod attached thereto. A plurality of the insulating module layers or elements may be mounted on the anchor rod. The anchor rod may be dimensioned to extend at least partially through the insulating module, e.g., so that it extend in an orientation transverse to the major surfaces of at least two of the insulating module layers or elements. Typically the anchor rod is dimensioned such that it extends transversely through at least a majority of the insulating module layers (or elements) in the module.
For a more complete understanding of the features and advantages of the present insulating modules, reference is now made to the detailed description section along with the accompanying figures and in which:
While making and using various embodiments of the present method and composition are discussed in detail below, it should be appreciated that the present application provides many applicable inventive concepts that can be embodied in a wide variety of specific contexts. The specific embodiments discussed herein are merely illustrative of specific ways to make and use the present method and apparatus and are not intended to limit the scope of the invention.
Referring to
As described herein, the insulating module may include an access passage 105, which allows a tool to be is inserted into the hot face of the module and engages a fastening device for attaching the insulating module to the surface of a furnace casing. In some embodiments, the insulating module may include a removable sleeve portion (not shown) which ensures that the passage remains open. Following the attachment operation, as the tool is withdrawn, the removable sleeve portion may be manually removed from the module through its hot face following attachment or affixation to the furnace wall. As noted above, access to the fastening device 180 is gained through the hot face 106 of the module. That is, the fibrous refractory material comprising the hot face of the module may be displaced to gain access to the fastener and to perform the attaching operation. Once the attachment has taken place and the tool removed, the refractory fibers generally will relax and fill the passage 105. In some instances, the refractory fibers may not be sufficiently resilient to allow this to occur immediately after removal of the attachment tool. To facilitate the rearrangement of the fibrous material, the hot face of the module may be manipulated manually to ensure closure of the passage 105.
As noted above, the two sections of an insulating module layer according to the present application may be joined together by a puzzle joint formed by the interlocking engagement of two or more tab and slot pairs.
The present application provides a refractory module comprising a plurality of insulating module layers arranged such that their major surfaces are contacted in a side-by-side orientation. The insulating module layers are commonly formed from refractory insulation material material, e.g., from a fibrous refractory blanket or mat. Each layer includes a first section having at least one slot extending therein from a first joint edge; and a second section having at least one tab extending from a second joint edge thereof. The slot(s) has an inner contour which substantially corresponds in shape to the outer contour of the tab(s), such that when a tab is inserted in interlocking engagement into a correspondingly configured slot, the edges of the first and second sections are held in juxtaposition (typically in edge-to-edge contact) along a section juncture. In certain exemplary embodiments, each tab may have an expanding trapezoid outer contour. Typically, the sections are positioned such that all of the first sections have an edge which is exposed to the hot face of the module and all of the second sections have an edge which is exposed to the cold face of the module. The first sections typically have a tab clearance of at least about two (2) inches in order to ensure that the refractory insulation material material used to form the cold face section is not exposed temperatures which could degrade the material. As used herein, the term “tab clearance” refers to the distance between the outside edge (typically the hot face edge of the section) of an insulating module layer section with a slot in its joint edge and the closest portion of any tab from another section interlockingly engaged with the slot bearing section. For example, in the insulating module layer depicted in
In many embodiments, the first section of each insulating module layer includes a first refractory insulation material and the second section of each insulating module layer includes a second refractory insulation material which is different from the first refractory insulation material. The first and second refractory insulation materials may be formed from fibers selected from soluble fibers, fiber glass, mineral fibers, alumina fibers, zirconia fibers, alumina-zirconia fibers, alumina-silica-zirconia fibers, alumina-silica fibers (e.g., mullite fibers), and/or chromia-alumina-silica fibers. In some versions of the present insulating module, the first section of each insulating module layer includes a hot face refractory insulation material comprising mullite fibers; and the second section of each insulating module layer comprises a cold face refractory insulation material comprising alumina-silica-zirconia fibers.
In various embodiments, the major surfaces of the insulating module layers may be held in contact in a side-by-side orientation using a variety of methods known to those of skill in the art. For example, the insulating module layers may be held together in the side-by-side orientation by one or more plastic fasteners, which have an elongated filament with outwardly extending end sections. The elongated filament dimensioned to extend at least partially through at least two of the insulating module layers such that the filament end sections engage the layers and hold them in position. In other embodiments, the insulating module layers may be held in a side-by-side orientation using metal clips. In still other embodiments, the insulating module layers may be placed in side-by-side orientation and subjected to a compressive force applied a to the outer major faces of the two outermost insulating module layers until the total thickness of the combined layers has been compressed by a desired amount. Such modules may be referred to as having the insulating module layers “compressingly engaged” in side-by-side orientation. Typically, the adjacent layers have been compressingly engaged by application of a compression force in a direction substantially perpendicular to the major surfaces of the layers. In some embodiments, other than having the anchor rods of an optionally included fastening device pass transversely through the first section of the insulating module layers, such compressing engagement may be the only method employed to keep the plurality of layers positioned in side-by-side orientation. In other embodiments, in addition to these methods of holding the insulating module layers in position, the module may be wrapped or encircled by banding to aid in positioning the layers during shipping, handling and installation. In yet other embodiments, a combination of two or more of the above described methods may be employed to hold the insulating module layers in a side-by-side orientation.
In the embodiments of the insulating module layers described herein, the two sections of a layer include correspondingly shaped tab(s) and slot(s) which are configured to form a “puzzle joint.” As employed herein, the term “puzzle joint” refers to a joint formed by the interlocking engagement of one or more tabs and correspondingly shaped and positioned slots where at least some portion of each tabs' outer contour extends laterally in an outward direction, that is at least one edge of the tab profile extends laterally in an outward direction from a line perpendicular to the tab base in an outward direction with respect to the tab base. Examples of such tab configurations are shown in
As discussed above, in certain embodiments the insulating module layers may be positioned in a side-by-side orientation and then by applying a compressive force to the outer major faces of the two outermost insulating module layers, the total thickness of the combined layers is compressed down to a desired thickness. Such layers are referred to a “compressingly engaged.” The term “compression factor” is used herein to refer to the amount of compression applied used herein the term “compression factor” refers to the ratio—(the total thickness of the combined insulating module layers before compression):(the total thickness of the combined insulating module layers after compression). Where this technique is employed in the production of the present term modules, an insulating module suitably has a compression factor (“CF”) of at least about 1.05. Modules with compression factors ranging from about 1.05 to 2 are quite suitable for use in the present insulation methods. Quite commonly, the present insulating modules may have a compression factor of about 1.1 to 1.5.
In the puzzle joints described herein, the slot may be configured to extend completely through the thickness of an insulating module layer section, that is the inner contour of the slot extends completely through from one major surface to the opposing major surface of the section. In some embodiments, however, the slot may be a groove in which the inner contour extends only partially into that thickness of the insulating module layer section, that is where the inner contour of the slot does not extend completely through from one major surface to the opposing major surface of the section. In each case, the shape and thickness of the tab on the corresponding other section of the insulating module layer is commonly configured in a substantially similar manner such that the tab and slot can be positioned in interlocking engagement. To avoid confusion, as used herein, the terms “outer contour” (in reference to a tab) and “inner contour” (in reference to a slot) refer to the contour of the tab or slot with respect to a major surface of the insulating module layer section intersected by the tab or slot.
Illustrative Embodiments
Reference is made in the following to a number of illustrative embodiments of the subject matter described herein. The following embodiments describe illustrative embodiments that may include various features, characteristics, and advantages of the subject matter as presently described. Accordingly, the following embodiments should not be considered as being comprehensive of all of the possible embodiments or otherwise limit the scope of the methods, materials and compositions described herein.
One embodiment provides a refractory module comprising a plurality of insulating module layers arranged such that their major surfaces are positioned in a side-by-side orientation. Each of the insulating module layers are commonly formed from a fibrous refractory blanket or mat. Each layer typically includes first and second sections joined together along a section juncture by the interlocking engagement of a tab extending from an edge of one section with a slot in an edge of the other section, where the slot has an inner contour which substantially corresponds in shape to the outer contour of the tab. Typically, the sections are positioned such that all of the first sections have an edge which is exposed to the hot face of the module and all of the second sections have an edge which is exposed to the cold face of the module. For example, each first section may include a hot face refractory insulation material having a temperature rating of about 3,000° F. (e.g., a mullite fiber material such as Maftec® 3000 Blanket with a density of about 6 pcf) and each second section may include a cold face refractory insulation material having a temperature rating of no more than about 2,600° F. (e.g., an alumina-silica-zirconia fiber material such as 2600 HTZ Blanket with a density of about 8 pcf).
In some exemplary embodiments, each tab may commonly be centrally positioned on a joint edge of the insulating module layer section from which it extends. The tabs are typically dimensioned such that the tab base has a width that is about 20-40% of the width of the insulating module layer (and correspondingly is typically about 20-40% of the width of the section edge from which it extends). Where such tabs have an enlarging outer contour, the widest portion of the tab contour may suitably have a width that is about 30-50% of the width of the insulating module layer. Such the tabs may have an enlarging trapezoid outer contour. Suitable tabs may have a tab extension length of at least about one inch and, commonly about one to two inches.
In one exemplary embodiment, the present insulating module includes insulating module layers in which the two sections of each layer are formed from different refractory insulation materials, typically in the form of a fibrous refractory mat or blanket. Commonly, the sections on the side of the module to be exposed to a furnace interior, the “hot face,” are formed from a refractory insulation material which has a temperature rating which is at least about 400 or 500° F. higher than the temperature rating of the other sections which make up the “cold face” of the module. For example, the module layer sections exposed to the hot face may be formed from mullite fibers (with a temperature rating of about 3,000° F.) while the sections exposed on the cold face of the module may be formed from a refractory insulation material having a lower temperature rating, e.g., an alumina-silica-zirconia fiber material with a temperature rating of about 2,600° F.
The present insulating modules may be in the form of a cube, e.g., a twelve inch cube where the major faces of each insulating module layer measure about twelve (12) inches by twelve (12) inches and sufficient layers are positioned in a side-by-side orientation to create a twelve (12) inch thick module. This may be done by positioning twelve one (1) inch thick insulating module layers in a side-by-side orientation to create the twelve (12) inch thick module. In other embodiments, more than twelve one (1) inch thick insulating module layers, e.g., fourteen to sixteen of such insulating module layers may be positioned in a side-by-side orientation and then by applying a compressive force to the outer major faces of the two outermost insulating module layers, the total thickness of the combined layers is compressed down to about twelve (12) inches. Other embodiments may be formed by positioning eight to twelve insulating module layers with a one and one-half (1½) inch thickness in a side-by-side orientation and, if necessary, compressing the layers to provide a desired thickness of the insulating module.
In many embodiments, the module may also include the support member and anchor rods of a fastening device for attaching the insulating module to a furnace wall disposed in the module, e.g., in the manner depicted in
In another embodiment, the present application provides an insulating module which includes a plurality of insulating module layers arranged with their major surfaces in a side-by-side orientation, where each layer has a first section with one or more slots extending therein from its slot joint edge; and a second section with one or more tabs extending from a tab joint edge thereof. The first and second sections each comprise a refractory insulation material, e.g., the first and second sections may each be formed from a fibrous refractory blanket. Each tab on a second section is interlocking engaged with a paired slot in the corresponding first section (i.e., the first section from the same insulating module layer) and each slot has an inner contour which substantially corresponds in shape to an outer contour of its paired tab. As illustrated by
In another embodiment, the present application provides an insulating module which includes a plurality of insulating module elements. The insulating module elements may have a flattened rectangular box shape and be arranged with their major surfaces in a side-by-side orientation. Often the major surfaces of the insulating module elements may have a substantially square shape (i.e., square prism shape). Each insulating module element may include one or two hot face pieces, which may be formed from refractory insulation material, and one or two cold face pieces, which may also be formed from refractory insulation material (typically a different refractory insulation material from that used to form the hot face piece(s)). For example, an insulating module element may be formed by folding a “hot face” fibrous refractory blanket in a “U-shape” and joining the ends (“joint edges”) of the U-shaped piece to the joint edges of two pieces of “cold face” fibrous refractory blanket (see, e.g., illustrative insulating module element depicted in
The insulating modules described herein may be produced by a process which includes forming a plurality of insulating module layers or elements by interlockingly engaging a tab(s) on one or two cold face sections formed from refractory insulation material with a correspondingly positioned and shaped slot(s) in the joint edge(s) of a hot face section formed from refractory insulation material, such that the hot and cold face sections are held in juxtaposition along a section juncture(s). A plurality of the insulating module layers or elements are then positioned with their major surfaces positioned in a side-by-side orientation such that all of the hot face sections have an edge (or folded edge) exposed to one side of the bundle of layers/elements and all of the cold face sections have an edge exposed to an opposite side of the bundle of layers/elements. The insulating module layers/elements are typically positioned such that adjacent layers/elements have section junctures located in a manner such that each section juncture is offset with respect to the section juncture in any adjacent layer/element. In most instances, this assembled bundle of insulating module layers/elements is then subjected to a compressive force applied to the outer major faces of the two outermost insulating module layers/elements. The bundle of layers/elements is then compressed until the total thickness of the combined layers/elements has been compressed by a desired amount, e.g., until a compression factor (“CF”) of at least about 1.05 and, more commonly about 1.1 to 1.5, has been achieved. If desired, during the assembly of the bundle the layers/elements can be divided into two groups positioned in a side-by-side orientation and the anchor rod(s) of a fastening device can be inserted through spaced apart holes provided through the cold face sections of the insulating module layers/elements. The spaced apart holes are commonly dimensioned and adapted to receive the anchor rod(s) such that the rods extend transversely completely through all but the two outermost insulating module layers of a mounting assembly. The assembled bundle of insulating module layers/elements including the anchor rod(s) and any other desired pieces of a fastening device can then be subjected to a compression operation as described above.
It will be readily apparent to one skilled in the art that varying substitutions and modifications may be made to the methods and compositions disclosed herein without departing from the scope and spirit of the invention. The terms and expressions which have been employed are used as terms of description and not of limitation, and there is no intention that in the use of such terms and expressions of excluding any equivalents of the features shown and described or portions thereof, but it is recognized that various modifications are possible within the scope of the invention. Thus, it should be understood that although the present invention has been illustrated by specific embodiments and optional features, modifications and/or variations of the concepts herein disclosed may be resorted to by those skilled in the art, and that such modifications and variations are considered to be within the scope of this invention.
In addition, where features or aspects of the invention are described in terms of Markush groups or other grouping of alternatives, those skilled in the art will recognize that the invention is also thereby described in terms of any individual member or subgroup of members of the Markush group or other group.
Also, unless indicated to the contrary, where various numerical values are provided for embodiments, additional embodiments are described by taking any two different values as the endpoints of a range. Such ranges are also within the scope of the invention described herein.
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