GB592271A - Superregenerative receiver - Google Patents

Superregenerative receiver

Info

Publication number
GB592271A
GB592271A GB1350/45A GB135045A GB592271A GB 592271 A GB592271 A GB 592271A GB 1350/45 A GB1350/45 A GB 1350/45A GB 135045 A GB135045 A GB 135045A GB 592271 A GB592271 A GB 592271A
Authority
GB
United Kingdom
Prior art keywords
quench
voltage
frequency
amplifier
control
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
Application number
GB1350/45A
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.)
BAE Systems Aerospace Inc
Original Assignee
Hazeltine 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 Hazeltine Corp filed Critical Hazeltine Corp
Publication of GB592271A publication Critical patent/GB592271A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03DDEMODULATION OR TRANSFERENCE OF MODULATION FROM ONE CARRIER TO ANOTHER
    • H03D11/00Super-regenerative demodulator circuits
    • H03D11/02Super-regenerative demodulator circuits for amplitude-modulated oscillations

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Circuits Of Receivers In General (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

592,271. Valve receiving circuits; automatic gain control. HAZELTINE CORPORATION. Jan. 16, 1945, No. 1350. Convention date, Feb. 11, 1944. [Class 40 (v)] In a super-regenerative receiver, a control potential is developed dependent on an operating condition of the receiver to vary the characteristic of the quench voltage. Both amplitude and frequency of the quench voltage may be varied by the control potential to cause variations in the band width or sensitivity of the receiver. The control potential may be derived, from a separate aerial or a preceding radio frequency amplifier. The valve 10<1>, Fig. 3, connected to the tuned circuit comprising an inductance 11 and stray capacity C<1> is fed with a quench voltage over transformer 141 from the heptode 17<1>, the inner grid and anode of which are connected in an oscillatory circuit consisting of an inductance 19<1> and condenser 20<1> with feedback coil 22<1>. In the absence of an incoming signal, the receiver noise causes valve 10<1> to oscillate-during each positive cycle of the quench voltage, the oscillations being rectified.by diode 30<1> to produce a voltage across the load resistance 33<1>. The quench frequency component, fed through amplifier 411 and rectifier 42<1> develops a control potential across potentiometers 43, 44 having their centre taps earthed. The potential on the slider of potentiometer, 44 varies the bias on the outer control grid of heptode 17<1> to vary the gain and hence the amplitude of the quench voltage. The potential of the slider of potentiometer 43 is applied to the grid of reactance valve 25, the anode of which is back coupled to the grid over condenser 26, to .cause variations in the frequency generated by the inner electrodes of the heptode 17<1>. By suitable adjustment of the sliders on potentiometers 43, 44, the band width or sensitivity of the receiver, may be maintained constant or varied according to any desired law. The demodulated signal appearing across load resistances 33<1> is fed to a normal amplifier, pulse modulated signals due to their low modulation frequency being ineffective in varying the control voltage developed across potentiometers 43, 44. When receiving C.W. signals,. the control voltage varies with the incoming signal to give an A.V.C. action. For the response of pulse modulated signals the amplifier 41<1> may be arranged to have the maximum response at some frequency less than the quench component and minimum response at that frequency, the control voltage being developed from the noise component. In a transponder for use as a beacon for an interrogating aircraft, Fig. 4, the grid of the receiving valve 60 is normally biassed off, the quench frequency oscillator 69, through the intermediate amplifier 71, removing the paralysing bias, periodically. The received signal is fed to the tuned circuit comprising inductance 61 and stray capacity C<11> over coupling condenser 86 and inductance 87, the amplified oscillations being rectified by diode 75. The quench frequency component appearing across the load 78 is passed through amplifier 81 to diode 82, the control voltage developed across load resistance 84 being used to vary the gain of the intermediate amplifier 71. The signal from load 78 also feeds a pulse generator 97 which is only operated by signals above a predetermined amplitude, the output pulsing the transmitter valve 90 which utilises the common tuned circuit 61, C<11> feeding the aerial 88. Due to the now of cathode current during the oscillations, condenser 94 charges up to terminate the pulse after a predetermined time, the condenser 94 discharging over resistance 95 between pulses. Specification 592,269 is referred to.
GB1350/45A 1944-02-11 1945-01-16 Superregenerative receiver Expired GB592271A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US521932A US2414992A (en) 1944-02-11 1944-02-11 Superregenerative receiver

Publications (1)

Publication Number Publication Date
GB592271A true GB592271A (en) 1947-09-12

Family

ID=24078726

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1350/45A Expired GB592271A (en) 1944-02-11 1945-01-16 Superregenerative receiver

Country Status (5)

Country Link
US (1) US2414992A (en)
BE (1) BE473729A (en)
ES (1) ES183398A1 (en)
FR (1) FR947556A (en)
GB (1) GB592271A (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL79489C (en) * 1943-03-13
US2468084A (en) * 1944-01-08 1949-04-26 Standard Telephones Cables Ltd Radio communicating system
US2532307A (en) * 1944-07-29 1950-12-05 Gerard C Hess Signal responsive system
US2501186A (en) * 1944-10-13 1950-03-21 Hazeltine Research Inc Wave-signal receiver
US2467564A (en) * 1944-10-13 1949-04-19 Hazeltine Research Inc Wave-signal receiver, including a disabling arrangement
US2454415A (en) * 1945-02-24 1948-11-23 Rca Corp Autoamtic gain control circuit
NL129550C (en) * 1945-09-29
US2572088A (en) * 1945-12-22 1951-10-23 Sperry Corp Ultra high frequency coded transmitter system utilizing stored energy received by the system
US2588444A (en) * 1946-02-27 1952-03-11 Ferranti Ltd Wave signal responder system
US2536801A (en) * 1946-03-01 1951-01-02 Philco Corp Superregenerative receiver
US2679043A (en) * 1946-05-21 1954-05-18 Us Sec War Beacon receiver
US2526267A (en) * 1946-09-24 1950-10-17 Hazeltine Research Inc Superregenerative wave-signal translating system
US2594916A (en) * 1947-11-26 1952-04-29 Rca Corp Automatic gain control circuits
US2679583A (en) * 1948-08-23 1954-05-25 Bendix Aviat Corp Superregenerative detector of frequency modulated signals
US2541981A (en) * 1948-09-17 1951-02-20 Ben R Smutek Concrete block packing machine

Also Published As

Publication number Publication date
US2414992A (en) 1947-01-28
FR947556A (en) 1949-07-06
BE473729A (en)
ES183398A1 (en) 1948-06-16

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