US3140416A - Gaseous discharge device - Google Patents

Gaseous discharge device Download PDF

Info

Publication number
US3140416A
US3140416A US192602A US19260262A US3140416A US 3140416 A US3140416 A US 3140416A US 192602 A US192602 A US 192602A US 19260262 A US19260262 A US 19260262A US 3140416 A US3140416 A US 3140416A
Authority
US
United States
Prior art keywords
gaseous discharge
gas
discharge device
boron trifluoride
atmosphere
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
US192602A
Inventor
Harold A Sleeper
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.)
Varian Medical Systems Inc
Original Assignee
Varian Associates Inc
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 Varian Associates Inc filed Critical Varian Associates Inc
Priority to US192602A priority Critical patent/US3140416A/en
Application granted granted Critical
Publication of US3140416A publication Critical patent/US3140416A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J17/00Gas-filled discharge tubes with solid cathode
    • H01J17/02Details
    • H01J17/04Electrodes; Screens

Definitions

  • the present invention relates in general to gaseous discharge devices and more particularly to such gaseous discharge devices having improved deionization characteristics useful, for example, in microwave switching tubes such as TR, pre-TR and ATR tubes for radar.
  • the present day radar systems commonly employ gaseous discharge devices to produce the rapid switching times necessary for single antenna operation.
  • the transmitreceive or TR tube protects the sensitive receiving apparatus by means of an intense ionized discharge extending across the transmission path.
  • Such tubes generally employ an electron capture agent or attachment gas such as water vapor, in the gaseous atmosphere to enhance the deionization or recovery time between the transmission cycles.
  • Water vapor as anattachment gas has serious limitations for many high power TR tube applications. More specifically, its use is generally prohibited in high power applications.
  • the probable upper limit, in X-band for example, for the water vapor attachment mechanism is about 500 kilowatts peak power and 500 watts average power. The limit occurs because the deionization occurs during the transmitter pulse, as well as after the pulse, it follows that an increased amount of energy must be supplied to sustain the ionization during transmission. This additional energy, called arc loss, is translated almost entirely into thermal energy. Even though the arc loss is only a small percentage of the total transmitted power, in very high power systems, this added heat can cause rapid, catastrophic failure of the switching element.
  • Another difliculty encountered with the use of water vapor as an attachment gas is that for extremely low temperature operation such as, for example, at -55 C. the partial pressure of the water vapor drops to only a fraction of a millimeter due to condensation thereby losing any benefit obtained from the attachment gas in reducing the deionization time, such that, until such time as the tube is sufiiciently heated, the radar will lose its short range capability.
  • boron trifluoride is utilized as an attachment gas in combination with a noble gas to form the ionizable atmosphere.
  • the boron trifluoride attachment gas readily permits relatively short recovery times useful for short range radar applications while retaining its proper operating characteristics down to temperatures well below 55 C. and also serving to permit extremely high power operation. For example, recovery times of 25 microseconds to 3 db points have been obtained at megawatts peak power and '20 kilowatts 3,140,416 Patented July 7, 1964 Fee average power at L-band frequencies of 1300 megacycles. It has been found that typically the deionization time is approximately halved by the use of boron trifluoride attachment gas as compared to a pure argon or noble gas ionizable atmosphere in the same envelope and at the same power levels.
  • the principal object of the present invention is to provide improved deionization characteristics for gaseous discharge devices.
  • One feature of the present invention is the provision of a quantity of boron trifluoride gas added to the ionizable atmosphere of a gaseous discharge device for decreasing the deionization time and permitting extremely low temperature operation.
  • Another feature of the present invention is the provision of a microwave gaseous discharge switching tube containing a mixture of noble gas and boron trifluoride gas whereby the recovery time of the switch tube is minimized and low temperature operation and high power operation characteristics enhanced.
  • Another feature of the present invention is the same as the preceding feature wherein the noble gas is argon and a preponderance of the mixture by partial pressure is boron trifluoride, whereby stable recovery time characteristics are obtained over prolonged operating lifetimes.
  • FIG. 1 is a perspective view of an illustrative pretransmit-receive tube embodiment
  • FIG. 2 is an enlarged cross-sectional view of the structure of FIG. 1 taken along line 2-2 in the direction of the arrows.
  • FIGS. 1 and 2 illustrate a pre-transmit-receive microwave switching gaseous discharge device of the broadband type suitable for operation over a relatively wide range of microwave frequencies.
  • This class of pre-TR tube characteristically has a length of rectangular waveguide 1 with mounting flanges 2 and 3 disposed adjacent to the ends thereof.
  • Flange 2 is considered as the input flange, and is coupled to the transmitter, while the receiving apparatus, not shown, is coupled to the output flange 3 typically via the intermediary of a separate transmit-receive gaseous discharge device, not shown.
  • a metallic frame 4 having a centrally located resonant aperture 5 is preferably fabricated from an electrically and thermally conductive metal such as aluminum, steel or brass.
  • a tubular gaseous discharge member 6 is disposed substantially closing OK the central aperture 5 in the plate 4.
  • Gaseous discharge member 6 is of the folded cylinder type, that is, it comprises an annular gaseous discharge chamber formed by the space defined between two concentric cylinders sealed together at their ends.
  • the cylindrical walls of the discharge member 6 are made of a suitable dielectric material such as, for example, glass or quartz, the latter being utilized when high power operation is anticipated.
  • the annular chamber 7 defined by the annulus between the two concentric cylinders is evacuated and filled to a reduced pressure with a suitable gaseous mixture forming an ionizable atmosphere, the constituent components of which and the characteristics of which will be more fully described below.
  • a pair of metallic straps 8 are disposed at each end of the tubular gaseous discharge element 6 and serve to clamp the element 6 into the opening 5.
  • the constituent components of the ionizable gaseous atmosphere, employed in the annular gas chamber 7 of the present invention, are any noble gas, preferably argon, at reduced pressure of approximately 2 millimeters of mercury intermixed with boron trifluoride gas at a partial pressure of approximately 20 millimeters of mercury.
  • the noble gas reduces the firing power level necessary to produce ionization of the gaseous atmosphere.
  • the boron trifluoride gas serves to reduce the deionization time and readily permits the gaseous discharge device to operate down to extremely low temperatures such as, for example, those below -55 C.
  • a preponderance of boron trifluoride gas facilitates stable long life operation because of the clean up of boron trifluoride with operating life time and high power levels.
  • An identical structure utilizing an ionizable gas atmosphere consisting only of argon at a pressure of a few millimeters of mercury and operable to the same power levels exhibited a deionization time of approximately 120 microseconds.
  • novel ionizable gas atmosphere embodiment of the present invention has been described as utilized in a folded cylinder pre-TR tube it is equally applicable to other gaseous discharge devices such as, for
  • standard resonant element TR tubes of the type shown in US. Patent No. 2,965,787 and to ATR tubes and like where it is desired to reduce the deionization time and to improve the lowtemperature operating characteristics and high power handling capabilities of the gaseous discharge device.
  • a gaseous discharge device comprising a hermetically sealed envelope containing an ionizable atmosphere, and a quantity of boron trifluoride gas contained within said envelope to provide means for decreasing the deionization time of the gaseous discharge device during operation thereof.
  • said hermetically sealed envelope is made of a dielectric material and said ionizable atmosphere contains a quantity of a noble gas for decreasing the minimum power required for firing of said gaseous discharge device in operation.
  • a microwave transmit-receive switching tube comprising, a hermetically sealed envelope containing an ionizable atmosphere, and said atmosphere including a partial pressure of noble gas and boron trifluoride gas at pressures substantially less than atmospheric pressure.

Description

July 7, 1964 H. A. SLEEPER GASEOUS DISCHARGE DEVICE Filed May 4, 1962 INVENTOR. HAROLD A. SLEE PER ATTORNEY United States Patent 3,140,416 GASEOUS DISCHARGE DEVICE Harold A. Sleeper, South Groveland, Mass, assignor, by mesne assignments, to Varian Associates, Palo Alto,
Calif., a corporation of California Filed May 4, 1962, Ser. No. 192,602 5 Claims. (Cl. 313-223) The present invention relates in general to gaseous discharge devices and more particularly to such gaseous discharge devices having improved deionization characteristics useful, for example, in microwave switching tubes such as TR, pre-TR and ATR tubes for radar.
The present day radar systems commonly employ gaseous discharge devices to produce the rapid switching times necessary for single antenna operation. The transmitreceive or TR tube protects the sensitive receiving apparatus by means of an intense ionized discharge extending across the transmission path. Such tubes generally employ an electron capture agent or attachment gas such as water vapor, in the gaseous atmosphere to enhance the deionization or recovery time between the transmission cycles.
The need for a predictable short recovery time arises from the fact that low power return signals from targets must pass through the switching element without serious attenuation, at a time represented by the system minimum design range. In systems capable of operating down to short ranges the absolute recovery time must be in the order of a few microseconds.
The majority of the TR tubes made in past years, as well as the majority of tubes still used in low power equipments, use a mixture of a pure noble gas, such as argon, in combination with a controlled amount of an attachment gas, such as water vapor, to produce a rapid recovery or deionization time. Historically, the argon-Water vapor system has been the most widely used.
Water vapor as anattachment gas has serious limitations for many high power TR tube applications. More specifically, its use is generally prohibited in high power applications. For example, the probable upper limit, in X-band for example, for the water vapor attachment mechanism is about 500 kilowatts peak power and 500 watts average power. The limit occurs because the deionization occurs during the transmitter pulse, as well as after the pulse, it follows that an increased amount of energy must be supplied to sustain the ionization during transmission. This additional energy, called arc loss, is translated almost entirely into thermal energy. Even though the arc loss is only a small percentage of the total transmitted power, in very high power systems, this added heat can cause rapid, catastrophic failure of the switching element.
Another difliculty encountered with the use of water vapor as an attachment gas is that for extremely low temperature operation such as, for example, at -55 C. the partial pressure of the water vapor drops to only a fraction of a millimeter due to condensation thereby losing any benefit obtained from the attachment gas in reducing the deionization time, such that, until such time as the tube is sufiiciently heated, the radar will lose its short range capability.
In the present invention boron trifluoride is utilized as an attachment gas in combination with a noble gas to form the ionizable atmosphere. The boron trifluoride attachment gas readily permits relatively short recovery times useful for short range radar applications while retaining its proper operating characteristics down to temperatures well below 55 C. and also serving to permit extremely high power operation. For example, recovery times of 25 microseconds to 3 db points have been obtained at megawatts peak power and '20 kilowatts 3,140,416 Patented July 7, 1964 Fee average power at L-band frequencies of 1300 megacycles. It has been found that typically the deionization time is approximately halved by the use of boron trifluoride attachment gas as compared to a pure argon or noble gas ionizable atmosphere in the same envelope and at the same power levels.
The principal object of the present invention is to provide improved deionization characteristics for gaseous discharge devices.
One feature of the present invention is the provision of a quantity of boron trifluoride gas added to the ionizable atmosphere of a gaseous discharge device for decreasing the deionization time and permitting extremely low temperature operation.
' Another feature of the present invention is the provision of a microwave gaseous discharge switching tube containing a mixture of noble gas and boron trifluoride gas whereby the recovery time of the switch tube is minimized and low temperature operation and high power operation characteristics enhanced.
Another feature of the present invention is the same as the preceding feature wherein the noble gas is argon and a preponderance of the mixture by partial pressure is boron trifluoride, whereby stable recovery time characteristics are obtained over prolonged operating lifetimes.
Other features and advantages of the present invention will become apparent upon a perusal of the specification taken in connection with the accompanying drawings wherein:
FIG. 1 is a perspective view of an illustrative pretransmit-receive tube embodiment, and
FIG. 2 is an enlarged cross-sectional view of the structure of FIG. 1 taken along line 2-2 in the direction of the arrows.
Referring to the drawings, FIGS. 1 and 2 illustrate a pre-transmit-receive microwave switching gaseous discharge device of the broadband type suitable for operation over a relatively wide range of microwave frequencies. This class of pre-TR tube characteristically has a length of rectangular waveguide 1 with mounting flanges 2 and 3 disposed adjacent to the ends thereof. Flange 2 is considered as the input flange, and is coupled to the transmitter, while the receiving apparatus, not shown, is coupled to the output flange 3 typically via the intermediary of a separate transmit-receive gaseous discharge device, not shown.
A metallic frame 4 having a centrally located resonant aperture 5 is preferably fabricated from an electrically and thermally conductive metal such as aluminum, steel or brass.
A tubular gaseous discharge member 6 is disposed substantially closing OK the central aperture 5 in the plate 4. Gaseous discharge member 6 is of the folded cylinder type, that is, it comprises an annular gaseous discharge chamber formed by the space defined between two concentric cylinders sealed together at their ends. The cylindrical walls of the discharge member 6 are made of a suitable dielectric material such as, for example, glass or quartz, the latter being utilized when high power operation is anticipated. The annular chamber 7 defined by the annulus between the two concentric cylinders is evacuated and filled to a reduced pressure with a suitable gaseous mixture forming an ionizable atmosphere, the constituent components of which and the characteristics of which will be more fully described below.
A pair of metallic straps 8 are disposed at each end of the tubular gaseous discharge element 6 and serve to clamp the element 6 into the opening 5.
In operation, high input power entering the waveguide 1 via flange assembly 2 upon intercepting the annular ionizable atmosphere within the chamber 7 thereby ionizes the atmosphere rendering it conductive and serving to reflect all but a small fraction of the energy back out the input port, thereby protecting the receiver circuitry, not shown from the high input power levels.
The constituent components of the ionizable gaseous atmosphere, employed in the annular gas chamber 7 of the present invention, are any noble gas, preferably argon, at reduced pressure of approximately 2 millimeters of mercury intermixed with boron trifluoride gas at a partial pressure of approximately 20 millimeters of mercury. The noble gas reduces the firing power level necessary to produce ionization of the gaseous atmosphere. The boron trifluoride gas serves to reduce the deionization time and readily permits the gaseous discharge device to operate down to extremely low temperatures such as, for example, those below -55 C. A preponderance of boron trifluoride gas facilitates stable long life operation because of the clean up of boron trifluoride with operating life time and high power levels.
Other proportions of noble gas with boron trifluoride have been found operable. For example 7 millimeters argon with 1 millimeter of boron trifluoride was operable but turned out to have an increasing deionization time with operating life due to boron trifluoride clean up, such that the advantage over argon was lost with appreciable operating time. Therefore where operating time at high power is a major consideration a preponderance of boron trifluoride is preferred.
A folded cylinder pre-TR tube having an ionizable gas atmosphere, with 2 millimeters argon and 20 millimeters of boron trifluoride, satisfactorily operated at L-band frequency of 1300 megacycles with peak power of megawatts and average power of 20 kilowatts with recovery times of approximately 25 microseconds to the 3 db point. An identical structure utilizing an ionizable gas atmosphere consisting only of argon at a pressure of a few millimeters of mercury and operable to the same power levels exhibited a deionization time of approximately 120 microseconds.
Although the novel ionizable gas atmosphere embodiment of the present invention has been described as utilized in a folded cylinder pre-TR tube it is equally applicable to other gaseous discharge devices such as, for
example, standard resonant element TR tubes of the type shown in US. Patent No. 2,965,787 and to ATR tubes and like where it is desired to reduce the deionization time and to improve the lowtemperature operating characteristics and high power handling capabilities of the gaseous discharge device.
Since many changes could be made in the above construction and many apparently widely different embodiments of this invention could be made without departing from the scope thereof, it is intended that all matter contained in the above construction or shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.
What is claimed is:
1. A gaseous discharge device comprising a hermetically sealed envelope containing an ionizable atmosphere, and a quantity of boron trifluoride gas contained within said envelope to provide means for decreasing the deionization time of the gaseous discharge device during operation thereof.
2. The apparatus according to claim 1 wherein said hermetically sealed envelope is made of a dielectric material and said ionizable atmosphere contains a quantity of a noble gas for decreasing the minimum power required for firing of said gaseous discharge device in operation.
3. The apparatus according to claim 2 wherein said ionizable atmosphere contains a preponderance by partial pressure of said boron trifluoride.
4. The apparatus according to claim 3 wherein said noble gas is argon.
5. A microwave transmit-receive switching tube comprising, a hermetically sealed envelope containing an ionizable atmosphere, and said atmosphere including a partial pressure of noble gas and boron trifluoride gas at pressures substantially less than atmospheric pressure.
References Cited in the file of this patent UNITED STATES PATENTS 1,286,316 Hewitt Dec. 3, 1918 1,944,825 Millner Jan. 23, 1934 2,799,804 Biondi July 16, 1957

Claims (1)

1. A GASEOUS DISCHARGE DEVICE COMPRISING A HERMETICALLY SEALED ENVELOPE CONTAINING AN IONIZABLE ATMOSPHERE, AND A QUANTITY OF BORON TRIGLUORIDE GAS CONTAINED WITHIN SAID ENVELOPE TO PROVIDE MEANS FOR DECREASING THE DEIONIZATION TIME OF THE GAGEOUS DISCHARGE DEVICE DURING OPERATION THEREOF.
US192602A 1962-05-04 1962-05-04 Gaseous discharge device Expired - Lifetime US3140416A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US192602A US3140416A (en) 1962-05-04 1962-05-04 Gaseous discharge device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US192602A US3140416A (en) 1962-05-04 1962-05-04 Gaseous discharge device

Publications (1)

Publication Number Publication Date
US3140416A true US3140416A (en) 1964-07-07

Family

ID=22710346

Family Applications (1)

Application Number Title Priority Date Filing Date
US192602A Expired - Lifetime US3140416A (en) 1962-05-04 1962-05-04 Gaseous discharge device

Country Status (1)

Country Link
US (1) US3140416A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5566056A (en) * 1994-02-07 1996-10-15 Tii Industries, Inc. Coaxial transmission line surge arrestor
US5657196A (en) * 1994-12-08 1997-08-12 Tii Industries, Inc. Coaxial transmission line surge arrestor
US5724220A (en) * 1994-12-08 1998-03-03 Tii Industries, Inc. Coaxial transmission line surge arrestor with fusible link

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1286316A (en) * 1913-10-20 1918-12-03 Cooper Hewitt Electric Co Electric translating apparatus.
US1944825A (en) * 1928-12-18 1934-01-23 Gen Electric Electric incandescent lamp
US2799804A (en) * 1952-10-21 1957-07-16 Westinghouse Electric Corp Radar transmit receive switch

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1286316A (en) * 1913-10-20 1918-12-03 Cooper Hewitt Electric Co Electric translating apparatus.
US1944825A (en) * 1928-12-18 1934-01-23 Gen Electric Electric incandescent lamp
US2799804A (en) * 1952-10-21 1957-07-16 Westinghouse Electric Corp Radar transmit receive switch

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5566056A (en) * 1994-02-07 1996-10-15 Tii Industries, Inc. Coaxial transmission line surge arrestor
US5657196A (en) * 1994-12-08 1997-08-12 Tii Industries, Inc. Coaxial transmission line surge arrestor
US5724220A (en) * 1994-12-08 1998-03-03 Tii Industries, Inc. Coaxial transmission line surge arrestor with fusible link

Similar Documents

Publication Publication Date Title
US2422190A (en) Ultra high frequency coupling device and system
US2557961A (en) Transmission system for highfrequency currents
US2748351A (en) Microwave windows and gaseous devices
US2627573A (en) Wave guide duplexer
US3140416A (en) Gaseous discharge device
US4575692A (en) Microwave discharge apparatus and method with dual function priming resonator
US2693583A (en) Electronic cutoff switch
US2813999A (en) High power r.-f. switch tube
US2922124A (en) Microwave transmission control device
US2540148A (en) Ultra high frequency powerselective protective device
US2734171A (en) Heins
US2745072A (en) Wave guide gas switching device
US2903623A (en) Electric discharge devices
US3209285A (en) Folded cylinder gaseous discharge device
US2879485A (en) Broad band electronic switch
US3728650A (en) Ghost-mode shifted dielectric window
US2922131A (en) Folded cylinder gaseous discharge device
US3521197A (en) High frequency power limiter device for a waveguide
US3015822A (en) Ionized-gas beam-shifting tschebyscheff array antenna
US2965787A (en) Gaseous discharge device
US3147450A (en) Folded cylinder gaseous discharge device
US3497833A (en) Fast recovery high-mean-power pre-tr switch
US2789272A (en) Rotatable shutter and transmitreceive device
US2738418A (en) Transmission control devices adapted as a switch
US3480828A (en) Thyratron waveguide switch with density enhancement for operation in 27 to 40 ghz. range