[go: up one dir, main page]

US2234002A - Temperature compensated magnetic core inductor - Google Patents

Temperature compensated magnetic core inductor Download PDF

Info

Publication number
US2234002A
US2234002A US238025A US23802538A US2234002A US 2234002 A US2234002 A US 2234002A US 238025 A US238025 A US 238025A US 23802538 A US23802538 A US 23802538A US 2234002 A US2234002 A US 2234002A
Authority
US
United States
Prior art keywords
coil
inductance
core
magnetic core
temperature
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US238025A
Inventor
Robert L Harvey
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RCA Corp
Original Assignee
RCA Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by RCA Corp filed Critical RCA Corp
Priority to US238025A priority Critical patent/US2234002A/en
Application granted granted Critical
Publication of US2234002A publication Critical patent/US2234002A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F27/00Details of transformers or inductances, in general
    • H01F27/008Details of transformers or inductances, in general with temperature compensation

Definitions

  • This invention relates to magnetic core inductance devices for use in radio and' other systems for the communication of intelligence and has special reference to the provision of improvements in magnetic core inductors for tuned circuits designed to .be operated at a predetermined fixed frequency.
  • An object of the present invention is to provide a magnetic core inductor which shall exhibit a. substantially zero temperature coeilicient of inductance or' a temperature ceefilcient of inductance of either sign and of a desired low value.
  • Another object of the invention is to provide a low loss intermediate or high frequency magnetic core inductor and one characterized by a high degree of stability irrespective of aging and varying conditions of temperature and humidity.
  • Another object of the invention is to provide a magnetic core inductor wherein the effect of changes in the diameter and in the spacing of the turns of the inductor or due to miscellaneous changes in external circuit components, caused compensating changes in the relative position of the coil with respect to the core.
  • Still another objectl of the invention is to provide a simple, inexpensive, trouble-free temperature compensated magnetic core inductor and one which lends itself readily to mass production methods.
  • Figure 2 is a side elevational view of a magnetic core coupling unit, and form therefor, constructed in accordance with the invention
  • Figure 3 is a diagram of two magnetically coupled circuits which will be referred to in explaining the invention.
  • Figure 4 is a chart comparing the operating characteristics of the device of Fig. 2 with prior art devices.
  • Figure 5 is a chart showing the'eiect -of the thickness of the coil form of Figs. 1 and 2 upon the temperature-inductance characteristic.
  • a magnetic core is presented to the interior of a coil which is mounted upon the outer surface of a hollow form comprising an insulating substance which has a very large coeicient of expansion.
  • the magnetic core is maintained in a fixed position within the core so that, when the device is subjected to increased temperatures, the n form expands and the coil is moved with respect to the magnetic core to thereby compensatev for changes in the inductance of the coil incident to the expansion and elongation of its turns.
  • substantially any desired low temperature coelcient of inductance may be achieved simply by varying the length and thickness of the coil form or by altering the position of the coil'thereon.
  • the material of which the coil form is constituted should be substantially immune to moisture and should possess certain other desirable mechanical and electrical properties.
  • polystyrene (or polystyrol, as it is sometimes called) meets all of the above requirements and, further, is inexpensive both as to its initial cost and cost of processing.
  • F designates generally a hollow form made of polystyrene, upon the outer surface of which an inductance coil L is wound or mounted in any suitable manner.
  • Form F is preferably provided with an integral'mounting flange f adjacent an end thereof.
  • a magnetic core M which is preferably constituted of comminuted insulated granules of the ore magnetite or of powdered iron, molded in a known manner.
  • the diameter of the core M is such as to give it a sliding nt within thebore of the form F when a moving force is exerted thereon as through a threaded brass or like rod R.
  • One end of the threaded rod R is preferably embedded in the core material during the molding operation and its free end extends through a threaded knurled metal bushing B which is force fitted into the otherwise open end of the coil form F.
  • a threaded knurled metal bushing B which is force fitted into the otherwise open end of the coil form F.
  • the end of the coil form may be softened by preheating prior to receiving the knurled end of the bushing B.
  • 'I'he bushing B may be bifurcated as indicated at b to cause it to grip the rod R and thereby prevent undesired movement of the core L within the cylinder F once its position has been fixed.
  • vAs in prior art, magnetic core inductors, the relative position of the core and coil determines the edective inductance of the coil, thus, maximum inductance is achieved when the core is entirely within the coil.
  • the coil form F is constituted of a material which has a large coeiiicient of expansion.
  • the coil form is made of polystyrene, its coeiiicient of linear expansion is substantially six times that of the meftal (i. e., brass) of which the adjusting rod R and bushing B are formed. Accordingly, when the coil form is subjected to an increase in temperature, it will expand and be elongated to a much greater extent than the bushing B and .the rod R to which the core C is afiixed.
  • the degree of compensation is a function of the distance between the centerline of the bushing or stud-support B and the center line of the coil L, i. e., distance :r in Fig. 1
  • substantially any desired degree and sign of compensation may be achieved by simply altering the mechanical length of the form and the position of the coil thereon.
  • the general rule is the greater the value of 1:, the more negative the temperature coeflicient of inductance.
  • the degree of compensation may also be controlled to a useful extent by altering the thickness dimension of the coil form and by using materials having a coefficient of expansion other than that of brass for the bushing B and adjusting rod R..
  • Fig. 2 shows a high frequency coupling unit constructed in accordance with lthe principle of the invention.
  • the coil form F here comprises a hollow cylinder constituted of polystyrene and provided with outwardly extending flanges f1, i, one at each end of the cylinder.
  • flanges f1 i, one at each end of the cylinder.
  • One of these flanges, say flange f2 is preferably provided with orifices O which receive mounting studs s for attachment to the chassis base of a radio receiver, in which case the opposite end of the form is left free to permit of unrestrained expansion and contraction due to temperature changes.
  • the opposed surfaces of the flanges l1, P may each be used for mounting fixed capacitors C1 C2 and terminal elements tl t1l through which connections may be made tothe circuits with which the device is to be associated.
  • the conductor w which serves to connect upper capacitor Cl rto the bottom terminal t* may be provided with a slack portion w1 to prevent the application of any restraining force to the coil form when it is elon ⁇ gated due to increased temperatures.
  • a primary coil Ll and a secondary coil L2 are mounted in suitably spaced energy transfer relation on the outer surface of the coil form.
  • Each coil is provided with a magnetic core M1, M1, respectively, mounted for slidable movement, as described in connection with Fig. l, within the bore of the cylindrical form F.
  • Fig 3 shows, symbolically, a coupling device of the type described in connection with Fig. 2 suitably connected in the intermediate frequency amplifying stages of a superheterodyne receiver.
  • 'I'he primary winding L1 has the fixed capacitor C1 connected across its terminals and the resonant circuit thus formed is connected to the plate p1 of a thermionic amplifier v1.
  • the secondary winding L2 of the coupling unit has the fixed capacitor C2 connected across its terminals and the resonant circuit thus formed is connected to the input electrode a of the amplifier v2.
  • the inductance As previously described, and as indicated by the ⁇ conventional symbols in Fig. 3, the inductance,
  • I PCn may be adjusted by relative movement of the cores M1, M2 with respect to the coils individual thereto.
  • the combined temperature characteristic of the tube, capacitor, wiring, etc., of the circuit should first be determined. This will usually be found to be of positive value. The proper value of :r (see Fig. 1) to exactly compensate for such temperature characteristic should then be determined and the coupling unit designed with this value in mind.
  • Curve L shows how the inductance of a unit, constructed in accordance with the invention, changes when the position of its magnetic core is altered. At zero, on the bottom scale, the core is in register with the coil (i. e., completely within the coil). Between the limits 4/16 and 6/16", read on the same scale, the change in inductance is maximum, that is Vto say, the greatest change of inductance is achieved for a given movement of the core when it moves between the limits.
  • Curve A shows the temperature-inductance characteristic of a unit having a coil form constructed of a phenolic compound is of a positive sign throughout the entire range of movement of the core.
  • Curves B and C show the temperature inductance characteristic of two magnetic core inductors having coil forms constituted of polystyrene. The only physical difference between these two units is in their value of 1: (see Fig. 1). It will be noted in connection with both curves B and C that their minimum slope occurs between the same range (i. e., 4/16" to 6/16") that the maximum change in inductance (curve L) occurs.
  • Fig. 5 shows how the thickness of the coil form affects the temperature compensation when the core is within the working range shown in Fig. 4. Referring to Fig. 5, it will be noted that it is possible to have a Zero or any reasonable positive or negative temperature-inductance characteristic by simply altering the thickness dimension of the form upon which the coil is mounted.
  • a temperature compensated inductor comprising a coil form, a coil mounted on said form, a. magnetic core for altering the eiective inductance of said coil mounted for movement adjacent said coil and form, adjustable means for maintaining said core in a relatively fixed position with respect to said coil, said form being constituted of an insulating substance having a temperature coefficient of expansion which is relatively large with respect to the temperature coeilicient of expansion of said adjustable means and having its length so proportioned with respect to its mass that 'when it is subject to temperature changes it will cause that degree and direction of movement between said coil and core required to produce a desired change in the eiective inductance of said coil.
  • a temperature compensated inductor comprising a hollow cylindrical form, a coil mounted on the outer surface of said form remote from an end thereof, a magnetic core mounted for slidable movement within said form, adjustable means for maintaining said core in a relatively xed position with respect to said end of said form, said form being constituted of an insulating substance having a coefficient of linear expansion substantially greater than that of said first-mentioned means whereby said coil is moved with respect to said core when said form is subjected to variations in temperature.
  • a temperature compensated inductor comprising a hollow cylinder constituted essentially of polystyrene, a coil intimately secured to the outer surface of said cylinder, a magnetic core within said cylinder, and means comprising a rod connected to said core and a bushing connected to said cylinder for moving said core with respect to said coil, said rod and bushing having a coefficient of linear expansion which is substantially less than that of the material of which said coil form is constituted.
  • a device for coupling two tuned circuits comprising a coil form constituted essentially of polystyrene, primary and secondary coils mounted in energy transfer relation on said coil form, magnetic cores individual tosaid coils for regulating the eiective inductancethereof, means secured to said form and having a temperature coefficient of linear expansion substantially less than that of polystyrene for relatively moving said cores with respect to said coils over a range of movement calculated to produce a maximum change of inductance in said coils, the dimensions of said coil form and the relative positions of said coils thereon being so chosen that said device exhibits a temperature coeilicient of inductance of a desired sign and value over said range of maximum change in inductance.
  • a temperature compensated inductor comprising a coil form, a coil mounted on said form, a magnetic core mounted for movement adjacent said form and coil, means mounted on said form for adjusting the position of said core with respect to said coil whereby to change the effective inductance of said coil, said form being constituted of an insulating substance having a coeiicient of linear expansion substantially greater than that of said core adjusting means, whereby said coil is moved with respect to said core when said form is subject to variations in temperature.
  • a temperature compensated inductor comprising a coil form constituted of an insulating substance having a coemcient of linear expansion of the order of 65-102X10-8, a coil mounted on said form remote from an end thereof, a magnetic core for regulating the effective inductance of said coil, means supported adjacent said end of said form and having a substantially lower coe'icient of expansion than said insulating material for moving said core with respect to said coil over a range of movement calculated to produce a maximum change of inductance in said coil, the dimensions of said coil form and the position of said coil with respect to said end of said form being so chosen that said device exhibits a temperature coefiicient of inductance of a desired signv and value over said range of maximum change in inductance.

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Coils Or Transformers For Communication (AREA)

Description

March 4, 1941. R, L, HARVEY 2,234,002
TEMPERATURE COMPENSATED MAGNETIC CORE INDUCTOR Filed Oct. 5l, 1938 CENTER L/NL' 0F co/L F 4 fm1 L -lao y +a- 9a Suventor .Patented Mar. 4, 1941 UNITED sTATEs TEMPERATRE COMPENSATED MAGNETIC CORE INDUCTOR Robert L; Harvey, oaklyn, N. J., asignor to naar Corporation of America, a corporation of Dela- Ware Application October 31, 1938, Serial No. 238,025
s claims.
This invention relates to magnetic core inductance devices for use in radio and' other systems for the communication of intelligence and has special reference to the provision of improvements in magnetic core inductors for tuned circuits designed to .be operated at a predetermined fixed frequency.
While the invention will be described as applied to coupling units designed for use in the intermediate frequency stages of a superheterodyne radio receiver, it will be understood that the disclosure in this respect is merely illustrative for purposes ofexplaining the inventive concept.
An object of the present invention is to provide a magnetic core inductor which shall exhibit a. substantially zero temperature coeilicient of inductance or' a temperature ceefilcient of inductance of either sign and of a desired low value.
Another object of the invention is to provide a low loss intermediate or high frequency magnetic core inductor and one characterized by a high degree of stability irrespective of aging and varying conditions of temperature and humidity.
Another object of the invention is to provide a magnetic core inductor wherein the effect of changes in the diameter and in the spacing of the turns of the inductor or due to miscellaneous changes in external circuit components, caused compensating changes in the relative position of the coil with respect to the core.
Still another objectl of the invention is to provide a simple, inexpensive, trouble-free temperature compensated magnetic core inductor and one which lends itself readily to mass production methods.
Other objects and advantages, together with certain details of construction, will be apparent and the invention itself will be best understood by reference to the following specification and to the accompanying drawing, wherein- Figure 1 is an enlarged longitudinal sectional View of so much of a magnetic core inductor as is necessary for an understanding of the principle of the invention;
Figure 2 is a side elevational view of a magnetic core coupling unit, and form therefor, constructed in accordance with the invention;
Figure 3 is a diagram of two magnetically coupled circuits which will be referred to in explaining the invention;
Figure 4 is a chart comparing the operating characteristics of the device of Fig. 2 with prior art devices; and
by variations in the ambient, will be obviated by,
Figure 5 is a chart showing the'eiect -of the thickness of the coil form of Figs. 1 and 2 upon the temperature-inductance characteristic.
Like vreference characters designate the same or corresponding parts in all figures.
In order to obviate changes in inductance due to changes in temperature, the prior art dictates the use of coil forms and other parts constituted of quartz and -other materials having a substantially 'tero coefficient of expansion. (See, for examp e, Marrison 1,836,808, n 1,910,957.) a d Llewellyn In accordance with the present invention, a magnetic core is presented to the interior of a coil which is mounted upon the outer surface of a hollow form comprising an insulating substance which has a very large coeicient of expansion. The magnetic core is maintained in a fixed position within the core so that, when the device is subjected to increased temperatures, the n form expands and the coil is moved with respect to the magnetic core to thereby compensatev for changes in the inductance of the coil incident to the expansion and elongation of its turns. When thematerial constituting the form is properly n chosen, substantially any desired low temperature coelcient of inductance may be achieved simply by varying the length and thickness of the coil form or by altering the position of the coil'thereon. In addition to exhibiting a large coeiiicient of expansion, the material of which the coil form is constituted should be substantially immune to moisture and should possess certain other desirable mechanical and electrical properties. v
As evidenced by the comparative table below, polystyrene (or polystyrol, as it is sometimes called) meets all of the above requirements and, further, is inexpensive both as to its initial cost and cost of processing.
In Fig. 1, F designates generally a hollow form made of polystyrene, upon the outer surface of which an inductance coil L is wound or mounted in any suitable manner. Form F is preferably provided with an integral'mounting flange f adjacent an end thereof. Presented to the interior of the form F and coil L is a magnetic core M which is preferably constituted of comminuted insulated granules of the ore magnetite or of powdered iron, molded in a known manner. The diameter of the core M is such as to give it a sliding nt within thebore of the form F when a moving force is exerted thereon as through a threaded brass or like rod R. One end of the threaded rod R is preferably embedded in the core material during the molding operation and its free end extends through a threaded knurled metal bushing B which is force fitted into the otherwise open end of the coil form F. In order to insure a tight fit the end of the coil form may be softened by preheating prior to receiving the knurled end of the bushing B. 'I'he bushing B may be bifurcated as indicated at b to cause it to grip the rod R and thereby prevent undesired movement of the core L within the cylinder F once its position has been fixed. vAs in prior art, magnetic core inductors, the relative position of the core and coil determines the edective inductance of the coil, thus, maximum inductance is achieved when the core is entirely within the coil.
As previously set forth, the coil form F is constituted of a material which has a large coeiiicient of expansion. Where, as in the instant case, the coil form is made of polystyrene, its coeiiicient of linear expansion is substantially six times that of the meftal (i. e., brass) of which the adjusting rod R and bushing B are formed. Accordingly, when the coil form is subjected to an increase in temperature, it will expand and be elongated to a much greater extent than the bushing B and .the rod R to which the core C is afiixed. Since the coil L is intimately attached to the core form F, elongation of the form will cause the coil to be moved with respect to the core M thereby altering the effective inductance of the coil no less certainly than if the core had been moved with respect to the coil by a sliding force exerted through the adjusting rod R.
As will hereinafter more fully appear. the degree of compensation is a function of the distance between the centerline of the bushing or stud-support B and the center line of the coil L, i. e., distance :r in Fig. 1 Thus substantially any desired degree and sign of compensation may be achieved by simply altering the mechanical length of the form and the position of the coil thereon. The general rule is the greater the value of 1:, the more negative the temperature coeflicient of inductance. The degree of compensation may also be controlled to a useful extent by altering the thickness dimension of the coil form and by using materials having a coefficient of expansion other than that of brass for the bushing B and adjusting rod R..
Fig. 2 shows a high frequency coupling unit constructed in accordance with lthe principle of the invention. The coil form F here comprises a hollow cylinder constituted of polystyrene and provided with outwardly extending flanges f1, i, one at each end of the cylinder. One of these flanges, say flange f2, is preferably provided with orifices O which receive mounting studs s for attachment to the chassis base of a radio receiver, in which case the opposite end of the form is left free to permit of unrestrained expansion and contraction due to temperature changes. The opposed surfaces of the flanges l1, P may each be used for mounting fixed capacitors C1 C2 and terminal elements tl t1l through which connections may be made tothe circuits with which the device is to be associated. The conductor w which serves to connect upper capacitor Cl rto the bottom terminal t* may be provided with a slack portion w1 to prevent the application of any restraining force to the coil form when it is elon` gated due to increased temperatures.
A primary coil Ll and a secondary coil L2 are mounted in suitably spaced energy transfer relation on the outer surface of the coil form. Each coil is provided with a magnetic core M1, M1, respectively, mounted for slidable movement, as described in connection with Fig. l, within the bore of the cylindrical form F.
Fig 3 shows, symbolically, a coupling device of the type described in connection with Fig. 2 suitably connected in the intermediate frequency amplifying stages of a superheterodyne receiver. 'I'he primary winding L1 has the fixed capacitor C1 connected across its terminals and the resonant circuit thus formed is connected to the plate p1 of a thermionic amplifier v1. The secondary winding L2 of the coupling unit has the fixed capacitor C2 connected across its terminals and the resonant circuit thus formed is connected to the input electrode a of the amplifier v2. As previously described, and as indicated by the `conventional symbols in Fig. 3, the inductance,
and hence the frequency of the resonant circuits LIC, I PCn may be adjusted by relative movement of the cores M1, M2 with respect to the coils individual thereto.
In constructing a coupling unit for use in a particular circuit, fthe combined temperature characteristic of the tube, capacitor, wiring, etc., of the circuit should first be determined. This will usually be found to be of positive value. The proper value of :r (see Fig. 1) to exactly compensate for such temperature characteristic should then be determined and the coupling unit designed with this value in mind.
Referring now to Fig. 4 which shows four curves A, B, C and L: Curve L shows how the inductance of a unit, constructed in accordance with the invention, changes when the position of its magnetic core is altered. At zero, on the bottom scale, the core is in register with the coil (i. e., completely within the coil). Between the limits 4/16 and 6/16", read on the same scale, the change in inductance is maximum, that is Vto say, the greatest change of inductance is achieved for a given movement of the core when it moves between the limits. Curve A shows the temperature-inductance characteristic of a unit having a coil form constructed of a phenolic compound is of a positive sign throughout the entire range of movement of the core. Curves B and C show the temperature inductance characteristic of two magnetic core inductors having coil forms constituted of polystyrene. The only physical difference between these two units is in their value of 1: (see Fig. 1). It will be noted in connection with both curves B and C that their minimum slope occurs between the same range (i. e., 4/16" to 6/16") that the maximum change in inductance (curve L) occurs.
Assuming now as a specific example that the tube, capacitor and wiring of one of the circuits (i. e., primary or secondary) of Fig. 3 has been found to exhibit a temperature-capacitance characteristic of +.2%. It is obvious that to achieve a circuit having -a zero temperature-frequency characteristic the inductor must exhibit a tem- ISU perature coeiiicient of inductance of -.2%. Reierring, therefore, to curve B of Fig. 4, we nd that this temperature-inductance characteristic (as read on the left-hand scale) is achieved when the value of (Fig. l) is substantially "V8".
In the above example, it is assumed that the thickness of the coil form is substantially of an inch. Fig. 5 shows how the thickness of the coil form affects the temperature compensation when the core is within the working range shown in Fig. 4. Referring to Fig. 5, it will be noted that it is possible to have a Zero or any reasonable positive or negative temperature-inductance characteristic by simply altering the thickness dimension of the form upon which the coil is mounted.
Various modifications of the invention will be apparent to those skilled in the art. It is to be understood, therefore, that the foregoing is to be interpreted as illustrative and not in a limiting sense except as required by the prior art, and by the spirit of the appended claims.
What is claimed is:
i. A temperature compensated inductor comprising a coil form, a coil mounted on said form, a. magnetic core for altering the eiective inductance of said coil mounted for movement adjacent said coil and form, adjustable means for maintaining said core in a relatively fixed position with respect to said coil, said form being constituted of an insulating substance having a temperature coefficient of expansion which is relatively large with respect to the temperature coeilicient of expansion of said adjustable means and having its length so proportioned with respect to its mass that 'when it is subject to temperature changes it will cause that degree and direction of movement between said coil and core required to produce a desired change in the eiective inductance of said coil.
2. A temperature compensated inductor comprising a hollow cylindrical form, a coil mounted on the outer surface of said form remote from an end thereof, a magnetic core mounted for slidable movement within said form, adjustable means for maintaining said core in a relatively xed position with respect to said end of said form, said form being constituted of an insulating substance having a coefficient of linear expansion substantially greater than that of said first-mentioned means whereby said coil is moved with respect to said core when said form is subjected to variations in temperature.
3. The invention as set forth in claim 1 and wherein said core-adjusting means is comprised of brass and said form is constituted essentially of polystyrene.
4. A temperature compensated inductor comprising a hollow cylinder constituted essentially of polystyrene, a coil intimately secured to the outer surface of said cylinder, a magnetic core within said cylinder, and means comprising a rod connected to said core and a bushing connected to said cylinder for moving said core with respect to said coil, said rod and bushing having a coefficient of linear expansion which is substantially less than that of the material of which said coil form is constituted.
5. A device for coupling two tuned circuits, said device comprising a coil form constituted essentially of polystyrene, primary and secondary coils mounted in energy transfer relation on said coil form, magnetic cores individual tosaid coils for regulating the eiective inductancethereof, means secured to said form and having a temperature coefficient of linear expansion substantially less than that of polystyrene for relatively moving said cores with respect to said coils over a range of movement calculated to produce a maximum change of inductance in said coils, the dimensions of said coil form and the relative positions of said coils thereon being so chosen that said device exhibits a temperature coeilicient of inductance of a desired sign and value over said range of maximum change in inductance.
6. A temperature compensated inductor comprising a coil form, a coil mounted on said form, a magnetic core mounted for movement adjacent said form and coil, means mounted on said form for adjusting the position of said core with respect to said coil whereby to change the effective inductance of said coil, said form being constituted of an insulating substance having a coeiicient of linear expansion substantially greater than that of said core adjusting means, whereby said coil is moved with respect to said core when said form is subject to variations in temperature.
7. The invention as set forth in claim 6 and wherein said core adjusting means is comprised of metal and said coil form is constituted essentially of polystyrene.
8. A temperature compensated inductor comprising a coil form constituted of an insulating substance having a coemcient of linear expansion of the order of 65-102X10-8, a coil mounted on said form remote from an end thereof, a magnetic core for regulating the effective inductance of said coil, means supported adjacent said end of said form and having a substantially lower coe'icient of expansion than said insulating material for moving said core with respect to said coil over a range of movement calculated to produce a maximum change of inductance in said coil, the dimensions of said coil form and the position of said coil with respect to said end of said form being so chosen that said device exhibits a temperature coefiicient of inductance of a desired signv and value over said range of maximum change in inductance.
ROBERT L. HARVEY.
US238025A 1938-10-31 1938-10-31 Temperature compensated magnetic core inductor Expired - Lifetime US2234002A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US238025A US2234002A (en) 1938-10-31 1938-10-31 Temperature compensated magnetic core inductor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US238025A US2234002A (en) 1938-10-31 1938-10-31 Temperature compensated magnetic core inductor

Publications (1)

Publication Number Publication Date
US2234002A true US2234002A (en) 1941-03-04

Family

ID=22896177

Family Applications (1)

Application Number Title Priority Date Filing Date
US238025A Expired - Lifetime US2234002A (en) 1938-10-31 1938-10-31 Temperature compensated magnetic core inductor

Country Status (1)

Country Link
US (1) US2234002A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2437345A (en) * 1943-02-13 1948-03-09 Zenith Radio Corp Temperature compensated variable inductance
US2489645A (en) * 1947-06-03 1949-11-29 United Air Lines Inc Method and tool for tuning closely coupled circuits
US2717364A (en) * 1951-02-05 1955-09-06 Collins Radio Co Temperature compensation of permeability tuned circuits
US2869087A (en) * 1954-04-23 1959-01-13 Cgs Lab Inc Magnetic apparatus
US2954538A (en) * 1956-05-15 1960-09-27 Avco Mfg Corp Temperature compensated permeabilitytuned inductor
DE1096436B (en) * 1956-03-01 1961-01-05 Max Braun Fa Temperature-independent high-frequency coil with a highly permeable core
DE975398C (en) * 1943-02-24 1961-11-16 Porzellanfabrik Kahla Self-induction coil with adjustable inductance and adjustable temperature coefficient of inductance, especially for high frequency purposes
US3183126A (en) * 1960-04-19 1965-05-11 Physical Sciences Corp Method of making magnetic transducers
US4639697A (en) * 1984-09-13 1987-01-27 Raytheon Company Temperature compensation circuitry
US20230386724A1 (en) * 2019-06-04 2023-11-30 Lrt Sensors Llc Temperature insensitive inductor

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2437345A (en) * 1943-02-13 1948-03-09 Zenith Radio Corp Temperature compensated variable inductance
DE975398C (en) * 1943-02-24 1961-11-16 Porzellanfabrik Kahla Self-induction coil with adjustable inductance and adjustable temperature coefficient of inductance, especially for high frequency purposes
US2489645A (en) * 1947-06-03 1949-11-29 United Air Lines Inc Method and tool for tuning closely coupled circuits
US2717364A (en) * 1951-02-05 1955-09-06 Collins Radio Co Temperature compensation of permeability tuned circuits
US2869087A (en) * 1954-04-23 1959-01-13 Cgs Lab Inc Magnetic apparatus
DE1096436B (en) * 1956-03-01 1961-01-05 Max Braun Fa Temperature-independent high-frequency coil with a highly permeable core
US2954538A (en) * 1956-05-15 1960-09-27 Avco Mfg Corp Temperature compensated permeabilitytuned inductor
US3183126A (en) * 1960-04-19 1965-05-11 Physical Sciences Corp Method of making magnetic transducers
US4639697A (en) * 1984-09-13 1987-01-27 Raytheon Company Temperature compensation circuitry
US20230386724A1 (en) * 2019-06-04 2023-11-30 Lrt Sensors Llc Temperature insensitive inductor

Similar Documents

Publication Publication Date Title
US2234002A (en) Temperature compensated magnetic core inductor
US2391038A (en) Electrical device
US1913978A (en) Inductance and capacity
US2182071A (en) Adjustable coupling system
US2354365A (en) Coupling device for adjustable coupling systems
US2630560A (en) Radio-frequency transformer
US2173908A (en) Temperature compensated high-q lines or circuits
US2489114A (en) Variable inductance device
US2168351A (en) Adjustable magnetic-core inductor
US2346584A (en) Coupling device
US2645718A (en) Variable inductance structure
US2364291A (en) Intermediate frequency transformer
US2598467A (en) Compensating means for variable inductances having magnetic cores
US1978600A (en) Permeability-tuned resonant circuit
US1937583A (en) Oscillation generator
US2271983A (en) Capacitor
US2598810A (en) Wide range high-frequency tuner
US1836808A (en) Inductance coil
US2618749A (en) Electrical impedance unit
US2322722A (en) Permeability tuning system
US2980797A (en) Variable tuner
US2989630A (en) Tuning apparatus
US2462884A (en) Electrical choke
US2265390A (en) Temperature compensated inductance
US2334178A (en) Variable inductance device