US2498340A - Antenna tuning control system - Google Patents

Antenna tuning control system Download PDF

Info

Publication number
US2498340A
US2498340A US584393A US58439345A US2498340A US 2498340 A US2498340 A US 2498340A US 584393 A US584393 A US 584393A US 58439345 A US58439345 A US 58439345A US 2498340 A US2498340 A US 2498340A
Authority
US
United States
Prior art keywords
coil
resonance
circuit
motor
antenna
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
US584393A
Inventor
William B Morrison
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
Application granted granted Critical
Publication of US2498340A publication Critical patent/US2498340A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/02Transmitters
    • H04B1/04Circuits

Definitions

  • My present invention relates to an antenna tuning control system, and more particularly to a control system for automatically adjusting the inductance of an antenna tuning coil to a value such that the antenna circuit will be in exact resonance at a selected operatin frequency of a transmitter or receiver to which the antenna circuit is coupled.
  • the invention may find general application in systems where it is desired to provide for the automatic adjustment of a tunable device in response to a transmitted or received radio signal
  • Another object of the invention is to provide means automatically operated in response to antenna current for adjusting the tuning of the antenna circuit.
  • a still further object of the invention is to provide, as the antenna tuning means, a rotary inductance coil which is motor-operated, in response to antenna current, to a position such that it tunes the antenna circuit to resonance, suitable control means being provided to cause substantially instantaneous stoppage of the mo tor at the resonant-adjusted position or the coil.
  • a more specific object of my invention is to provide a rotary tuning coil for the antenna circuit, a reversible motor for rotating the coil first in one direction and then in the other to vary its inductance, antenna-current responsive means, and a control circuit operated by the latter means for deenergizing the motor at the instant the coil is rotated to a position where 2, it provides the requisite inductance to tune the antenna circuit to resonance.
  • Fig. 1 is a schematic circuit diagram of the antenna tuning control system in accordance with the invention
  • Figs. 2a, 2b and 2c are certain voltage curves which will serve to explain certain aspects of the invention.
  • Fig. 3 is a view in elevation and partly in section of the antenna tuning coil and the elements associated therewith, including the driving motor, and
  • Fig. 4 is a sectional view of Fig. 3 taken on the line 4-4 of Fig. 3.
  • the antenna tuning coil which is of the rotary type, is shown at I.
  • a variable tap 2 is electrically connected by a conductive connection 2' to the coil at one end 3, the opposite end 3 being connected to the antenna A.
  • tap 2 is in the form of a roller and the conductive connection 2' is in the form of a rod along which the roller is adapted to slide in the axial direction.
  • a reversible motor indicated at t is adapted, when energized, to rotate the coil through suitable reduction gearing represented by the dash line 5. Rotation of the coil causes the variable tap or roller to travel up or down as viewed in Fig. 1, or to the left or right as viewed in Fig. 3, in contact with the coil turns,- depending upon the direction of motor travel, thereby introducing a varying amount of coil inductance into the antenna circuit.
  • the motor is provided with a pair of reversing windings 6 and l, to the common terminal of which there is connected the motor field winding 8 in series with a brake coil 9 whichis grounded at one end.
  • the other terminals of windings 6 and l are connected, respectively, to switch contacts l0 and II with which there is adapted to cooperate a movable switch arm l2.
  • a second switch arm 13' is movable between a grounded contact l4 and a blank contact l5, and a relay coil [6 is adapted, when energized, to actuate both switch arms 12 and t3 in unison from their normal upper positions, as shown, to their lower positions by means represented diagrammatically by the dash line H.
  • 6 is grounded at one end and is connected at its other end to a conductor l8 which in turn is connected to the switch arm l2.
  • a radio frequency choke I9 is connected between the switch arm l3 and a conductor 25 leading from the low end 3 of the tuning coil.
  • the block at 24 represents the power amplifier of the transmitter and is the same as that designated 24 in the application above mentioned.
  • the power amplifieroutput is fed to the antenna circuit through a coupling condenser 25 (corresponding to the condenser designated 41 in said application), the condenser being connected to the junction between transformer primary 2
  • the transformer T is provided with a secondary winding 26 divided into two sections 21 and 28 by a tap 29, the outer ends of the coil sections being connected, respectively, through resistances 30 of suitable values to the contacts of a dry-disc rectifier 3
  • the coil sections 21 and 28 are so proportioned that together with the distributed capacity of the circuit including the rectifier they resonate at approximately 3 and 6 me. However, by means of the resistances 30 the current-frequency curve is sufficiently fiattened to provide a substantially uniform output from the rectifier over the operating range of the transmitter of 2 to 8 mo.
  • a radio frequency bypass condenser 32 Connected between the tap 29 and the rectifier 3
  • a meter 51 for indicating antenna current is shunted across the portion 35.
  • a discharge tube for controlling the operation of the motor 4 in response to the antenna current is shownat 38.
  • This tube is shown as a twin-triode, the type used being a SJ 6, separate tubes or a twin tube of a different type having similar characteristics may be used instead.
  • the lead 34 which is the negative side of the rectifier output is connected to the grid 39 of the first tube section through a coupling resistor 49 and also to the grid 4
  • the plate 43 of the first section is connected through a load resistor 44 to a source of potential represented by 150 v. and the plate 45 of thesecond section is connected through a relay coil 46 to the same potential source.
  • the plate 45 is also connected to the low end of choke 22 by way of a resistor 45'.
  • Condenser 41 is a bypass condenser for the plate circuit of the second tube section, being connected between the low potential side of relay coil 46 and cathode 48 of the tube, and condenser 49 is a coupling condenser which serves to couple the plate circuit of the first tube section'to the grid 4
  • a resistor 56 is connected from grid 4
  • the cathode of the control tube is adapted to be connected to ground through a switch 55 which may be constituted as a push-button for manual operation or for the particular application herein disclosed be controlled by automatic tuning mechanism.
  • the relay coil 46 is adapted, upon being energized, to actuate a gang of switch arms indicated at 56, 57 and 58.
  • the switch arm 56 is connected by way of a conductor 59 to lead 33 and by way of a conductor 66 to the +12 v. conductor 5
  • of switch 56 is blank while the lower contact 62 has connected to it the conductor is which leads from the motor-reversing switch arm l2.
  • the upper contact 63 of switch 57 is blank, there being connected to the lower contact 64 and to the switch arm 57 a pair of conductors which lead to the transmitter on switch (not shown).
  • the upper contact 65 of switch 58 is connected to grid 4
  • Tube 38 controls the current through the relay coil 46 which in turn, actuates or pulls-in the three switch arms, 56, 5'5 and 58 when it is energized.
  • the relay coil is thus energized when the tube is in a conducting condition and is nonenergized when the tube is biased to cut-off.
  • the conducting condition of the tube is controlled as follows: Antenna current through transformer T is fed to the rectifier 3
  • a negative D. C. voltage of the form shown in Fig. 2a is obtained.
  • This negative voltage is applied to the grid 39 of the first section of the tube through resistor 40, being amplified approximately twenty times in this section of the tube, and is then coupled to the grid 4
  • the voltage induced on one plate of a condenser varies as the rate of change of voltage on the other plate, the voltage appearing on grid 4
  • the diiferential voltage curve as the antenna coil passes through resonance is shown in Fig. 2b.
  • some of the D. C. resonance voltage from the rectifier output is fed to grid 4
  • the tuning-coil driving motor 4 is a D. C. motor of the reversible type. Power to the motor is switched on by theswitch arm 56 when actuated to its lower contact 62 by the relay 46 and thus the motor runs only when the relay 46 is energized.
  • the motor will always rotate the coil to the point of maximum inductance, that is, in a direction such that tap or roller 2 travels towards the coil end 3. This is so because at the beginning of the cycle the position of switch I2 is as shown in the drawing in contact with the upper contact l0, thereby completing the motor circuit through the field Winding 6 which iseffective to rotate the motor in the abovedesignated direction.
  • Switch [2- is brought downto its contact I I to complete the motor circuit through the other field winding I, thereby rotating the tuning coil in the opposite direction to cause the tap or roller 2 to recede from the maximum inductance position. at coil end 3 so that the inductance in the antenna circuit is gradually diminished-
  • the. relay coil i6 is energized during the time the motor circuit is energized, the switches l2 and i3 which are. adaptedto be controlled. thereby are not actuated to their low contacts, the reason being that normally the relay armature 10' (Fig. 4) is spaced a sufficient distance from the pole of the relay so as not tobe attracted thereto in the presence of current through. the. relay.
  • an actuator H carried by a motor-driven Geneva gear 12- strikes an arm 13 attached to or formed integral with the armature 70 which is pivotedat ll to urge the armaturetowards the relay pole.
  • the energized relay will therefore hold thearmature in attracted position.
  • Formed integrally with or otherwisev attached to the armature is amember which, in the attracted-position of the armature,.actuates theswitch armsv I2 and I3 to the lower contacts, as seen in Fig. 1.
  • this causes the motor to reverse its direction of operation, thereby rotating the antenna coil so that. its effective inductance is. reduced, and causes also the ground connection. for resistor 45 to be brokenat contact.
  • the control relay 45 is normally in. a non-energizedstate. To initiate operation of the control tube it isnecessary that the cathode 48 of the. tubev be grounded. Thisis accomplished by the closure of switch 55. which may be performed manually, or, when used in connetion with a system such as described in the above-mentioned application which is adapted for automatic tuning, the switch may be arranged for closureautomatically at a proper point in the sequence of automatic tuning operations.
  • control tube The manner of operation of the control tube is as follows: Withthe control switch 55 open, the cathode 48 is 12 volts positive, being. connected to the +12 v. conductor through the resistor 52; and the grid 41 is at- 6 voltspositive,
  • the relay continues to be energized.
  • the cathode With the opening of switch 55 at this time by the removal of the finger or otherwise, the cathode is brought back to -H2 volts, and since the grid is also at +12 volts, the tube operates, or is conductive, with zero grid bias, and the relay coil 46 continues tobe energized by the normal. plate current of the tube.
  • the motor has begun to drive the tuning coil l to its maximum inductance position whereat the motor reversal occurs as previously explained.
  • the motor drive for the rotary tuning coil 1 may be seen from the constructional views shown in Figs. 3 ands.
  • the coil is enclosed in a cylindrical case I" and is mounted on a shaft 16 which is journalled at its opposite ends in a pair of side members Ti and 18.
  • the shaft end at the right has afnxed to it a pinion 19 which meshes with.
  • Gearedto gear 80 is a driving pinion 82 freely mounted on themotor shaft 83 and is adapted to be driven thereby through a-friction clutch plate 84 which avoids placing on the manual drive, later tobe described, an unduly. heavy load due to the motor armature and the brake mechanism.
  • the gear train 82, Hand 19 constitute the reduction gearing which has been indicatedinFig. l by the dash line '5.
  • the gear 80 is-provided-with a drive pin 85 for the Geneva camor gear 12 which is freely mounted on the right-hand end of the coil shaft.
  • Thev gear ll is designed to makeone complete revolution. for the time it takes the roller 2 to travel on its-conductive rod 2 from one end of the coil-to the other.
  • actuator will rock-the armature 10 towards the holding, relay l6 and-also throw the switches [2 and I3' to theiropposite contacts as heretofore explained.
  • a stop pin 81 carried by an end cover plate 88, serves to limit further travel of actuator H and gear 12.
  • the motor having thus reversed its direction of operation, the gear will rotate in the opposite direction, or as indicated by the solid arrow 89. If the coil does not pass through resonance, gear 12 will be rotated to said opposite limit of its travel, the actuator 1
  • H coacts with arm 13 to withdraw the armature H!
  • a hand wheel or crank 90 at the end of a shaft 9! which is provided at its other end with a transverse slot 92 adapted to receive a similarly shaped extension 93 on the coil shaft Hi. Normally parts 92 and 93 are disengaged due to the action of a coil spring 94.
  • crank 90 is pressed in to permit engagement between the female portion of shaft 9
  • a control system operative upon application of alternating currents to said oscillatory circuit to vary said component to tune said oscillatory circuit substantially to resonance with said alternating currents, said control system including a power operated device, means controlled by said power operated device to vary said component in one direction to one extremity of said rangeof movement and thereupon to vary said component in the other direction toward the other extremity of said range of movement, a control circuit associated with said power operated device to cease said variation of said component in said other direction at a position of said component at which resonance of said oscillatory circuit with said alternatingcurrents is obtained,
  • control circuit comprising means to derive a unidirectional voltage proportional to said alternating currents, said voltage increasing rapidly as resonance is approached to a maximum at resonance and decreasing in complementary manner after resonance is passed, an electron discharge system having at least a cathode element,-
  • a control element and an anode element a relay having the actuating winding thereof connected to said anode element and having an armature coupled in circuit with said power operated device to render the same operable when said electron discharge system is conducting, and means to render said electron discharge system conducting to initiate said variation of saidcomponentbysaid power operated device, the improvement comprising a network to which a portion of said voltage is applied to derive a bi-directional voltage in creasing rapidly in one direction as resonance is approached, reversing and passing through zero at resonance, and reversing and decreasing in complementary manner after resonance is passed, means to combine said voltages to produce a resultant voltage increasing rapidly in one direction only as resonance is passed, and means to apply said resultant voltage to said control element of said electron discharge system to block" the same when said component is at a position tuning said oscillatory circuit substantially to resonance with said alternating currents, thereby to deenergize said relay and cause cessation of said variation of said component.
  • a control system operative upon application of alternating currents to said oscillatory circuit to vary said component to tune said oscillatory circuit substantially to resonance with said alternating currents, said control system including a power operated device arranged to vary said element from one extremity toward the other extremity of said range of movement, a control circuit associated with said power operated device to cease said variation at a position of said component at which resonance of said oscillatory" circuit with said alternating currents is obtained, said control circuit comprising means to derive a unidirectional Voltage proportional to said alternating currents, said voltage rapidly as resonance is approached to a maxi mum at resonance and decreasing in correspond means to render said electron discharge conduct-" ing to initiate said variation of said element by said power operated device, the improvement comprising a network to which a portion of said voltage is applied to derive a bi-directional volt-
  • a control system operative upon application of alternating currents to said oscillatory circuit to adjust said component to tune said oscillatory circuit substantially to resonance with said altcrnating currents, said control system including a reversible motor, mechanical linkage under the control of said motor to drive said component in one direction to one extremity of said range of movement and thereupon to drive said component in the opposite direction toward the other extremity of said range of movement, a control circuit electrically associated with said motor to cease said adjustment at a position of said component at which resonance of said oscillatory circuit with said alternating currents is obtained, said control circuit comprising a rectifier coupled to said oscillatory circuit to derive a unidirectional voltage proportional to the alternating current therein, an electron discharge system having at least a cathode element, a control grid and an anode, a relay having the
  • a control system operative upon application of alternating currents to said oscillatory circuit to adjust said component to tune said oscillatory circuit substantially to resonance with said alternating currents, said control system including a reversible motor, mechanical linkage under the control of said motor to drive said component in one direction to one extremity of said range of movement and thereupon to drive said component in the opposite direction toward the other extremity of said range of movement, a control cireuit electrically associated with said motor to cease said adjustment at a position of said component at which resonance of said oscillatory circuit with said alternating currents is obtained, said control circuit comprising a transformer coupled to said oscillatory circuit, a rectifier coupled to said transformer to derive a unidirectional voltage proportional to the alternating current therein, an electron discharge system having at least a cathode element, a control grid
  • a control system for tuning an oscillatory circuit having a component Variable over a predetermined range of mechanical movement to tune said oscillatory circuit over a prearranged frequency spectrum including a power device to drive said component over said range of movement, and a control circuit to interrupt said power device upon said component reaching a position at which said oscillatory circuit is tuned to resonance with a signal applied thereto, said control circuit comprising means to derive a voltage proportional to the current flowing in said oscillatory circuit, said voltage having a waveform rising to a maximum at the frequency at which resonance is obtained, means to alter the waveform of said voltage to produce a potential having a waveform having an intermediate value at the frequency at which resonance is obtained, electron discharge means coupled to control said power device and biased to maintain said power device normally operative, and means to apply said potential to said electron discharge means to block the same when said potential attains said intermediate Value thereby to render said power device inoperative.

Description

CURRENT TO TRANSMITTER "0N" SWITCH INVENTOR. WIA 1. MM 5 Maw/sow M TTORNEY A N N E T N A 3 Sheets-Sheet 1 BY A FIG.1
-F iEVERSIBLE MOTOR W B MORRISON ANTENNA TUNING CONTROL SYSTEM TRANSMITTER POWER AMPLIFIER Feb. 21, 1950 Filed March 25, 1945 OPERATED MANUALLY 0R CONTROLLED BY AUTOMATIC TUNING MECHANISM- Feb. 21, 1950 w, MORRISON 2,498,340
ANTENNA TUNING CONTROL SYSTEM Filed March 23, 1945 3 Sheets-Sheet 3 IN V EN TOR W/L 1 MM 6. MORPASO/V TTORNEY Patented Feb. 21, 1950 UNITED STATES PATENT OFFICE ANTENNA TUNING CONTROL SYSTEM William B. Morrison, Verdun, Quebec, Canada,
assignor, by inesne assignments, to Radio Corporation of America, New York, N. Y., a corporation of Delaware Application March 23, 1945, Serial No. 584,393 In Canada January 22, 1-945 Claims. 1
My present invention relates to an antenna tuning control system, and more particularly to a control system for automatically adjusting the inductance of an antenna tuning coil to a value such that the antenna circuit will be in exact resonance at a selected operatin frequency of a transmitter or receiver to which the antenna circuit is coupled.
Although the invention may find general application in systems where it is desired to provide for the automatic adjustment of a tunable device in response to a transmitted or received radio signal, the invention as disclosed herein is applied to a transmitter recelver set utilized in a two=way communication system which is described and claimed in an application, Serial No. 584,392, filed concurrently herewith, by J ohn C. E. Mitchell and the present applicant, which application is now U. S. Patent No. 2,433,290, granted Dec. 23, 1947.
In the operation of a transmitter designed to operate on any one of a plurality of carrier fre= quencies, or a transmitter-receiver set for two way communication, such as described in the above-mentioned application, it is often necessary to change over from one operating frequency or carrier to another, and frequently at short notice. It is therefore advantageous and desirable that the antenna circuit, in addition to the tunable circuits of the transmitter-receiver set, betuned to exact resonance, and as quickly as po'ssibl'e.
Accordingly, it is one of the main objects of my invention to provide automatically-operated means for adjusting the tuning of the antenna circuit of a transmitter to exact resonance at the transmitted frequency.
Another object of the invention is to provide means automatically operated in response to antenna current for adjusting the tuning of the antenna circuit.
A still further object of the invention is to provide, as the antenna tuning means, a rotary inductance coil which is motor-operated, in response to antenna current, to a position such that it tunes the antenna circuit to resonance, suitable control means being provided to cause substantially instantaneous stoppage of the mo tor at the resonant-adjusted position or the coil.
A more specific object of my invention is to provide a rotary tuning coil for the antenna circuit, a reversible motor for rotating the coil first in one direction and then in the other to vary its inductance, antenna-current responsive means, and a control circuit operated by the latter means for deenergizing the motor at the instant the coil is rotated to a position where 2, it provides the requisite inductance to tune the antenna circuit to resonance.
The novel features characteristic of my invention are set forth with particularity in the appended claims. The invention itself, however, as to its organization, circuit arrangement and mode of operation, together with further objects and advantages thereof, will best be understood by reference to the following description taken in connection with the accompanying drawing, in which:
Fig. 1 is a schematic circuit diagram of the antenna tuning control system in accordance with the invention,
Figs. 2a, 2b and 2c are certain voltage curves which will serve to explain certain aspects of the invention,
Fig. 3 is a view in elevation and partly in section of the antenna tuning coil and the elements associated therewith, including the driving motor, and
Fig. 4 is a sectional view of Fig. 3 taken on the line 4-4 of Fig. 3.
Referring to Fig. 1, the antenna tuning coil, which is of the rotary type, is shown at I. A variable tap 2 is electrically connected by a conductive connection 2' to the coil at one end 3, the opposite end 3 being connected to the antenna A. As
shown in Fig. 3, tap 2 is in the form of a roller and the conductive connection 2' is in the form of a rod along which the roller is adapted to slide in the axial direction. A reversible motor indicated at t is adapted, when energized, to rotate the coil through suitable reduction gearing represented by the dash line 5. Rotation of the coil causes the variable tap or roller to travel up or down as viewed in Fig. 1, or to the left or right as viewed in Fig. 3, in contact with the coil turns,- depending upon the direction of motor travel, thereby introducing a varying amount of coil inductance into the antenna circuit.
The motor is provided with a pair of reversing windings 6 and l, to the common terminal of which there is connected the motor field winding 8 in series witha brake coil 9 whichis grounded at one end. The other terminals of windings 6 and l are connected, respectively, to switch contacts l0 and II with which there is adapted to cooperate a movable switch arm l2. A second switch arm 13' is movable between a grounded contact l4 and a blank contact l5, and a relay coil [6 is adapted, when energized, to actuate both switch arms 12 and t3 in unison from their normal upper positions, as shown, to their lower positions by means represented diagrammatically by the dash line H. The relay coil |6 is grounded at one end and is connected at its other end to a conductor l8 which in turn is connected to the switch arm l2. A radio frequency choke I9 is connected between the switch arm l3 and a conductor 25 leading from the low end 3 of the tuning coil.
Connected to the antenna lead 26 is the primary winding 2| of a transformer T, and in series therewith is a coil 22 which together with a shunt condenser 23 constitute a radio frequency antenna filter. The block at 24 represents the power amplifier of the transmitter and is the same as that designated 24 in the application above mentioned. The power amplifieroutput is fed to the antenna circuit through a coupling condenser 25 (corresponding to the condenser designated 41 in said application), the condenser being connected to the junction between transformer primary 2| and the choke 22.
The transformer T is provided with a secondary winding 26 divided into two sections 21 and 28 by a tap 29, the outer ends of the coil sections being connected, respectively, through resistances 30 of suitable values to the contacts of a dry-disc rectifier 3|. The coil sections 21 and 28 are so proportioned that together with the distributed capacity of the circuit including the rectifier they resonate at approximately 3 and 6 me. However, by means of the resistances 30 the current-frequency curve is sufficiently fiattened to provide a substantially uniform output from the rectifier over the operating range of the transmitter of 2 to 8 mo.
Connected between the tap 29 and the rectifier 3| is a radio frequency bypass condenser 32, and connected between a conductor 33 from the output electrode of the rectifier. and, a conductor 34 leading from the tap 29 are the rectifier load resistors 35 and 36. A meter 51 for indicating antenna current is shunted across the portion 35.
A discharge tube for controlling the operation of the motor 4 in response to the antenna current is shownat 38. Although this tube is shown as a twin-triode, the type used being a SJ 6, separate tubes or a twin tube of a different type having similar characteristics may be used instead. The lead 34 which is the negative side of the rectifier output is connected to the grid 39 of the first tube section through a coupling resistor 49 and also to the grid 4| of the second tube section through a coupling resistor 42. The plate 43 of the first section is connected through a load resistor 44 to a source of potential represented by 150 v. and the plate 45 of thesecond section is connected through a relay coil 46 to the same potential source. The plate 45 is also connected to the low end of choke 22 by way of a resistor 45'. Condenser 41 is a bypass condenser for the plate circuit of the second tube section, being connected between the low potential side of relay coil 46 and cathode 48 of the tube, and condenser 49 is a coupling condenser which serves to couple the plate circuit of the first tube section'to the grid 4| of the second section. ,A resistor 56 is connected from grid 4| to a +12 v. conductor to which cathode 48 is also connected through a resistor 52, and a second cathode resistor 53 is connected to a +6 v. conductor, 54. The cathode of the control tube is adapted to be connected to ground through a switch 55 which may be constituted as a push-button for manual operation or for the particular application herein disclosed be controlled by automatic tuning mechanism.
The relay coil 46 is adapted, upon being energized, to actuate a gang of switch arms indicated at 56, 57 and 58. The switch arm 56 is connected by way of a conductor 59 to lead 33 and by way of a conductor 66 to the +12 v. conductor 5|, the lead 33 from the rectifier also being connected to conductor 69. The upper contact 6| of switch 56 is blank while the lower contact 62 has connected to it the conductor is which leads from the motor-reversing switch arm l2. The upper contact 63 of switch 57 is blank, there being connected to the lower contact 64 and to the switch arm 57 a pair of conductors which lead to the transmitter on switch (not shown). The upper contact 65 of switch 58 is connected to grid 4| of the second tube section by way of a conductor 66, and the switch arm itself is connected to the +6 v. conductor 54 by way of a conductor 6'! which includes a resistor 68, the lower contact 69 of switch 58 being blank.
Tube 38 controls the current through the relay coil 46 which in turn, actuates or pulls-in the three switch arms, 56, 5'5 and 58 when it is energized. The relay coil is thus energized when the tube is in a conducting condition and is nonenergized when the tube is biased to cut-off. The conducting condition of the tube is controlled as follows: Antenna current through transformer T is fed to the rectifier 3|, there being developed across the load resistors 35 and 35 a D. C. potential which varies directly as the R. F. current fed into the antenna from the power amplifier 24 of the transmitter. Thus, when the antenna circuit including its coil passes through resonance, a negative D. C. voltage of the form shown in Fig. 2a is obtained. This negative voltage is applied to the grid 39 of the first section of the tube through resistor 40, being amplified approximately twenty times in this section of the tube, and is then coupled to the grid 4| of the second tube section through the coupling condenser 45. As the voltage induced on one plate of a condenser varies as the rate of change of voltage on the other plate, the voltage appearing on grid 4| through condenser 49 is the difierential of the resonance curve shown in Fig. 2a. The diiferential voltage curve as the antenna coil passes through resonance is shown in Fig. 2b. In addition, some of the D. C. resonance voltage from the rectifier output is fed to grid 4| through resistor 42. The relative amplitudes of these two voltages on grid 4| are as shown in Figs. 2a and 2b and the resulting voltage is the sum of these voltages shown in Fig. 2c. 1 The above action results in a sharp increase in negative voltage with great enough amplitude to produce plate current cut-ofi in the tube at the instant the antenna coil reaches the point at which resonance for the antenna circuit is obtained.
The tuning-coil driving motor 4 is a D. C. motor of the reversible type. Power to the motor is switched on by theswitch arm 56 when actuated to its lower contact 62 by the relay 46 and thus the motor runs only when the relay 46 is energized. When the tuning-up cycle is started, the motor will always rotate the coil to the point of maximum inductance, that is, in a direction such that tap or roller 2 travels towards the coil end 3. This is so because at the beginning of the cycle the position of switch I2 is as shown in the drawing in contact with the upper contact l0, thereby completing the motor circuit through the field Winding 6 which iseffective to rotate the motor in the abovedesignated direction. This precaution is nec- 5' essary in order to prevent the relay throwing out or becoming deenergized on an harmonic of the; desired frequency. This is accomplished by causing a residual current to flow through. the coil of relay 46 by tying the resistor 45' to ground whenthe antenna coil is tuned down to maximum inductance, the ground connection being completed through coils 22 and i9 and the closed position of switch l3 as shown. When the coil reaches the end of its travel, the direction of motor operation is reversed and the ground connection for resistor 45' is broken at It in a manner to be described in connection with Fig. 4. Switch [2- is brought downto its contact I I to complete the motor circuit through the other field winding I, thereby rotating the tuning coil in the opposite direction to cause the tap or roller 2 to recede from the maximum inductance position. at coil end 3 so that the inductance in the antenna circuit is gradually diminished- Although the. relay coil i6 is energized during the time the motor circuit is energized, the switches l2 and i3 which are. adaptedto be controlled. thereby are not actuated to their low contacts, the reason being that normally the relay armature 10' (Fig. 4) is spaced a sufficient distance from the pole of the relay so as not tobe attracted thereto in the presence of current through. the. relay. However, when the tuning coil reachesthe end of its travel, an actuator H carried by a motor-driven Geneva gear 12- strikes an arm 13 attached to or formed integral with the armature 70 which is pivotedat ll to urge the armaturetowards the relay pole. The energized relay will therefore hold thearmature in attracted position. Formed integrally with or otherwisev attached to the armature is amember which, in the attracted-position of the armature,.actuates theswitch armsv I2 and I3 to the lower contacts, as seen in Fig. 1. As mentioned previously, this causes the motor to reverse its direction of operation, thereby rotating the antenna coil so that. its effective inductance is. reduced, and causes also the ground connection. for resistor 45 to be brokenat contact. 14; Although actuator H is withdrawn from the arm 13 by movement of the. ear 12 in the. oppositev direction, relay l6 holds its armature lv inv attracted position, and switches. 12 and I3' will be closed while the antenna tuning coil tunes. back up. The switches will pull back to their positionsas shown. in Fig. 1. when. the tuning adjustmentis. completed and the motor voltage. is. shut.
ofiat contactfii-upon the opening of switch56.
The control relay 45 is normally in. a non-energizedstate. To initiate operation of the control tube it isnecessary that the cathode 48 of the. tubev be grounded. Thisis accomplished by the closure of switch 55. which may be performed manually, or, when used in connetion with a system such as described in the above-mentioned application which is adapted for automatic tuning, the switch may be arranged for closureautomatically at a proper point in the sequence of automatic tuning operations. I
The manner of operation of the control tube is as follows: Withthe control switch 55 open, the cathode 48 is 12 volts positive, being. connected to the +12 v. conductor through the resistor 52; and the grid 41 is at- 6 voltspositive,
The grid consequence the relay coil is deenergized, and the motor" is inoperative by reason-of switch arm being. on its upper contact 6 I.
Upon the: closure of switch 55, the cathode is connected to ground, grid 41 still remaining at +6 volts. There will result, therefore, an instantaneous high plate current through the tube to cause energization ofrelay 46 which in turn will pull inthe several switches 56, 51 and 58. Power to the motor will then be applied through switch 56 closed oncontact- 62-, and the +6 volt connection to grid 4| will be broken at contact 55. There will, however, be applied to the grid a bias of +12 volts through the resistor 50 which is large enough (1 megohm) to limit the grid current to a safe value. With the cathode still at ground potential (switch 55 remaining closed up to this point,v it being. only necessary that switch 55 be closed. for a fraction of a second) and the grid being at +12 volts, the relay continues to be energized. With the opening of switch 55 at this time by the removal of the finger or otherwise, the cathode is brought back to -H2 volts, and since the grid is also at +12 volts, the tube operates, or is conductive, with zero grid bias, and the relay coil 46 continues tobe energized by the normal. plate current of the tube. In the meantime the motor has begun to drive the tuning coil l to its maximum inductance position whereat the motor reversal occurs as previously explained.
At the point-of resonance of the antenna circuit, there occurs a sharp increase-in the negative bias on grid 4|, asexplained above inconnection with the curve of Fig. 2c. As a consequence the plate current of the tube cuts off and the controlrelay coil is deenergized, opening the motor energizing circuit at contact 62. By means of the brake coil 9 which is deenergized simultaneously with the motor, a mechanical brake device (not shown) but which may be of any suitable construction, is. released to brake the motor.
The motor drive for the rotary tuning coil 1 may be seen from the constructional views shown in Figs. 3 ands. The coil is enclosed in a cylindrical case I" and is mounted on a shaft 16 which is journalled at its opposite ends in a pair of side members Ti and 18. The shaft end at the right has afnxed to it a pinion 19 which meshes with. a gear mounted on a stud shaft 8| supported from the member 18. Gearedto gear 80 is a driving pinion 82 freely mounted on themotor shaft 83 and is adapted to be driven thereby through a-friction clutch plate 84 which avoids placing on the manual drive, later tobe described, an unduly. heavy load due to the motor armature and the brake mechanism.- The gear train 82, Hand 19 constitute the reduction gearing which has been indicatedinFig. l by the dash line '5.
The gear 80 is-provided-with a drive pin 85 for the Geneva camor gear 12 which is freely mounted on the right-hand end of the coil shaft. Thev gear ll is designed to makeone complete revolution. for the time it takes the roller 2 to travel on its-conductive rod 2 from one end of the coil-to the other.
In the direction'of rotation of the gear 12,.
as indicated by the dotted arrow 86, the roller 2 as s een in-Fig. 3.- The actuator H is shown dotted in Fig. 4 at a position just prior to the roller reaching this. limit of travel. With the next stepping: movement of the Geneva gear 12, the
actuator will rock-the armature 10 towards the holding, relay l6 and-also throw the switches [2 and I3' to theiropposite contacts as heretofore explained. A stop pin 81, carried by an end cover plate 88, serves to limit further travel of actuator H and gear 12. The motor having thus reversed its direction of operation, the gear will rotate in the opposite direction, or as indicated by the solid arrow 89. If the coil does not pass through resonance, gear 12 will be rotated to said opposite limit of its travel, the actuator 1| being indicated at that position in full lines, where it is in contact with the stop pin 81. Just prior to reaching this limiting position, H coacts with arm 13 to withdraw the armature H! from relay l6 and releases the pressure of member 15 on switch arms l2 and [3 to cause their return to the position shown in Fig. 1. The cycle will then start anew and continue to operate until a tuning position corresponding to the transmitted carrier is 10- cated, or until the transmitter is shut down. I
' For tuning the antenna coil manually there is provided a hand wheel or crank 90 at the end of a shaft 9! which is provided at its other end with a transverse slot 92 adapted to receive a similarly shaped extension 93 on the coil shaft Hi. Normally parts 92 and 93 are disengaged due to the action of a coil spring 94. When it is desired to manually adjust the tuning coil, crank 90 is pressed in to permit engagement between the female portion of shaft 9|, and the male portion of shaft 16. The crank is then rotated until the antenna circuit is tuned to resonance, which condition will'be indicated by the maximum deflection of the tuning meter 31 (see Fig. 1). In manual operation the coupling between the driving shaft 9| and the driven shaft 16 is direct. The gear 80, however, is rotated through pinion [9 to provide rotation of a calibrated antenna tuning dial 95, which dial is directly coupled to gear 12. The calibrations of dial 95 are viewable through an opening 96 formed in a cover plate While I have shown a particular embodiment of my invention, it will, of course,-be understood that I do not wish to be limited thereto, since various modifications may be made in the circuit arrangement, in the instrumentalities, and in the mechanical construction employed without departing from the spirit and scope of my invention as set forth in the appended claims, and I contemplate by the appended claims to' cover any such modifications as fall within the true spirit and scope of my invention.
What I claim is:
1. In a circuit arrangement comprising an cs cillatory circuit having a component thereof variable in opposite directions over a predetermined range of mechanical movement to tune said oscillatory circuit over a prearranged frequency spectrum, a control system operative upon application of alternating currents to said oscillatory circuit to vary said component to tune said oscillatory circuit substantially to resonance with said alternating currents, said control system including a power operated device, means controlled by said power operated device to vary said component in one direction to one extremity of said rangeof movement and thereupon to vary said component in the other direction toward the other extremity of said range of movement, a control circuit associated with said power operated device to cease said variation of said component in said other direction at a position of said component at which resonance of said oscillatory circuit with said alternatingcurrents is obtained,
said control circuit comprising means to derive a unidirectional voltage proportional to said alternating currents, said voltage increasing rapidly as resonance is approached to a maximum at resonance and decreasing in complementary manner after resonance is passed, an electron discharge system having at least a cathode element,-
a control element and an anode element, a relay having the actuating winding thereof connected to said anode element and having an armature coupled in circuit with said power operated device to render the same operable when said electron discharge system is conducting, and means to render said electron discharge system conducting to initiate said variation of saidcomponentbysaid power operated device, the improvement comprising a network to which a portion of said voltage is applied to derive a bi-directional voltage in creasing rapidly in one direction as resonance is approached, reversing and passing through zero at resonance, and reversing and decreasing in complementary manner after resonance is passed, means to combine said voltages to produce a resultant voltage increasing rapidly in one direction only as resonance is passed, and means to apply said resultant voltage to said control element of said electron discharge system to block" the same when said component is at a position tuning said oscillatory circuit substantially to resonance with said alternating currents, thereby to deenergize said relay and cause cessation of said variation of said component.
2. In a circuit arrangement comprising an oscillatory circuit having a component thereof variable over a predetermined range of mechan-' ical movement to tune said oscillatory circuit over a prearranged frequency spectrum, a control" system operative upon application of alternating currents to said oscillatory circuit to vary said component to tune said oscillatory circuit substantially to resonance with said alternating currents, said control system including a power operated device arranged to vary said element from one extremity toward the other extremity of said range of movement, a control circuit associated with said power operated device to cease said variation at a position of said component at which resonance of said oscillatory" circuit with said alternating currents is obtained, said control circuit comprising means to derive a unidirectional Voltage proportional to said alternating currents, said voltage rapidly as resonance is approached to a maxi mum at resonance and decreasing in correspond means to render said electron discharge conduct-" ing to initiate said variation of said element by said power operated device, the improvement comprising a network to which a portion of said voltage is applied to derive a bi-directional volt-"- age increasing rapidly in one direction as resonance is approached, reversing and passingthrough zero at resonance, and reversing and decreasing in corresponding manner after resonance -ispassed, means to combine said voltages to produce a resultant voltage increasing rapidly in one direction only as resonance is passed, and means to apply said resultant voltage to said control element of said electron discharge sys- =tem to block the same when said component is I increasing at a position tuning said oscillatory circuit substantially to resonance with said alternating currents, thereby to deenergize said relay and cause cessation of said variation of said component.
3. In a circuit arrangement comprising an oscillatory circuit having a tuning component reversibly variable over a predetermined range of mechanical movement to tune said oscillatory circuit over a prearranged frequency spectrum, a control system operative upon application of alternating currents to said oscillatory circuit to adjust said component to tune said oscillatory circuit substantially to resonance with said altcrnating currents, said control system including a reversible motor, mechanical linkage under the control of said motor to drive said component in one direction to one extremity of said range of movement and thereupon to drive said component in the opposite direction toward the other extremity of said range of movement, a control circuit electrically associated with said motor to cease said adjustment at a position of said component at which resonance of said oscillatory circuit with said alternating currents is obtained, said control circuit comprising a rectifier coupled to said oscillatory circuit to derive a unidirectional voltage proportional to the alternating current therein, an electron discharge system having at least a cathode element, a control grid and an anode, a relay having the actuating winding thereof connected to said anode and having an armature coupled in circuit with said power operated device to render the same operable when said electron discharge system is conducting, and a switch arranged to alter the bias on said electron discharge system to render the same conducting to drive said component in said one direction by said motor, a differentiating network coupled to said rectifier to derive a bi-directional Voltage increasing rapidly in one direction as resonance is approached, reversing and passing through zero at resonance, and reversing and decreasing in corresponding manner after resonance is passed, means to combine said voltages to produce a resultant voltage increasing rapidly in one direction only as resonance is passed, and means to apply said resultant voltage to the control grid of said electron discharge system to block the same when said component is adjusted to tune said oscillatory circuit substantially to resonance with said alternating current, thereby to deenergize said relay and halt the progress of said motor.
4. In a circuit arrangement comprising an oscillatory circuit having a tuning component reversiblv variable over a predetermined range of mechanical movement to tune said oscillatory circuit over a prearranged frequency spectrum, a control system operative upon application of alternating currents to said oscillatory circuit to adjust said component to tune said oscillatory circuit substantially to resonance with said alternating currents, said control system including a reversible motor, mechanical linkage under the control of said motor to drive said component in one direction to one extremity of said range of movement and thereupon to drive said component in the opposite direction toward the other extremity of said range of movement, a control cireuit electrically associated with said motor to cease said adjustment at a position of said component at which resonance of said oscillatory circuit with said alternating currents is obtained, said control circuit comprising a transformer coupled to said oscillatory circuit, a rectifier coupled to said transformer to derive a unidirectional voltage proportional to the alternating current therein, an electron discharge system having at least a cathode element, a control grid and an anode, a relay having the actuating winding thereof connected to said anode and having an armature coupled in circuit with said power operated device to render the same operable when said electron discharge system is conducting, and a switch arranged to alter the bias on said electron discharge system to render the same conducting to drive said component in said one direction by said motor, an amplifying electron discharge system coupled to said rectifier and a differentiating network to derive a differential voltage, means to combine said voltages to produce a resultant voltage increasing rapidly in one direction only as resonance is passed, and means to apply said resultant voltage to the control grid of said electron discharge system to block the same when said component is adjusted to tune said oscillatory circuit substantially to resonance with said alternating current, thereby to deenergize said relay and halt the progress of said motor.
5. A control system for tuning an oscillatory circuit having a component Variable over a predetermined range of mechanical movement to tune said oscillatory circuit over a prearranged frequency spectrum, including a power device to drive said component over said range of movement, and a control circuit to interrupt said power device upon said component reaching a position at which said oscillatory circuit is tuned to resonance with a signal applied thereto, said control circuit comprising means to derive a voltage proportional to the current flowing in said oscillatory circuit, said voltage having a waveform rising to a maximum at the frequency at which resonance is obtained, means to alter the waveform of said voltage to produce a potential having a waveform having an intermediate value at the frequency at which resonance is obtained, electron discharge means coupled to control said power device and biased to maintain said power device normally operative, and means to apply said potential to said electron discharge means to block the same when said potential attains said intermediate Value thereby to render said power device inoperative.
WM. B. MORRISON.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 793,777 Fessenden July 4, 1905 1,395,987 Round Nov. 1, 1921 1,620,204 Heising Mar. 8, 1927 1,626,724 Demarest et a1. May 3, 1927 1,684,261 Brown ept. 11, 1928 1,794,932 Usselman Mar. 3, 1931 1,819,904 Love Aug. 18, 1931 1,907,965 Hansell May 9, 1933 2,098,331 Bowman Nov. 9, 1937 2,175,554 Bliss Oct. 10, 1939 2,262,218 Andrews Nov. 11, 1941 2,270,917 Appleton Jan. 27, 1942 2,297,800 Read Oct. 6, 1942 2,304,871 Andrews Dec. 15, 1942 2,363,285 Bartholy Nov. 21, 1944 (Other references on following page) UNITED STATES PATENTS FOREIGN PATENTS Number Name Date Number Country Date 2,369,542 Dietrich Feb. 13, 1945 425,626 Great Britain Mar. 19, 1935 2,375,133 Polkinghorn May 1, 1945 5 2,382,203 Chandler Aug. 14, 1945, OTHER REFERENCES 2,462,856 Ginzton Mar. 1, 1949 Ser. No. 363,862, Dolle et al. (A. C.) published May 25, 1943.
US584393A 1945-01-22 1945-03-23 Antenna tuning control system Expired - Lifetime US2498340A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA2498340X 1945-01-22

Publications (1)

Publication Number Publication Date
US2498340A true US2498340A (en) 1950-02-21

Family

ID=4176219

Family Applications (1)

Application Number Title Priority Date Filing Date
US584393A Expired - Lifetime US2498340A (en) 1945-01-22 1945-03-23 Antenna tuning control system

Country Status (1)

Country Link
US (1) US2498340A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2755375A (en) * 1951-06-07 1956-07-17 Bendix Aviat Corp Remote frequency control
US2810070A (en) * 1954-06-18 1957-10-15 Acf Ind Inc Automatic antenna tuner
US2824220A (en) * 1953-11-25 1958-02-18 Aeronautical Comm Equipment In Radio transmitter tuner
US2886752A (en) * 1957-01-31 1959-05-12 Collins Radio Co Servosystem adapted for automatic adjustment of radio transmitters

Citations (20)

* 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.
US1395987A (en) * 1921-03-24 1921-11-01 Rca Corp Wireless signaling apparatus
US1620204A (en) * 1924-12-29 1927-03-08 Western Electric Co Frequency indication and control
US1626724A (en) * 1923-12-31 1927-05-03 American Telephone & Telegraph Frequency-controlling system
US1684261A (en) * 1925-12-29 1928-09-11 Gen Electric Automatic antenna regulator
US1794932A (en) * 1927-09-01 1931-03-03 Rca Corp Frequency modulation
US1819904A (en) * 1927-08-12 1931-08-18 Gen Electric Antenna regulator
US1907965A (en) * 1927-11-01 1933-05-09 Rca Corp Automatic tuning
GB425626A (en) * 1933-09-30 1935-03-19 Leonard Hildersley Brown A device for automatic and remote control of tuning apparatus in radio receiving sets
US2098331A (en) * 1934-04-21 1937-11-09 Bowman William John Automatic station selector for radio receivers
US2175554A (en) * 1936-11-14 1939-10-10 Bliss Morse Res Corp Variable inductance
US2262218A (en) * 1938-07-18 1941-11-11 Edward F Andrews Radio receiver
US2270917A (en) * 1939-02-08 1942-01-27 Rca Corp Electrical remote control system
US2297800A (en) * 1941-11-01 1942-10-06 Westinghouse Electric & Mfg Co Standard frequency oscillator
US2304871A (en) * 1938-07-18 1942-12-15 Edward F Andrews Radio receiver
US2363285A (en) * 1940-10-16 1944-11-21 Westinghouse Electric & Mfg Co Remote control
US2369542A (en) * 1937-12-10 1945-02-13 Dietrich Hans Leo Receiver
US2375133A (en) * 1940-09-24 1945-05-01 Bell Telephone Labor Inc Automatic tuning
US2382203A (en) * 1944-01-12 1945-08-14 Colonial Radio Corp Automatic tuning control circuit
US2462856A (en) * 1942-05-19 1949-03-01 Sperry Corp Transmitter and/or receiver circuits

Patent Citations (20)

* 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.
US1395987A (en) * 1921-03-24 1921-11-01 Rca Corp Wireless signaling apparatus
US1626724A (en) * 1923-12-31 1927-05-03 American Telephone & Telegraph Frequency-controlling system
US1620204A (en) * 1924-12-29 1927-03-08 Western Electric Co Frequency indication and control
US1684261A (en) * 1925-12-29 1928-09-11 Gen Electric Automatic antenna regulator
US1819904A (en) * 1927-08-12 1931-08-18 Gen Electric Antenna regulator
US1794932A (en) * 1927-09-01 1931-03-03 Rca Corp Frequency modulation
US1907965A (en) * 1927-11-01 1933-05-09 Rca Corp Automatic tuning
GB425626A (en) * 1933-09-30 1935-03-19 Leonard Hildersley Brown A device for automatic and remote control of tuning apparatus in radio receiving sets
US2098331A (en) * 1934-04-21 1937-11-09 Bowman William John Automatic station selector for radio receivers
US2175554A (en) * 1936-11-14 1939-10-10 Bliss Morse Res Corp Variable inductance
US2369542A (en) * 1937-12-10 1945-02-13 Dietrich Hans Leo Receiver
US2262218A (en) * 1938-07-18 1941-11-11 Edward F Andrews Radio receiver
US2304871A (en) * 1938-07-18 1942-12-15 Edward F Andrews Radio receiver
US2270917A (en) * 1939-02-08 1942-01-27 Rca Corp Electrical remote control system
US2375133A (en) * 1940-09-24 1945-05-01 Bell Telephone Labor Inc Automatic tuning
US2363285A (en) * 1940-10-16 1944-11-21 Westinghouse Electric & Mfg Co Remote control
US2297800A (en) * 1941-11-01 1942-10-06 Westinghouse Electric & Mfg Co Standard frequency oscillator
US2462856A (en) * 1942-05-19 1949-03-01 Sperry Corp Transmitter and/or receiver circuits
US2382203A (en) * 1944-01-12 1945-08-14 Colonial Radio Corp Automatic tuning control circuit

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2755375A (en) * 1951-06-07 1956-07-17 Bendix Aviat Corp Remote frequency control
US2824220A (en) * 1953-11-25 1958-02-18 Aeronautical Comm Equipment In Radio transmitter tuner
US2810070A (en) * 1954-06-18 1957-10-15 Acf Ind Inc Automatic antenna tuner
US2886752A (en) * 1957-01-31 1959-05-12 Collins Radio Co Servosystem adapted for automatic adjustment of radio transmitters

Similar Documents

Publication Publication Date Title
US2098331A (en) Automatic station selector for radio receivers
US2245829A (en) Remote control system
US2025218A (en) Remote control apparatus for radioreceivers
US2498340A (en) Antenna tuning control system
US2462856A (en) Transmitter and/or receiver circuits
US2426580A (en) Radio receiver
US2930955A (en) Remote control system for a television receiver
US2245347A (en) Radio remote control system
US1883163A (en) Remote control device
US2550430A (en) Electronically controlled tuner
US2044645A (en) Radio receiving system
US2666853A (en) Stop-on-signal radio apparatus
US2218905A (en) Wireless and like receiver, and tuning control apparatus for use therewith
US2078060A (en) Remote control system for radio receivers
US2063295A (en) Radio receiver
GB649537A (en) Improvements in stop-on-signal radio apparatus
US2491020A (en) Echo ranging apparatus
US2541018A (en) Stop-on-signal radio apparatus
US2011953A (en) Electrical transmission system
US2490591A (en) Motor-driven tuning control for radio receivers
US2404101A (en) Remote control of radio receivers
US2474527A (en) Remote-control system
US2210425A (en) Automatic tuning control system
US2000084A (en) Short wave receiver arrangement
US2155882A (en) Teletype apparatus