US3603864A - Current dependent filter inductance - Google Patents

Current dependent filter inductance Download PDF

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US3603864A
US3603864A US889555A US3603864DA US3603864A US 3603864 A US3603864 A US 3603864A US 889555 A US889555 A US 889555A US 3603864D A US3603864D A US 3603864DA US 3603864 A US3603864 A US 3603864A
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magnetic core
auxiliary
airgap
inductance
current
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Sherwood Thaler
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National Aeronautics and Space Administration NASA
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F37/00Fixed inductances not covered by group H01F17/00
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F21/00Variable inductances or transformers of the signal type
    • H01F21/02Variable inductances or transformers of the signal type continuously variable, e.g. variometers
    • H01F21/08Variable inductances or transformers of the signal type continuously variable, e.g. variometers by varying the permeability of the core, e.g. by varying magnetic bias
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F29/00Variable transformers or inductances not covered by group H01F21/00
    • H01F29/14Variable transformers or inductances not covered by group H01F21/00 with variable magnetic bias
    • H01F2029/143Variable transformers or inductances not covered by group H01F21/00 with variable magnetic bias with control winding for generating magnetic bias

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  • ABSTRACT A current dependent variable inductance having U.S. a and flux coupled magnetic core portion cross. 336/178 sectional areas that vary betweenmaximum and minimum [5 it. values in planes perpendicular to the flux Current flow of greater than a given magnitude in the winding causes satu- [50] Field of Search 321/10; ration f the minimum core area and generation f f i i 323/1, 6; 336/165, 1 flux in an adjacent auxiliary airgap. The lengths of the fringing flux lines and accordingly of the auxiliary airgap vary directly [56] References CIM with the saturation current in the winding. Thus, the value of UNITED STATES PATENTS inductance provided by the winding varies inversely with that 2,015,534 9/1935 Rose 321/10 X current.
  • This invention relates to a current dependent variable inductance and is specifically suited for use as an inductive element in input filter chokes of AC or DC power supplies.
  • inductance In the design of filter circuits for AC-DC power supplies, it is customary to minimize the value of inductance so as to reduce the weight and cost of the inductance element required. Optimum performance in the way of regulation, however, is realized only if the inductance value is equal to or greater than the circuit's critical inductance. This .is the inductance value required to prevent current from decreasing to zero during any part of the cycle.
  • Critical inductance L is a well-known phenomenon discussed in Reference Data for Radio Engineers (3rd ed.), pages 183-185, 1949, Knickerbocker Printing Company, N.Y., N.Y., and for a particular configuration is equal to K/I where K is a constant and I is the DC output current.
  • L is a variable having a maximum value determined by the minimum level of output current and corresponding to the minimum inductance value required for optimum filter circuit performance.
  • the inductance elements current-carrying requirements which also effect weight and cost must be determined by the maximum value of DC output current. Because of these designs criteria, the typical nonvariable inductance element of an input choke filter provides an unnecessarily large value of inductance for high output current levels and an unnecessarily large current rating for low output current levels.
  • variable inductances for which inductance values vary inversely with current.
  • inductances include swinging chokes that utilize the characteristic B-I-I slope of an iron core to establish the desired variation in inductance, iron-cored inductances that include an independently energized control winding that selectively controls inductance by varying the level of magnetic flux produced, and various types of mechanically adjusted inductances in which inductance values are altered either by switching mechanisms that modify the circuit relationship between plural coils or by relative physical displacement of either inductance coils or magnetic cores. All such previous elements suffer from certain disadvantages.
  • core material may not be available with a B-H loop that will provide a swinging choke with the particular operating characteristics desired for a particular application.
  • Externally controlled variable inductances although offering wide ranges of operation, entail the sometimes undesirable use of separate control windings and circuits.
  • the time delays inherently required by mechanically controlled variable inductances to effect switching or mechanical displacements are not acceptable in all applications.
  • the object of the invention is to provide an improved variable inductance for use in input choke filter circuits of AC-DC power supplies.
  • the invention is characterized by the provision of a currentdependent variable inductance that is suited particularly for use as an inductive element in choke input filters of AC-DC power supplies.
  • the inductance comprises a winding on a magnetic core with pole pieces that define a primary airgap and establish therewith a magnetic flux path.
  • the core further includes a longitudinal portion of reduced cross section and including cross-sectional areas in planes perpendicular to the flux path that vary between maximum and minimum values. Current flow through the winding at levels above a predetermined value induces saturation of the longitudinal core portion at the reduced cross section thereby generating fringe flux in an auxiliary gap adjacent thereto.
  • the length of the fringe flux lines and correspondingly of the auxiliary airgap vary directly dependent upon the level of current flow in the winding above the predetermined value. Consequently, the inductance values provided by the inductance element varies inversely with current flow through its winding.
  • the varying cross section of the longitudinal core portion is selected so as to provide an inductance value substantially equal to K/I over a predetermined current operating range; where K is a constant and I,, is the value of DC output current from a choke input filter.
  • K is a constant and I, is the value of DC output current from a choke input filter.
  • Another feature of the invention is provision of an electrical inductance of the above type wherein the longitudinal core portion of reduced cross section includes pole sections on opposite sides'of the primary airgap and with areas of minimum cross section directly adjacent thereto.
  • the auxiliary airgap produced by saturation of the core is parallel to the primary airgap.
  • Another feature of the invention is the provision of an electrical inductance of the above types wherein the pole sections of reduced cross section are formed by a plurality of magnetic laminations stacked in planes perpendicular to the flux path.
  • the employment of stacked magnetic laminations of different size establish the variations in cross-sectional area in a simple construction and eliminates problems that would be introduced, for example, by attempts to produce the desired variable cross section by machining. Also, the thin laminations reduce eddy current losses, particularly in high-frequency applications.
  • FIG. 1 is a schematic circuit diagram of an AC-DC power supply employing a preferred inductance element embodiment of the invention
  • FIG. 2 is an enlarged view of the pole pieces shown on the inductance core of FIG. 1;
  • FIG. 3 is a view of one of the pole pieces shown in FIG. 2 looking in the direction of arrows 3-3;
  • FIG. 4 is a schematic illustration of another inductance element embodiment of the invention.
  • FIG. 5 is a graph illustrating performance characteristics of a conventional inductance and of the inductance embodiment shown in FIGS. 1-3.
  • FIG. I Shown in FIG. I is a transformer having a primary winding 11 connected to a source of AC power and a secondary winding 12 connected to a rectifier 13.
  • the DC output of the rectifier 13 is applied to a filter circuit 14 including an inductance winding 15 and a capacitance l6.
  • Appearing on output terminal 17 is the filtered DC output of the filter circuit 14.
  • Supporting the inductance winding 15 is a horseshoe magnetic core 18 that provides with primary airgap 19 a path for magnetic flux generated by current in the winding 15.
  • the core 18 includes a main section 20 that terminates with longitudinally spaced pole pieces sections 21 and 22 disposed on opposite sides of the primary airgap l9.
  • each of the pole pieces 21 and 22 is formed by a plurality of symmetrically stacked, square magnetic laminations 23-26 of different size.
  • cross-sectional areas of each of the pole pieces 21 and 22 in planes perpendicular to the magnetic flux path vary between maximum and minimum values.
  • the maximum value is established by the cross-sectional area of the main core section 20 while the minimum value is established by the smallest laminations 26 located directly adjacent the primary airgap 19.
  • the laminations 23-26 are stacked in order of size so as to provide each of the pole pieces 21 and 22 with cross-sectional areas that vary in a uniform sense between the maximum and minimum values.
  • the flow of a given minimum magnitude of current through the winding 15 induces saturation of the smallest magnetic laminations 26 shown in FIG. 2.
  • Further increases in the winding current generates fringe flux in an annular auxiliary airgap 29 surrounding the pole pieces 21 and 22 and parallel to the primary airgap 19.
  • the length of the fringe flux lines also increase as does the effective length of the auxiliary gap 29.
  • the predominant portion of the fringe flux lines terminate at the edges of the laminations 25 so that the spacing therebetween establishes the length of the auxiliary gap 29.
  • fringe flux lines also extend between the more distantly spaced laminations 23 and 24 so as to extend the effective length of the auxiliary airgap 29.
  • the effective length of the auxiliary airgap 29 is directly dependent upon the current flowing in the winding 15.
  • inductance provided by the winding 15 is inversely dependent upon the total airgap length which in this case includes both the primary airgap 19 and the auxiliary airgap 29. Consequently, the inductance value exhibited by the filter circuit 14 is inversely dependent upon the magnitude of current flowing in the winding 15 at levels above that required to saturate the minimum sized core portion 26.
  • relative sizes for laminations 23-26 can be determined so as to provide an arbitrary relationship between the circuit inductance (L) provided by the filter l4 and the DC current output (1 flowing through the winding 15.
  • the relative dimensions of the laminations 23-26 are selected to establish a relationship such that L is substantially constant over the range of output current values desired at the output terminal 17.
  • relatively uniform ratio exists between the actual inductance provided by winding and the critical inductance I.., required by the filter circuit 14. This is possible because, as noted above, the critical inductance L also varies inversely with current flow through the inductance winding. Because of the substantially constant ratio, the value of inductance provided by the winding 15 need not be greater than necessary at high-current values. The above-described design criteria are therefore altered and the requirement for an oversized inductance element is eliminated.
  • FIG. 4 illustrates another variable inductance embodiment of the invention.
  • a winding 31 is coiled on a magnetic core 32 that includes a main C-shaped section 33 and a longitudinal portion 34 of reduced cross section. Separating the longitudinal portion 34 from the C-shaped section 33 are a pair of primary airgaps 35 and 36.
  • the cross-sectional area of the spool-shaped core portion 34 varies between maximum and minimum values. The maximum value exists at its terminal faces 37 and 38 directly adjacent the airgaps 35 an 36 and the minimum value exists at its midsection 39.
  • FIG. 4 The operation and construction of the embodiment shown in FIG. 4 is similar to that described above in connection with FIGS. 1-3. However, in this case an auxiliary gap 41 is formed in the annular volume surrounding the spool-shaped core piece 34 in response to currentmagnitudes in the winding 31 that saturate the core portion corresponding to the reduced cross section at the midsection 39.
  • the auxiliary airgap 41 that accommodates fringe flux emanating from the spool-shaped core piece 34 is in series with the primary airgaps 35 and 36 rather than in parallel therewith as in the embodiment of FIGS. 1-3.
  • FIG. 5 is a graph comparing normalized performance characteristics of a conventional nonvariable inductance (curve A) and of a current dependent inductance according to the invention (curve B).
  • Curve A Current through the inductance is plotted on the abscissa axis and a normalized value of current x inductance value provided by the winding is plotted on the ordinate axis.
  • Both curves A and B begin at a current value corresponding to the initial saturation of the longitudinal core portion s minimum cross-sectional area 26 (FIG. 2).
  • Curve B indicates only a 40 percent variation in the value of inductance for an inductance according to the present invention.
  • a substantial improvement is made toward the desired objective of an inductance that provides a current dependent value of inductance equal to K/I.
  • the desired saturation of the reduced cross-sectional core portion can be induced by externally controlled and isolated signals.
  • different portions of a core can be constructed of materials possessing different saturation levels or B vs. II curves to achieve various desired effects.
  • An electrical inductance comprising:
  • a magnetic core having a pair of spaced-apart pole forces defining an airgap
  • an elongated spool-shaped auxiliary magnetic core section separate from said magnetic core and disposed in said airgap to provide a pair of primary airgaps as defined between said pole faces and the ends of said elongate auxiliary magnetic core section,
  • auxiliary airgap means defined by said auxiliary magnetic core section with the cross-sectional areas of said magnetic core section residing in planes perpendicular to the flux path varying between a maximum value at its end to a minimum value intermediate its ends with the annular volume surrounding the spool-shaped core section constituting an auxiliary airgap in series with said primary airp a winding on said magnetic core with terminals adapted for connection in an electrical circuit;
  • said minimum value of cross-sectional area selected to saturate at magnetic flux levels produced in said flux path by electrical currents in said winding above a given value so as to generate fringe flux in said auxiliary gap in direct dependence upon the values of current in said winding above said given value.
  • a power supply comprising:
  • a rectifier means adapted for connection to a source of AC power
  • a filter means connected to receive the output from said rectifier means
  • a current-responsive variable inductance means comprised by said filter means, said inductance means comprising;
  • a magnetic core having a pair of spaced-apart pole face defining an airgap
  • an elongate spool-shaped auxiliary magnetic core section separate from said magnetic core and disposed in said airgap to provide a pair of primary airgaps as defined between said pole faces and the ends of said elongate auxiliary magnetic core section,
  • auxiliary airgap means defined by said auxiliary magnetic core section with the cross-sectional areas of said auxiliary magnetic core section residing in planes perpendicular to the flux path varying between a maximum value at its said auxiliary airgap means defined by said varying crosssectional areas providing a variable inductance value which is equal to or greater than the critical inductance of said filter means.
  • auxiliary airgap means defined by said varying cross-sectional areas provides a variable inductance substantially equal to K/l over a predetermined current operating range of said power supply wherein K is a constant and I is the value of DC output current from said filter means.

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Abstract

A current dependent variable inductance having a winding and flux coupled magnetic core portion with cross-sectional areas that vary between maximum and minimum values in planes perpendicular to the flux path. Current flow of greater than a given magnitude in the winding causes saturation of the minimum core area and generation of fringing flux in an adjacent auxiliary airgap. The lengths of the fringing flux lines and accordingly of the auxiliary airgap vary directly with the saturation current in the winding. Thus, the value of inductance provided by the winding varies inversely with that current.

Description

States Patent [72] Inventor Sherwood Thaler Lexington, Mass. [21 Appl. No. 889,555 [22] Filed Dec.3l, 1969 [45} Patented Sept. 7, 1971 [73] Assignee The United States of America as represented by the Administrator of the National Aeronautics and Space Administration [54] CURRENT DEPENDENT FILTER INDUCTANCE Primary Examiner-Lee T. Hix
Assistant Examiner--A. D. Pellinen Attorneys-John R. Manning, Marvin J. Mamock and Marvin F. Matthews 3 Claims, 5 Drawing Figs.
ABSTRACT: A current dependent variable inductance having U.S. a and flux coupled magnetic core portion cross. 336/178 sectional areas that vary betweenmaximum and minimum [5 it. values in planes perpendicular to the flux Current flow of greater than a given magnitude in the winding causes satu- [50] Field of Search 321/10; ration f the minimum core area and generation f f i i 323/1, 6; 336/165, 1 flux in an adjacent auxiliary airgap. The lengths of the fringing flux lines and accordingly of the auxiliary airgap vary directly [56] References CIM with the saturation current in the winding. Thus, the value of UNITED STATES PATENTS inductance provided by the winding varies inversely with that 2,015,534 9/1935 Rose 321/10 X current.
(NORMALIZED IN PATENTEDSEP ns-m 3.603864 SHEET 2 [IF 2 A-CONVENTIONAL B-IMPROVED CONSTRUCTION IOO- I E l E 80" I g I i so-- I m I A 2 I 4 40"- s I D I o g 20-- l immu'wum 4 5 DESIGN CURRENT (AMPS) CURRENT INVENTOR= SHERWOOD THALER,
ATTORNEYS CURRENT DEPENDENT FILTER INDUCTANCE ORIGIN OF THE INVENTION The invention described herein was made by an employee of the United States Government and may be manufactured and'used by or for the government for governmental purposes without the payment of any royalties thereon or therefor.
BACKGROUND OF THE INVENTION This invention relates to a current dependent variable inductance and is specifically suited for use as an inductive element in input filter chokes of AC or DC power supplies.
In the design of filter circuits for AC-DC power supplies, it is customary to minimize the value of inductance so as to reduce the weight and cost of the inductance element required. Optimum performance in the way of regulation, however, is realized only if the inductance value is equal to or greater than the circuit's critical inductance. This .is the inductance value required to prevent current from decreasing to zero during any part of the cycle. Critical inductance (L is a well-known phenomenon discussed in Reference Data for Radio Engineers (3rd ed.), pages 183-185, 1949, Knickerbocker Printing Company, N.Y., N.Y., and for a particular configuration is equal to K/I where K is a constant and I is the DC output current. Thus, L is a variable having a maximum value determined by the minimum level of output current and corresponding to the minimum inductance value required for optimum filter circuit performance. Conversely, the inductance elements current-carrying requirements which also effect weight and cost must be determined by the maximum value of DC output current. Because of these designs criteria, the typical nonvariable inductance element of an input choke filter provides an unnecessarily large value of inductance for high output current levels and an unnecessarily large current rating for low output current levels.
Attempts to alleviate the above problem have resulted in many types of variable inductances for which inductance values vary inversely with current. Examples of such inductances include swinging chokes that utilize the characteristic B-I-I slope of an iron core to establish the desired variation in inductance, iron-cored inductances that include an independently energized control winding that selectively controls inductance by varying the level of magnetic flux produced, and various types of mechanically adjusted inductances in which inductance values are altered either by switching mechanisms that modify the circuit relationship between plural coils or by relative physical displacement of either inductance coils or magnetic cores. All such previous elements suffer from certain disadvantages. For example, core material may not be available with a B-H loop that will provide a swinging choke with the particular operating characteristics desired for a particular application. Externally controlled variable inductances, although offering wide ranges of operation, entail the sometimes undesirable use of separate control windings and circuits. Finally, the time delays inherently required by mechanically controlled variable inductances to effect switching or mechanical displacements are not acceptable in all applications.
The object of the invention, therefore, is to provide an improved variable inductance for use in input choke filter circuits of AC-DC power supplies.
SUMMARY OF THE INVENTION The invention is characterized by the provision of a currentdependent variable inductance that is suited particularly for use as an inductive element in choke input filters of AC-DC power supplies. The inductance comprises a winding on a magnetic core with pole pieces that define a primary airgap and establish therewith a magnetic flux path. The core further includes a longitudinal portion of reduced cross section and including cross-sectional areas in planes perpendicular to the flux path that vary between maximum and minimum values. Current flow through the winding at levels above a predetermined value induces saturation of the longitudinal core portion at the reduced cross section thereby generating fringe flux in an auxiliary gap adjacent thereto. By utilizing cross-sectional areas in the longitudinal core portion that vary in a uniform sense between the maximum and minimum values, the length of the fringe flux lines and correspondingly of the auxiliary airgap vary directly dependent upon the level of current flow in the winding above the predetermined value. Consequently, the inductance values provided by the inductance element varies inversely with current flow through its winding.
According to a featured inductance element embodiment of the above type, the varying cross section of the longitudinal core portion is selected so as to provide an inductance value substantially equal to K/I over a predetermined current operating range; where K is a constant and I,, is the value of DC output current from a choke input filter. According to this arrangement, and inductance element having a core with a selected variation in cross section can provide a current dependent variable inductance substantially equal to the input filters critical inductance over a predetermined operating range.
Another feature of the invention is provision of an electrical inductance of the above type wherein the longitudinal core portion of reduced cross section includes pole sections on opposite sides'of the primary airgap and with areas of minimum cross section directly adjacent thereto. In this case the auxiliary airgap produced by saturation of the core is parallel to the primary airgap.
Another feature of the invention is the provision of an electrical inductance of the above types wherein the pole sections of reduced cross section are formed by a plurality of magnetic laminations stacked in planes perpendicular to the flux path. The employment of stacked magnetic laminations of different size establish the variations in cross-sectional area in a simple construction and eliminates problems that would be introduced, for example, by attempts to produce the desired variable cross section by machining. Also, the thin laminations reduce eddy current losses, particularly in high-frequency applications.
DESCRIPTION OF THE DRAWINGS These and other objects and features of the invention will become more apparent upon a perusal of the following description taken in conjunction with the accompanying drawings wherein:
FIG. 1 is a schematic circuit diagram of an AC-DC power supply employing a preferred inductance element embodiment of the invention;
FIG. 2 is an enlarged view of the pole pieces shown on the inductance core of FIG. 1;
FIG. 3 is a view of one of the pole pieces shown in FIG. 2 looking in the direction of arrows 3-3;
FIG. 4 is a schematic illustration of another inductance element embodiment of the invention; and
FIG. 5 is a graph illustrating performance characteristics of a conventional inductance and of the inductance embodiment shown in FIGS. 1-3.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Shown in FIG. I is a transformer having a primary winding 11 connected to a source of AC power and a secondary winding 12 connected to a rectifier 13. The DC output of the rectifier 13 is applied to a filter circuit 14 including an inductance winding 15 and a capacitance l6. Appearing on output terminal 17 is the filtered DC output of the filter circuit 14. Supporting the inductance winding 15 is a horseshoe magnetic core 18 that provides with primary airgap 19 a path for magnetic flux generated by current in the winding 15. The core 18 includes a main section 20 that terminates with longitudinally spaced pole pieces sections 21 and 22 disposed on opposite sides of the primary airgap l9.
As shown more clearly in FIGS. 2 and 3, each of the pole pieces 21 and 22 is formed by a plurality of symmetrically stacked, square magnetic laminations 23-26 of different size. Thus, cross-sectional areas of each of the pole pieces 21 and 22 in planes perpendicular to the magnetic flux path vary between maximum and minimum values. The maximum value is established by the cross-sectional area of the main core section 20 while the minimum value is established by the smallest laminations 26 located directly adjacent the primary airgap 19. Furthermore, the laminations 23-26 are stacked in order of size so as to provide each of the pole pieces 21 and 22 with cross-sectional areas that vary in a uniform sense between the maximum and minimum values.
During operation of the power supply shown in FIG. 1, the flow of a given minimum magnitude of current through the winding 15 induces saturation of the smallest magnetic laminations 26 shown in FIG. 2. Further increases in the winding current generates fringe flux in an annular auxiliary airgap 29 surrounding the pole pieces 21 and 22 and parallel to the primary airgap 19. As the value of saturating current flow increases the length of the fringe flux lines also increase as does the effective length of the auxiliary gap 29. For example, after initial saturation of the laminations 26, the predominant portion of the fringe flux lines terminate at the edges of the laminations 25 so that the spacing therebetween establishes the length of the auxiliary gap 29. At higher saturation levels, fringe flux lines also extend between the more distantly spaced laminations 23 and 24 so as to extend the effective length of the auxiliary airgap 29. Thus, the effective length of the auxiliary airgap 29 is directly dependent upon the current flowing in the winding 15.
The value of inductance provided by the winding 15, however is inversely dependent upon the total airgap length which in this case includes both the primary airgap 19 and the auxiliary airgap 29. Consequently, the inductance value exhibited by the filter circuit 14 is inversely dependent upon the magnitude of current flowing in the winding 15 at levels above that required to saturate the minimum sized core portion 26. With appropriate analytical, empirical or experimental methods, relative sizes for laminations 23-26 can be determined so as to provide an arbitrary relationship between the circuit inductance (L) provided by the filter l4 and the DC current output (1 flowing through the winding 15. Preferably, the relative dimensions of the laminations 23-26 are selected to establish a relationship such that L is substantially constant over the range of output current values desired at the output terminal 17. In that case relatively uniform ratio exists between the actual inductance provided by winding and the critical inductance I.., required by the filter circuit 14. This is possible because, as noted above, the critical inductance L also varies inversely with current flow through the inductance winding. Because of the substantially constant ratio, the value of inductance provided by the winding 15 need not be greater than necessary at high-current values. The above-described design criteria are therefore altered and the requirement for an oversized inductance element is eliminated.
FIG. 4 illustrates another variable inductance embodiment of the invention. As shown, a winding 31 is coiled on a magnetic core 32 that includes a main C-shaped section 33 and a longitudinal portion 34 of reduced cross section. Separating the longitudinal portion 34 from the C-shaped section 33 are a pair of primary airgaps 35 and 36. Again, the cross-sectional area of the spool-shaped core portion 34 varies between maximum and minimum values. The maximum value exists at its terminal faces 37 and 38 directly adjacent the airgaps 35 an 36 and the minimum value exists at its midsection 39.
The operation and construction of the embodiment shown in FIG. 4 is similar to that described above in connection with FIGS. 1-3. However, in this case an auxiliary gap 41 is formed in the annular volume surrounding the spool-shaped core piece 34 in response to currentmagnitudes in the winding 31 that saturate the core portion corresponding to the reduced cross section at the midsection 39. Thus, in this embodiment the auxiliary airgap 41, that accommodates fringe flux emanating from the spool-shaped core piece 34 is in series with the primary airgaps 35 and 36 rather than in parallel therewith as in the embodiment of FIGS. 1-3.
FIG. 5 is a graph comparing normalized performance characteristics of a conventional nonvariable inductance (curve A) and of a current dependent inductance according to the invention (curve B). Current through the inductance is plotted on the abscissa axis and a normalized value of current x inductance value provided by the winding is plotted on the ordinate axis. Both curves A and B begin at a current value corresponding to the initial saturation of the longitudinal core portion s minimum cross-sectional area 26 (FIG. 2). As shown by curve A, the conventional inductance experiences an percent variation in inductance value over the indicated current operating range. Curve B, however, indicates only a 40 percent variation in the value of inductance for an inductance according to the present invention. Thus, a substantial improvement is made toward the desired objective of an inductance that provides a current dependent value of inductance equal to K/I.
Alternative embodiments of the invention also are possible. For example, the desired saturation of the reduced cross-sectional core portion can be induced by externally controlled and isolated signals. Additionally, different portions of a core can be constructed of materials possessing different saturation levels or B vs. II curves to achieve various desired effects.
What I claim is:
1. An electrical inductance comprising:
a magnetic core having a pair of spaced-apart pole forces defining an airgap;
an elongated spool-shaped auxiliary magnetic core section separate from said magnetic core and disposed in said airgap to provide a pair of primary airgaps as defined between said pole faces and the ends of said elongate auxiliary magnetic core section,
said magnetic core with said magnetic core section and said primary airgaps providing a magnetic flux path;
auxiliary airgap means defined by said auxiliary magnetic core section with the cross-sectional areas of said magnetic core section residing in planes perpendicular to the flux path varying between a maximum value at its end to a minimum value intermediate its ends with the annular volume surrounding the spool-shaped core section constituting an auxiliary airgap in series with said primary airp a winding on said magnetic core with terminals adapted for connection in an electrical circuit;
said minimum value of cross-sectional area selected to saturate at magnetic flux levels produced in said flux path by electrical currents in said winding above a given value so as to generate fringe flux in said auxiliary gap in direct dependence upon the values of current in said winding above said given value.
2. A power supply comprising:
a rectifier means adapted for connection to a source of AC power;
a filter means connected to receive the output from said rectifier means;
a current-responsive variable inductance means comprised by said filter means, said inductance means comprising;
a magnetic core having a pair of spaced-apart pole face defining an airgap;
an elongate spool-shaped auxiliary magnetic core section separate from said magnetic core and disposed in said airgap to provide a pair of primary airgaps as defined between said pole faces and the ends of said elongate auxiliary magnetic core section,
said magnetic core with said magnetic core section and said primary airgaps providing a magnetic flux path;
auxiliary airgap means defined by said auxiliary magnetic core section with the cross-sectional areas of said auxiliary magnetic core section residing in planes perpendicular to the flux path varying between a maximum value at its said auxiliary airgap means defined by said varying crosssectional areas providing a variable inductance value which is equal to or greater than the critical inductance of said filter means.
3. The invention as described in claim 1,
wherein said auxiliary airgap means defined by said varying cross-sectional areas provides a variable inductance substantially equal to K/l over a predetermined current operating range of said power supply wherein K is a constant and I is the value of DC output current from said filter means.

Claims (3)

1. An electrical inductance comprising: a magnetic core having a pair of spaced-apart pole forces defining an airgap; an elongated spool-shaped auxiliary magnetic core section separate from said magnetic core and disposed in said airgap to provide a pair of primary airgaps as defined between said pole faces and the ends of said elongate auxiliary magnetic core section, said magnetic core with said magnetic core section and said primary airgaps providing a magnetic flux path; auxiliary airgap means defined by said auxiliary magnetic core section with the cross-sectional areas of said magnetic core section residing in planes perpendicular to the flux path varying between a maximum value at its end to a minimum value intermediate its ends with the annular volume surrounding the spool-shaped core section constituting an auxiliary airgap in series with said primary airgaps; a winding on said magnetic core with terminals adapted for connection in an electrical circuit; said minimum value of cross-sectional area selected to saturate at magnetic flux levels produced in said flux path by electrical currents in said winding above a given value so as to generate fringe flux in said auxiliary gap in direct dependence upon the values of current in said winding above said given value.
2. A power supply comprising: a rectifier means adapted for connection to a source of AC power; a filter means connected to receive the output from said rectifier means; a current-responsive variable inductance means comprised by said filter means, said inductance means comprising; a magnetic core having a pair of spaced-apart pole face defining an airgap; an elongate spool-shaped auxiliary magnetic core section separate from said magnetic core and disposed in said airgap to provide a pair of primary airgaps as defined between said pole faces and the ends of said elongate auxiliary magnetic core section, said magnetic core with said magnetic core section and said primary airgaps providing a magnetic flux path; auxiliary airgap means defined by said auxiliary magnetic core section with the cross-sectional areas of said auxiliary magnetic core section residing in planes perpendicular to the flux path varying between a maximum value at its end to a minimum value intermediate its ends with the annular volume surrounding the spool-shaped core section constituting an auxiliary airgap in series with said primary airgaps; a winding on said magnetic core with terminals adapted for connection in an electrical circuit; said minimum value of cross-sectional area selected to saturate at magnetic flux levels produced in said flux path by electrical currents in said winding above a given value so as to generate fringe flux in said auxiliary airgap in direct dependence upon the value of current in said winding above said given value, said auxiliary airgap means defined by said varying cross-sectional areas providing a variable inductance value which is equal to or greater than the critical inductance of said filter means.
3. The invention as described in claim 1, wherein said auxiliary airgap means defined by said varying cross-sectional areas provides a variable inductance substantially equal to K/I over a predetermined current operating range of said power supply wherein K is a constant and I is the value of DC output current from said filter means.
US889555A 1969-12-31 1969-12-31 Current dependent filter inductance Expired - Lifetime US3603864A (en)

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Cited By (14)

* Cited by examiner, † Cited by third party
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US3868561A (en) * 1973-03-30 1975-02-25 Aeg Elotherm Gmbh Resonant circuit transformer
US3894279A (en) * 1974-01-04 1975-07-08 Gen Electric Apparatus for synchronous smoothing of current ripple
US4282567A (en) * 1976-10-26 1981-08-04 Texas Instruments Incorporated Modified power transformer for self-oscillating converter regulator power supply
US4293905A (en) * 1979-06-18 1981-10-06 Power Control Corporation Method and apparatus for controlling power and optimizing power factor in an AC-to-DC converter
EP0107266A1 (en) * 1982-07-06 1984-05-02 Northern Telecom Limited Output filter having swinging inductor
US4728918A (en) * 1984-09-24 1988-03-01 Siemens Aktiengesellschaft Storage coil with air gap in core
US5177433A (en) * 1990-01-23 1993-01-05 Siemens Aktiengesellschaft Current-voltage transformer for electronic house-service meter
US5440225A (en) * 1992-02-24 1995-08-08 Toko Kabushiki Kaisha Core for coil device such as power transformers, choke coils used in switching power supply
US6657528B1 (en) * 2000-08-25 2003-12-02 Astec International Limited Slope gap inductor for line harmonic current reduction
GB2463503A (en) * 2008-09-16 2010-03-17 Cambridge Semiconductor Ltd Crossed ridges in a gap of a ferrite core arrangement
US20110199174A1 (en) * 2010-02-18 2011-08-18 Carsten Bruce W Inductor core shaping near an air gap
US20150109086A1 (en) * 2013-10-21 2015-04-23 Industry-Academic Cooperation Foundation Gyeongsang National University Core and coil component including the same
US20150302982A1 (en) * 2013-09-03 2015-10-22 U.S. Army Research Laboratory Attn: Rdrl-Loc-I Mems tunable inductor
WO2021099724A1 (en) 2019-11-21 2021-05-27 Commissariat A L'energie Atomique Et Aux Energies Alternatives Electromagnetic induction device

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US2015534A (en) * 1933-05-27 1935-09-24 Westinghouse Electric & Mfg Co Filter system for mercury-arc rectifiers
US2025093A (en) * 1932-10-26 1935-12-24 United American Bosch Corp Inductance device
US2413108A (en) * 1945-03-14 1946-12-24 Stromberg Carlson Co Recording and reproducing head for magnetic recording
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US3143686A (en) * 1962-08-14 1964-08-04 Rca Corp Flyback transformer and transistorized deflection circuit

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US2025093A (en) * 1932-10-26 1935-12-24 United American Bosch Corp Inductance device
US2015534A (en) * 1933-05-27 1935-09-24 Westinghouse Electric & Mfg Co Filter system for mercury-arc rectifiers
US2413108A (en) * 1945-03-14 1946-12-24 Stromberg Carlson Co Recording and reproducing head for magnetic recording
US2469266A (en) * 1946-08-14 1949-05-03 Indiana Steel Products Co Magnetic transducer having an irregular nonmagnetic gap
US2585932A (en) * 1948-07-29 1952-02-19 Magnetic Equipment Inc Device for reducing noise in magnetic recording systems
US3143686A (en) * 1962-08-14 1964-08-04 Rca Corp Flyback transformer and transistorized deflection circuit

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3868561A (en) * 1973-03-30 1975-02-25 Aeg Elotherm Gmbh Resonant circuit transformer
US3894279A (en) * 1974-01-04 1975-07-08 Gen Electric Apparatus for synchronous smoothing of current ripple
US4282567A (en) * 1976-10-26 1981-08-04 Texas Instruments Incorporated Modified power transformer for self-oscillating converter regulator power supply
US4293905A (en) * 1979-06-18 1981-10-06 Power Control Corporation Method and apparatus for controlling power and optimizing power factor in an AC-to-DC converter
EP0107266A1 (en) * 1982-07-06 1984-05-02 Northern Telecom Limited Output filter having swinging inductor
US4728918A (en) * 1984-09-24 1988-03-01 Siemens Aktiengesellschaft Storage coil with air gap in core
US5177433A (en) * 1990-01-23 1993-01-05 Siemens Aktiengesellschaft Current-voltage transformer for electronic house-service meter
US5440225A (en) * 1992-02-24 1995-08-08 Toko Kabushiki Kaisha Core for coil device such as power transformers, choke coils used in switching power supply
US6657528B1 (en) * 2000-08-25 2003-12-02 Astec International Limited Slope gap inductor for line harmonic current reduction
GB2463503A (en) * 2008-09-16 2010-03-17 Cambridge Semiconductor Ltd Crossed ridges in a gap of a ferrite core arrangement
US20100085138A1 (en) * 2008-09-16 2010-04-08 Cambridge Semiconductor Limited Crossed gap ferrite cores
US8035472B2 (en) 2008-09-16 2011-10-11 Cambridge Semiconductor Limited Crossed gap ferrite cores
US20110199174A1 (en) * 2010-02-18 2011-08-18 Carsten Bruce W Inductor core shaping near an air gap
US8466766B2 (en) * 2010-02-18 2013-06-18 Peregrine Power, Llc Inductor core shaping near an air gap
US20150302982A1 (en) * 2013-09-03 2015-10-22 U.S. Army Research Laboratory Attn: Rdrl-Loc-I Mems tunable inductor
US9583250B2 (en) * 2013-09-03 2017-02-28 The United States Of America As Represented By The Secretary Of The Army MEMS tunable inductor
US20150109086A1 (en) * 2013-10-21 2015-04-23 Industry-Academic Cooperation Foundation Gyeongsang National University Core and coil component including the same
WO2021099724A1 (en) 2019-11-21 2021-05-27 Commissariat A L'energie Atomique Et Aux Energies Alternatives Electromagnetic induction device
FR3103624A1 (en) 2019-11-21 2021-05-28 Commissariat A L'energie Atomique Et Aux Energies Alternatives electromagnetic induction device

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