WO1997032319A1 - Module limiteur de surtension a autocompression, et procede de fabrication associe - Google Patents

Module limiteur de surtension a autocompression, et procede de fabrication associe Download PDF

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Publication number
WO1997032319A1
WO1997032319A1 PCT/US1997/002966 US9702966W WO9732319A1 WO 1997032319 A1 WO1997032319 A1 WO 1997032319A1 US 9702966 W US9702966 W US 9702966W WO 9732319 A1 WO9732319 A1 WO 9732319A1
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WO
WIPO (PCT)
Prior art keywords
array
subassembly
matrix
tape
matrix layer
Prior art date
Application number
PCT/US1997/002966
Other languages
English (en)
Inventor
Jeffrey Joseph Kester
Todd R. Hoover
David P. Bailey
Original Assignee
Cooper Industries, Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Cooper Industries, Inc. filed Critical Cooper Industries, Inc.
Priority to AU19759/97A priority Critical patent/AU1975997A/en
Publication of WO1997032319A1 publication Critical patent/WO1997032319A1/fr

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Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01C—RESISTORS
    • H01C7/00—Non-adjustable resistors formed as one or more layers or coatings; Non-adjustable resistors made from powdered conducting material or powdered semi-conducting material with or without insulating material
    • H01C7/10—Non-adjustable resistors formed as one or more layers or coatings; Non-adjustable resistors made from powdered conducting material or powdered semi-conducting material with or without insulating material voltage responsive, i.e. varistors
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01C—RESISTORS
    • H01C7/00—Non-adjustable resistors formed as one or more layers or coatings; Non-adjustable resistors made from powdered conducting material or powdered semi-conducting material with or without insulating material
    • H01C7/10—Non-adjustable resistors formed as one or more layers or coatings; Non-adjustable resistors made from powdered conducting material or powdered semi-conducting material with or without insulating material voltage responsive, i.e. varistors
    • H01C7/12—Overvoltage protection resistors

Definitions

  • the present invention relates generally to electrical power distribution equipment. More particularly, the invention relates to sub-assemblies or modules that contain discrete electrical components and that are employed in protective devices such as surge arresters. Still more particularly, the invention relates to apparatus and methods for applying an axially-compressive force to an array of electrical components and retaining those components under compression in end-to-end relationship within the module.
  • a surge arrester is a protective device that is commonly connected in parallel with a comparatively expensive piece of electrical equipment so as to shunt or divert the over-voltage- induced current surges safely around the equipment, thereby protecting the equipment and its internal circuitry from damage.
  • a surge arrester When caused to operate, a surge arrester forms a current path to ground having a very low impedance relative to the impedance of the equipment that it is protecting. In this way, current surges which would otherwise be conducted through the equipment are instead diverted through the arrester to ground.
  • the arrester operates to open the recently-formed current path to ground, thereby again isolating the distribution or transmission circuit in order to prevent the non-transient current of the system frequency from "following" the surge current to ground, such system frequency current being known as “power follow current. "
  • Conventional surge arresters typically include an elongate 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 ground, and an array of other electrical components forming a series path between the terminals.
  • These components typically include a stack of voltage-dependent, nonlinear resistive elements.
  • These nonlinear resistors or "varistors” are characterized by having a relatively high resistance at the normal steady-state voltage and a much lower resistance when the arrester is subjected to transient over-voltages.
  • it may also include one or more spark gap assemblies housed within the insulative enclosure and electrically connected in series with the varistors.
  • Some present-day arresters also include electrically-conducting spacer elements coaxially aligned with the varistors and gap assemblies. Electrodes of a variety of types and configurations may also be included in the component array in conventional arresters.
  • an axial load is placed on the elements in the array.
  • Such loading is typically applied by employing springs within the housing to urge the stacked elements into engagement with one another.
  • Good axial contact is important to ensure a relatively low contact resistance between the adjacent faces of the components, to ensure a relatively uniform current distribution through the elements, and to provide good heat transfer between the arrester elements in the array and the end terminals.
  • Another conventional means for supplying the required axial force is to wrap the stack of arrester elements with glass fibers so as to axially-compress the elements within the stack.
  • Examples of such prior art surge arresters include U.S. Patent Nos. 5,043,838, 5,138,517, 4,656,555 and 5,003,689. These patents generally describe rather elaborate techniques for winding the fibers about the ends of a stack of arrester components to apply the appropriate axial force to the components within the stack. Employing certain of these techniques requires the inclusion of specially-configured components within the stack, such as special end terminations for maintaining specific separations between the fibers (for example, U.S. Patent No. 5,043,838) or for creating a shoulder against which the fibers can be wound (for example, U.S. Patent No.
  • 5,043,838 discloses a filament wrapped arrester module that includes openings between the criss-cross pattern of windings. These openings are filled with an epoxy or similar insulating material that is permitted to rupture to allow the expulsion of gasses.
  • state of the art arresters may still occasionally fail with the expulsion of components or fragments of components. This may, in part, be due to the fact that once the internal components in these arresters fail, the resulting arc vaporizes the components and generates gas at a rate that cannot be vented quickly enough to prevent rupture of the arrester enclosure. Accordingly, there remains a need in the art for an arrester which, upon failure, will fail in a non-fragmenting and safe manner. A need also exists for an arrester whose components are axially compressed without the use of a spring.
  • the means would be easily applied to the external surfaces of the stacked components. It would be further advantageous if the compression means were to include features enhancing the tensile and cantilever strengths of the arrester assembly. Further, the device should provide a venting means for relieving gas pressure and preventing the electrical assembly from failing in a dangerous fashion, and should provide good bonding at each interfaces from the MOV stack outward without requiring complicated assembly procedures or costly waste.
  • the present invention comprises a surge arrester subassembly that includes a plurality of electrical components stacked in an axial array and an insulative coating disposed over the outer surface of the axial array.
  • the coating is preferably bonded to the outer surface of the array and applies both axially- and radially directed forces to said array to maintain the components of the array in good electrical contact.
  • the coating has a coefficient of thermal expansion that is greater than the coefficient of thermal expansion of the electrical components and is cured at a temperature in the range of the operating temperature of the components, so that when the coated array is cooled below the cure temperature, the coating will tend to shrink more than the electrical components, thereby exerting compressive forces on the array.
  • the present invention also may include both longitudinal and circumferential fibrous reinforcement within the coating, which reinforcement preferably comprises glass fibers. Those skilled in the art will understand that the present coating can be applied over the desired portions of the array so as to result in a predetermined coating thickness.
  • Figure 1 is a cross-sectional view of an electrical subassembly module made in accordance with the present invention
  • Figure 2 is a top view of a grooved electrode of the subassembly module shown in Figure
  • Figure 3 is an enlarged view of a portion of the subassembly module shown in Figure 1 ;
  • Figure 4 is an elevational view of the module shown in Figure 1 shown with layers of the insulative coating partially cut away;
  • Figure 5 is a top view of the subassembly module shown in Figure 1;
  • Figure 6 is an elevational view of the module of Figure 1 shown at an intermediate stage of assembly;
  • Figure 7 is an end view of the module of Figure 1 shown at another intermediate stage of assembly
  • Figure 8 is an elevation view of a surge arrester employing the subassembly module of Figure 1 ;
  • Figure 9 is an elevational view of an alternative embodiment of the present invention, with portions of the insulative coating partially cut-away; and Figure 10 is a top view of another alternative embodiment of the present invention.
  • Module 10 has particular utility when employed in a distribution class sir e arrester such as arrester 60 ( Figure 8). Accordingly, to best describe the features and adv ges of the present invention, module 10 will be described with reference to a 10KA heavy duty , _vV (8.4 KV MCOV) distribution class surge arrester 60.
  • the invention is not limited to use in a distribution class surge arrester, or in any size or rating of surge arrester, the invention instead having utility and advantages in any apparatus where it is necessary or desirable to retain an array or stack of electrical components under axial load.
  • module 10 generally comprises an array 20 of electrical components stacked in end-to-end arrangement and retained in that arrangement by an axially- applied force supplied by an insulative coating 16.
  • the present invention relates to the coating 16, and is not limited to any particular type, number or size of electrical components within array 20; for purposes of explanation, however, array 20 is depicted in Figure 1 as including three metal oxide varistors 12 ("MOV's"), a pair of terminal blocks 14 and a pair of contact plates 18.
  • MOV's metal oxide varistors 12
  • Each MOV 12 is made of metal oxide that preferably is formed into a short cylindrical disk having an upper face 30, a lower face 32 and an outer cylindrical surface 31.
  • MOV 12 may be of the same material used for any high energy, high voltage MOV disk, and is preferably made of a formulation of zinc oxide. See, for example, U.S. Patent 3,778,743 of the Matsushita Electric Industrial Co., Inc., Osaka, Japan, incorporated herein by reference.
  • MOV 12 will have a uniform microstructure throughout the MOV disk and the exponent n for the zinc oxide formulation of MOV 12 will be in the range of about 10-25 at the steady state system voltage. An exponent n of approximately 20 is most preferred.
  • the circular cross-section of MOV 12 have a diameter between approximately 1 to 3 inches to insure that there is sufficient surface area of between about 0.785 and 7.07 square inches to maintain the desired durability and recoverability of die MOV's.
  • MOV 12 have as small a cross-sectional area as possible in order to reduce the size, weight and cost of the arrester. As size is reduced, however, the durability and recoverability of the disk is lessened. Given these competing considerations, a diameter of approximately 1.6 inches is the most preferred.
  • the thickness of MOV 12 as measured between faces 30 and 32 is preferably about 0.75 inches. As understood by those skilled in the art, given a particular metal oxide formulation and a uniform or consistent microstructure throughout the MOV disk, the thickness of the MOV disk determines the operating voltage level.
  • MOV's 12 are coated with sprayed-on metallized coatings of molten aluminum having a thickness approximately equal to 0.002 to 0.010 inches.
  • MOV's 12 in the present invention are preferably formed without insulative collars on outer surface 31 as are typically employed in conventional arresters.
  • Contact plates 18 are disposed between the upper and lower faces 30, 32 of adjacent MOV's 12. As best shown in Figures 2 and 3, contact plates 18 generally comprise a metallic disk having outer edge 34. It is preferred that contact plates 18 include upper and lower ridged surfaces 38, 40 which generally take the form of concentric grooves such that an outermost ridge 42 is formed on each of the upper and lower surfaces 38, 40. Electrode 18 is preferably produced from annealed aluminum, but may also be made from brass or other conducting metals. Contact plates 18 have an outside diameter approximately equal to that of MOV's 12.
  • terminal 14 is disposed at each end of array 20 and is a relatively short, cylindrical block machined or cast from any conducting material, preferably aluminum. Terminals 14 have a diameter substantially equal to that of the collarless MOV's 12 and contact plates 18, and include a threaded bore 44 for receiving a threaded conducting stud 46.
  • the outer cylindrical surface 48 of the blocks may be knurled or ribbed or otherwise textured to facilitate the physical connection between the blocks and coating 16 as described more fully below.
  • Coating 16 retains MOV's 12, terminals 14 and contact plates 18 of array 20 in stacked, end-to-end relationship, and provides an axially compressive force as desired for insuring low contact resistance between the various electrical components and a uniform current distribution through the components.
  • coating 16 is bonded to the internal components and further seals the electrical components in array 20 preventing the undesired entry of moisture or other contaminants, and provides increased tensile and mechanical strength to the stacked array 20, and provides controlled venting of gases during an arrester failure.
  • coating 16 generally includes a matrix 21 of resinous layers and a plurality of axially aligned fibrous tape segments 24 and a spiral wrapped fibrous tape segment 28, segments 24 and 28 being embedded within matrix 21.
  • matrix 21 preferably includes a base resinous layer 22 and three outer resinous layers 25-27 ( Figure 4).
  • Resinous layers 22 and 25-27 are thermosetting resins selected from among the following: polyester resins, phenolic resins and epoxy resins.
  • the preferred resin further includes a flameout ingredient -tarticle fillers to control consistency, aid in modifying thermal expansion coefficient, and increi "ile strength, as known to those skilled in the art.
  • Resin layers 22, 25-27 may comprise a single re > ⁇ ulation, or they may comprise two to four different resins.
  • the resins used for layers 22, 2 are selected so as to have similar cure temperatures and so as to be mutually compatible with ti. uher resin layers making up matrix 21. Further, the resin of matrix 21 must be stable at high temperatures and high voltages, meaning that the cured resins in matrix 21 must not depolymerize or lose bonding strength at the temperatures and voltages to which the components in array 20 will be subjected during operation. Normal operating temperatures are typically between -60 and -t-60°C. Failure mode temperatures can be as high as 350° C. The material selected for layers 22, 25-27 undergoes no thermal degradation at or below the failure temperature of the electrical equipment.
  • insulative coating 16 when cured, have a coefficient of thermal expansion that is greater than the coefficient of thermal expansion of the electrical components in array 20. This will ensure that, at any temperature below its cure temperature, coating 16 will exert axially and radially compressive forces on array 20.
  • the components in array 20 typically have an average coefficient of thermal expansion in the range of
  • the material(s) of which coating 16 is formed have an coefficient of thermal expansion of at least 50 x 10 6 to 250 x 10 6 in/in/°C.
  • Each of layers 22, 25-27 may be applied by conventional spraying, dripping, rolling, powder falling, or fluidized bed methods, whichever is appropriate or convenient, depending upon the particular consistency of the resinous material and the equipment available.
  • layers 22, 25-27 of coating 16 are applied using a conventional fluidized bed process.
  • base layer 22 is applied to the outer cylindrical surfaces 31 of MOV's 12, outer surfaces 48 of terminals 14, and outer edge 34 of contact plates 18 and is applied so as to have a substantially uniform thickness of approximately 0.001 to 0.015 inches.
  • base layer 22 is chosen to have a high bonding strength to MOV's 12. Because of its ability to strongly adhere to the components of array 20, base layer 22 forms a secure base for the other constituents of coating 16, specifically tapes 24, 28 and outer layers 25-27. It is also preferred that, relative to layers 25-27, the resin of base layer 22 be relatively quick to achieve a first level of hardness so that tape segments 24, described below, are not placed in direct contact with the elements of array 20.
  • axially aligned fibrous tape segments 24 are resin impregnated fiberglass tape comprised of multiple fiberglass strands or bundles of strands that are arranged side by side in parallel rows and retained in that parallel relationship by the B-stage thermosetting resin that is preimpregnated or embedded within and surrounding the bundles.
  • fiberglass tape 24 is B-stage resin impregnated tape that is approximately 0.10 inches thick by 0.750 inches wide and has a length substantially equal to the length of array 20.
  • insulative coating 16 preferably further includes spiral wrapped tape 28 that is disposed about array 20.
  • Tape 28 is preferably also a B-stage resin impregnated fiberglass tape substantially identical to tape 24 previously described, except that tape 28 may be narrower.
  • Tape 28 again includes fiberglass strands or bundles of strands arranged in parallel rows that are held in position by embedded thermosetting epoxy resin.
  • coating 16 preferably includes four turns of tape 28 disposed about the outer surface 48 of upper terminal 14 and lower terminal 14, and a plurality of spaced apart turns disposed about the central portion of array 20.
  • Tape 28 is wrapped about the central portion of array 20 at a pitch of approximately 2 wraps per linear inch.
  • coating 16 is formed with polygonal regions 29 that are comprised entirely of resin layers 22, 25-27 and are free from fibrous tapes 24 or 28.
  • One or more tape segments 28 can be used to wrap the array 20 in this manner.
  • Resinous layers 25-27 are layers of resin that are applied separately as described below. Layers 25-27 are preferably, but not necessarily, are formed of the same resin as layer 22.
  • Layers 25-27 must adhere securely to base layer 22 and are applied, in part, to ensure that the glass fibers and bundles in tapes 24, 28 are completely and adequately wetted prior to module 10 being cured. It may be desirable to use different resins for one or more of layers 25-27, such as, for example to enhance the ability to wet, resins of lower viscosity or slower cure rate may be desired. In any event, each resin should be mutually compatible with the other resins selected. Additionally, it is preferred that resins for layers 25-27 be relatively slower to cure as compared to base layer 22 so that tape segments 24, 28 may be pressed and embedded within the preceding resinous layer prior to the resin setting up or hardening to an extent that would prevent the tape from being pressed into the preceding layer. Upon final curing, the thickness of coating 16 is preferably approximately .005 to .050 inch.
  • the method for manufacturing module 10 of the present invention generally comprises the following steps. First, the components of array 20 are heated to a temperature of between about 150 to 275 °C, the final temperature of this preheating step being dependent upon the type and characteristics of the resin(s) employed in coating 16. More specifically, the final preheat temperature is selected in the lower temperature range of 150 to 200°C so as to reduce gel rates, while finial cure temperature is set in the range of 225 to 275°C. Once heated, the components are then arranged in a conventional V-block type fixture in the desired axial relationship. An axially directed clamping force of between approximately 0 to 1500 psi is applied to the end terminals 14 of array 20. For convenience of manufacture, the component array is held in a horizontal plane.
  • a force sufficient to maintain component to component contact is required.
  • the preferred clamping force is approximately 50 to 150 psi.
  • the clamping force should be sufficient to ensure that MOV's 12, contact plates 18 and terminals 14 are in complete contact over substantially their entire areas of abutment. Good contact between the adjacent components in array 20 is important for uniform current distribution, low resistance and optimal heat dissipation through the stacked array 20.
  • base layer 22 is uniformly applied to the outer surfaces of the components in array 20.
  • a thin coating(.003 to .010 inches) of first outer layer 25 is immediately applied before the fast gelling layer 22 has started to gel.
  • First outer layer 25 has a relatively slower rate of hardening than base layer 22 so as to permit fibrous tape segments 24 to be partially embedded within layer 25.
  • Layers 22 and 25 serve to prevent fibrous tape segments 24 from contacting the outer radial surfaces of MOV's 12, terminals 14 and contact plates 18. It is important to avoid such contact because even though the fibrous tape has been impregnated with resin, it is still likely that minor levels of porosity or voids exist.
  • module 10 has the configuration shown in Figure 6.
  • the partially assembled module 10 coated with second outer layer 26.
  • An important function of layer 26 is to ensure mat the fiberglass strands or bundles within tape segments 24 are well wetted (resin saturated) and to ensure that no voids are created within coating 16.
  • tape 28 is applied. Beginning at one end of array 20, tape 28 is wrapped approximately four times around the knurled outer surface 48 of upper terminal 14 and then wound about the central portion of array 20 in a spiral fashion. The wrapping step is preferably completed with four final turns of tape 28 about lower terminal 14. Tape 28 is wrapped about array 20 at a time when layer 26 is still relatively soft such that tape 28 is at least partially embedded in layer 26.
  • Figure 7 shows module 10 at this stage of assembly. After tape 28 has been applied, module 10 is coated with a final outer layer 27.
  • layers 25-27 may comprise different resins, it is presently preferred that layers 25-27 consist of the same resinous material.
  • coating 16 has been described as have three discretely-applied outer layers 25-27 of resinous material, in practice, any desired number and combination of outer layers may be applied. While three such layers are presently preferred in the preferred embodiment, the important function served by the outer layers 25-27 is to thoroughly wet the fibers in tapes 24, 28 and depending on numerous factors, such as the characteristics of the resinous materials and of tapes 24, 28, this may be accomplished with more or fewer number of layers.
  • array 20 After final outer layer 27 has been applied, array 20, still held in compression by a clamping mechanism (not shown), and coating 16 are subjected to curing temperature o that layers 22 and 25-27 will cross-link and harden.
  • Matrix 21, comprising resin layers 22 and 25-27 are cured at a temperature which is well above the normal steady state operating temperature of the module, which is typically about 60°C. It is preferred that the final curing take place at a temperature above the maximum temperature that will be experienced by module 10 during operation. In instances when module 10 is employed in a surge arrester, the matrix 21 should cure at a temperature above the temperature that the module is likely to experience during a transient overvoltage. Such temperatures may be, for example, 250°C or more. Accordingly, the resins chosen for use in matrix 21 are preferably those that cure at a temperature of 250"C or more.
  • module 10 shown in Figures 1 and 4 will typically remain in an oven for approximately 10 to 30 minutes at the predetermined cure temperature before being removed from the oven and allowed to cool to room temperature. Because the resin layers 22, 25-27 are not completely cured until the final curing process, layers 22, 25-27 become integral with each adjacent layer, rather than forming discrete, discernable strata.
  • the shrinkage due to cure is enough to result in adequate compressive force such that the assembly would not have to be cured at the elevated temperature. It is preferred, however, that insulative coating 16, after curing, have a coefficient of thermal expansion that is greater than the coefficient of thermal expansion of the electrical components in array 20. As a result, upon cooling of the module 10, insulative coating 16 shrinks more than array 20 and thus imposes axially- and radially-compressive forces on array 20 to ensure that the components in array 20 remain in stacked relationship and to ensure that good electrical connection is maintained between the components in array 20. If a coating having a higher coefficient of thermal expansion is used and shrinkage during cure is not considered, then the cure temperature would have to be higher than the temperature experienced by the components at designed operating temperature, so as to ensure compressive forces at operating temperatures.
  • an object of this invention is to coordinate shrinkage during reaction (cure) and thermal expansion properties so as to maintain axial compression on the coated parts as well as to maintain a good dielectric interface to the component periphery.
  • the art of coordinating thermal expansion mismatch is well understood by those skilled in the art.
  • the novel aspect of the present invention is to use these coating parameters to control contact pressure in the stacked array of coated electrical components.
  • the degree of expansion mismatch is limited by the hardness and tensile strength of the coating. Generally, some degree of flexibility is desirable in order to control compressive forces over a narrower range. If materials are too hard or brittle, the force exerted on the MOV components will rise dramatically with falling temperature, while if the coatings are somewhat soft or elastic, the coating will begin to yield as forces increase.
  • particles of rubber filler such as ethylene vinyl acetate (EVA) or ethylene propylene rubbers (EPR) are used to enhance the flexibility of the cured resin.
  • EVA ethylene vinyl acetate
  • EPR ethylene propylene rubbers
  • Hardened matrix 21, in conjunction with longitudinally aligned fiberglass tape segments 24 and spiral wrapped tape segment 28, provides sufficient cantilever strength to module 10 to permit the module to tolerate the external forces that may be applied to the array when in use, such as in surge arrester 60 where the arrester and module will be subjected to wind forces and other unintentional, but occasionally-occurring, forces such as those that might be applied to the arrester during shipment or installation by utility personnel.
  • insulative coating 16 further includes a venting means permitting the module 10 to vent gas that may evolve during arrester component failure.
  • polygonal regions 29 serve as weakened wall regions through which venting may occur during component failure.
  • the pressure within module 10 will build as the internal arc burns adjacent materials. As the arc burns, the pressure within module 10 will increase until it reaches a magnitude that will cause weakened wall regions 29 to burst, so as to relieve the internal pressure and vent the evolved gas.
  • Arrester 60 generally includes module 10, polymeric housing 62, and arrester hanger 64.
  • Module 10 is disposed within polymeric housing 62 with an RTV silicone compound (not shown) filling any voids between module 10 and the inner surface of housing 62.
  • a threaded conducting stud 46 is disposed in bore 44 of each terminal 14. Upper stud 46 extends through housing 62 for threadedly engaging a terminal assembly (not shown). Lower stud 46 extends through an aperture (not shown) in hanger 62 for connection to ground lead disconnector 65. Threaded stud 67 extends from disconnector 65 for engaging a ground lead terminal assembly (not shown).
  • Housing 12 is sealed about module 10 at its upper and lower ends.
  • module 100 includes an insulative coating 116 comprising a matrix 121.
  • Matrix 121 includes a base layer of resinous material 122, substantially the same as resinous layer 22 previously described with reference to Figures 1-7.
  • Matrix 21 further includes one or more outer layers 125 of resinous material which has included therein relatively short fiber strands 126 intermixed with the resin material.
  • Base layer 122 and outer layer or layers 125 are applied by means of a fluidized bed or other known technique and cured as previously described with reference to the curing of insulative coating 16.
  • insulative coating 116 applies an axially compressive force to the arrester components in array 120.
  • Coating 116 has a coefficient of thermal expansion that is greater than the coefficient of thermal expansion of the components in array 120. Additionally, the fiberglass strands 126 randomly disposed within layers 125 provide strength and rigidity to module 100.
  • module 210 is shown in top view to best disclose another embodiment of the invention.
  • module 210 includes an axial array of MOV's 12 and contact plates 18 and terminals 14, all as previously described, that are coated and held in axial compression by insulative coating 211.
  • Coating 211 includes resinous layers 22, 25- 27 all as previously described.
  • Coating 211 further includes a plurality of axially aligned preimpregnated tape segments 224, 226 that are identified to tape segments 24 previously described. In this embodiment, however, the lateral edges of the innermost tape segments 224 are overlapped so that the entire circumference of the array of electrical components is covered by a layer 225 of axially-aligned tape segments 224.
  • the module 210 further includes axially-aligned tape segments 226 that are disposed at predetermined locations about layer 225 to provide arcuate regions 227 having multiple thicknesses of tape 224, 226 and other arcuate regions 229 having single thickness of tape 224.
  • a resinous layer that may be identical to any one of the previously- described outer layers 25-27 is applied between the taped layer 225 and tape segments 226 and another layer applied over the module 210 after tape segments 226 have been applied to thoroughly wet all tape segments 224 and 226. Thereafter, spiral wrapped tape segments 228 is applied outside tape segments 224 and 226 and a final outer resinous layer is applied.
  • module 210 will include relatively weaker wall regions 230 corresponding to regions 229 that have relatively thin regions of glass fiber reinforcement as compared to regions 227.
  • relatively weaker wall regions 230 and regions 227 may have any number of thicknesses of tape segments 224, 226 provided that the relatively weaker wall regions 230 have fewer thicknesses of tape 224, 226 than regions 227.
  • the embodiment thus described has particular application in surge arresters having a relatively large number of components in array 220 or where the MOV's are larger than MOV's 12 previously described, as may be the case with surge arresters having higher voltage or duty ratings than arrester 60 shown in Figure 8.

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  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Thermistors And Varistors (AREA)
  • Insulating Bodies (AREA)
  • Insulators (AREA)

Abstract

Un module limiteur de surtension (10), comportant un ensemble de varistors à oxyde métallique (26) et d'autres composants, comprend un revêtement isolant (28) qui permet d'appliquer une force de compression axiale à l'ensemble empilé. La pile de composants, tout en étant maintenue dans un état de compression axiale, reçoit le boîtier isolant renfermant une résine thermodurcissable qui, une fois durcie, a un coefficient d'expansion thermique supérieur à celui des composants de la pile. La pile revêtue est ensuite durcie à une température supérieure à la température maximale à laquelle, selon les prévisions, seront soumis les composants du limiteur de surtension. Après refroidissement, les composants de l'ensemble sont maintenus comprimés et le boîtier maintient entre eux un contact électrique adéquat. Des brins de fibres de verre (24) sont incorporés au boîtier pour le renforcement et la résistance à la rupture en flexion. L'invention concerne également un procédé de fabrication dudit module.
PCT/US1997/002966 1996-03-01 1997-02-26 Module limiteur de surtension a autocompression, et procede de fabrication associe WO1997032319A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU19759/97A AU1975997A (en) 1996-03-01 1997-02-26 Self-compressive surge arrester module and method of making same

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US1266796P 1996-03-01 1996-03-01
US60/012,667 1996-03-01

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WO1997032319A1 true WO1997032319A1 (fr) 1997-09-04

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PCT/US1997/002966 WO1997032319A1 (fr) 1996-03-01 1997-02-26 Module limiteur de surtension a autocompression, et procede de fabrication associe
PCT/US1997/003518 WO1997032382A1 (fr) 1996-03-01 1997-03-03 Module auto-compresseur de protection contre les surtensions et procede de fabrication

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PCT/US1997/003518 WO1997032382A1 (fr) 1996-03-01 1997-03-03 Module auto-compresseur de protection contre les surtensions et procede de fabrication

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EP (1) EP0954893B1 (fr)
JP (1) JP4327250B2 (fr)
KR (1) KR19990087547A (fr)
AR (1) AR006054A1 (fr)
AT (1) ATE473534T1 (fr)
AU (2) AU1975997A (fr)
BR (1) BR9707900A (fr)
CO (1) CO4600617A1 (fr)
DE (1) DE69739926D1 (fr)
MX (1) MX9701634A (fr)
NO (1) NO983997L (fr)
NZ (1) NZ331649A (fr)
PL (1) PL183435B1 (fr)
TW (1) TW382153B (fr)
WO (2) WO1997032319A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002013203A2 (fr) * 2000-08-02 2002-02-14 Gerardo Pagaza Melero Composition dielectrique destinee a la fabrication de structures isolantes
EP1067565A3 (fr) * 1999-07-09 2002-05-08 Kabushiki Kaisha Toshiba Limiteur de surtension et son procédé de fabrication
RU188116U1 (ru) * 2018-12-04 2019-03-29 Владимир Николаевич Хорохорин Разрядник длинно-искровой стержневой

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KR100464277B1 (ko) * 2002-06-26 2005-01-03 한국전기연구원 피뢰기 모듈 제조방법
SE527132C2 (sv) * 2003-04-30 2005-12-27 Abb Technology Ltd Ventilavledare
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JP6350611B2 (ja) * 2016-08-10 2018-07-04 株式会社明電舎 避雷器
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US5128824A (en) * 1991-02-20 1992-07-07 Amerace Corporation Directionally vented underground distribution surge arrester
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EP1067565A3 (fr) * 1999-07-09 2002-05-08 Kabushiki Kaisha Toshiba Limiteur de surtension et son procédé de fabrication
WO2002013203A2 (fr) * 2000-08-02 2002-02-14 Gerardo Pagaza Melero Composition dielectrique destinee a la fabrication de structures isolantes
WO2002013203A3 (fr) * 2000-08-02 2002-06-13 Melero Gerardo Pagaza Composition dielectrique destinee a la fabrication de structures isolantes
RU188116U1 (ru) * 2018-12-04 2019-03-29 Владимир Николаевич Хорохорин Разрядник длинно-искровой стержневой

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NO983997L (no) 1998-10-30
WO1997032382A1 (fr) 1997-09-04
EP0954893A4 (fr) 1999-11-10
AU2197697A (en) 1997-09-16
JP2000512074A (ja) 2000-09-12
NO983997D0 (no) 1998-08-31
EP0954893B1 (fr) 2010-07-07
AU727154B2 (en) 2000-12-07
BR9707900A (pt) 1999-07-27
NZ331649A (en) 2000-02-28
AU1975997A (en) 1997-09-16
DE69739926D1 (de) 2010-08-19
CO4600617A1 (es) 1998-05-08
EP0954893A1 (fr) 1999-11-10
PL328631A1 (en) 1999-02-15
JP4327250B2 (ja) 2009-09-09
MX9701634A (es) 1998-04-30
TW382153B (en) 2000-02-11
AR006054A1 (es) 1999-07-21
KR19990087547A (ko) 1999-12-27
PL183435B1 (pl) 2002-06-28
ATE473534T1 (de) 2010-07-15

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