US3237137A - Encapsulated toroidal inductor and the like - Google Patents

Encapsulated toroidal inductor and the like Download PDF

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US3237137A
US3237137A US297071A US29707163A US3237137A US 3237137 A US3237137 A US 3237137A US 297071 A US297071 A US 297071A US 29707163 A US29707163 A US 29707163A US 3237137 A US3237137 A US 3237137A
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winding
core
boot
assembly
central opening
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Albert D Flaminio
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Sangamo Electric Co
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Sangamo Electric Co
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F41/00Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties
    • H01F41/005Impregnating or encapsulating
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F27/00Details of transformers or inductances, in general
    • H01F27/02Casings
    • H01F27/022Encapsulation
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49002Electrical device making
    • Y10T29/4902Electromagnet, transformer or inductor
    • Y10T29/49073Electromagnet, transformer or inductor by assembling coil and core
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49915Overedge assembling of seated part
    • Y10T29/4992Overedge assembling of seated part by flaring inserted cup or tube end
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49908Joining by deforming
    • Y10T29/49938Radially expanding part in cavity, aperture, or hollow body

Definitions

  • the present invention relates to encapsulated toroidal inductors and the like.
  • These toroidal inductors comprise a magnetic core, preferably composed of paramagnetic metallic powders pressed and sinte'red together in the general form of a ring or doughnut having a central opening therethrough. Wound on this toroidal magnetic core are one or more windings, the turns of which pass successively through the central opening in the core and thence wind spirally outwardly around the surrounding ring structure of the core.
  • This unique form of rubber boot is preferably a cylindrical rubber tube which is inserted into the central opening in the core structure and winding assembly, which insertion occurs after the winding or windings have been wound through such central opening. As originally inserted, this rubber tube has projecting upper and lower ends extending outwardly above and below the top and bottom surfaces of the core structure and winding assembly.
  • this rubber tube-let us say the lower endis then stretched outwardly to a substantial degree, sufficient to permit this stretched lower end to be doubled back up over the outer peripheral surface of the winding on the core structure.
  • the other or upper projecting end of the rubber tube is similarly stretched outwardly to a substantial degree, sufficient to permit this stretched upper end to be pushed or doubled back down over the stretched lower end of the rubber tube, whereby the stretched upper end envelops or laps down over the stretched lower end of the rubber tube.
  • the high elasticity of the rubber tube insures that the lapped joint between the upper and lower ends will effectively exclude the encapsulating material in the subsequent encapsulating operation, so that there is no permeation of the material into the small spaces between the winding and the core, or into the spaces between the turns of the winding.
  • the high elasticity of the rubber tube or boot results in another advantage when the units are encapsulated in a vacuum casting technique.
  • the overlapped ends of the ice rubber boot act as an escape valve for permitting entrapped air to escape during the vacuum casting operation, but tightly seal and prevent the epoxy or other encapsulating material from thereafter entering the space between the turns of wire, thereby resulting in a void-free envelope or cast encapsulation.
  • a still further advantage of the rubber boot is that by excluding the epoxy from the spaces between the turns of the winding, the winding itself absorbs the strain due to the shrinkage of the epoxy, which strain can be very large.
  • FIGURE 1 is a side elevational view of the completed assembly of core structure and winding, showing the rubber tube or boot extending down through the central opening thereof, preliminary to the stretching and folding operations;
  • FIGURE 2 is a plan view of FIGURE 1;
  • FIGURE 3 is a transverse sectional view through the core and winding assembly and through the rubber tube, this view showing the first step of stretching outwardly the projecting lower end of the tube and doubling this stretched end backwardly and upwardly so as to have it envelop the outer periphery of the coil;
  • FIGURE 4 is .a plan view of FIGURE 3;
  • FIGURE 5 is a transverse sectional view similar to FIGURE 3, but showing the next step of stretching outwardly the projecting upper end of the rubber tube and folding this stretched end downwardly over the coil, and over the enveloping lower end of the rubber tube;
  • FIGURE 6 is the plan view of FIGURE 5;
  • FIGURE 7 illustrates a preliminary step of connecting the winding leads to the external pin terminals, etc
  • FIGURE 8 is a transverse sectional view illustrating in section the encapsulating outer cover for the inductor unit, corresponding to a section taken on the plane of the line 8-8 of FIGURE 9;
  • FIGURE 9 is a plan view of FIGURE 8.
  • the toroidal core composed of pressed powder is indicated at 10, and the central opening extending therethrough is indicated at 12.
  • Wound spirally around the toroidal ring 10 and through such central opening 12 is the coil or winding portion 14 of the unit.
  • this winding portion consists of a single winding having two end terminals, and possibly having one or more intermediate taps.
  • this winding portion would consist of the primary and secondary windings of the transformer.
  • This rubber tube or boot 16 consists of a natural rubber or a synthetic rubber, preferably of a composition having a very high degree of elasticity so that the boot is capable of being stretched to dimensions several times its original dimensions. Also, this rubber can be very thin, since it serves merely as a skin-tight protecting or covering membrane over the core-winding assembly, the latter being designated 18 in its entirety.
  • the length of the rub-ber boot 16 is such that the projecting upper and lower ends 16a and 16b are sufliciently long to produce a substantial degree of overlap between these ends when they are stretched outwardly and caused to envelope the core-winding assembly 18, as illustrated in FIGURES 56.
  • the stretching and enveloping operation can be started at either end; FIGURES 34 showing it as starting with the lower end 16b.
  • This lower end is stretched or belled outwardly and then pulled upwardly to have it envelope the major portion of the core-winding assembly in a direction from the bottom-side upwardly.
  • this stretched end 16b is sufficiently long to enable its end edge or extremity to be stretched part way across the top of the core-winding assembly 18.
  • the extremely tight cohesive overlap of the upper and lower ends 16a and 16b establishes a hermetic seal for the boot against the entrance of encapsulating material, air or any foreign matter from the outside to the inside.
  • the conductor ends 14a, 14b, etc. leading from the winding or windings 14 are extended outside of the finished boot for connection to terminals 20 projecting from the encapsulating shell.
  • FIGURE 7 I have illustrated the intermediate step of connecting the conductor ends 14a, 14b to the external terminal pins 20, and preparing the unit for encapsulation.
  • the unit is assembled over a tubular insert or stem 26, preferably composed of brass and provided with internal threads for receiving a machine screw.
  • a Washer is assembled over the insert 26 at one end of the boot covered core-winding assembly.
  • the coil ends or leads 14a, 14b are brought over the outside diameter of the washer 30 and are then soldered to the terminal pins 20.
  • the terminal pins 20 have anchored mounting in a disk-like base 32 of plastic, which is attached to the end of the stem 26 in spaced relation from the washer 34 This attachment is preferably effected through a nut 34 which is moulded in a raised control boss 36 and which has threaded engagement or like attachment over a reduced end of the stem 26.
  • Inwardly projecting spacer humps 37 formed integral with the mounting disk 32 space the washer 3t) and core-winding assembly 18 from the base mounting disk 32.
  • the outer face of the base mounting disk 32 has outwardly projecting spacer bumps 38, 38. If desired, one lap of tape 40 may be wrapped around the core-winding assembly 18, but this is purely optional.
  • the resulting unit assembly is then inserted into a thin cylindrical shell or sleeve 42 composed of Bakelite or other suitable plastic, and the disk-like mounting base 32 is then cemented to the end of the shell 42. Thereupon the assembly is subjected to the encapsulating operation, with the epoxy or other encapsulating material 44 filling the shell 42 and completely covering all surfaces of the corewinding assembly 18 in contact with the rubber boot 16. Following this, the open end of the shell 42, the epoxy material 44 therein, and the projecting end of the tubular stem 26 are then faced off to establish the desired length, and also to form a finished top surface on which can be imprinted the technical data regarding the inductance, etc. of the unit.
  • the rubber boot 16 affords several advantages, some of which have been briefly mentioned before.
  • the rubber boot results in a sealing covering over the core-winding assembly 18 which avoids pin holing, non-uniformity of thickness, and which can still be of a very thin, membrane-like thickness.
  • a further advantage arises in a vacuum casting type of encapsulation.
  • the overlapping ends 16a, 16b of the boot act very much as a valve and permit the entrapped air to escape during the evacuation, but seal and prevent the epoxy or other encapsulating material from entering the space between the turns of wire. This produces a voidfree envelope or cast encapsulation.
  • the rubber boot covering 16 also lends itself well to the transfer molding process of encapsulation.
  • a toroidal inductance unit the combination of a toroidal core structure of a magnetic material having a central opening therethrough, a winding wound spirally around said toroidal core structure and passing through said central opening, said core and winding constituting a core-Winding assembly, a generally cylindrical enveloping boot of thin, highly elastic material comprising an intermediate portion disposed in said central opening, said boot comprising upper and lower end portions extending from said intermediate portion, said upper end portion enveloping the upper end of said core-Winding assembly and extending down over at least a substantial portion of the outer surface thereof including a portion of said spiral winding, said lower end portion enveloping the lower end of said core-winding assembly and extending up over at least a substantial portion of the outer surface thereof and over at least a substantial portion of the lower part of said spiral winding, one of said end portions overlapping the other end portion, and a protective outer shell of insulating material enclosing the core-winding assembly and enveloping boot.
  • the method of constructing an encapsulated toroidal inductance unit comprising forming a toroidal corewinding assembly by first forming a toroidal core having a central opening Ttherethrough, then coiling a winding encircling said toroidal core and passing it through said central opening, passing a thin, highly elastic, cylindrical rubber boot through the central opening of said toroidal core-winding assembly, said rubber boot having upper and lower ends projecting beyond the top and bottom surfaces of said core-winding assembly, stretching one of said projecting ends outwardly and then doubling it back over the outer peripheral surface of said assembly and of said winding from one direction, stretching the other projecting end outwardly and then doubling it back over the outer peripheral surface of said assembly from the other direction, one of said stretched ends being lapped over the other stretched end whereby said boot completely envelops the core-winding assembly, and then encapsulating the resulting unit in an epoxy compound.
  • a toroidal magnetic core structure a winding wound around said core structure to constitute therewith a core-winding assembly
  • an enveloping boot of highly elastic material having one end passing through the center of said core structure, enveloping a substantial part of the lower peripheral surface of said corewinding assembly including the lower peripheral surfaces of said winding, and having its other end enveloping a substantial part of the upper peripheral surface of said core-winding assembly including the upper peripheral surfaces of said winding, one of said ends overlapping the other end, and a mass of encapsulating material enclosing said core-winding assembly and said enveloping boot, said enveloping boot preventing the mass of encapsulating material from penetrating into the spaces between the turns of said winding and from penetrating into the spaces between said winding and said core structure.
  • a toroidal inductance unit the combination of a toroidal magnetic core structure, a winding wound spirally around said toroidal core structure and passing through the central opening in said core structure, said core and Winding constituting a core-winding assembly, a highly elastic enveloping boot of generally cylindrical form pass ing through said central opening, one of the ends of said boot extending over the outer peripheral surface of said core-winding assembly from one direction, the other end,
  • a toroidal inductance unit the combination of a pressed powder toroidal core structure having a central opening there-through, a winding encircling said toroidal core structure and passing through said central opening, said core and winding together constituting a core-winding assembly, a resilient rubber boot of generally cylindrical form passing through said central opening, one of the ends of said rubber boot extending back to envelop the outer surface of said core structure and also at least a portion of the outer surface of said winding from one direction, the other end of said rubber boot extending back to envelop the outer surface of said core structure and also at least a portion of the outer surface of said Winding from the other direction, one of said boot ends overlapping the other end whereby said boot completely envelops the corewinding assembly, a tubular mounting stern passing through said central opening of the core-Winding assembly and through the intermediate portion of said boot, a mounting disk secured to one end portion of said stem, terminals projecting outwardly from said mounting disk and electrically connected to said winding,
  • an encapsulated electrical inductance unit of the class described the combination of a magnetic core structure, a winding wound around said core structure to form a core-winding assembly, a protective sheath in the form of a thin, one-piece tube of highly elastic material extending through the center of said core structure and stretched so as to elastically envelop the core-winding assembly with one of the ends of said tube overlapping the other end of the tube, whereby said protective sheath completely envelopes the inside, outside and top and bottom surfaces of said winding, and an encapsulating material encasing said core-winding assembly and said protective sheath, I
  • said protective sheath preventing the encapsulating material from penetrating into the spaces between the turns of said winding and from penetrating into the spaces between Winding and said core structure in the performance of the encapsulating operation.

Description

. Feb. 22, 1966 A. D FLAMINIO ENCAPSULATED TOROIDAL INDUCTOR AND THE LIKE i I I 1 l INVENTOR.
6766a Z717 BY K Filed Jul 23 W United States Patent O 3,237,137 ENCAPSULATED TOROIDAL INDUCTOR AND THE LIKE Albert D. Flaminio, Springfield, Ill., assignor to Sangarno Electric Company, Springfield, Ill., a corporation of Delaware Filed July 23, 1963, Ser. No. 297,071 6 Claims. Cl. 336209) The present invention relates to encapsulated toroidal inductors and the like.
These toroidal inductors comprise a magnetic core, preferably composed of paramagnetic metallic powders pressed and sinte'red together in the general form of a ring or doughnut having a central opening therethrough. Wound on this toroidal magnetic core are one or more windings, the turns of which pass successively through the central opening in the core and thence wind spirally outwardly around the surrounding ring structure of the core.
After the completion of the winding operation, the general practice heretofore has been to encapsulate each inductor unit directly into the encapsulating or insulating material. In many instances this results in such material coming into immediate contact with the individual turns of the winding, and also coming into direct contact with exposed portions of the pressed powder core structure. Otherwise stated, there is frequently a complete penetration by the encapsulating or potting material into the minute spaces between the turns of the windings, and also into the minute spaces between the turns of the winding and the surface of the pressed -powder core structure. This generally results in objectionable increases in distributed capacitance, in objectionable variations in change of temperature coeflicients, and in objectionable mechanical strain on the core which causes a further undesirable shift in inductance, and an undesirable increase in core losses.
I have avoided these objections by employing a unique form of rubber boot which is operative to envelop the entire assembly of the toroidal core ring and the windings wound thereon, before such assembly is contacted by the encapsulating material in the encapsulating operation. This unique form of rubber boot is preferably a cylindrical rubber tube which is inserted into the central opening in the core structure and winding assembly, which insertion occurs after the winding or windings have been wound through such central opening. As originally inserted, this rubber tube has projecting upper and lower ends extending outwardly above and below the top and bottom surfaces of the core structure and winding assembly. One of the projecting ends of this rubber tube-let us say the lower endis then stretched outwardly to a substantial degree, sufficient to permit this stretched lower end to be doubled back up over the outer peripheral surface of the winding on the core structure. Following this, the other or upper projecting end of the rubber tube is similarly stretched outwardly to a substantial degree, sufficient to permit this stretched upper end to be pushed or doubled back down over the stretched lower end of the rubber tube, whereby the stretched upper end envelops or laps down over the stretched lower end of the rubber tube. The high elasticity of the rubber tube insures that the lapped joint between the upper and lower ends will effectively exclude the encapsulating material in the subsequent encapsulating operation, so that there is no permeation of the material into the small spaces between the winding and the core, or into the spaces between the turns of the winding. The high elasticity of the rubber tube or boot results in another advantage when the units are encapsulated in a vacuum casting technique. In the performance of such method, the overlapped ends of the ice rubber boot act as an escape valve for permitting entrapped air to escape during the vacuum casting operation, but tightly seal and prevent the epoxy or other encapsulating material from thereafter entering the space between the turns of wire, thereby resulting in a void-free envelope or cast encapsulation. A still further advantage of the rubber boot is that by excluding the epoxy from the spaces between the turns of the winding, the winding itself absorbs the strain due to the shrinkage of the epoxy, which strain can be very large.
Other objects, features and advantages of the invention will be apparent from the following detailed description of one preferred embodiment thereof. In the accompanying drawings illustrating such embodiment:
FIGURE 1 is a side elevational view of the completed assembly of core structure and winding, showing the rubber tube or boot extending down through the central opening thereof, preliminary to the stretching and folding operations;
FIGURE 2 is a plan view of FIGURE 1;
FIGURE 3 is a transverse sectional view through the core and winding assembly and through the rubber tube, this view showing the first step of stretching outwardly the projecting lower end of the tube and doubling this stretched end backwardly and upwardly so as to have it envelop the outer periphery of the coil;
FIGURE 4 is .a plan view of FIGURE 3;
FIGURE 5 is a transverse sectional view similar to FIGURE 3, but showing the next step of stretching outwardly the projecting upper end of the rubber tube and folding this stretched end downwardly over the coil, and over the enveloping lower end of the rubber tube;
FIGURE 6 is the plan view of FIGURE 5;
FIGURE 7 illustrates a preliminary step of connecting the winding leads to the external pin terminals, etc;
FIGURE 8 is a transverse sectional view illustrating in section the encapsulating outer cover for the inductor unit, corresponding to a section taken on the plane of the line 8-8 of FIGURE 9; and
FIGURE 9 is a plan view of FIGURE 8.
Referring first to FIGURES 3 and 5, the toroidal core composed of pressed powder is indicated at 10, and the central opening extending therethrough is indicated at 12. Wound spirally around the toroidal ring 10 and through such central opening 12 is the coil or winding portion 14 of the unit. In the case of a simple inductor unit, this winding portion consists of a single winding having two end terminals, and possibly having one or more intermediate taps. In the case of a transformer type of unit, this winding portion would consist of the primary and secondary windings of the transformer.
After the winding portion 14 has been completely wound on the core It the rubber tube or boot 16 is passed down into or through the central opening 12, in approximately the relationship shown in FIGURES l and 2 of the drawings. This rubber tube or boot 16 consists of a natural rubber or a synthetic rubber, preferably of a composition having a very high degree of elasticity so that the boot is capable of being stretched to dimensions several times its original dimensions. Also, this rubber can be very thin, since it serves merely as a skin-tight protecting or covering membrane over the core-winding assembly, the latter being designated 18 in its entirety.
The length of the rub-ber boot 16 is such that the projecting upper and lower ends 16a and 16b are sufliciently long to produce a substantial degree of overlap between these ends when they are stretched outwardly and caused to envelope the core-winding assembly 18, as illustrated in FIGURES 56. The stretching and enveloping operation can be started at either end; FIGURES 34 showing it as starting with the lower end 16b. This lower end is stretched or belled outwardly and then pulled upwardly to have it envelope the major portion of the core-winding assembly in a direction from the bottom-side upwardly. In the exemplary proportions illustrated in FIGURE 3, this stretched end 16b is sufficiently long to enable its end edge or extremity to be stretched part way across the top of the core-winding assembly 18.
This operation is then repeated with respect to the upper end or leg 16a, which is stretched or, belied outwardly and is then pulled downwardly to have it" lope the major portion of the core-winding assembly, in a direction from the top side downwardly. As described above of the lower end, the end edge or extremity of this upper end 16; extends part way across the bottom surface of the corewinding assembly 18.
, The extremely tight cohesive overlap of the upper and lower ends 16a and 16b establishes a hermetic seal for the boot against the entrance of encapsulating material, air or any foreign matter from the outside to the inside. The conductor ends 14a, 14b, etc. leading from the winding or windings 14 are extended outside of the finished boot for connection to terminals 20 projecting from the encapsulating shell.
In FIGURE 7 I have illustrated the intermediate step of connecting the conductor ends 14a, 14b to the external terminal pins 20, and preparing the unit for encapsulation. The unit is assembled over a tubular insert or stem 26, preferably composed of brass and provided with internal threads for receiving a machine screw. A Washer is assembled over the insert 26 at one end of the boot covered core-winding assembly. The coil ends or leads 14a, 14b are brought over the outside diameter of the washer 30 and are then soldered to the terminal pins 20.
The terminal pins 20 have anchored mounting in a disk-like base 32 of plastic, which is attached to the end of the stem 26 in spaced relation from the washer 34 This attachment is preferably effected through a nut 34 which is moulded in a raised control boss 36 and which has threaded engagement or like attachment over a reduced end of the stem 26. Inwardly projecting spacer humps 37 formed integral with the mounting disk 32 space the washer 3t) and core-winding assembly 18 from the base mounting disk 32. Also, the outer face of the base mounting disk 32 has outwardly projecting spacer bumps 38, 38. If desired, one lap of tape 40 may be wrapped around the core-winding assembly 18, but this is purely optional.
The resulting unit assembly is then inserted into a thin cylindrical shell or sleeve 42 composed of Bakelite or other suitable plastic, and the disk-like mounting base 32 is then cemented to the end of the shell 42. Thereupon the assembly is subjected to the encapsulating operation, with the epoxy or other encapsulating material 44 filling the shell 42 and completely covering all surfaces of the corewinding assembly 18 in contact with the rubber boot 16. Following this, the open end of the shell 42, the epoxy material 44 therein, and the projecting end of the tubular stem 26 are then faced off to establish the desired length, and also to form a finished top surface on which can be imprinted the technical data regarding the inductance, etc. of the unit.
The use of the above described rubber boot 16 affords several advantages, some of which have been briefly mentioned before. For example, the rubber boot results in a sealing covering over the core-winding assembly 18 which avoids pin holing, non-uniformity of thickness, and which can still be of a very thin, membrane-like thickness. A further advantage arises in a vacuum casting type of encapsulation. The overlapping ends 16a, 16b of the boot act very much as a valve and permit the entrapped air to escape during the evacuation, but seal and prevent the epoxy or other encapsulating material from entering the space between the turns of wire. This produces a voidfree envelope or cast encapsulation. The rubber boot covering 16 also lends itself well to the transfer molding process of encapsulation.
While I have illustrated and described what I regard to be the preferred embodiment of my invention, nevertheless it will be understood that such is merely exemplary and that numerous modifications and rearrangements may be made therein Without departing from the essence of the invention.
I claim:
1. In a toroidal inductance unit, the combination of a toroidal core structure of a magnetic material having a central opening therethrough, a winding wound spirally around said toroidal core structure and passing through said central opening, said core and winding constituting a core-Winding assembly, a generally cylindrical enveloping boot of thin, highly elastic material comprising an intermediate portion disposed in said central opening, said boot comprising upper and lower end portions extending from said intermediate portion, said upper end portion enveloping the upper end of said core-Winding assembly and extending down over at least a substantial portion of the outer surface thereof including a portion of said spiral winding, said lower end portion enveloping the lower end of said core-winding assembly and extending up over at least a substantial portion of the outer surface thereof and over at least a substantial portion of the lower part of said spiral winding, one of said end portions overlapping the other end portion, and a protective outer shell of insulating material enclosing the core-winding assembly and enveloping boot.
2. The method of constructing an encapsulated toroidal inductance unit, comprising forming a toroidal corewinding assembly by first forming a toroidal core having a central opening Ttherethrough, then coiling a winding encircling said toroidal core and passing it through said central opening, passing a thin, highly elastic, cylindrical rubber boot through the central opening of said toroidal core-winding assembly, said rubber boot having upper and lower ends projecting beyond the top and bottom surfaces of said core-winding assembly, stretching one of said projecting ends outwardly and then doubling it back over the outer peripheral surface of said assembly and of said winding from one direction, stretching the other projecting end outwardly and then doubling it back over the outer peripheral surface of said assembly from the other direction, one of said stretched ends being lapped over the other stretched end whereby said boot completely envelops the core-winding assembly, and then encapsulating the resulting unit in an epoxy compound.
3. In an inductance unit of the class described, the combination of a toroidal magnetic core structure, a winding wound around said core structure to constitute therewith a core-winding assembly, an enveloping boot of highly elastic material having one end passing through the center of said core structure, enveloping a substantial part of the lower peripheral surface of said corewinding assembly including the lower peripheral surfaces of said winding, and having its other end enveloping a substantial part of the upper peripheral surface of said core-winding assembly including the upper peripheral surfaces of said winding, one of said ends overlapping the other end, and a mass of encapsulating material enclosing said core-winding assembly and said enveloping boot, said enveloping boot preventing the mass of encapsulating material from penetrating into the spaces between the turns of said winding and from penetrating into the spaces between said winding and said core structure.
4. In a toroidal inductance unit, the combination of a toroidal magnetic core structure, a winding wound spirally around said toroidal core structure and passing through the central opening in said core structure, said core and Winding constituting a core-winding assembly, a highly elastic enveloping boot of generally cylindrical form pass ing through said central opening, one of the ends of said boot extending over the outer peripheral surface of said core-winding assembly from one direction, the other end,
of said boot extending over the outer peripheral surface of said core-winding assembly from the other direction, one of said stretched ends being lapped over the other stretched end whereby the boot completely envelops the core-Winding assembly and completely covers the outer surface of said winding, and an outer insulating compound made to completely enclose said core-Winding assembly and said boot in an encapsulating operation, the overlapping ends of said rubber boot functioning as a one-way exhaust valve permitting air entrapped between the core structure and the winding and between the turns of said winding to escape outwardly during the encapsulating operation.
5. In a toroidal inductance unit, the combination of a pressed powder toroidal core structure having a central opening there-through, a winding encircling said toroidal core structure and passing through said central opening, said core and winding together constituting a core-winding assembly, a resilient rubber boot of generally cylindrical form passing through said central opening, one of the ends of said rubber boot extending back to envelop the outer surface of said core structure and also at least a portion of the outer surface of said winding from one direction, the other end of said rubber boot extending back to envelop the outer surface of said core structure and also at least a portion of the outer surface of said Winding from the other direction, one of said boot ends overlapping the other end whereby said boot completely envelops the corewinding assembly, a tubular mounting stern passing through said central opening of the core-Winding assembly and through the intermediate portion of said boot, a mounting disk secured to one end portion of said stem, terminals projecting outwardly from said mounting disk and electrically connected to said winding, a preformed shell into which said core-Winding assembly, rubber boot and stem are inserted, said mounting disk being secured to one end of said shell, and an encapsulating mass of insulating material in the other end of said shell.
6. In an encapsulated electrical inductance unit of the class described, the combination of a magnetic core structure, a winding wound around said core structure to form a core-winding assembly, a protective sheath in the form of a thin, one-piece tube of highly elastic material extending through the center of said core structure and stretched so as to elastically envelop the core-winding assembly with one of the ends of said tube overlapping the other end of the tube, whereby said protective sheath completely envelopes the inside, outside and top and bottom surfaces of said winding, and an encapsulating material encasing said core-winding assembly and said protective sheath, I
said protective sheath preventing the encapsulating material from penetrating into the spaces between the turns of said winding and from penetrating into the spaces between Winding and said core structure in the performance of the encapsulating operation.
References Cited by the Examiner UNITED STATES PATENTS 2,382,199 6/1942 Brink 336-229 X 2,965, 864 12/1960 La Patka et al 336192 X 3,162,934 12/1964 Moyers -29-155.57
BERNARD A. GILHEANY, Primary Examiner. JOHN F. BURNS, Examiner.
T. J. KOZMA, Assistant Examiner.

Claims (1)

1. IN A TOROIDAL INDUCTANCE UNIT, THE COMBINATION OF A TOROIDAL CORE STRUCTURE OF A MAGNETIC MATERIAL HAVING A CENTRAL OPENING THERETHROUGH, A WINDING WOUND SPIRALLY AROUND SAID TOROIDAL CORE STRUCTURE AND PASSING THROUGH SAID CENTRAL OPENING, SAID CORE AND WINDING CONSTITUTING A CORE-WINDING ASSEMBLY, A GENERALLY CYLINDRICAL ENVELOPING BOOT OF THIN, HIGLY ELASTIC MATERIAL COMPRISING AN INTERMEDIATE PORTION DISPOSED IN SAID CENTRAL OPENING, SAID BOOT COMPRISING UPPER AND LOWER END PORTIONS EXTENDING FROM SAID INTERMEDIATE PORTION, SAID UPPER END PORTION ENVELOPING THE UPPER END OF SAID CORE-WINDING ASSEMBLY AND EXTENDING DOWN OVER AT LEAST A SUBSTANTIAL PORTION OF THE OUTER SURFACE THEREOF INCLUDING A PORTION OF SAID
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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3359631A (en) * 1965-06-14 1967-12-26 Gen Electric Method of making electrical members
US3493908A (en) * 1968-04-24 1970-02-03 Pulse Eng Inc Component assemblage with cocoon means
US3710531A (en) * 1971-09-02 1973-01-16 Western Electric Co Method of encasing a toroidally shaped object with a heat shrinkable covering
US3753185A (en) * 1972-12-05 1973-08-14 W Mahan Metal detector search coil
US4160967A (en) * 1976-08-21 1979-07-10 Lucas Industries Limited Electrical coil assembly
US4707619A (en) * 1985-02-13 1987-11-17 Maxwell Laboratories, Inc. Saturable inductor switch and pulse compression power supply employing the switch
US4754250A (en) * 1985-08-05 1988-06-28 Firma Wilhelm Sedlbauer Gmbh Holding device for toroidal cores provided with windings
US5097404A (en) * 1990-01-08 1992-03-17 Technology Service Inc. Supply circuit or power supply unit for supplying electronic devices or the like with current or voltage
US5629842A (en) * 1995-04-05 1997-05-13 Zero Emissions Technology Inc. Two-stage, high voltage inductor
US5815059A (en) * 1991-04-26 1998-09-29 Lockheed Martin Corporation Coaxial isolation mounting of a toroidal transformer
US20110215891A1 (en) * 2010-03-03 2011-09-08 Honeywell International Inc. Inductor assembly
US20130051983A1 (en) * 2011-08-26 2013-02-28 Dyson Technology Limited Turbomachine

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2382199A (en) * 1942-06-09 1945-08-14 Gen Electric Electric apparatus
US2965864A (en) * 1956-10-26 1960-12-20 Burroughs Corp Magnetic core assembly
US3162934A (en) * 1961-01-18 1964-12-29 Sangamo Electric Co Method of producing an encapsulated core assembly

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2382199A (en) * 1942-06-09 1945-08-14 Gen Electric Electric apparatus
US2965864A (en) * 1956-10-26 1960-12-20 Burroughs Corp Magnetic core assembly
US3162934A (en) * 1961-01-18 1964-12-29 Sangamo Electric Co Method of producing an encapsulated core assembly

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3359631A (en) * 1965-06-14 1967-12-26 Gen Electric Method of making electrical members
US3493908A (en) * 1968-04-24 1970-02-03 Pulse Eng Inc Component assemblage with cocoon means
US3710531A (en) * 1971-09-02 1973-01-16 Western Electric Co Method of encasing a toroidally shaped object with a heat shrinkable covering
US3753185A (en) * 1972-12-05 1973-08-14 W Mahan Metal detector search coil
US4160967A (en) * 1976-08-21 1979-07-10 Lucas Industries Limited Electrical coil assembly
US4707619A (en) * 1985-02-13 1987-11-17 Maxwell Laboratories, Inc. Saturable inductor switch and pulse compression power supply employing the switch
US4754250A (en) * 1985-08-05 1988-06-28 Firma Wilhelm Sedlbauer Gmbh Holding device for toroidal cores provided with windings
US5097404A (en) * 1990-01-08 1992-03-17 Technology Service Inc. Supply circuit or power supply unit for supplying electronic devices or the like with current or voltage
US5815059A (en) * 1991-04-26 1998-09-29 Lockheed Martin Corporation Coaxial isolation mounting of a toroidal transformer
US5629842A (en) * 1995-04-05 1997-05-13 Zero Emissions Technology Inc. Two-stage, high voltage inductor
US20110215891A1 (en) * 2010-03-03 2011-09-08 Honeywell International Inc. Inductor assembly
US8203410B2 (en) 2010-03-03 2012-06-19 Honeywell International Inc. Inductor assembly
US20130051983A1 (en) * 2011-08-26 2013-02-28 Dyson Technology Limited Turbomachine
US9410442B2 (en) * 2011-08-26 2016-08-09 Dyson Technology Limited Turbomachine
US11668322B2 (en) 2011-08-26 2023-06-06 Dyson Technology Limited Turbomachine

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