US2436700A - Cavity resonator oscillator - Google Patents

Cavity resonator oscillator Download PDF

Info

Publication number
US2436700A
US2436700A US520296A US52029644A US2436700A US 2436700 A US2436700 A US 2436700A US 520296 A US520296 A US 520296A US 52029644 A US52029644 A US 52029644A US 2436700 A US2436700 A US 2436700A
Authority
US
United States
Prior art keywords
shell
rod
frequency
cavity
tube
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
US520296A
Inventor
Sterling C Spielman
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.)
Space Systems Loral LLC
Original Assignee
Philco Ford 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
Priority to US504745A priority Critical patent/US2436706A/en
Application filed by Philco Ford Corp filed Critical Philco Ford Corp
Priority to US520296A priority patent/US2436700A/en
Priority to GB30888/45A priority patent/GB603262A/en
Application granted granted Critical
Publication of US2436700A publication Critical patent/US2436700A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03LAUTOMATIC CONTROL, STARTING, SYNCHRONISATION, OR STABILISATION OF GENERATORS OF ELECTRONIC OSCILLATIONS OR PULSES
    • H03L1/00Stabilisation of generator output against variations of physical values, e.g. power supply
    • H03L1/02Stabilisation of generator output against variations of physical values, e.g. power supply against variations of temperature only
    • H03L1/021Stabilisation of generator output against variations of physical values, e.g. power supply against variations of temperature only of generators comprising distributed capacitance and inductance
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R33/00Coupling devices specially adapted for supporting apparatus and having one part acting as a holder providing support and electrical connection via a counterpart which is structurally associated with the apparatus, e.g. lamp holders; Separate parts thereof
    • H01R33/05Two-pole devices
    • H01R33/06Two-pole devices with two current-carrying pins, blades or analogous contacts, having their axes parallel to each other
    • H01R33/08Two-pole devices with two current-carrying pins, blades or analogous contacts, having their axes parallel to each other for supporting tubular fluorescent lamp
    • H01R33/0836Two-pole devices with two current-carrying pins, blades or analogous contacts, having their axes parallel to each other for supporting tubular fluorescent lamp characterised by the lamp holding means
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03BGENERATION OF OSCILLATIONS, DIRECTLY OR BY FREQUENCY-CHANGING, BY CIRCUITS EMPLOYING ACTIVE ELEMENTS WHICH OPERATE IN A NON-SWITCHING MANNER; GENERATION OF NOISE BY SUCH CIRCUITS
    • H03B5/00Generation of oscillations using amplifier with regenerative feedback from output to input
    • H03B5/18Generation of oscillations using amplifier with regenerative feedback from output to input with frequency-determining element comprising distributed inductance and capacitance
    • H03B5/1817Generation of oscillations using amplifier with regenerative feedback from output to input with frequency-determining element comprising distributed inductance and capacitance the frequency-determining element being a cavity resonator
    • H03B5/1835Generation of oscillations using amplifier with regenerative feedback from output to input with frequency-determining element comprising distributed inductance and capacitance the frequency-determining element being a cavity resonator the active element in the amplifier being a vacuum tube

Definitions

  • an ultra high frequency oscillator particularly one of the type comprising a resonant cavity and a so-called lighthouse type triode.
  • a resonant cavity oscillation generator such as that hereinafter described, is designed to function at extremely high frequencies and is often employed, as for example on aircraft, under conditions which entail subjection to a wide range of temperature variations while precluding the provision of temperature-controlled housing means capable of shielding the generator against such temperature variations.
  • the primary object of the invention is to provide simple and dependable frequency-regulating means operative to counteract the inuence of temperature changes tending to cause frequency deviations; and it is a further object to accomplish the above end without adding substantial bulk or weight to the generating equipment.
  • Fig. 1 is a longitudinal sectional view of a resonant cavity oscillation generator incorporate,I ing a preferred embodiment ofthe invention
  • Fig. 2 is a fragmentary sectional view corresponding in general to the upper end portion of Fig, 1l and' illustrating a modification l
  • the ultra high frequency oscillation generator depicted in Fig. 1 includes a resonant cavity, which is identified as a whole by reference numeral I0, and a three-electrode vacuum tube or triode I ⁇ I of the so-called lighthouse type.
  • the latter comprises a base I2 having a number of contact prongs I3,a glass envelope I4, an anode I5, a control grid I6, and a cathode iI of the heater type.
  • the anode is a solid cylindrical slug supported on a flat metal ring I8 from which it extends upwardly to form a contact terminal I5a and downwardly within the envelope of the tube to a plane closely adjacent and parallel to but out of contact with grid I6.
  • the grid consists of a ilat woven wire ⁇ network extending crosswise of the envelope, between the anode and cathode, and supported on a surrounding flat metal ring i9 which is spaced from ring I8 by the glass tube Ila constituting a part of the tube envelope.
  • Ring. I8 is soldered or brazed to anode I5 and is sealed to the upper end of glass tube Ila, and ring I9 is sealed to the lower end of glass tube M'a and also to the upper end of a second glass tube Hb upon which it rests and which, together with tube Ila, forms the glass portion of the envelope.
  • the glass of which tubes Ila and IIb are composed is of a variety which does not expand or contract substantially when subjected to the ambient temperature variations to be expected in the course of normal operation.
  • the lighthouse tube which may be a standard No. 464 or 446-is characterized by extremely close spacing between grid and anode and between grid and cathodewhich close spacing is necessitated by the requirement that electron transit time beas short as possible. But this close spacing of said electrodes, amounting in each case to only a few thousandths of an inch.
  • the purpose of the present invention is to counteract and offset the frequency-varying effect of the aforementioned variations of interelectrode spacing, as well as those arising from other possible variations' in the system,'when.
  • Ring 22 includes a band-like annular portion 22a which is slotted axially so that it is capable of being contracted into gripping engagement with the tube base by means of a, split clamping ring 23.
  • the lighthouse” tube can be withdrawn and rec placed upon loosening ring 23, which is normally held under contraction by a clamping screw 2l.
  • a metal cylinder 25 mounted within the cavity, concentrically with the shell 20, is a metal cylinder 25, known as a grid cylinder. This is slotted longitudinally at its lower end to render said lower end expansible to receive tube II; and it is internally grooved Y v circumferentially at 2t ring I9.
  • the present invention is not ,directly concerned with the function of grid cylinder 25, but it is' thought appropriate to mention that to engage and made electrical contact with the peripheral edge of grid' gage the external thread 28 of an elongate metal rod 29.
  • the plate rod which extends downwardly and is adapted at its lower end to withdrawably engage vthe cylindrical terminal portion Ilia of anode l5 and thereby edect electrical connection with the anode.
  • the adaptation of the lower end of the plate rod to render it withdrawably engageable with said anode terminal Illa. would glve'rise an increase iny the frequency of oscillation and vice versa. I conceived that it might.
  • I acterminal is accomplished by boring said lower end to form a thin resilient cylindrical wall, in-
  • cup-like metal element 32 Secured to plate rod 22 and concentric therewith, is a cup-like metal element 32 which is known as a plate choke. This constitutes, in conjunction with shelll 20, a quarter-wave line having the characteristics of a short circuit and operating in the same manner as a complete conductive closure of the space between plate rod 29 and the inside surface of the shell 22.
  • the plate rod constitutes the axial conductor of a co-axial line, of which shell 2@ is the outer conductor, and said rod also forms a second coaxial line section in conjunction with the grid cylinder.
  • a probe 32 which need not be described, serves as the mediuml for withdrawing high frequency energy from the cavity; and a terminal 36 provides means for connecting a plate current changes, without any supplemental provision, i
  • such as a temperature-controlled housing capable of serving as a shield against such ambient temperature variations.
  • the problem presented was to reduce to a permissible value or, if possible, completely alleviate the aforementioned frequency instability; and to do so without resorting to a protective housing which would increase the weight and bulk of the equipment besides introducing certain inconveniences which it was desirable to avoid.
  • the change of length of the rod within the cavity is the factor which determines the movement of the lower end of the rod, so far as this invention is concerned, and it will accordingly be apparent that the length of rod 29 within the cavity is a criticalfactor in determining the sumciency of correction.
  • the shell 20 of two lengthwise adjoining parts, one being composed of Invar and the other of some other metal, such as copper. This would permit of a predetermined lengthwise expansion and contraction 'of the shell which could be used to offset excessive expansion and contraction of the plate rod in the event such an expedient be found necessary. Such a modication would not of necessity involve any structural change but merely a substitution of material throughout a portion of the length of shell 20. This obviously requires no additional illustration.
  • An oscillation generator comprising a tubular metal shell, a vacuum tube secured to one to said grid and extending longitudinally within said shell toward the other end thereof, and a inder and said shellin response to temperature changes, whereby to counteract frequency devi- Y ations due ⁇ particularly to the effects of such changes on the electrodes of said tube.
  • An oscillation generator comprising a tubular metal shell, a vacuum tube secured to one end-of said shell and extending longitudinally therein, said tube having an electrode terminal disposed within said shell, and a conductive member adjustably secured to the ⁇ other end of said shell and extending longitudinally therein in wiping engagement with said terminal, adjustment of said member effecting tuning adjustment of the generator, said shell and said member being composed at least in part of materials having diierent coeilicients of expansion to counteract frequency deviations duel to temperature changes, and said conductive member compris- ⁇ ing two serially connected sections composed of metals having diierent coeilicients of expansion.

Description

'Feb 24, 1948. s C, sPlELMAN 2,436,700
CAVITY RESONATOR OSC ILLATOR Filed Jan. 29, 1944 Patente-d Feb; 1
CAVITY RESONATOR OSCILLATOR Sterling C. Spiclman, Huntingdon Valley, Pa., assignor, by mesne assignments, to Philco Corporation, Philadelphia, Pa., a corporation of Pennsylvania Application January 29, 1944, Serial No. 520,296'.
2 Claims. (Cl. 315-39) This invention has to do with the problem of maintaining constant, as nearly as possible, the
frequency of electrical oscillations generated by an ultra high frequency oscillator, particularly one of the type comprising a resonant cavity and a so-called lighthouse type triode.
A resonant cavity oscillation generator, such as that hereinafter described, is designed to function at extremely high frequencies and is often employed, as for example on aircraft, under conditions which entail subjection to a wide range of temperature variations while precluding the provision of temperature-controlled housing means capable of shielding the generator against such temperature variations.
The primary object of the invention is to provide simple and dependable frequency-regulating means operative to counteract the inuence of temperature changes tending to cause frequency deviations; and it is a further object to accomplish the above end without adding substantial bulk or weight to the generating equipment.
The invention can best be described and explained by referring to the drawings wherein,
Fig. 1 is a longitudinal sectional view of a resonant cavity oscillation generator incorporate,I ing a preferred embodiment ofthe invention;I and Fig. 2 is a fragmentary sectional view corresponding in general to the upper end portion of Fig, 1l and' illustrating a modification l The ultra high frequency oscillation generator depicted in Fig. 1 includes a resonant cavity, which is identified as a whole by reference numeral I0, and a three-electrode vacuum tube or triode I\I of the so-called lighthouse type. The latter comprises a base I2 having a number of contact prongs I3,a glass envelope I4, an anode I5, a control grid I6, and a cathode iI of the heater type. The anode is a solid cylindrical slug supported on a flat metal ring I8 from which it extends upwardly to form a contact terminal I5a and downwardly within the envelope of the tube to a plane closely adjacent and parallel to but out of contact with grid I6.
The grid consists of a ilat woven wire `network extending crosswise of the envelope, between the anode and cathode, and supported on a surrounding flat metal ring i9 which is spaced from ring I8 by the glass tube Ila constituting a part of the tube envelope. Ring. I8 is soldered or brazed to anode I5 and is sealed to the upper end of glass tube Ila, and ring I9 is sealed to the lower end of glass tube M'a and also to the upper end of a second glass tube Hb upon which it rests and which, together with tube Ila, forms the glass portion of the envelope. The glass of which tubes Ila and IIb are composed is of a variety which does not expand or contract substantially when subjected to the ambient temperature variations to be expected in the course of normal operation. The lighthouse tubewhich may be a standard No. 464 or 446-is characterized by extremely close spacing between grid and anode and between grid and cathodewhich close spacing is necessitated by the requirement that electron transit time beas short as possible. But this close spacing of said electrodes, amounting in each case to only a few thousandths of an inch. is a detriment with respect to the maintenance of constant frequency because any variation of temperature of the anode or cathode or both, such as would be consequent upon marked changes of ambient temperature, or of load, will cause changes in the inter-electrode spacings which, though dimensionally small, amount to a substantial percentage of the total spacing and thus tend to bring about relatively large capacity variations which result in correspondingly large frequency deviations. The purpose of the present invention is to counteract and offset the frequency-varying effect of the aforementioned variations of interelectrode spacing, as well as those arising from other possible variations' in the system,'when.
trally apertured to receive said tube base. Ring 22 includes a band-like annular portion 22a which is slotted axially so that it is capable of being contracted into gripping engagement with the tube base by means of a, split clamping ring 23.
The lighthouse" tube can be withdrawn and rec placed upon loosening ring 23, which is normally held under contraction by a clamping screw 2l. Mounted within the cavity, concentrically with the shell 20, is a metal cylinder 25, known as a grid cylinder. This is slotted longitudinally at its lower end to render said lower end expansible to receive tube II; and it is internally grooved Y v circumferentially at 2t ring I9. The present invention is not ,directly concerned with the function of grid cylinder 25, but it is' thought appropriate to mention that to engage and made electrical contact with the peripheral edge of grid' gage the external thread 28 of an elongate metal rod 29. known as the plate rod, which extends downwardly and is adapted at its lower end to withdrawably engage vthe cylindrical terminal portion Ilia of anode l5 and thereby edect electrical connection with the anode. The adaptation of the lower end of the plate rod to render it withdrawably engageable with said anode terminal Illa. would glve'rise an increase iny the frequency of oscillation and vice versa. I conceived that it might. be feasible to take advantage o'f the longitudinal expansion and contraction jof plate rod 29, which would inevitably accompany rising and fallingambienttemperatures, respectively: and that such movements might be made capable'of and suiiicient to largely or wholly offset the aforementioned frequency deviations; It is apparent that since plate rod 29 and shell were heretofore both composed of copper or brass andtherefore possessed the same coemcient of expansion, little or no movement of rod 29 relatively to anode terminal Ita would occur in response to ambient temperature changes; but I perceived that if a sufficient and appropriate difference of expansion could b e brought about as between shell 20 and rod 29, my objective might be achieved, at least in part.
Bysubstituting Invar in place of copper as the metalv from which shell 20 is composed, I acterminal is accomplished by boring said lower end to form a thin resilient cylindrical wall, in-
serting a contact bushing 30 into the bore and securing the same by silver soldering or brazing, and then longitudinally slotting the bored porcomplished at once a large expansion dierence which resulted in a correspondingly substantial tion, together with bushing 2t, to form an expansible socket into which the cylindrical terminal la is easily insertable. To the upper end of plate rod 29 is attached a knob 3i by means of which the rod can ,be rotated and thus caused to move up or down by virtue of thread 2B; and the purpose of so doing is to eect tuning adjustments of the generator.
Secured to plate rod 22 and concentric therewith, is a cup-like metal element 32 which is known as a plate choke. This constitutes, in conjunction with shelll 20, a quarter-wave line having the characteristics of a short circuit and operating in the same manner as a complete conductive closure of the space between plate rod 29 and the inside surface of the shell 22.
The plate rod constitutes the axial conductor of a co-axial line, of which shell 2@ is the outer conductor, and said rod also forms a second coaxial line section in conjunction with the grid cylinder.
A probe 32, which need not be described, serves as the mediuml for withdrawing high frequency energy from the cavity; and a terminal 36 provides means for connecting a plate current changes, without any supplemental provision, i
such as a temperature-controlled housing, capable of serving as a shield against such ambient temperature variations.
The problem presented was to reduce to a permissible value or, if possible, completely alleviate the aforementioned frequency instability; and to do so without resorting to a protective housing which would increase the weight and bulk of the equipment besides introducing certain inconveniences which it was desirable to avoid.
The solution of the problem arose from my observation that increased ambient temperature caused the frequency to decrease. Having in mind thata movement of plate rod 29 downwardly, as viewed in Fig. l, relatively to anode Alongitudinal movement of rod 29 in the appropriate direction to counteract the previously mentioned adverse effect of ambient temperature changes; and I discovered that the regulation which could thus be effected remained remarkably constant throughout the entire range of temperature variations which experience indicated were likely to be encountered.
The tuning loi" the cavity to correct for deviations from the assigned frequency, which is ordinarily accomplished by moving the plate rod longitudinally, is mainly a function of the movement of the lower end of the rod along the anode terminal l5a and `is not to any substantial extent a direct function of the change in the length of therod within the cavity. But, of course, the change of length of the rod within the cavity is the factor which determines the movement of the lower end of the rod, so far as this invention is concerned, and it will accordingly be apparent that the length of rod 29 within the cavity is a criticalfactor in determining the sumciency of correction. In other words, if the-rod is too long, Within the cavity, it obviously over-compensates the frequency deviation and if it is too short, within the cavity, it will undercompensate said deviation. The length of rod outside the cavity is, manifestly, of no consequence.
To determine upon a design which will afford adequate regulation in any particular case, the most direct procedure is rst to ascertain experimentally the extent of frequency deviation per degree of temperature change for the triode it is intended to employ when operating within the prescribed frequency band, and then determine how much movement of the plate rod is needed to ofsetthe frequency deviation. Having ascertained that data and knowing the coemcients of expansion of the metals composing the plate rod and the shell respectively, it is a simple matsult when employing a structure like that oi' Fig. 1, resort may be had to the modiilcation shown in Fig. 2 wherein the plate rod is made in two parts-the lower portion 3B being composed of essary additional length is afforded by the Invar extension.
If the occasion should arise, it would be entirely feasible to make the shell 20 of two lengthwise adjoining parts, one being composed of Invar and the other of some other metal, such as copper. This would permit of a predetermined lengthwise expansion and contraction 'of the shell which could be used to offset excessive expansion and contraction of the plate rod in the event such an expedient be found necessary. Such a modication would not of necessity involve any structural change but merely a substitution of material throughout a portion of the length of shell 20. This obviously requires no additional illustration.
I claim:
1. An oscillation generator, comprising a tubular metal shell, a vacuum tube secured to one to said grid and extending longitudinally within said shell toward the other end thereof, and a inder and said shellin response to temperature changes, whereby to counteract frequency devi- Y ations due `particularly to the effects of such changes on the electrodes of said tube.
conductive member secured to said other end of shell a coaxial line and also forming with said' grid cylinder a second coaxial line, said shell and said member being composed at least in part of 2. An oscillation generator, comprising a tubular metal shell, a vacuum tube secured to one end-of said shell and extending longitudinally therein, said tube having an electrode terminal disposed within said shell, and a conductive member adjustably secured to the` other end of said shell and extending longitudinally therein in wiping engagement with said terminal, adjustment of said member effecting tuning adjustment of the generator, said shell and said member being composed at least in part of materials having diierent coeilicients of expansion to counteract frequency deviations duel to temperature changes, and said conductive member compris- `ing two serially connected sections composed of metals having diierent coeilicients of expansion.
STERLING C. SPIELMAN.
REFERENCES CITED The following references Iare of record in the ille of this patent:
UNITED STATES PATENTS Number Name Date 1,913,978 Ewen June 13, 1933 2,109,880 Dow Mar. 1, 1938 2,146,365 Batchelor ..--1 Feb. 7, 1939 2,251,085 Unk July 29, 1941 2,284,405 AMcArthur May 26, 1942 2,374,810 Fremlin May 1, 1945 2,408,817 Snow Oct. 8, 1946 Y FOREIGN PATENTS Number Country Date 422,869 Great Britain Jan. 2l', 1935
US520296A 1943-10-02 1944-01-29 Cavity resonator oscillator Expired - Lifetime US2436700A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US504745A US2436706A (en) 1943-10-02 1943-10-02 Lamp holder for tubular lamps
US520296A US2436700A (en) 1944-01-29 1944-01-29 Cavity resonator oscillator
GB30888/45A GB603262A (en) 1944-01-29 1945-11-16 Resonant cavity oscillators

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US520296A US2436700A (en) 1944-01-29 1944-01-29 Cavity resonator oscillator

Publications (1)

Publication Number Publication Date
US2436700A true US2436700A (en) 1948-02-24

Family

ID=24071990

Family Applications (1)

Application Number Title Priority Date Filing Date
US520296A Expired - Lifetime US2436700A (en) 1943-10-02 1944-01-29 Cavity resonator oscillator

Country Status (2)

Country Link
US (1) US2436700A (en)
GB (1) GB603262A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2478574A (en) * 1946-06-14 1949-08-09 Aircraft Radio Corp Tube support and shield
US2582846A (en) * 1944-04-19 1952-01-15 Neher Henry Victor Microwave amplifier
US2627578A (en) * 1945-11-14 1953-02-03 Norman E Klein Tunable high-frequency oscillator
US2859434A (en) * 1955-11-08 1958-11-04 Gen Railway Signal Co Speed measuring apparatus for railroad classification yards
US3173104A (en) * 1961-09-05 1965-03-09 Trak Microwave Corp Coaxial microwave oscillator
US3173106A (en) * 1961-09-05 1965-03-09 Trak Microwave Corp Microwave oscillator with bimetal temperature compensation
US3902138A (en) * 1974-07-22 1975-08-26 Gen Electric Temperature stabilized coaxial cavity microwave oscillator
US4677403A (en) * 1985-12-16 1987-06-30 Hughes Aircraft Company Temperature compensated microwave resonator

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1913978A (en) * 1929-06-14 1933-06-13 Rca Corp Inductance and capacity
GB422869A (en) * 1932-11-12 1935-01-21 Meaf Mach En Apparaten Fab Nv Improvements in electric discharge devices
US2109880A (en) * 1935-10-30 1938-03-01 Rca Corp Temperature compensation
US2146365A (en) * 1934-12-13 1939-02-07 John C Batchelor Electron emitter
US2251085A (en) * 1939-03-23 1941-07-29 Rca Corp Short electromagnetic wave oscillatory circuit
US2284405A (en) * 1940-08-17 1942-05-26 Gen Electric High frequency apparatus
US2374810A (en) * 1939-12-22 1945-05-01 Int Standard Electric Corp Electron discharge apparatus
US2408817A (en) * 1943-11-29 1946-10-08 Sperry Gyroscope Co Inc Electron discharge apparatus

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1913978A (en) * 1929-06-14 1933-06-13 Rca Corp Inductance and capacity
GB422869A (en) * 1932-11-12 1935-01-21 Meaf Mach En Apparaten Fab Nv Improvements in electric discharge devices
US2146365A (en) * 1934-12-13 1939-02-07 John C Batchelor Electron emitter
US2109880A (en) * 1935-10-30 1938-03-01 Rca Corp Temperature compensation
US2251085A (en) * 1939-03-23 1941-07-29 Rca Corp Short electromagnetic wave oscillatory circuit
US2374810A (en) * 1939-12-22 1945-05-01 Int Standard Electric Corp Electron discharge apparatus
US2284405A (en) * 1940-08-17 1942-05-26 Gen Electric High frequency apparatus
US2408817A (en) * 1943-11-29 1946-10-08 Sperry Gyroscope Co Inc Electron discharge apparatus

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2582846A (en) * 1944-04-19 1952-01-15 Neher Henry Victor Microwave amplifier
US2627578A (en) * 1945-11-14 1953-02-03 Norman E Klein Tunable high-frequency oscillator
US2478574A (en) * 1946-06-14 1949-08-09 Aircraft Radio Corp Tube support and shield
US2859434A (en) * 1955-11-08 1958-11-04 Gen Railway Signal Co Speed measuring apparatus for railroad classification yards
US3173104A (en) * 1961-09-05 1965-03-09 Trak Microwave Corp Coaxial microwave oscillator
US3173106A (en) * 1961-09-05 1965-03-09 Trak Microwave Corp Microwave oscillator with bimetal temperature compensation
US3902138A (en) * 1974-07-22 1975-08-26 Gen Electric Temperature stabilized coaxial cavity microwave oscillator
US4677403A (en) * 1985-12-16 1987-06-30 Hughes Aircraft Company Temperature compensated microwave resonator

Also Published As

Publication number Publication date
GB603262A (en) 1948-06-11

Similar Documents

Publication Publication Date Title
US2374810A (en) Electron discharge apparatus
US2436700A (en) Cavity resonator oscillator
US2606302A (en) Temperature compensated cavity resonator structure
US2407974A (en) Ultra high frequency device
US1945545A (en) Frequency control system
US2267520A (en) Oscillation generator system
US2561727A (en) Tuning of electrical resonators
US2623194A (en) Tuner for high-frequency tubes
US2473827A (en) Electronic discharge device of the cavity resonator type
US3252116A (en) Combined tuning and stabilization means for cavity resonators
US2432193A (en) Microwave oscillator
US2539218A (en) Temperature compensating system for oscillators
US2456896A (en) Ultra high frequency device
US3706910A (en) Coaxial magnetron slot mode suppressor
US2300315A (en) Oscillation generator circuit
US2681997A (en) Feedback coupling means
US2104554A (en) Line resonator
US2428609A (en) High-frequency electric discharge device
US2605421A (en) Tuner for lighthouse tube cavity resonators
US2915669A (en) High voltage switching tubes
US2547372A (en) Grid-controlled electron discharge device
US3902138A (en) Temperature stabilized coaxial cavity microwave oscillator
US2532215A (en) Cathode structure
US3368163A (en) Ruggedized high frequency apparatus
US2884602A (en) Transmit-receive cells