The invention relates to surge arresters and other types of electrical power distribution equipment, and more particularly to mechanical reinforcement of a monolithic disk or a bonded disk stack used in such equipment.
Electrical transmission and distribution equipment is subject to voltages within a fairly narrow range under normal operating conditions. However, system disturbances, such as lightning strikes and switching surges, may produce momentary or extended voltage levels that greatly exceed the levels experienced by the equipment during normal operating conditions. These voltage variations often are referred to as over-voltage conditions.
If not protected from over-voltage conditions, critical and expensive equipment, such as transformers, switching devices, computer equipment, and electrical machinery, may be damaged or destroyed by over-voltage conditions and associated current surges. Accordingly, it is routine practice for system designers to use surge arresters to protect system components from dangerous over-voltage conditions.
A surge arrester is a protective device that commonly is connected in parallel with a comparatively expensive piece of electrical equipment so as to shunt or divert over-voltage-induced current surges safely around the equipment, and thereby protect the equipment and its internal circuitry from damage. When exposed to an over-voltage condition, the surge arrester operates in a low impedance mode that provides a current path to electrical ground having a relatively low impedance. The surge arrester otherwise operates in a high impedance mode that provides a current path to ground having a relatively high impedance. The impedance of the current path is substantially lower than the impedance of the equipment being protected by the surge arrester when the surge arrester is operating in the low-impedance mode, and is otherwise substantially higher than the impedance of the protected equipment.
Upon completion of the over-voltage condition, the surge arrester returns to operation in the high impedance mode. This prevents normal current at the system frequency from following the surge current to ground along the current path through the surge arrester.
Conventional surge arresters typically include an elongated outer enclosure or housing made of an electrically insulating material, a pair of electrical terminals at opposite ends of the enclosure for connecting the arrester between a line-potential conductor and electrical ground, and one or more other electrical components that form a series electrical path between the terminals. These components typically include a stack of one or more voltage-dependent, nonlinear resistive elements that are referred to as varistors. A varistor is characterized by having a relatively high resistance when exposed to a normal operating voltage, and a much lower resistance when exposed to a larger voltage, such as is associated with over-voltage conditions. In addition to or in place of varistors, a surge arrester also may include one or more spark gap assemblies housed within the insulative enclosure and electrically connected in series with the varistors. Some arresters also include one or more electrically-conductive spacer elements coaxially aligned with the varistors and gap assemblies.
For proper arrester operation, contact must be maintained between the components of the stack. To accomplish this, it is known to apply an axial load to the one or more elements of the stack. Good axial contact is important to ensure a relatively low contact resistance between the adjacent faces of the elements, to ensure a relatively uniform current distribution through the elements, and to provide good heat transfer between the elements and the end terminals.
One way to apply this load is to employ springs within the housing to urge the one or more stacked elements into engagement with one another. Another way to apply the load is to encase the stack of one or more arrester elements in glass fibers so as to axially-compress the elements within the stack. For bonded disk stacks or monolithic disks with a sufficiently high rating, such as, for example, a rating greater than 6 kV, these methods are usually sufficient to sustain a static mechanical load but may not be sufficient to withstand the thermo-mechanical forces experienced by the one or more elements during a high current impulse such as, for example, a 100 kA impulse.
When the bonded disk stack or monolithic disk with a sufficiently high rating, such as, for example, a rating greater than 6 kV, is subjected to a high current impulse, the resulting thermo-mechanical forces tend to cause cracking of the surge arrester elements, which tend to crack in mid-plane when subjected to the thermo-mechanical forces of a high current impulse. For bonded disk stacks of more than one element, there also may be cracking near the center of the bonded disk column or the monolithic element. The tendency of an element to crack during high current impulses limits the size of an individual surge arrester element as well as the overall length of a stack of bonded surge arrester elements. There is a height-diameter ratio where a monolithic disk or a bonded disk stack will be subject to thermo-mechanical failure due to a high current impulse, typically in the form of a crack at the mid-plane.
In one general aspect, a mechanically reinforced electrical apparatus includes at least one electrical element having a reinforcing structure attached to the outer surface of the electrical element. The reinforcing structure may include a fiber matrix pre-impregnated with a resin. The fiber matrix may be any woven or interwoven fabric, sheet, tape, or strip. The fiber matrix may encompass any form factor, and may be narrow or wide as needed to selectively reinforce the bonded disk stack or monolithic element. The fiber matrix typically has a pre-formed woven or interwoven pattern. However, the fiber matrix also may take other forms, such as the form of a collection of fiber segments. The fiber matrix is pre-impregnated with resin, and is applied to the electrical elements as desired.
Implementations may include one or more of the following features. For example, the electrical element may be a monolithic metal-oxide varistor (“MOV”) disk or a bonded MOV disk stack. Each end of the monolithic disk is in contact with a terminal accessible from the exterior of the apparatus. Monolithic disks may be rated, for example, greater than 6 kV and, more particularly, between 6 kV and 800 kV. The electrical apparatus may be built to withstand at least one approximately 100 kA impulse. The fibers in the fiber matrix may be oriented in a predetermined orientation, oriented parallel to an axis of the electrical element, or oriented in a random direction. The fibers in the fiber matrix may be of a predetermined length, a uniform length, and/or of more than one length. The fibers in the fiber matrix may be any insulated fibrous material such as, for example, fiberglass, Kevlar, Nextel, or a similar material.
In one implementation, the fiber matrix is made with a predetermined woven or interwoven pattern such that, when applied to the electrical element, the fibers are at a pre-determined angle. For example, the pattern may be a back and forth wind pattern, or any other woven or interwoven pattern. The predetermined angle may be an angle less than approximately 50 degrees, such as, for example, an angle between approximately 3 degrees and approximately 10 degrees. The fiber matrix may be circumferentially applied to the electrical element. The fiber matrix may be applied to the electrical element in layers to a predetermined thickness, such as, for example, approximately up to one-quarter of an inch, and more typically approximately twenty thousandths of an inch. The fiber matrix may also be vertically applied or may be combined with, for example, a vertically applied matrix and/or fiber segments embedded in resin.
In another implementation, the pre-impregnated fiber matrix is vertically (i.e., longitudinally) applied. In one implementation, the vertical application may have at least one piece of matrix that may be vertically oriented along an axis of the electrical element. The vertical application may also have a single piece of matrix placed in a vertical orientation along an axis of the electrical element with sufficient width to cover the majority of an outer surface of the electrical element. The vertical application may have a predetermined thickness. The fiber matrix may also be circumferentially applied or may be combined with, for example, a circumferentially applied matrix and/or fiber segments embedded in resin.
In another implementation, the reinforcing structure may have at least one layer of pre-impregnated fiber matrix applied circumferentially with fibers oriented at a predetermined angle and at least one layer of pre-impregnated fiber matrix applied vertically. In another implementation, the reinforcing structure may have a coating of fiber segments embedded in a resin.
In another general aspect, reinforcing an electrical apparatus includes providing at least one electrical element, preparing a reinforcing layer for application to the outer surface of at least one electrical element, and applying the reinforcing layer to at least a portion of the outer surface of at least one electrical element. The reinforcing layer has a fiber matrix pre-impregnated with resin.
Implementations may include one or more of the features discussed above and one or more of the following features. For example, the element may be heated to a sufficient temperature for application of the fiber matrix, such as, for example, to between approximately 100 degrees and 200 degrees Fahrenheit. In another implementation, post application processing of the reinforcing layer may be performed. The post application processing may include curing or heating the element. The heating may be done in an oven, by a forced air gun, or by other suitable method. The element may be heated to a sufficient temperature for curing. For example, the element may be heated to between approximately 250 degrees and 400 degrees Fahrenheit.
In another general aspect, reinforcing an electrical apparatus includes providing at least one electrical element, preparing a reinforcing layer for application to the outer surface of at least one electrical element, and applying the reinforcing layer to at least a portion of the outer surface of at least one electrical element. The reinforcing layer has a mixture of fibers pre-impregnated with resin.
Implementations may include one or more of the features of discussed above and one or more of the following features. For example, the reinforcing layer may be applied by coating the element by dipping the element in a mixture of fibers and resin, casting the element in a pre-impregnated fiber matrix, powder coating the element in a fiber matrix, coating the element in a fiber matrix, or other suitable techniques.
The mechanically-reinforced electrical apparatus, which may be, for example, a surge arrester, offers considerable advantages. For example, the mechanical reinforcement restricts the tendency of a bonded stack of elements or a monolithic element to crack during a high current impulse. In this manner, the length or thickness of the monolithic element or the bonded stack can be increased without a subsequent increase in the risk of cracking during an impulse. The element or the bonded stack also can be left at a conventional length and have a decreased likelihood that the element or the bonded stack will crack as compared to a non-reinforced monolithic element or bonded stack of the same dimensions. To minimize the cost of reinforcement, the reinforcing structure can be placed only in those areas where the crack is likely to occur, typically in the area around and including the center of the element or the bonded stack along its length. As a result, increased-length monolithic elements can be produced that are longer than those currently used in surge arresters. Also, the use of bonded disk stacks becomes practical. This use promises to increase the applicability of monolithic elements, such as MOVs to bonded disk stack surge arresters as well as to monolithic surge arresters.
Other features and advantages will be apparent from the description, the drawings, and the claims.
Like reference symbols in the various drawings indicate like elements.
Referring to
Elements 115 of the bonded element stack 105 are stacked in an end-to-end relationship and bonded together at their end surfaces. Since the elements 115 of the stack 105 are affirmatively bound together, the arrester 110 does not need to include a mechanism or structure for applying an axial load to the elements. The bonding supplies sufficient mechanical strength for a static load.
The surge arrester 110 may be implemented as any class of surge arrester, including a station, intermediate, or distribution class surge arrester. For example, in distribution class systems, a monolithic element of up to approximately 6 kV to approximately 9 kV may be used. A bonded disk stack may include, for example, multiples of 3 kV, 6 kV, or 9 kV elements bonded together. However, other values such as 1 kV or 10 kV may be used for the individual element, and the arrester is not limited to any particular combination of voltage ratings. It should also be understood that the module 100 may be used in other types of surge arresters, and in other electrical protective equipment.
The bonded element stack 105 may include different numbers of elements 115, and elements 115 of different sizes or types. Examples include varistors, capacitors, thyristors, thermistors, and resistors. Typically, the elements 115 are cylindrical, though the elements 115 may include other shapes as well. For purposes of explanation, the stack is shown as including three metal oxide varistors (“MOVs”) 115 and a pair of terminals 120.
Referring also to
The MOVs may be sized according to the desired application. For example, in one set of implementations, the MOV may have a diameter between approximately 1 to 3 inches, such that the upper and lower faces 125, 130 each have surface areas of between about 0.785 and 7.07 square inches.
Given a particular metal oxide formulation and a uniform or consistent microstructure throughout the MOV, the thickness of the MOV determines the operating voltage level of the MOV. In one implementation, each MOV is about 0.75 inches thick. In some implementations, this thickness may be tripled.
It is desirable to minimize the cross-sectional areas of the MOVs so as to minimize the size, weight and cost of the arrester. However, the durability and recoverability of the MOVs tend to be directly related to the sizes of the MOVs. In view of these competing considerations, MOVs having diameters of approximately 1.6 inches have been used.
The upper and lower faces 125, 130 may be metallized using, for example, sprayed-on coatings of molten aluminum or brass. In some implementations, these coatings have a thickness of approximately 0.002 to 0.010 inches. The outer cylindrical surface 135 is covered by an insulative collar.
A terminal 120 is disposed at each end of the stack 105. Each terminal 120 typically is a relatively short, cylindrical block formed from a conductive material, such as, for example, aluminum. Each terminal 120 has a diameter substantially equal to that of an MOV 115. In some implementations, each terminal also may include a threaded bore 150 in which may be positioned a threaded conductive stud 155. In general, the terminals 120 may be thinner than terminals associated with modules that, for example, are encased with a structural layer to provide an axial load on the components of the module. This reduced thickness may result from changes in the geometry of the device, or simply because thicker metal is not needed for bonding with the structural layer.
As shown in
As noted above, elements of the bonded element stack 105 may be bonded together at their end faces, such that the stack 105 serves as both the electrically-active component and the mechanical support structure of an electrical protective device, such as the surge arrester 110. The bonding provides a mechanically-compliant, electrically-conductive joint between the MOVs, which reduces the deleterious effects of the thermo-mechanical forces associated with service operating conditions and thus lengthens the expected service life of the surge arrester.
The bonding may be implemented to form a mechanically-compliant joint using combinations of electrically-conductive materials and mechanically-compliant materials. In general, the joint reduces or dampens axial tensile forces by having a Young's modulus substantially below that of the disks that it separates and bonds. For example, the necessary compliance of the joint is achieved by the joint having Young's modulus that is less than half of the Young's modulus of the MOV disk. More particularly, the Young's modulus of the joint may be between approximately one-eightieth and one-tenth of the Young's modulus of the electrical components separated by the joint. Even more particularly, the Young's modulus of the joint may be approximately one-fortieth of the Young's modulus of the electrical components. For example, in one implementation, the disks have a Young's modulus of 16,000,000 pounds per square inch (psi), and the joint has a Young's modulus of approximately 400,000 psi. In some applications, the joint will have a thickness of approximately 0.25 inches. The bonding joint also may be implemented using a single material that is electrically-conductive and mechanically-compliant. The MOV disks optionally may be metallized with, for example, copper, aluminum, or brass. Examples of the electrically-conductive and mechanically-compliant joint are described in U.S. application Ser. No. 09/577,837, filed May 25, 2000, by Michael M. Ramarge, David P. Bailey, Thomas C. Hartman, Roger S. Perkins, Alan P. Yerges, Michael G. Scharrer, and Lisa C. Sletson, titled “Compliant Joint Between Electrical Components,” which is incorporated by reference.
In the above examples, the adhesive can be, for example, a polymer, such as a polyimide, polyamide, polyester, polyurethane, elastomer, silicone, or epoxy. The adhesive can be made electrically-conductive by adding a conductive material, such as silver, a silver alloy, and/or carbon black. The polymer and polymer composite laminates of the examples described above also can be one or more of the polymers listed above. The polymer composite laminates may be fiber reinforced, or formulated with fillers, such as reinforcing fillers to modify the mechanical properties of the laminate, or extending fillers to modify the physical properties of the laminate. The polymers and polymer composite laminates can be made electrically-conductive by adding conductive materials, such as silver, silver alloys, and/or carbon black.
In general, the joints described above will function between any pair of components in which a mechanically-compliant and electrically-conductive joint is necessary or desirable. For example, the joints described above can be formed between different electrical components, such as between an end terminal and a MOV disk.
Referring to
The length or thickness of a monolithic element is limited because the thermo-mechanical forces associated with some impulses will crack the element. For example, because of the likelihood of cracking, most monolithic elements do not exceed a rating of 9 kV. As described below in detail, the electrical component module 200 may be reinforced to enable it to better withstand the thermo-mechanical shock of a high current impulse. In this manner, the monolithic element can be lengthened beyond the length of conventional 9 kV monolithic elements. The ability to use longer monolithic elements provides considerable cost savings in the manufacture of the elements and the manufacture of surge arresters incorporating the monolithic elements.
Like the surge arrester 110, the surge arrester 210 may be implemented as any class of surge arrester, including a station, an intermediate, and a distribution class surge arrester. For example, a monolithic element typically may be used in distribution systems of up to approximately 6 kV to approximately 9 kV. As noted above, a monolithic element with a rating greater than 9 kV has an increased likelihood of cracking during an impulse. Thus, monolithic elements having a rating greater than 9 kV generally are not used in conventional applications. It should be understood that the module 200 may be used in other types of surge arresters, and in other electrical protective equipment.
The monolithic element 205 may be configured in different sizes or types, such as varistors, capacitors, thyristors, thermistors, and resistors. Typically, the element 205 is cylindrical, though the element 205 may be configured in other shapes as well. For purposes of explanation, the surge arrester 210 is shown as including a single monolithic MOV 205 and one pair of terminals 120.
Referring also to
Given a particular metal oxide formulation and a uniform or consistent microstructure throughout the monolithic MOV 205, the thickness of the monolithic MOV determines its operating voltage level. In one implementation, the monolithic MOV 205 is about three to six inches thick. In some implementations, this thickness may be increased by, for example, as much as three inches.
A terminal 120 is disposed at each end of the monolithic MOV 205. The terminals 120 may have any or all of the features described above. For example, each terminal 120 may have a diameter substantially equal to that of the monolithic MOV 205.
As shown in
Referring to
The reinforcing structure 305 provides mechanical reinforcement to the reinforced electrical component module 300 to permit the module to withstand the thermo-mechanical shock of a high current impulse. The structure 305 may provide mechanical reinforcement to the entire module 300 or to a selected portion of the module 300. The reinforcing structure 305 typically provides constraining forces in the axial direction and/or the circumferential hoop direction of the reinforced electrical component module 300. The constraining forces provided by the reinforcing structure 305 are sufficient to allow the reinforced module 300 to withstand the thermo-mechanical shock of a high current impulse without cracking. More particularly, the reinforcing structure 305 allows the reinforced electrical component module 300 to withstand a larger thermo-mechanical shock than could be withstood by an equivalent non-reinforced electrical component module 100.
The reinforcing structure 305 is attached to the outer surface 135 of the stack 105, and may be attached to the outer surface of at least a portion of one or more elements 115 . The reinforcing structure 305 also may be applied to the upper face 125 of the topmost element and/or may be applied to the lower face 130 of the bottommost element. The reinforcing structure typically is applied vertically (i.e., longitudinally) or circumferentially, or both, and may encase a portion of the upper face 125 of the topmost element and/or the lower face 130 of the bottommost element. Where there is more than one element, the reinforcing structure 305 typically is applied to the outer surface 135 of each element 115 of the bonded disk stack 105. However, as shown in
The reinforcing structure 305 may include at least one layer of a pre-impregnated fiber matrix 310. The fiber matrix may be any woven or interwoven fabric, sheet, tape or strip. The fiber matrix may take other forms, such as, for example, a collection of fiber segments. The fiber matrix may encompass any form factor, and may be narrow or wide as needed to selectively reinforce the bonded disk stack or monolithic element. The fiber matrix typically has a preformed woven or interwoven pattern. The fiber matrix is pre-impregnated with resin, and is applied to the electrical elements as desired. The pre-impregnated fiber matrix 310 is pre-formed and typically has fibers oriented in a set orientation. Implementations include fibers oriented to be parallel, perpendicular or at any other angle with respect to an axis of the stack 105. Another implementation includes fibers that are randomly oriented. The length of the fibers in the pre-impregnated fiber matrix 310 may be predetermined or random. Implementations include fibers that are, for example, continuous, of at least one predetermined length, or random in length. The fiber matrix 310 typically is pre-impregnated with resin. The matrix may be, for example, dipped, cast, powder cast, or otherwise pre-impregnated. The fibers may be any insulating fibrous material such as, for example, fiberglass, Kevlar, or Nextel.
As shown in
Referring to
Referring to
Referring to
Referring to
The reinforcing structure 305 increases the resistance of the stack 105 to impulse cracking. In this manner, the length or thickness of the stack can be increased without a subsequent increase in the risk of cracking during an impulse. The stack also can be left at a conventional length so as to provide a decreased likelihood that the stack will crack as compared to a non-reinforced stack of the same dimensions. To minimize the cost of reinforcement, the reinforcing structure can be placed only in those areas where the crack is likely to occur, which typically is in the area around and including the center of the stack along its length.
Referring to
The reinforcing structure 405 is used to provide mechanical reinforcement to the electrical component module 205 in order to withstand the thermo-mechanical shock of a high current impulse, and may provide mechanical reinforcement to the entire reinforced electrical component module 400 or to a selected portion of the reinforced electrical component module 400. The reinforcing structure 405 typically provides axial and/or circumferential constraining forces around the reinforced electrical component module 400. The constraining forces provided by the reinforcing structure 405 are sufficient to allow the reinforced electrical component module 400 to withstand the thermo-mechanical shock of a high current impulse without cracking.
The reinforcing structure 405 is attached to at least a portion of the outer surface 235 of the monolithic MOV 205. The reinforcing structure 405 also may be applied to the upper face 225 of the MOV 205 and/or may be applied to the lower face 230 of the MOV 205.
The reinforcing structure 405 may include at least one layer of pre-impregnated fiber matrix 410. The pre-impregnated fiber matrix 410 typically has fibers oriented in a predetermined orientation. Implementations include fibers oriented to be parallel, perpendicular, or at any other angle with respect to an axis of the MOV 205. Another implementation includes fibers that are randomly oriented. The length of the fibers in the pre-impregnated fiber matrix 410 may be predetermined or random. Implementations include fibers that are, for example, continuous, of at least one predetermined length, or random in length. The fiber matrix 410 typically is pre-impregnated with resin. The fiber matrix may be, for example, dipped, cast, powder cast, or otherwise pre-impregnated. The fibers may be made of any insulating fibrous material. For example, the fibers may be made of fiberglass, Kevlar, or Nextel.
As shown in
Referring to
Referring to
Referring to
Referring to
The reinforcing structure 405 increases the resistance of the monolithic MOV 205 to impulse cracking. In this manner, the length or thickness of the MOV can be increased without a subsequent increase in the risk of cracking during an impulse. The MOV also can be left at a conventional length so as to have a decreased likelihood of cracking relative to a non-reinforced monolithic MOV of the same dimensions. To minimize the cost of reinforcement, the reinforcing structure can be placed only in those areas where the crack is likely to occur, typically in the area around and including the center of the MOV along its length. As a result, increased-length monolithic MOVs can be produced that are longer than those currently used in surge arresters. Also, the use of bonded disk stacks becomes practical. Thus, this use will increase the applicability of monolithic MOVs to bonded disk stack surge arresters as well as monolithic surge arresters.
The reinforcing structure 305, 405, which may include at least one layer of pre-impregnated fiber matrix 310, 410, is prepared for application to the component module 100, 400 (step 515). For example, the fiber matrix 310, 410 maybe embedded in an epoxy matrix, or the fibers of the matrix 310, 410 may be oriented in a predetermined or random direction. In another implementation, fiber segments 315, 415 may be mixed in an epoxy 320, 420. The fibers 315, 415 may be, for example, of a predetermined length or a random length.
The reinforcing structure 305, 405 is applied to the component module 100, 400 (step 520). For example, the reinforcing structure 305 may be applied to at least a portion of at least one disk 115 of a bonded disk stack 105, or the reinforcing structure 405 may be applied to at least a portion of a monolithic disk stack 205. The reinforcing structure 305, 405 may be applied by, for example, circumferentially and/or vertically applying pre-impregnated fiber matrix 310, 410, as described above. In another implementation, the reinforcing structure 305, 405 may be applied as a coating. For example, the reinforcing structure 305, 405 may be applied as a coating of fiber segments 315, 415 mixed in resin 320, 420, as described above.
Post-application processing is performed on the reinforcing structure 305, 405 after it is applied to the component module 100, 400 (step 525). The post-application processing may include curing of the resin, such as heating the structure to between approximately 250° F. and approximately 400° F. for approximately 60 minutes to approximately 120 minutes. Again the heating may be performed in an oven or by the use of a forced air heat gun or other suitable methods. The module and structure 305, 405 then are inserted into the housing 165 (step 530). The surge arrester with the reinforced component module 100, 400 is ready to be used in service and to better withstand the thermo-mechanical shock of a high current impulse.
The reinforcing structures described above can be applied to the component module of any surge arrester, including surge arresters rated greater than 6 kV, and more particularly, rated between 6 kV and 800 kV, and can be applied to component modules to withstand a 100 kA current impulse. For example, the reinforcing structures can be applied to a component module of a 700 kV surge arrester used, for example, in a high voltage station application. Multiple layers of the fiber matrix pre-impregnated with a resin can be purchased and applied to the component module and each individual layer cured or all of the layers cured in a single step. The multiple layers serve to provide two forms of mechanical reinforcement. The first form of reinforcement is to support the structure itself and reduce the need for the housing to provide mechanical support. As such, the housing can be reduced in size and thickness. This will advantageously reduce the cost of the resulting surge arrester.
Other implementations are within the scope of the following claims.
Number | Name | Date | Kind |
---|---|---|---|
3913127 | Suzuki et al. | Oct 1975 | A |
4404614 | Koch et al. | Sep 1983 | A |
4656555 | Raudabaugh | Apr 1987 | A |
4851955 | Doone et al. | Jul 1989 | A |
4899248 | Raudabaugh | Feb 1990 | A |
4962440 | Johnnerfelt et al. | Oct 1990 | A |
4992906 | Doone et al. | Feb 1991 | A |
5003689 | Doone et al. | Apr 1991 | A |
5043838 | Sakich | Aug 1991 | A |
5047891 | Nedriga | Sep 1991 | A |
5128824 | Yaworski et al. | Jul 1992 | A |
5159748 | Doone et al. | Nov 1992 | A |
5218508 | Doone | Jun 1993 | A |
5225265 | Prandy et al. | Jul 1993 | A |
5363266 | Wiseman et al. | Nov 1994 | A |
5497138 | Malpiece et al. | Mar 1996 | A |
5570264 | Lundquist et al. | Oct 1996 | A |
5602710 | Schmidt et al. | Feb 1997 | A |
5608597 | Holmström et al. | Mar 1997 | A |
5912611 | Berggren et al. | Jun 1999 | A |
5926356 | Sakich et al. | Jul 1999 | A |
5936826 | Schmidt | Aug 1999 | A |
6008975 | Kester et al. | Dec 1999 | A |
6008977 | Thatcher | Dec 1999 | A |
6185813 | Donnola | Feb 2001 | B1 |
6396676 | Doone et al. | May 2002 | B1 |
6483685 | Ramarge et al. | Nov 2002 | B1 |
Number | Date | Country |
---|---|---|
03034522 | Feb 1991 | JP |
11340635 | Dec 1995 | JP |
Number | Date | Country | |
---|---|---|---|
20030043526 A1 | Mar 2003 | US |