US2448296A - Tunable inductance - Google Patents

Tunable inductance Download PDF

Info

Publication number
US2448296A
US2448296A US644173A US64417346A US2448296A US 2448296 A US2448296 A US 2448296A US 644173 A US644173 A US 644173A US 64417346 A US64417346 A US 64417346A US 2448296 A US2448296 A US 2448296A
Authority
US
United States
Prior art keywords
coil
rod
inductance
tubular mount
chassis
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
US644173A
Inventor
Jr Raymond J Cary
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.)
United States, WAR, Secretary of
US SEC WAR
Original Assignee
US SEC WAR
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 US SEC WAR filed Critical US SEC WAR
Priority to US644173A priority Critical patent/US2448296A/en
Application granted granted Critical
Publication of US2448296A publication Critical patent/US2448296A/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
    • H01F21/00Variable inductances or transformers of the signal type
    • H01F21/02Variable inductances or transformers of the signal type continuously variable, e.g. variometers
    • H01F21/06Variable inductances or transformers of the signal type continuously variable, e.g. variometers by movement of core or part of core relative to the windings as a whole

Definitions

  • Thisinvention relates to electrical apparatus and more particularly to improvements in tunable inductances.
  • the conventional tuned-circuit inductance for high frequency amplifier circuits is a helical coil.
  • the inductance of this coil may be either fixed or variable.
  • the variable inductance coil usually has a hollow core in which a plug of magnetic material (e. g., polyiron) or non-magnetic material (e. g., brass) may be moved to vary the inductance of the coil.
  • the distributed capacity and the capacity to ground of this conventional coil which together with other stray tube and wiring capacities determine the stray shunt capacitance, may be of sufiicient magnitude to seriously affect the gain-bandwidth factor of the circuit.
  • the distributed capacity of the coil and its capacity to ground must be made as small as possible.
  • An object of the present invention is to :provide a tunable inductance for use with high frequency amplifier circuits in which the shunt capacity to ground is minimized.
  • a further object of the invention is to provide such a tunable inductance with a minimum distributed capacity.
  • a still further object is to provide such a tunable inductance with a readily-adjustable stable tuning control.
  • the present invention is a mechanism for axially expanding or contracting a helical coil thereby varying its inductance.
  • the coil is wound about a dielectric rod and one end of the coil is rigidly aflixe-d to the dielectric rod.
  • the dielectric rod moves axially within a tubular mount which is rigidly affixed to the amplifier chassis. The other end of the coil is maintained fixed with respect to the chassis. Hence, axial motion of the dielectric rod within the tubular mount will expand or contract the coil axially, and consequently will vary its inductance.
  • numeral I designates a dielectric rod having an external shoulder near one end. While the material of rod D is a dielectric in the present embodiment, other materials may be used, under different requirements.
  • the rod I0 is disposed within a metallic tubular mount Ii. One end of the tubular mount II has an external thread I2 whereby the mount may be secured to a chassis I3. The other end of tubular mount I I has an internal thread I4. The tubular mount II has an internal shoulder beyond the internal thread I4.
  • a section of rod I0 extends externally beyond tubular mount II.
  • a helical coil I5 is disposed about this external section of rod I0.
  • One end of coil I 5 is rigidly aflixed to a :pin I6 which extends through the end of rod Ill.
  • the other end of coil I5 is fixed to a tie-point pin I1.
  • the pin I1 is swedged to a protrusion on an insulating block I8. Insulating block I8 is maintained in a fixed position with respect to the chassis I3 by means of a screw I9.
  • the tie-point pin I1 is here shown as insulated from chassis I3 by means of the insulating block I 8. Pin I! could of course be grounded directly to chassis I3 if desired.
  • Axial motion of rod ID with respect "to tubular mount II is efiected by an adjusting screw 20 moving within thread I4 and applying pressure to one end of rod ID.
  • the pressure between rod III and screw 20 is maintained by a spring 2
  • the inductance of coil I5 may be varied by adjusting the screw 20.
  • One end of coil I5 is maintained fixed by pin I! and therefore axial motion of rod I0 caused by rotation of the adjusting screw 20 will either expand or contract coil I5, thereby changing the axial spacing or pitch of coil I5 and consequently its inductance.
  • the rod I0 accurately follows the motion of the screw 20 because of the pressure of the spring 2
  • also serves to prevent vibration along the axis of the coil, which vibration if present would vary the inductance of the coil introducing a vibration modulation in the output circuit.
  • the invention results in having the coil I5 characterized by a low distributed capacity and by a low shunt capacity to ground.
  • the coil I5 may be sufiiciently removed from the chassis I3 to minimize shunt capacity to ground.
  • the possibility of widely spacing the turns on coil I5 in conjunction with the use of the dielectric rod I0 tends to minimize the distributed capacity of coil [5.
  • a tunable inductance including a tubular mount having an internal thread at one end thereof, a dielectric rod disposed partly within.

Landscapes

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

Description

R. J. CARY, JR 2,448,296
TUNABLE INDUCTANCE Filed Jan. 29, 1946 INVENTOR RAYMOND J. CARYJR. BY
ATToRNEv Patented Aug. 31 1948 TUNABLE INDUCTANCE Raymond J. Cary, Jr., Long Beach, Calif., assignor to the United States of America as represented by the Secretary of War Application January 29, 1946. Serial No. 644,173
1 Claim. 1
Thisinvention relates to electrical apparatus and more particularly to improvements in tunable inductances.
The conventional tuned-circuit inductance for high frequency amplifier circuits is a helical coil. The inductance of this coil may be either fixed or variable. The variable inductance coil usually has a hollow core in which a plug of magnetic material (e. g., polyiron) or non-magnetic material (e. g., brass) may be moved to vary the inductance of the coil.
At very high radio frequencies, the distributed capacity and the capacity to ground of this conventional coil, which together with other stray tube and wiring capacities determine the stray shunt capacitance, may be of sufiicient magnitude to seriously affect the gain-bandwidth factor of the circuit. To obtain the maximum gainbandwidth factor, the distributed capacity of the coil and its capacity to ground must be made as small as possible.
An object of the present invention is to :provide a tunable inductance for use with high frequency amplifier circuits in which the shunt capacity to ground is minimized.
A further object of the invention is to provide such a tunable inductance with a minimum distributed capacity.
A still further object is to provide such a tunable inductance with a readily-adjustable stable tuning control.
Other objects and advantages of the invention will be apparent during the course of the following description.
Essentially the present invention is a mechanism for axially expanding or contracting a helical coil thereby varying its inductance. The coil is wound about a dielectric rod and one end of the coil is rigidly aflixe-d to the dielectric rod. The dielectric rod moves axially within a tubular mount which is rigidly affixed to the amplifier chassis. The other end of the coil is maintained fixed with respect to the chassis. Hence, axial motion of the dielectric rod within the tubular mount will expand or contract the coil axially, and consequently will vary its inductance.
In the accompanying drawing forming a part of this specification, the single figure is a crosssectional view illustrating one embodiment of the invention.
In the figure, numeral I designates a dielectric rod having an external shoulder near one end. While the material of rod D is a dielectric in the present embodiment, other materials may be used, under different requirements. The rod I0 is disposed within a metallic tubular mount Ii. One end of the tubular mount II has an external thread I2 whereby the mount may be secured to a chassis I3. The other end of tubular mount I I has an internal thread I4. The tubular mount II has an internal shoulder beyond the internal thread I4.
A section of rod I0 extends externally beyond tubular mount II. A helical coil I5 is disposed about this external section of rod I0. One end of coil I 5 is rigidly aflixed to a :pin I6 which extends through the end of rod Ill. The other end of coil I5 is fixed to a tie-point pin I1. The pin I1 is swedged to a protrusion on an insulating block I8. Insulating block I8 is maintained in a fixed position with respect to the chassis I3 by means of a screw I9. Hence, it is obvious that the end of coil I5 which is attached to pin I! will be maintained in a fixed position with respect to chassis I3 and tubular mount II. The tie-point pin I1 is here shown as insulated from chassis I3 by means of the insulating block I 8. Pin I! could of course be grounded directly to chassis I3 if desired.
Axial motion of rod ID with respect "to tubular mount II is efiected by an adjusting screw 20 moving within thread I4 and applying pressure to one end of rod ID. The pressure between rod III and screw 20 is maintained by a spring 2| which is disposed about rod I0 and between the external shoulder of rod I0 and the internal shoulder of tubular mount I I.
The inductance of coil I5 may be varied by adjusting the screw 20. One end of coil I5 is maintained fixed by pin I! and therefore axial motion of rod I0 caused by rotation of the adjusting screw 20 will either expand or contract coil I5, thereby changing the axial spacing or pitch of coil I5 and consequently its inductance.
The rod I0 accurately follows the motion of the screw 20 because of the pressure of the spring 2|. The pressure of spring 2| also serves to prevent vibration along the axis of the coil, which vibration if present would vary the inductance of the coil introducing a vibration modulation in the output circuit.
The invention results in having the coil I5 characterized by a low distributed capacity and by a low shunt capacity to ground. The coil I5 may be sufiiciently removed from the chassis I3 to minimize shunt capacity to ground. The possibility of widely spacing the turns on coil I5 in conjunction with the use of the dielectric rod I0 tends to minimize the distributed capacity of coil [5.
It will be apparent that there may be deviations from the invention as described which still fall fairly within the spirit and scope of the invention What is claimed is:
A tunable inductance including a tubular mount having an internal thread at one end thereof, a dielectric rod disposed partly within.
said tubular body portion and extending externally beyond said tubular mount at the other end thereof, screw means associated with said internal thread and adapted to apply pressure to;
the end of said rod which is disposed within said tubular mount, spring meansdisposed" about said rod and adapted to maintain the pressure between said rod and said screw means, a helical coil of conducting material disposed'about the.
external portion of said dielectric rod, one end of said coil being rigidly affixed to said dielectric rod and the other end fixed with respect to said tubular mount, whereby the motionof said screw 4 means within said internal thread will move said dielectric rod axially with respect to said mount thereby varying the pitch of said helical coil and changing the inductance thereof.
RAYMOND J. CARY, JR.
REFERENCES CITED The following references are of record in the 0 file of this patent:
UNITED STATES PATENTS Great Britain June 4,. 1925
US644173A 1946-01-29 1946-01-29 Tunable inductance Expired - Lifetime US2448296A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US644173A US2448296A (en) 1946-01-29 1946-01-29 Tunable inductance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US644173A US2448296A (en) 1946-01-29 1946-01-29 Tunable inductance

Publications (1)

Publication Number Publication Date
US2448296A true US2448296A (en) 1948-08-31

Family

ID=24583760

Family Applications (1)

Application Number Title Priority Date Filing Date
US644173A Expired - Lifetime US2448296A (en) 1946-01-29 1946-01-29 Tunable inductance

Country Status (1)

Country Link
US (1) US2448296A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2646684A (en) * 1950-03-07 1953-07-28 Pye Ltd Radio-frequency tuning device
US2870630A (en) * 1954-03-05 1959-01-27 Sivertsen Jens Inductance strain gauges
US2927289A (en) * 1955-07-21 1960-03-01 Sivertsen Jens Inductance strain gauges
US5347257A (en) * 1990-02-23 1994-09-13 Stocker & Yale, Inc. Varying inductances
US5438261A (en) * 1994-02-16 1995-08-01 Caterpillar Inc. Inductive sensing apparatus for a hydraulic cylinder
US5497804A (en) * 1994-06-27 1996-03-12 Caterpillar Inc. Integral position sensing apparatus for a hydraulic directional valve

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US793777A (en) * 1905-03-30 1905-07-04 Reginald A Fessenden Condenser.
US1533749A (en) * 1923-06-11 1925-04-14 Meirowsky Oskar Inductance
GB234570A (en) * 1924-03-13 1925-06-04 Labouchere Hillyer Bainbridge Improvements in or relating to variable inductances
US2252919A (en) * 1939-01-10 1941-08-19 Lewis D Eckard Multiwave variable resonator
US2294881A (en) * 1939-08-03 1942-09-08 Internat Telephone & Radio Mfg High frequency impedance unit
US2332868A (en) * 1939-09-30 1943-10-26 Nowak Alfred High frequency variable inductance

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US793777A (en) * 1905-03-30 1905-07-04 Reginald A Fessenden Condenser.
US1533749A (en) * 1923-06-11 1925-04-14 Meirowsky Oskar Inductance
GB234570A (en) * 1924-03-13 1925-06-04 Labouchere Hillyer Bainbridge Improvements in or relating to variable inductances
US2252919A (en) * 1939-01-10 1941-08-19 Lewis D Eckard Multiwave variable resonator
US2294881A (en) * 1939-08-03 1942-09-08 Internat Telephone & Radio Mfg High frequency impedance unit
US2332868A (en) * 1939-09-30 1943-10-26 Nowak Alfred High frequency variable inductance

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2646684A (en) * 1950-03-07 1953-07-28 Pye Ltd Radio-frequency tuning device
US2870630A (en) * 1954-03-05 1959-01-27 Sivertsen Jens Inductance strain gauges
US2927289A (en) * 1955-07-21 1960-03-01 Sivertsen Jens Inductance strain gauges
US5347257A (en) * 1990-02-23 1994-09-13 Stocker & Yale, Inc. Varying inductances
US5438261A (en) * 1994-02-16 1995-08-01 Caterpillar Inc. Inductive sensing apparatus for a hydraulic cylinder
US5497804A (en) * 1994-06-27 1996-03-12 Caterpillar Inc. Integral position sensing apparatus for a hydraulic directional valve

Similar Documents

Publication Publication Date Title
US2338134A (en) Variable tuning system
US2394391A (en) Stable tuning device for high-frequency radio circuits
US2611094A (en) Inductance-capacitance resonance circuit
US2403349A (en) Combination coil and condenser
US2753530A (en) High q. frequency tuner
US2469168A (en) Loop-antenna tuning system
US2448296A (en) Tunable inductance
US2392664A (en) Ultra high frequency filter
US2182071A (en) Adjustable coupling system
US2450192A (en) Ultra high frequency tuning unit
US2645718A (en) Variable inductance structure
US2728052A (en) Adjustable band pass filter
US2431425A (en) Variable inductance device
US2780727A (en) Resonant circuit
US2561727A (en) Tuning of electrical resonators
US2398112A (en) Combined capacitive and inductive tuning unit
US2568310A (en) Inductance coil structure
US2601445A (en) Ultrahigh-frequency structure
US2600278A (en) Variable capacity cavity tuning
US2980797A (en) Variable tuner
US2641647A (en) Tuning device
US1978600A (en) Permeability-tuned resonant circuit
US2531231A (en) Variable permeability tuning device
US2206250A (en) Transformer
US2458071A (en) Adjustable inductor