US2561417A - Impedance matched frequency converter - Google Patents

Impedance matched frequency converter Download PDF

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US2561417A
US2561417A US596949A US59694945A US2561417A US 2561417 A US2561417 A US 2561417A US 596949 A US596949 A US 596949A US 59694945 A US59694945 A US 59694945A US 2561417 A US2561417 A US 2561417A
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transmission
energy
impedance
section
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Alden H Ryan
John P Hagen
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    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03DDEMODULATION OR TRANSFERENCE OF MODULATION FROM ONE CARRIER TO ANOTHER
    • H03D9/00Demodulation or transference of modulation of modulated electromagnetic waves
    • H03D9/06Transference of modulation using distributed inductance and capacitance
    • H03D9/0608Transference of modulation using distributed inductance and capacitance by means of diodes
    • H03D9/0616Transference of modulation using distributed inductance and capacitance by means of diodes mounted in a hollow waveguide

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  • This invention relates to transmission-line sections and particularly to a transmission-line section into which may be coupled two independent sources of electrical energy and from which'electricalenergy may be derived from a point on the section matching the impedanceof the energy deriving means.
  • an object of this invention is to produce a heterodyning device in. which maximum transfer of energy is provided by impedance matching.
  • Another object of the invention is; to produce a heterodyning device to which energy may be applied and from which energy may be derived at a point thereon such that the impedance of the energy-deriving means is matched to that of the device.
  • Another object of the invention is to produce, in the form or a transmission-line section, a heterodyning device from which heterodyned en'- ergy may be removed at a point matchinga the impedance of the energy-removing means.
  • a further object of the invention is tocreate a heterodyning device, in the form of a transmission-line section, to which energymay be applied at a point on the section matching the impedance of the energy-applying means and from which energy may be derived at a point on the section matching the impedance of the energy-deriving means.
  • the present invention will now be described as comprising a resonant transmission-line section having the prop.- erty that the impedance looking into. the line section varies along its length.
  • a first source of energy from a receiving antenna.
  • This coupling is made at a point on the line section such that the impedance of the section at that point applied to the line are heterodyned to produce a beat.
  • Energy of the beat frequency is derived from the section by a detecting means coupled; thereinto at a point matching the impedance of the detecting means, thereby providing maximum energy transfer from the line section to the detecting means.
  • A. transmission-line section in the form of a. resonant transmission line in the form of a. resonant transmission line, equal in length to an odd number of quarter wave lengths at the frequency of. the energy within the line, presents an impedance looking into. the line at any point which varies as a sine relation along the line, as will bemore fully explained hereinafter.
  • the impedance looking into the section will be a minimum (zero) at the short-circuited. end of. the line, will rise to.
  • the impede ance of the section will be of very low magnitude.
  • the detecting means is connected between transmission-line conductors, the exact point being chosen in accordance with the im pedance of the detecting means.
  • FIG. 3 shows a cross section of the transmission-line section taken along line 33 of Figs. 1 and 2;
  • Fig. 4 shows a schematic diagram depicting the equivalent circuit of the transmission-line section.
  • line section is shown in the form of a coaxial transmission line having an outer conductor I and an inner conductor H.
  • Conductor I0 is closed at one end thereof by a wall I2 and at the other end thereof by a cylindrical plug I3.
  • Plug I3 also constitutes a short-circuiting memb'er'for one 'end of the line section, supporting Portion l of inner conductor I I is movable axially within a portion- I4 ofthe inner conductor ll.
  • portion I4 of inner conductor II extends therethrough into the chamber formed by outer conductor I0 and wall l2.
  • At the other end-portion l5 extends exteriorly of the outer conductor [0 and terminates in a threaded member I6 having a knurled tuning knob IT.
  • a boss 20, integral with plug I3 and portion I4 of inner conduetor II, is threaded internally to receive threaded mernber Hi. It will be readily seen that rotationof knob I! will shorten or lengthen the transmission line, comprised of conductors I0 and II, by virtue of the axial movement of portion I5 of inner conductor II thereby produced.
  • the distance'between the short-circuited end of the transmission-line section at plug I 3 and the open-circuited end of the line seetiori at the end of inner conductor II is made approximately equal to three-quarters wavelengthG/m) at the operating frequency of thesection.
  • Transmission line-2i carries received energy from an antenna and is terminated in a coupling loop23.
  • Transmission line 22 is terminated in a conducting button 24 forming capacitive coupling between transmission line 22 and inner conductor II.
  • line 22 is disposed on the opposite side of conductor II from line 2
  • a detecting means is connected between the inner and outer condoctors.
  • the de tecting means comprises a crystal contained within crystal holder 25. Crystal holder 25 is inserted into the space between conductors I0 and l I' through an opening 26 in outer conductor Ill. Contact between the crystal and inner conductor I! is made through spring clips 27 attached to portion Id of inner conductor II. The other terminal of the crystal is connected to a conducting member 30 which is in turn connected to-the inner conductor of a coaxial trans- Referring to the drawings, the transmission- 4 mission line 3
  • Conducting member 30 is separated from plate 32, bearing the entire crystal assembly, by an annular mica insulator 33 which forms a capacitive connection between outer conductor l0 and the inner conductor of transmission line 3
  • a cap 34 permits insertion and removal of crystal holder 25.
  • Screws 35 anchored in outer conductor I0 extend through axially elongated slots in plate 32, thereby providing limited axial adjustment of crystal holder 25 with respect to spring clip 21. This permits adjustment-in the impedance point at which the crystal in holder 25 derives energy from the transmission-line section.
  • the beat frequency existing by virtue of the heterodyning of energy from transmission lines 2I and 22 is rectified in the crystal of holder 25 and the intermediate frequency component of the derived energy is transmitted through line 3
  • the high frequency components of the energy are'by-passed through the condenser formed by annular dielectric member 33 and do not-reach the vIF amplifier.
  • the input impedance to the transmission-line section thus described will vary as a sine funcs tion, as will be particularly described below.
  • the impedance at any point along the line is given approximately by the following relation:
  • the relationship above indicates that the input impedance along the line becomes zero at the short-circuited end of the line and at each half wavelength x) away therefrom; and becomes a maximum at every odd quarter wavelength AA, %X etc.) away from the short-circuited end of the transmission-line section. It will be noted further that this impedance is purely resistive.
  • the formula given above is very accurate for high values of Q.
  • the formula is least accurate 'in the region where x equals an odd half wavelength /370 but even in this region the deviation from the value of Z as calculated from the above formula isvery slight.
  • a transmission-line section was constructed having a Q of approximately 100 and a characteristic impedance, Z0, of approximately ohms.
  • the impedance at a distance one-half wavelength away from the shorted end of the transmission line i. e., where x e uals V H was calculated to be 0.4 ohm at a phase angle of .005 radians. It will be understood that the above values as calculated are only approximate, inasmuch as the end effect of wall I2 and other minor factors have been neglected. It will thus be seen that even at the oint of greatest in:
  • the formula given above is very close to the actual conditions encountered.
  • the detecting crystal in holder 25 had an impedance of approximately 200 ohms. Therefore, in order to match the impedance of the crystal to that of the line it was merely necessary to slide the crystal holder 25 along the line within spring clip 21, a distance equal to .04A away from the half-wave point.
  • maximum energy transfer from the antenna to the transmission-line seotion may be obtained by applying antenna line 2! to the line section at a low impedance point and making final adjustment in coupling by rotation of coupling loop 23.
  • antenna energy in transmission line 2! and energy derived from the transmission-line section by the detecting means it is important that the impedances be closely matched in order that maximum transfer of energy may take place.
  • the coupling of the detecting means to the transmission-line section is made direct, and the impedance relation-- ship between that of the crystal and that of the line section is in a one-to-one ratio.
  • the point of application of transmission line 21 to the transmission-line section need not neces" sarily be that point at which the impedance of the transmission line 2! matches the impedance of the transmission-line section. This is because of the impedance transformation taking place in the inductive coupling between the transmissionline section and the coupling loop 23.
  • the transmission-line section need not be necessarily three-quarters wavelength long so long as a resonant transmission line is used which will produce the impedance relation given by the approximate formula stated hereinbefore.
  • a coaxial transmission line section having an inner and an outer conductor, means for adjusting the length of the inner conductor, coaxial line and coupling loop means for applying energy to said section from one side thereof, the coupling loop being rotatable for impedance matching, coaxial line and capacitive coupling means for applying energy to said section on the opposite side of said section from said coaxial line and coupling loop means, and a non-linear impedance mem-- ber connected between the inner and. outer conductors of said section at a point on said section having an impedance that matches the impedance of said member.
  • a coaxial transmission line section having an outer conductor shorted at one end and having an inner conductor extending into the outer conductor a distance of wavelength from the shorted end, coaxial line and coupling loop means for applying energy to said section from one side thereof near the shorted end, the coupling loop being rotatable for impedance matching, coaxial line and capacitive coupling means for applying energy to said section on the opposite side of said section from said coaxial line and.

Description

July 24, 1951 A. H. RYAN HAL IMPEDANCE MATCHED FREQUENCY CONVERTER Filed May 51, 1945 l a y l6 Hi 0 mm 4 l2-. 27 I4 20} TO LE TO ANTENNA 33 25 I 2: I47 F I TO LOCAL OSCILLATOR Elma/whom ALDEN H. RYAN JOHN P. HAGEN wW W Patented July 24, 1951 IMPEDANCE MATCHED FREQUENCY CONVERTER Alden H. Ryan, Alexandria, and John P. Hagen, Arlington, Va.
Applicati'onMay 31, 1945, Serial No. 596,949
(Granted under the act of, March 3, 1883, as amended April 30,. 1928; 3700. G. 757) 2 Claims.
This invention relates to transmission-line sections and particularly to a transmission-line section into which may be coupled two independent sources of electrical energy and from which'electricalenergy may be derived from a point on the section matching the impedanceof the energy deriving means.
In heterodyning, or mixing, two separate sources of energy and deriving therefrom a single output energy, it is often desirable that maximum transfer of energy take place between the several energy transmitting means comprising the heterodyning system. To effect this result, it is necessary that the impedances of the means which feed, and the means which derives, energy from the heterodyning device match the impedance of the heterodyning device at the respective points of application thereto.
Therefore an object of this invention is to produce a heterodyning device in. which maximum transfer of energy is provided by impedance matching.
Another object of the invention. is; to produce a heterodyning device to which energy may be applied and from which energy may be derived at a point thereon such that the impedance of the energy-deriving means is matched to that of the device.
Another object of the invention is to produce, in the form or a transmission-line section, a heterodyning device from which heterodyned en'- ergy may be removed at a point matchinga the impedance of the energy-removing means.
A further object of the invention is tocreate a heterodyning device, in the form of a transmission-line section, to which energymay be applied at a point on the section matching the impedance of the energy-applying means and from which energy may be derived at a point on the section matching the impedance of the energy-deriving means.
With these objects in mind, the present invention will now be described as comprising a resonant transmission-line section having the prop.- erty that the impedance looking into. the line section varies along its length. Into the transmission line section is coupled a first source of energy from a receiving antenna. This coupling is made at a point on the line section such that the impedance of the section at that point applied to the line are heterodyned to produce a beat. Energy of the beat frequency is derived from the section by a detecting means coupled; thereinto at a point matching the impedance of the detecting means, thereby providing maximum energy transfer from the line section to the detecting means.
A. transmission-line section in the form of a. resonant transmission line, equal in length to an odd number of quarter wave lengths at the frequency of. the energy within the line, presents an impedance looking into. the line at any point which varies as a sine relation along the line, as will bemore fully explained hereinafter. By constructing the transmission-line section short circuited atone end and open circuited at the other end, and equal in length to threeequarters wavelength (%A) of the energy coupled into the line, the impedance looking into the section will be a minimum (zero) at the short-circuited. end of. the line, will rise to. a maximum, depending on the Q10f the line, at a point one-quarter wavelength (MQO away from the short-circuited end, and will drop to a minimum (almost zero) at a point one-half wavelength /2).) away from the short-circuited end of the transmission-line section.
This property of a three quarter wavelength transmission-line section, short-circuited at one end and open circuited at the other, is made use of in the present invention in the following manner. In the vicinity of the short-circuited end of the line, energy from a receiving antenna is applied inductively as by loop coupling. Since in this region the line-section impedance is. low, impedance matching between the section. and the transmission line carrying energy from. the antenna may be readily accomplished, as by varying the coupling between the loop and the section. Into the line is also coupled a source of energy from a local oscillator tuned approximately to the frequency of the incoming antenna. energy. There isv thus produced the conventional intermediate frequency beat. A standing wave of energy thus exists, on the transmission-line section. which is tuned to an electrical length of threequarters wavelength (%A) at the frequency of the incoming antenna energy.
As explained hereinbefore, in the region onehalf wavelength away from the short-circuited end of the transmission line section, the impede ance of the section will be of very low magnitude. In this region thedetecting means is connected between transmission-line conductors, the exact point being chosen in accordance with the im pedance of the detecting means. i
' A particular embodiment of the heterodyning Fig. 3 shows a cross section of the transmission-line section taken along line 33 of Figs. 1 and 2; and
Fig. 4 shows a schematic diagram depicting the equivalent circuit of the transmission-line section.
line section is shown in the form of a coaxial transmission line having an outer conductor I and an inner conductor H. Conductor I0 is closed at one end thereof by a wall I2 and at the other end thereof by a cylindrical plug I3. Plug I3 also constitutes a short-circuiting memb'er'for one 'end of the line section, supporting Portion l of inner conductor I I is movable axially within a portion- I4 ofthe inner conductor ll.
portion I4 of inner conductor II, and extends therethrough into the chamber formed by outer conductor I0 and wall l2. At the other end-portion l5 extends exteriorly of the outer conductor [0 and terminates in a threaded member I6 having a knurled tuning knob IT. A boss 20, integral with plug I3 and portion I4 of inner conduetor II, is threaded internally to receive threaded mernber Hi. It will be readily seen that rotationof knob I! will shorten or lengthen the transmission line, comprised of conductors I0 and II, by virtue of the axial movement of portion I5 of inner conductor II thereby produced. In the particular embodiment under description, the distance'between the short-circuited end of the transmission-line section at plug I 3 and the open-circuited end of the line seetiori at the end of inner conductor II is made approximately equal to three-quarters wavelengthG/m) at the operating frequency of thesection.
Into the transmission-line section thus described and shown schematically in Fig. 4 are coupled two sources of energy from coaxial transmission lines zl and 22, respectively. Transmission line-2i carries received energy from an antenna and is terminated in a coupling loop23. Transmission line 22 is terminated in a conducting button 24 forming capacitive coupling between transmission line 22 and inner conductor II. In order to minimize direct coupling between these two sources of energy, line 22 is disposed on the opposite side of conductor II from line 2|.
In this manner two sources 'of energy of approximately the same frequency may be hetero dyned within the transmission line section.
At a point approximately one-half wavelength away from the short-circuited end of the transmission-line section, a detecting means is connected between the inner and outer condoctors. in the present embodiment, the de tecting means comprises a crystal contained within crystal holder 25. Crystal holder 25 is inserted into the space between conductors I0 and l I' through an opening 26 in outer conductor Ill. Contact between the crystal and inner conductor I! is made through spring clips 27 attached to portion Id of inner conductor II. The other terminal of the crystal is connected to a conducting member 30 which is in turn connected to-the inner conductor of a coaxial trans- Referring to the drawings, the transmission- 4 mission line 3|. Conducting member 30 is separated from plate 32, bearing the entire crystal assembly, by an annular mica insulator 33 which forms a capacitive connection between outer conductor l0 and the inner conductor of transmission line 3|. A cap 34 permits insertion and removal of crystal holder 25. Screws 35 anchored in outer conductor I0 extend through axially elongated slots in plate 32, thereby providing limited axial adjustment of crystal holder 25 with respect to spring clip 21. This permits adjustment-in the impedance point at which the crystal in holder 25 derives energy from the transmission-line section.
The beat frequency existing by virtue of the heterodyning of energy from transmission lines 2I and 22 is rectified in the crystal of holder 25 and the intermediate frequency component of the derived energy is transmitted through line 3| to a conventional intermediate frequency amplifier. The high frequency components of the energy are'by-passed through the condenser formed by annular dielectric member 33 and do not-reach the vIF amplifier. i
The input impedance to the transmission-line section thus described will vary as a sine funcs tion, as will be particularly described below. The impedance at any point along the line is given approximately by the following relation:
mission-line section. )\='wavelength {of energy applied to transmission.
line section.
The relationship above indicates that the input impedance along the line becomes zero at the short-circuited end of the line and at each half wavelength x) away therefrom; and becomes a maximum at every odd quarter wavelength AA, %X etc.) away from the short-circuited end of the transmission-line section. It will be noted further that this impedance is purely resistive. The formula given above is very accurate for high values of Q. The formula is least accurate 'in the region where x equals an odd half wavelength /370 but even in this region the deviation from the value of Z as calculated from the above formula isvery slight. In a particular embodiment a transmission-line section was constructed having a Q of approximately 100 and a characteristic impedance, Z0, of approximately ohms. With these parameters, the impedance at a distance one-half wavelength away from the shorted end of the transmission line, i. e., where x e uals V H was calculated to be 0.4 ohm at a phase angle of .005 radians. It will be understood that the above values as calculated are only approximate, inasmuch as the end effect of wall I2 and other minor factors have been neglected. It will thus be seen that even at the oint of greatest in:
accuracy the formula given above is very close to the actual conditions encountered. In the transmission-line section actually constructed the detecting crystal in holder 25 had an impedance of approximately 200 ohms. Therefore, in order to match the impedance of the crystal to that of the line it was merely necessary to slide the crystal holder 25 along the line within spring clip 21, a distance equal to .04A away from the half-wave point.
In like manner, maximum energy transfer from the antenna to the transmission-line seotion may be obtained by applying antenna line 2! to the line section at a low impedance point and making final adjustment in coupling by rotation of coupling loop 23. No attempt is generally made to match the impedance of trans mission line 22 to that of the transmission-line section, inasmuch as a great deal of energy is available from the local oscillator, and no effort need be made to conserve it. However, in the case of antenna energy in transmission line 2! and energy derived from the transmission-line section by the detecting means, it is important that the impedances be closely matched in order that maximum transfer of energy may take place. For the embodiment illustrated, the coupling of the detecting means to the transmission-line section is made direct, and the impedance relation-- ship between that of the crystal and that of the line section is in a one-to-one ratio. However, the point of application of transmission line 21 to the transmission-line section need not neces" sarily be that point at which the impedance of the transmission line 2! matches the impedance of the transmission-line section. This is because of the impedance transformation taking place in the inductive coupling between the transmissionline section and the coupling loop 23. In. order to attain optimum impedance matching between transmission line 2| and the transmission-line section, it is simply necessary to rotate coupling loop 23 thereby varying the coupling and hence the impedance transformation ratio.
While the specific embodiment shown and described herein, illustrates the antenna coupling as being of the inductive type, the local oscillator as being of the capacitive type, and the detector coupling as being of the conductive type, it is obvious that for most purposes these three types are interchangeable. Accordingly, it will be understood that the invention is not limited to a particular type of coupling for any particular purpose.
It will be readily apparent that the transmission-line section need not be necessarily three-quarters wavelength long so long as a resonant transmission line is used which will produce the impedance relation given by the approximate formula stated hereinbefore.
It is to be understood that the embodiment of this invention described above is exemplary only;
and the scope thereof is not to be limited to this description, but will be pointed out more panticularly in the appended claims.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
What is claimed is:
1. In a device for heterodyning energy, a coaxial transmission line section having an inner and an outer conductor, means for adjusting the length of the inner conductor, coaxial line and coupling loop means for applying energy to said section from one side thereof, the coupling loop being rotatable for impedance matching, coaxial line and capacitive coupling means for applying energy to said section on the opposite side of said section from said coaxial line and coupling loop means, and a non-linear impedance mem-- ber connected between the inner and. outer conductors of said section at a point on said section having an impedance that matches the impedance of said member.
2. In a device for heterodyning energy, a coaxial transmission line section having an outer conductor shorted at one end and having an inner conductor extending into the outer conductor a distance of wavelength from the shorted end, coaxial line and coupling loop means for applying energy to said section from one side thereof near the shorted end, the coupling loop being rotatable for impedance matching, coaxial line and capacitive coupling means for applying energy to said section on the opposite side of said section from said coaxial line and. coupling loop means, and a crystal rectifier connected between the inner and outer conductors of said section at a point A; wavelength from the shorted end. thereof.
ALDEN H. RYAN. JOHN P. I-IAGEN.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,142,159 Southworth et a1. Jan. 3, 1939 2,177,272 Zottu W Oct. 24, 1939 2,236,004 MacLean Mar. 2 5, 1941 2,408,420 Ginzton Oct. 1, 1946 2,423,416 Sontheimer et al. -1" July 1, 1947 2,433,386 Montgomery W Dec. 30, 1947 2,433,387 Mumford Dec. 30, 1947 2,436,830 Sharpless Mar. 2, 1948 2,455,657 Cork et al. Dec. 7, 1948 2,469,222 Atwood et al. May 3, 1949
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2712062A (en) * 1949-04-12 1955-06-28 Rca Corp Converter circuits
US2748354A (en) * 1950-05-31 1956-05-29 Gen Electric Wide band television tuning circuit
US2787705A (en) * 1951-06-25 1957-04-02 Hazeltine Research Inc High-frequency wave-signal tuning device
DE1065026B (en) * 1956-10-30 1959-09-10 Standard Elek K Lorenz Ag Waveguide bridge circuit for microwaves
US2918636A (en) * 1956-11-27 1959-12-22 Adler Electronics Inc Resonant unit
US3111629A (en) * 1959-01-07 1963-11-19 Microwave Ass Reactance or parametric amplifier
US3324425A (en) * 1965-06-24 1967-06-06 Varian Associates Adjustable electromagnetic coupling apparatus
US3638126A (en) * 1969-08-21 1972-01-25 George Ctirad Spacek High-frequency converter

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US2142159A (en) * 1939-01-03 Apparatus for receiving electromag
US2177272A (en) * 1936-04-22 1939-10-24 Rca Corp Short wave electron discharge system
US2236004A (en) * 1938-07-30 1941-03-25 Rca Corp Ultra high frequency signaling system
US2408420A (en) * 1944-01-13 1946-10-01 Sperry Gyroscope Co Inc Frequency multiplier
US2423416A (en) * 1944-03-30 1947-07-01 Rca Corp Nonfrequency-selective reflectometer
US2433387A (en) * 1943-12-31 1947-12-30 Bell Telephone Labor Inc Ultra high frequency receiver
US2433386A (en) * 1941-09-26 1947-12-30 Standard Telephones Cables Ltd Ultra high frequency mixer circuit
US2436830A (en) * 1943-04-19 1948-03-02 Bell Telephone Labor Inc Transmission system and method
US2455657A (en) * 1942-09-01 1948-12-07 Emi Ltd Circuit arrangement for mixing oscillations
US2469222A (en) * 1943-12-01 1949-05-03 Rca Corp Crystal rectifier converter

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2142159A (en) * 1939-01-03 Apparatus for receiving electromag
US2177272A (en) * 1936-04-22 1939-10-24 Rca Corp Short wave electron discharge system
US2236004A (en) * 1938-07-30 1941-03-25 Rca Corp Ultra high frequency signaling system
US2433386A (en) * 1941-09-26 1947-12-30 Standard Telephones Cables Ltd Ultra high frequency mixer circuit
US2455657A (en) * 1942-09-01 1948-12-07 Emi Ltd Circuit arrangement for mixing oscillations
US2436830A (en) * 1943-04-19 1948-03-02 Bell Telephone Labor Inc Transmission system and method
US2469222A (en) * 1943-12-01 1949-05-03 Rca Corp Crystal rectifier converter
US2433387A (en) * 1943-12-31 1947-12-30 Bell Telephone Labor Inc Ultra high frequency receiver
US2408420A (en) * 1944-01-13 1946-10-01 Sperry Gyroscope Co Inc Frequency multiplier
US2423416A (en) * 1944-03-30 1947-07-01 Rca Corp Nonfrequency-selective reflectometer

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2712062A (en) * 1949-04-12 1955-06-28 Rca Corp Converter circuits
US2748354A (en) * 1950-05-31 1956-05-29 Gen Electric Wide band television tuning circuit
US2787705A (en) * 1951-06-25 1957-04-02 Hazeltine Research Inc High-frequency wave-signal tuning device
DE1065026B (en) * 1956-10-30 1959-09-10 Standard Elek K Lorenz Ag Waveguide bridge circuit for microwaves
US2918636A (en) * 1956-11-27 1959-12-22 Adler Electronics Inc Resonant unit
US3111629A (en) * 1959-01-07 1963-11-19 Microwave Ass Reactance or parametric amplifier
US3324425A (en) * 1965-06-24 1967-06-06 Varian Associates Adjustable electromagnetic coupling apparatus
US3638126A (en) * 1969-08-21 1972-01-25 George Ctirad Spacek High-frequency converter

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