US3319948A - Annealing box for transformer cores - Google Patents

Annealing box for transformer cores Download PDF

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US3319948A
US3319948A US579447A US57944766A US3319948A US 3319948 A US3319948 A US 3319948A US 579447 A US579447 A US 579447A US 57944766 A US57944766 A US 57944766A US 3319948 A US3319948 A US 3319948A
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core
box
plates
annealing
pair
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US579447A
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Olsen Willy
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HK Porter Co Inc
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HK Porter Co Inc
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F27/00Details of transformers or inductances, in general
    • H01F27/24Magnetic cores
    • H01F27/245Magnetic cores made from sheets, e.g. grain-oriented
    • H01F27/2455Magnetic cores made from sheets, e.g. grain-oriented using bent laminations
    • 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
    • H01F41/02Apparatus 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 for manufacturing cores, coils, or magnets
    • H01F41/0206Manufacturing of magnetic cores by mechanical means

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  • This invention relates generally to apparatus for and a method of assembling wound type transformer cores of the type shown and described in detail in the co-pending United States patent application of Willy Olsen and Howard D. Tindall, Ser. No. 151,655, filed Nov. 13, 1961, and entitled, Transformer Core Construction and Method of Producing Same.
  • Wound transformer cores of this type have superior magnetic characteristics resulting in lower core losses and higher transformer efiiciencies.
  • the superiority of wound transformer cores as compared to cores made of solid sections or punched la-minations is well known to workers in the art and need not be detailed herein.
  • a wound transformer core made from a single continuously wound strip of core material will normally exhibit better magnetic properties than a transformer core fabricated of strips which have ends butted or lapped to form a composite core.
  • manufacturing economics dictate that wound cores should be made from a plurality of strips of core material rather than from a single continuous strip even though the joints inherent in such a construction tend to degrade the magnetic eificiency of the core structure. Therefore, considerable effort has been concentrated upon ways of minimizing the deleterious effects of the joints while maintaining the manufacturing benefits which flow from the jointed type of core construction.
  • the composite transformer usually including at least two cores each of which is disposed about one leg of the coil structure so that one leg of each core is disposed within the coil window in such manner as to cause the coil window to be substantially completely filled.
  • the preformed core corners are necessarily deformed by straightening in order to be passed through the window, particularly with regard to the outer laminations of the cores, with the consequent introduction of mechanical stresses and strains into the laminations of the cores.
  • the introduced stresses alter the magnetic properties of the core in an adverse manner and are, of course, undesirable.
  • This condition is aggravated in most wound core constructions by the fact that the core laminations have a high space factor at the corners and are prevented from readily shifting relative to one another as they are stressed while being passed through the coil window. This increases the strains introduced at the corners and further degrades the core performance.
  • a primary object of this invention is to provide novel apparatus for and a method of making a wound transformer core of rectangular or square form characterized by a high space factor throughout the straight sided regions of the core together with a space factor at the corners of the core sufiiciently low to allow for relatively free interlaminar movement during assembly of the core to its coil structure to thereby prevent the creation of mechanical stresses and strains in the core material and preserve the magnetic properties of an unstressed core.
  • Another object of this invention is to provide a novel apparatus for and method of making a wound transformer core structure which is built up from a plurality of internested core sections wherein the outermost core section functions as a retainer for the additional core sections nested successively therewithin.
  • a further object of this invention is to provide novel apparatus for fabrication of the wound core structure including an open ended box structure within which the core sections are internested prior to forming into the ultimately desired shape to transport the unformed internested core sections from an assembly point to a forming apparatus, whereby the forming apparatus may be operated continuously.
  • Yet another object of this invention is to provide a novel apparatus for making wound transformer cores which includes a multiple part annealing box structure which is assembled about the wound core structure during the course of forming the same from the internested unforrned core sections.
  • a further object of this invention is to provide novel apparatus for removing the annealed formed core structure from the aforesaid annealing box without subjecting the annealed core to mechanical strains and stresses which would impair the magnetic properties of the core.
  • FIGURE 1 illustrates a perspective view of the open ended assembly ibox within which the several unfor-rned core sections are to be internested;
  • FIGURE 2 illustrates the assembly box of FIGURE 1 with a pair of side plates disposed therewithin effective to cover the side openings through the assembly box;
  • FIGURE 3 is a perspective view illustrating the disposition of the core sections into the assembly box in order beginning with the outermost section and ending with the innermost section;
  • FIGURE 4 illustrates a top plan view of the assembly box with all of the core sections internested and disposed therewithin;
  • FIGUES 5 and 6 illustrate the application of pressure to the side plates of the assembly box to move the same inward and permit removal of the assembly box upward and away from the core assembly;
  • FIGURES 7 and 8 show successive steps in forming the core to the desired rectangular shape
  • FIGURES 9 through 15 illustrate the steps of constructing the annealing box about the formed core;
  • FIG- URE being a partial vertical section as would be seen when viewed along the line 10-40 of FIGURE 9;
  • FIGURES 16 through 20 illustrate the apparatus for and steps carried out in removing the annealing box from the annealed formed core, FIGURES 16 and 17 being side and top views respectively of the apparatus as would be seen when viewed along the lines 16-16 and 17-17 of FIGURES 17 and 16; and
  • FIGURE 21 is a perspective of the finished core formed by the apparatus and method of the present invention.
  • FIGURES 1 to 4 in which there is seen the core assembly box 30 and the unformed core structure 31 made up of a plurality of concentrically internested annular core sections 32 through 35.
  • Each of the core sections 32 through 35 is made up of a plurality of concentrically internested end abutting strips with the end abutments of the strips being successively offset from one another in staircase fashion.
  • the end abutment regions of each of the outer. core sections 32, 33 and 34 are observed to be themselves disposed in offset fashion along one side of the core assembly while the end abutments of the innermost core section 35 are observed to be disposed diametrically across the core.
  • the core assembly box 30 is of rectangular parallelepiped form with the top and bottom surfaces removed having a pair of opposite end walls 36 and a pair of opposite side walls 37, the side walls 37 being rectangularly substantially centrally apertured upwardly from the bottom edge of the box and stopping short of the top edge so that the side walls 37 appear generally to be of inverted U shape.
  • Secured to the inside face of each of the side walls 37 at opposite side edges of the rectangular apertures through the side walls are vertically extending guides 38 between which are rem'ovably disposed side plates 39 which cover the apertures through the sidewalls 37.
  • these side plates 39 also form part of the annealing box and function as pressure applying platens which are acted upon by the rams of the forming device.
  • the core 31 is now built up in the core assembly box 30 between the side plates 39 by first placing the outermost core section 32 downward within the box in a manner best seen in FIGURE 3.
  • the outer lamination of the core section 32 has its abutting ends secured together by means of a piece of tape to prevent the natural resilience of the core strip material from causing this core section to spring open, the outer core section hand forced into a generally ovoid shape, as seen in FIGURE 4, so that the resilience of the section causes it to expand into firm engagement with the side plates 39 to thereby positionally stabilize the core section within the assembly box.
  • the inner core sections are now successively internested within the outer core section 32 to form the composite unformed core 31 held securely within the core assembly box 30 and ready for forming.
  • the assembly of an unformed core into a core assembly box may be carried out at any convenient location and not necessarily at the forming apparatus. Consequently a number of such unformed cores may be assembled at a convenient location and may be then transported to the forming apparatus so that the cores may be then successively formed one immediately after the other with no loss of time at the forming apparatus as would be the case if it were necessary to assemble each of the unforrned core structures at the forming apparatus. In this way, the production efficiencies are realized.
  • the core assembly box 30 containing an unformed core 31 is placed upon the table of the forming apparatus with the open bottom ends of the apertures through the side walls 37 being disposed downward and in alignment with a pair of spaced apart colinearly disposed rams 40 at least one of which is reciprocable relatively to the other.
  • one of the rams 40 is driven toward the other so as to clamp the side plates 39 between the rams 4b, the rams engaging the outer surfaces of the side plates through the openings in the assembly box side walls 37.
  • the ram motion is continued until the side plates 39 are moved toward one another sufliciently to disengage the same from the assembly box 30, the core 31 of course becoming more elongated in the process.
  • the core box 30 is thus disengaged from the side plates 39 and may be lifted vertically upward and completely removed, in the manner seen in FIGURE 6.
  • a mandrel 41 of generally rectangular shape is placed within the elongated central opening of the core and the compressive action of the rams 40 is resumed until the inside lamination of the innermost core section is pressed firmly against opposite sides of the mandrel 41 in the manner illustrated in FIGURE 7, it being observed that the joints of the core sections are tightly clamped between the central mandrel 41 and the side plates 39.
  • a pair of opposite end plates 42 are now moved into engagement with opposite ends of the core 31 by means of a pair of end rams 43, the ram pressure being continuously exerted until the ends of the core 31 are squared off in the manner illustrated in FIGURE 8.
  • the central opening of the core has also become rectangular and that gaps 44 are observed to intervene the adjacent core sections at the corners of the core. Additionally there also exist slight gaps between the individual laminations of each core section in these same corner regions although these cannot be clearly shOWn on the drawing. This looseness in the corners reduces the space factor in these regions of the core so that the core sections may be much more readily flexed when installing the same through the window of the preformed coil structure to thereby eliminate the high mechanical stresses which adversely affect the core magnetic characteristics and which are developed in core structures which have high space factors in the corner regions thereof.
  • an annealing box frame 45 of rectangular shape and provided with depending side flanges 46 is fitted downward upon the upper surface of the core 31 so that the side flanges 46 close fittingly enclose the upper outer marginal edges of the side plates 39 and end plates 42.
  • the lower edges of the side flanges 46 are cut upwardly inward as at 47 for reasons which will subsequently appear, and the central part of the frame 45 is cut out as at 48 so that heat from the annealing oven may circulate freely through the inside region of the formed core.
  • the rams 40 and 43 are now retracted and the core 31 with the enclosing side and end plates and annealing box frame 45 is turned upside down as a unit as shown in FIGURE 12.
  • the rams 40 and 43 are now again moved inwardly into engagement with the side plates 39 and end plates 42 to compress the same so that a second annealing box frame 45 may be moved downward into seating engagement with the core 31 to enclose also the free upper marginal edges of the side plates 39 and end plates 42 as shown in FIGURES 13 and 14.
  • the rams 40 and 43 are again retracted, as in FIGURE 14, and the composite assembly of the formed core within its annealing box may now be removed from the forming apparatus and will appear as shown in FIGURE 15.
  • the boxed formed core may now be annealed, subsequently cooled, and then the core may be removed from the annealing box in the manner to be now described.
  • FIGURES 16 through 20 illustrate a rectangular table frame 49 supported by legs 50 and supporting a magnetically susceptible top plate 51, as for example made of steel plate.
  • a pair of spaced apart horizontal supports 52 Spaced downwardly from the top 51 and extending transversely therebeneath and secured at opposite ends to the table support structure are a pair of spaced apart horizontal supports 52 which carry thereupon a magnet structure including an energizable field 53 and poles 54, the poles 54 being in surface contact with the underside of top plate 51.
  • Fixedly secured to and extending upward from the frame 49 is a support frame having a pair of vertical members 55 which carry a transversely extending horizontal top member 56, members 55 and 56 being illustrated as of channel shape in cross section.
  • a cylinder 58 Suspended vertically from the horizontal top support 56 as by means of a suspension bolt 57 is a cylinder 58 within which is disposed for vertical reciprocation a piston head which is connected to the piston rod 59 observed in FIGURE 16 to extend below the cylinder 58.
  • the piston may be moved upward within the cylinder 38 by injection of hydraulic pressure through the port 60 and venting through the port 61, while the piston may be lowered by the reverse procedure.
  • the piston rod 59 will of course rise or lower in accordance with the motion of the piston head within the cylinder 58 and will carry with it the triangular frame 62 coupled to the lower end of the piston rod 59 as by means of the shackle 63.
  • the triangular frame 62 includes a horizontally extending bar 64 whose opposite ends terminate in vertically oriented cylindrical sleeves 65 disposed within the channel shaped vertical supports 55 and through which vertically extend the guide rods 66 which latter are fixedly secured to the vertical supports 55 as by means of the anchor blocks 67 seen in FIGURE 16.
  • Slidably disposed upon the horizontal bar 64 of the triangular frame 62 are a pair of hooks 68 whose hook like projections are pointed toward one another and inclined upward as most clearly seen in the showing of FIGURE 20.
  • the annealed formed core 31 enclosed within the annealing box in the manner shown in FIGURE is placed upon the top plate 51 above the magnet structure so that one of the annealing box frames 45 is disposed flatwise upon the top plate in generally overlying relation to the magnet structure, the annealing box being so positioned that the hooks 68 may be moved inward toward it along the horizontal bar 64 of the triangular frame 62 to permit the upwardly turned hook ends to underlie the inwardly upwardly cut lower edges 47 of the side flanges 46 of the upper annealing box frame 45.
  • the magnet structure is now energized to strongly magnetically hold the annealing box and core contained therewithin downward upon the top plate 51.
  • the slidable hooks 68 are moved inward to underlie the opposite ends of the frame side flanges as shown by the dotted line showing in FIGURE 16.
  • the piston within the cylinder 58 is now subjected to upward lifting force by hydraulic or pneumatic pressure applied through the cylinder port 66, thus causing the piston rod 59 to rise and carry with it the triangular frame 62 and slidable hooks 68.
  • the hooks 68 anchor under the annealing box frame side flanges 46, as shown in the detail of FIGURE 20, and continued upward movement of the frame 62 results in the upward removal of the annealing box upper cover 45 as illustrated in FIGURE 18.
  • the magnet structure is now deenergized and removed frame 45 is lifted from the hooks 68 and set aside, after which the hooks 68 are slid outward away from one another and the frame 62 is again lowered by releasing the pressure on the piston within the cylinder 58.
  • the partially housed core structure may now be turned top for bottom so that what was formerly the bottom frame of the annealing box now becomes the top frame.
  • the magnet structure is now again reenergized and the hooks 68 are slid inward to underlie the side flanges 46 of the remaining annealing box frame 45, after which actuation of the piston removes this remaining frame 45.
  • Deenergization of the magnet now releases the side plates 39 and end plates 42 of the annealing box structure from the finished core 31, this being illustrated in the showing of FIGURE 19.
  • the mandrel 41 may now be lifted out of the core window to leave the completed annealed formed core 31 which appears as shown in FIGURE 21.
  • An annealing box for holding in desired form the internested plural turns of a centrally windowed rectangularly formed wound transformer core during annealing, comprising in combination, a pair of identical centrally apertured rectangular rigid frame members each provided with peripherally extending side flanges turned at right angles to the principal plane of the frame member, a pair of rigid side plates of length less than that of the formed core length and of a height substantially the same as that of the core, a pair of rigid end plates of length less than that of the width of the formed core and of a height equal to that of the said side plates, the box structure being formed by the disposition of the said side and end plates in flat surface contact with the sides and ends respectively of the formed rectangular core, and with the plates held in position by disposition of the frame members respectively against the upper and lower edges of the said plates with the upper and lower outside marginal edges of the plates held against outward movement by disposition against the inside faces of the frame members side flanges, the box structure being held together by the radially outward directed force exerted by the formed core on the
  • annealing box as set forth in claim 1 wherein said frame members and side plates and end plates are made of material having high thermal conductivity, wherein the central apertures of said frame members are sufficiently large to permit direct heat flow into the core structure from the annealing oven, and wherein the lengths of the said side and end plates are sufliciently less than the length and width of the core to expose the outside of the corners of the core to the direct heat of the annealing oven.
  • An annealing box for holding in desired form the internested plural turns of a centrally windowed rectangularly formed wound transformer core during annealing, comprising in combination, a pair of identical rectangular rigid frame members each provided with flanges turned at right angles to the principal plane of the frame member, a pair of rigid side plates of a height substantially the same as that of the core, a pair of rigid end plates of a height equal to that of the said side plates, the box structure being formed *by the disposition of the said side and end plates in flat surface contact with the sides and ends respectively of the formed rectangular core, and with the plates held in position by disposition of the frame members respectively against the upper and lower edge of the said plates with the upper and lower outside marginal edges of the plates held against outward movement by disposition against the inside faces of the frame members flanges, the box structure being held together by the radially outward directed force exerted by the formed core on the side and end plates which strongly biases the latter into firm engagement against the flanges of the frame members.
  • An annealing box for holding in desired form the internested plural turns of a formed Wound transformer core during annealing, comprising in combination, a pair of identical rigid frame members each provided with flanges turned at an angle to the principal plane of the frame member, and a plurality of rigid plates of a height substantially equal to the core height, the box structure being formed by the disposition of the said rigid plates in fiat surface contact with the flat outer surface areas of the outside turn of the formed wound transformer core, and with the plates held in position by disposition of the frame members respectively against the upper and lower edges of the said plates with the upper and lower outside marginal edges of the plates held against outward movement by disposition against the inside faces of the frame members flanges, the box structure being held together by the radially outward directed force exerted by the formed core on the plates which strongly biases the latter into firm engagement against the flanges of the frame members.

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  • Power Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Manufacturing Cores, Coils, And Magnets (AREA)

Description

May 16, 1967 w. OLSEN 3,319,948
ANNEALING BOX FOR TRANSFORMER CORES Original Filed Oct. 24, 1963 4 Sheets-Sheet l INVENTOR.
W I LLY OLS EN May 16, 1967 W. OLSEN 3,319,948
ANNEALING BOX FOR TRANSFORMER CORES Original Filed Oct. 24, 1963 4 Sheets-Sheet 2 I I F" 1 l .f II I ll l k I I .l IR 1 1- L 1.
I" NlLLY OLSEN ATTO/fA E) May 16, 1967 w. OLSEN 3,319,948
ANNEALING BOX FOR TRANSFORMER CORES Original Filed Oct. 24 1963 4 Sheets-Sheet 5 INVENTOR.
WI LLY OLSEN May 16, 1967 w. OLSEN ANNEALING BOX FOR TRANSFORMER CORES 4 Sheets-Sheet 4 Original Filed Oct. 24 1963 INVENTOR.
W I LLY o LSE H United States Patent 4 Claims. (Cl. 263-49) This application is a division of application Ser. No. 318,726, filed Oct. 24, 1963, now abandoned.
This invention relates generally to apparatus for and a method of assembling wound type transformer cores of the type shown and described in detail in the co-pending United States patent application of Willy Olsen and Howard D. Tindall, Ser. No. 151,655, filed Nov. 13, 1961, and entitled, Transformer Core Construction and Method of Producing Same.
Wound transformer cores of this type have superior magnetic characteristics resulting in lower core losses and higher transformer efiiciencies. The superiority of wound transformer cores as compared to cores made of solid sections or punched la-minations is well known to workers in the art and need not be detailed herein. Moreover, it is also known that a wound transformer core made from a single continuously wound strip of core material will normally exhibit better magnetic properties than a transformer core fabricated of strips which have ends butted or lapped to form a composite core. Nevertheless, as a practical matter, manufacturing economics dictate that wound cores should be made from a plurality of strips of core material rather than from a single continuous strip even though the joints inherent in such a construction tend to degrade the magnetic eificiency of the core structure. Therefore, considerable effort has been concentrated upon ways of minimizing the deleterious effects of the joints while maintaining the manufacturing benefits which flow from the jointed type of core construction.
In nearly all instances it is desirable to form a transformer core so that it is of rectangular or square shape having a corresponding rectangular or square central opening or window to accommodate the transformer coil structure in order that the over all transformer may be made as compact as possible, the composite transformer usually including at least two cores each of which is disposed about one leg of the coil structure so that one leg of each core is disposed within the coil window in such manner as to cause the coil window to be substantially completely filled. This type of structure creates problems with regard to the installation of the preformed cores through the coil window since there is very little unoccupied coil window space in the finished assembly and the corners of the core structure must be passed through the window in order to close the core.
The preformed core corners are necessarily deformed by straightening in order to be passed through the window, particularly with regard to the outer laminations of the cores, with the consequent introduction of mechanical stresses and strains into the laminations of the cores. The introduced stresses alter the magnetic properties of the core in an adverse manner and are, of course, undesirable. This condition is aggravated in most wound core constructions by the fact that the core laminations have a high space factor at the corners and are prevented from readily shifting relative to one another as they are stressed while being passed through the coil window. This increases the strains introduced at the corners and further degrades the core performance.
Attempts have been made in the past to reduce the severity of this problem by the use of various forming 3,319,948 Patented May 16, 1967 methods directed toward reducing the space factor at the corners, as for example by the use of insert shims in the corner regions as the core is being wound. Unfortunately, these known methods are either uneconomic or also tend to reduce the space factor in the straight sided legs and yoke regions of the core where a high space factor is desirable. The superior transformer core construction fully described and illustrated in the aforesaid copending United States patent application, and which is also shown in the drawings appended hereto is economically producible by utilization of the apparatus and method according to the present invention to be hereafter described.
A primary object of this invention is to provide novel apparatus for and a method of making a wound transformer core of rectangular or square form characterized by a high space factor throughout the straight sided regions of the core together with a space factor at the corners of the core sufiiciently low to allow for relatively free interlaminar movement during assembly of the core to its coil structure to thereby prevent the creation of mechanical stresses and strains in the core material and preserve the magnetic properties of an unstressed core.
Another object of this invention is to provide a novel apparatus for and method of making a wound transformer core structure which is built up from a plurality of internested core sections wherein the outermost core section functions as a retainer for the additional core sections nested successively therewithin.
A further object of this invention is to provide novel apparatus for fabrication of the wound core structure including an open ended box structure within which the core sections are internested prior to forming into the ultimately desired shape to transport the unformed internested core sections from an assembly point to a forming apparatus, whereby the forming apparatus may be operated continuously.
Yet another object of this invention is to provide a novel apparatus for making wound transformer cores Which includes a multiple part annealing box structure which is assembled about the wound core structure during the course of forming the same from the internested unforrned core sections.
A further object of this invention is to provide novel apparatus for removing the annealed formed core structure from the aforesaid annealing box without subjecting the annealed core to mechanical strains and stresses which would impair the magnetic properties of the core.
The foregoing and other objects of the invention will become clear from a reading of the following specification in conjunction with an examination of the appended drawings, wherein:
FIGURE 1 illustrates a perspective view of the open ended assembly ibox within which the several unfor-rned core sections are to be internested;
FIGURE 2 illustrates the assembly box of FIGURE 1 with a pair of side plates disposed therewithin effective to cover the side openings through the assembly box;
FIGURE 3 is a perspective view illustrating the disposition of the core sections into the assembly box in order beginning with the outermost section and ending with the innermost section;
FIGURE 4 illustrates a top plan view of the assembly box with all of the core sections internested and disposed therewithin;
FIGUES 5 and 6 illustrate the application of pressure to the side plates of the assembly box to move the same inward and permit removal of the assembly box upward and away from the core assembly;
FIGURES 7 and 8 show successive steps in forming the core to the desired rectangular shape;
FIGURES 9 through 15 illustrate the steps of constructing the annealing box about the formed core; FIG- URE being a partial vertical section as would be seen when viewed along the line 10-40 of FIGURE 9;
FIGURES 16 through 20 illustrate the apparatus for and steps carried out in removing the annealing box from the annealed formed core, FIGURES 16 and 17 being side and top views respectively of the apparatus as would be seen when viewed along the lines 16-16 and 17-17 of FIGURES 17 and 16; and
FIGURE 21 is a perspective of the finished core formed by the apparatus and method of the present invention.
In the several figures, like elements are denoted by like reference characters.
Referring now to the figures, consider first FIGURES 1 to 4 in which there is seen the core assembly box 30 and the unformed core structure 31 made up of a plurality of concentrically internested annular core sections 32 through 35. Each of the core sections 32 through 35 is made up of a plurality of concentrically internested end abutting strips with the end abutments of the strips being successively offset from one another in staircase fashion. The end abutment regions of each of the outer. core sections 32, 33 and 34 are observed to be themselves disposed in offset fashion along one side of the core assembly while the end abutments of the innermost core section 35 are observed to be disposed diametrically across the core. This arrangement of the end abutments of the several core sections which together make up the composite core is for the purpose of subsequently providing optimum ease of assembly of the finished structure through the windows of the coil structure with which the cores are to be used in forming a finished transformer, all as set forth in detail in the forementioned copending patent application.
The core assembly box 30 is of rectangular parallelepiped form with the top and bottom surfaces removed having a pair of opposite end walls 36 and a pair of opposite side walls 37, the side walls 37 being rectangularly substantially centrally apertured upwardly from the bottom edge of the box and stopping short of the top edge so that the side walls 37 appear generally to be of inverted U shape. Secured to the inside face of each of the side walls 37 at opposite side edges of the rectangular apertures through the side walls are vertically extending guides 38 between which are rem'ovably disposed side plates 39 which cover the apertures through the sidewalls 37. As will be subsequently seen, these side plates 39 also form part of the annealing box and function as pressure applying platens which are acted upon by the rams of the forming device.
The core 31 is now built up in the core assembly box 30 between the side plates 39 by first placing the outermost core section 32 downward within the box in a manner best seen in FIGURE 3. The outer lamination of the core section 32 has its abutting ends secured together by means of a piece of tape to prevent the natural resilience of the core strip material from causing this core section to spring open, the outer core section hand forced into a generally ovoid shape, as seen in FIGURE 4, so that the resilience of the section causes it to expand into firm engagement with the side plates 39 to thereby positionally stabilize the core section within the assembly box. The inner core sections are now successively internested within the outer core section 32 to form the composite unformed core 31 held securely within the core assembly box 30 and ready for forming.
The assembly of an unformed core into a core assembly box, as just described, may be carried out at any convenient location and not necessarily at the forming apparatus. Consequently a number of such unformed cores may be assembled at a convenient location and may be then transported to the forming apparatus so that the cores may be then successively formed one immediately after the other with no loss of time at the forming apparatus as would be the case if it were necessary to assemble each of the unforrned core structures at the forming apparatus. In this way, the production efficiencies are realized.
Refer now to FIGURES 5 through 8 in order, the core assembly box 30 containing an unformed core 31 is placed upon the table of the forming apparatus with the open bottom ends of the apertures through the side walls 37 being disposed downward and in alignment with a pair of spaced apart colinearly disposed rams 40 at least one of which is reciprocable relatively to the other. As best seen in FIGURE 5, one of the rams 40 is driven toward the other so as to clamp the side plates 39 between the rams 4b, the rams engaging the outer surfaces of the side plates through the openings in the assembly box side walls 37. The ram motion is continued until the side plates 39 are moved toward one another sufliciently to disengage the same from the assembly box 30, the core 31 of course becoming more elongated in the process. The core box 30 is thus disengaged from the side plates 39 and may be lifted vertically upward and completely removed, in the manner seen in FIGURE 6.
With the core 31 in its elongated form as seen in FIG- URES 5 and 6, a mandrel 41 of generally rectangular shape is placed within the elongated central opening of the core and the compressive action of the rams 40 is resumed until the inside lamination of the innermost core section is pressed firmly against opposite sides of the mandrel 41 in the manner illustrated in FIGURE 7, it being observed that the joints of the core sections are tightly clamped between the central mandrel 41 and the side plates 39. A pair of opposite end plates 42 are now moved into engagement with opposite ends of the core 31 by means of a pair of end rams 43, the ram pressure being continuously exerted until the ends of the core 31 are squared off in the manner illustrated in FIGURE 8.
As also best seen in FIGURE 8, it is observed that the central opening of the core has also become rectangular and that gaps 44 are observed to intervene the adjacent core sections at the corners of the core. Additionally there also exist slight gaps between the individual laminations of each core section in these same corner regions although these cannot be clearly shOWn on the drawing. This looseness in the corners reduces the space factor in these regions of the core so that the core sections may be much more readily flexed when installing the same through the window of the preformed coil structure to thereby eliminate the high mechanical stresses which adversely affect the core magnetic characteristics and which are developed in core structures which have high space factors in the corner regions thereof.
As best seen in FIGURES 9, 10 and 11, with the core formed as shown in FIGURE 8 and with the side plates 39 and end plates 42 in position as shown, an annealing box frame 45 of rectangular shape and provided with depending side flanges 46 is fitted downward upon the upper surface of the core 31 so that the side flanges 46 close fittingly enclose the upper outer marginal edges of the side plates 39 and end plates 42. 'The lower edges of the side flanges 46 are cut upwardly inward as at 47 for reasons which will subsequently appear, and the central part of the frame 45 is cut out as at 48 so that heat from the annealing oven may circulate freely through the inside region of the formed core.
The rams 40 and 43 are now retracted and the core 31 with the enclosing side and end plates and annealing box frame 45 is turned upside down as a unit as shown in FIGURE 12. The rams 40 and 43 are now again moved inwardly into engagement with the side plates 39 and end plates 42 to compress the same so that a second annealing box frame 45 may be moved downward into seating engagement with the core 31 to enclose also the free upper marginal edges of the side plates 39 and end plates 42 as shown in FIGURES 13 and 14. The rams 40 and 43 are again retracted, as in FIGURE 14, and the composite assembly of the formed core within its annealing box may now be removed from the forming apparatus and will appear as shown in FIGURE 15. The boxed formed core may now be annealed, subsequently cooled, and then the core may be removed from the annealing box in the manner to be now described.
Turning now to FIGURES 16 through 20, consider first FIGURES 16 and 17 which illustrate a rectangular table frame 49 supported by legs 50 and supporting a magnetically susceptible top plate 51, as for example made of steel plate. Spaced downwardly from the top 51 and extending transversely therebeneath and secured at opposite ends to the table support structure are a pair of spaced apart horizontal supports 52 which carry thereupon a magnet structure including an energizable field 53 and poles 54, the poles 54 being in surface contact with the underside of top plate 51. Fixedly secured to and extending upward from the frame 49 is a support frame having a pair of vertical members 55 which carry a transversely extending horizontal top member 56, members 55 and 56 being illustrated as of channel shape in cross section.
Suspended vertically from the horizontal top support 56 as by means of a suspension bolt 57 is a cylinder 58 within which is disposed for vertical reciprocation a piston head which is connected to the piston rod 59 observed in FIGURE 16 to extend below the cylinder 58. The piston may be moved upward within the cylinder 38 by injection of hydraulic pressure through the port 60 and venting through the port 61, while the piston may be lowered by the reverse procedure. The piston rod 59 will of course rise or lower in accordance with the motion of the piston head within the cylinder 58 and will carry with it the triangular frame 62 coupled to the lower end of the piston rod 59 as by means of the shackle 63. The triangular frame 62 includes a horizontally extending bar 64 whose opposite ends terminate in vertically oriented cylindrical sleeves 65 disposed within the channel shaped vertical supports 55 and through which vertically extend the guide rods 66 which latter are fixedly secured to the vertical supports 55 as by means of the anchor blocks 67 seen in FIGURE 16. Slidably disposed upon the horizontal bar 64 of the triangular frame 62 are a pair of hooks 68 whose hook like projections are pointed toward one another and inclined upward as most clearly seen in the showing of FIGURE 20.
The annealed formed core 31 enclosed within the annealing box in the manner shown in FIGURE is placed upon the top plate 51 above the magnet structure so that one of the annealing box frames 45 is disposed flatwise upon the top plate in generally overlying relation to the magnet structure, the annealing box being so positioned that the hooks 68 may be moved inward toward it along the horizontal bar 64 of the triangular frame 62 to permit the upwardly turned hook ends to underlie the inwardly upwardly cut lower edges 47 of the side flanges 46 of the upper annealing box frame 45.
The magnet structure is now energized to strongly magnetically hold the annealing box and core contained therewithin downward upon the top plate 51. Next, the slidable hooks 68 are moved inward to underlie the opposite ends of the frame side flanges as shown by the dotted line showing in FIGURE 16. The piston within the cylinder 58 is now subjected to upward lifting force by hydraulic or pneumatic pressure applied through the cylinder port 66, thus causing the piston rod 59 to rise and carry with it the triangular frame 62 and slidable hooks 68. The hooks 68 anchor under the annealing box frame side flanges 46, as shown in the detail of FIGURE 20, and continued upward movement of the frame 62 results in the upward removal of the annealing box upper cover 45 as illustrated in FIGURE 18. The magnet structure is now deenergized and removed frame 45 is lifted from the hooks 68 and set aside, after which the hooks 68 are slid outward away from one another and the frame 62 is again lowered by releasing the pressure on the piston within the cylinder 58.
With the magnet deenergized the partially housed core structure may now be turned top for bottom so that what was formerly the bottom frame of the annealing box now becomes the top frame. The magnet structure is now again reenergized and the hooks 68 are slid inward to underlie the side flanges 46 of the remaining annealing box frame 45, after which actuation of the piston removes this remaining frame 45. Deenergization of the magnet now releases the side plates 39 and end plates 42 of the annealing box structure from the finished core 31, this being illustrated in the showing of FIGURE 19. The mandrel 41 may now be lifted out of the core window to leave the completed annealed formed core 31 which appears as shown in FIGURE 21.
Having now described my invention in connection with particularly illustrated embodiments thereof it will be appreciated that modifications and variations of the same may now occur from time to time to those persons normally skilled in the art without departing from the essential scope or spirit of my invention, and accordingly it is intended to claim the same broadly as well as specifically as indicated by the appended claims.
What is claimed as new and useful is:
1. An annealing box for holding in desired form the internested plural turns of a centrally windowed rectangularly formed wound transformer core during annealing, comprising in combination, a pair of identical centrally apertured rectangular rigid frame members each provided with peripherally extending side flanges turned at right angles to the principal plane of the frame member, a pair of rigid side plates of length less than that of the formed core length and of a height substantially the same as that of the core, a pair of rigid end plates of length less than that of the width of the formed core and of a height equal to that of the said side plates, the box structure being formed by the disposition of the said side and end plates in flat surface contact with the sides and ends respectively of the formed rectangular core, and with the plates held in position by disposition of the frame members respectively against the upper and lower edges of the said plates with the upper and lower outside marginal edges of the plates held against outward movement by disposition against the inside faces of the frame members side flanges, the box structure being held together by the radially outward directed force exerted by the formed core on the side and end plates which strongly biases the latter into firm engagement against the side flanges of the frame members.
2. The annealing box as set forth in claim 1 wherein said frame members and side plates and end plates are made of material having high thermal conductivity, wherein the central apertures of said frame members are sufficiently large to permit direct heat flow into the core structure from the annealing oven, and wherein the lengths of the said side and end plates are sufliciently less than the length and width of the core to expose the outside of the corners of the core to the direct heat of the annealing oven.
3. An annealing box for holding in desired form the internested plural turns of a centrally windowed rectangularly formed wound transformer core during annealing, comprising in combination, a pair of identical rectangular rigid frame members each provided with flanges turned at right angles to the principal plane of the frame member, a pair of rigid side plates of a height substantially the same as that of the core, a pair of rigid end plates of a height equal to that of the said side plates, the box structure being formed *by the disposition of the said side and end plates in flat surface contact with the sides and ends respectively of the formed rectangular core, and with the plates held in position by disposition of the frame members respectively against the upper and lower edge of the said plates with the upper and lower outside marginal edges of the plates held against outward movement by disposition against the inside faces of the frame members flanges, the box structure being held together by the radially outward directed force exerted by the formed core on the side and end plates which strongly biases the latter into firm engagement against the flanges of the frame members.
4. An annealing box for holding in desired form the internested plural turns of a formed Wound transformer core during annealing, comprising in combination, a pair of identical rigid frame members each provided with flanges turned at an angle to the principal plane of the frame member, and a plurality of rigid plates of a height substantially equal to the core height, the box structure being formed by the disposition of the said rigid plates in fiat surface contact with the flat outer surface areas of the outside turn of the formed wound transformer core, and with the plates held in position by disposition of the frame members respectively against the upper and lower edges of the said plates with the upper and lower outside marginal edges of the plates held against outward movement by disposition against the inside faces of the frame members flanges, the box structure being held together by the radially outward directed force exerted by the formed core on the plates which strongly biases the latter into firm engagement against the flanges of the frame members.
References Cited by the Examiner UNITED STATES PATENTS 1,643,756 9/1927 Sullivan 263-49 1,908,242 5/1933 Henderson 263-49 3,223,955 12/1965 Olsen et al 29-15557 X FREDERICK L. MATTESON, ]R., Primary Examiner.
D. A. TAMBURRO, Assistant Examiner.

Claims (1)

1. AN ANNEALING BOX FOR HOLDING IN DESIRED FORM THE INTERNESTED PLURAL TURNS OF A CENTRALLY WINDOWED RECTANGULARLY FORMED WOUND TRANSFORMER CORE DURING ANNEALING, COMPRISING IN COMBINATION, A PAIR OF IDENTICAL CENTRALLY APERTURED RECTANGULAR RIGID FRAME MEMBERS EACH PROVIDED WITH PERIPHERALLY EXTENDING SIDE FLANGES TURNED AT RIGHT ANGLES TO THE PRINCIPAL PLANE OF THE FRAME MEMBER, A PAIR OF RIGID SIDE PLATES OF LENGTH LESS THAN THAT OF THE FORMED CORE LENGTH AND OF A HEIGHT SUBSTANTIALLY THE SAME AS THAT OF THE CORE, A PAIR OF RIGID END PLATES OF LENGTH LESS THAN THAT OF THE WIDTH OF THE FORMED CORE AND OF A HEIGHT EQUAL TO THAT OF THE SAID SIDE PLATES, THE BOX STRUCTURE BEING FORMED BY THE DISPOSITION OF THE SAID SIDE AND END PLATES IN FLAT SURFACE CONTACT WITH THE
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3517917A (en) * 1967-06-12 1970-06-30 Central Transformer Corp Annealing form and methods
US3988107A (en) * 1975-08-12 1976-10-26 Ferro Corporation Sagger construction
US4449925A (en) * 1979-05-12 1984-05-22 Williams Alan E Heating device and method of heating articles
US5705782A (en) * 1996-09-30 1998-01-06 Gerback; David Internal coil spot welding device

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1643756A (en) * 1925-09-18 1927-09-27 Chrobaltic Tool Company Carburizing box
US1908242A (en) * 1930-09-23 1933-05-09 Driver Harris Co Container for treating metal articles by heat
US3223955A (en) * 1961-11-13 1965-12-14 Porter Co Inc H K Transformer core construction and method of producing same

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1643756A (en) * 1925-09-18 1927-09-27 Chrobaltic Tool Company Carburizing box
US1908242A (en) * 1930-09-23 1933-05-09 Driver Harris Co Container for treating metal articles by heat
US3223955A (en) * 1961-11-13 1965-12-14 Porter Co Inc H K Transformer core construction and method of producing same

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3517917A (en) * 1967-06-12 1970-06-30 Central Transformer Corp Annealing form and methods
US3988107A (en) * 1975-08-12 1976-10-26 Ferro Corporation Sagger construction
US4449925A (en) * 1979-05-12 1984-05-22 Williams Alan E Heating device and method of heating articles
US5705782A (en) * 1996-09-30 1998-01-06 Gerback; David Internal coil spot welding device

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