US2721972A - High sensitivity ionization gauge - Google Patents
High sensitivity ionization gauge Download PDFInfo
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- US2721972A US2721972A US302640A US30264052A US2721972A US 2721972 A US2721972 A US 2721972A US 302640 A US302640 A US 302640A US 30264052 A US30264052 A US 30264052A US 2721972 A US2721972 A US 2721972A
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- 230000035945 sensitivity Effects 0.000 title description 5
- 150000002500 ions Chemical class 0.000 description 23
- 239000007789 gas Substances 0.000 description 17
- 238000010438 heat treatment Methods 0.000 description 7
- 230000004048 modification Effects 0.000 description 7
- 238000012986 modification Methods 0.000 description 7
- 238000000034 method Methods 0.000 description 5
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 4
- 229910052753 mercury Inorganic materials 0.000 description 4
- 238000005259 measurement Methods 0.000 description 3
- 238000001179 sorption measurement Methods 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 241000518994 Conta Species 0.000 description 1
- 101000952234 Homo sapiens Sphingolipid delta(4)-desaturase DES1 Proteins 0.000 description 1
- 208000036366 Sensation of pressure Diseases 0.000 description 1
- 102100037416 Sphingolipid delta(4)-desaturase DES1 Human genes 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000005591 charge neutralization Effects 0.000 description 1
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J41/00—Discharge tubes for measuring pressure of introduced gas or for detecting presence of gas; Discharge tubes for evacuation by diffusion of ions
- H01J41/02—Discharge tubes for measuring pressure of introduced gas or for detecting presence of gas
- H01J41/04—Discharge tubes for measuring pressure of introduced gas or for detecting presence of gas with ionisation by means of thermionic cathodes
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L21/00—Vacuum gauges
Definitions
- FIG.5 JEROME ROTHSTEIN BY a A -r roam/5y
- This invention relates to an electron discharge device for measuring low pressures in vacuum systems by the measurement of ionization of the residual gas molecules by electrons emitted from the cathode of the device.
- the usual ionization type of vacuum gauge is constructed as a normal triode, with a plate and grid and a hot cathode within said plate and grid.
- the grid is charged positively, and the anode is charged negatively with respect to the cathode.
- the envelope is connected to the system in which the pressure is to be measured, and the cathode is heated to emit electrons. The electrons are accelerated toward the grid, and collide with the residual gas molecules thus ionizing them. The positively charged ions are then attracted to the negative anode, where they are neutralized.
- the ion current to the anode is thus a measure of the number of residual gas molecules and thus of the pressure in the system.
- This type of vacuum gauge will measure down to about mm. of mercury.
- This lower limit is due to the fact that at these low pressures the electrons accelerated by the positive grid strike the grid with sutficient energy to generate soft X-rays, which in turn strike the anode, because the anode almost completely surrounds the grid, and these X-rays cause emission of photoelectrons from the anode which are collected by the grid.
- This electron current from the anode becomes of sufficient magnitude to mask the ion current to the anode at about 10-" mm. of mercury.
- a modification of this standard type of vacuum gauge uses a fine wire anode, a cylindrical grid surrounding the anode, and a cathode outside of the grid. The operation is the same, but by making the anode small, a much smaller fraction of the X-rays strike the anode, so the photocurrent is much less.
- This simple modification enables measurements down to about 10 mm. of mercury.
- the triode ionization type gauge can be used with the flash filament technique to extend the lower limit of measurement.
- the filament is cleaned of adsorbed gas, then allowed to remain cold on the vacuum to be measured. Residual gas is adsorbed on the filament over a period of time, after which the filament is quickly heated to incandescence, or flashed.
- the high temperature drives oil the adsorbed gases, giving a puff of gas which is measured ballistically by the ionization gauge in the usual manner.
- the greater the degree of vacuum the longer it takes to adsorb a measurable quantity of gas.
- the limitation of the standard ionization vacuum gauge and its modifications is the photocurrent from the anode caused by the soft X-rays generated by the electrons striking the grid at high velocity, and, in the case of the flash filament technique, the time required for the cold filament to adsorb a measurable quantity of gas becomes prohibitively long for very low pressures.
- a further object is to provide an ionization type vacuum gauge which is capable of measuring pressures much lower than other vacuum gauges.
- Another object is to provide a vacuum gauge capable o measuring routinely down to l0 mm. of mercury, and perhaps lower under ideal conditions.
- Another object is to provide a vacuum gauge capable of operating as a conventional, Bayard-Alpert, or improved ionization vacuum gauge, depending on the pres sure range,and on the connections and potentials applied.
- Another object is to provide a vacuum gauge capable of operation with the flash filament technique with materially shortened adsorption time.
- Fig. l is a perspective view partly cut away of a preferred embodiment of the invention.
- Fig. 2 is a top view of Fig. l and includes a schematic representation of the applied potentials.
- Fig. 3 is the voltage distance relationship in the diode when the gauge is operated in the improved manner.
- Fig. 4 is a top view of a modification of Fig. 1.
- Fig. 5 is a circuit used with the modification of Fig. 4.
- Fig. 1 a preferred embodiment of the improved ionization gauge comprising an envelope 9 in which 10 is a triode section in which 12 is a cathode, which is heated (heater source not shown) to emit electrons, consisting preferably of a strand of pure tungsten wire, and said cathode 12 is charged positively with respect to the triode anode 15 and said cathode 12 is charged negatively with respect to the triode grid 13.
- 10 is a triode section in which 12 is a cathode, which is heated (heater source not shown) to emit electrons, consisting preferably of a strand of pure tungsten wire, and said cathode 12 is charged positively with respect to the triode anode 15 and said cathode 12 is charged negatively with respect to the triode grid 13.
- Diode 11 also has its cathode 14 heated (heater source not shown) to emit electrons, and also consists preferably of a strand of pure tungsten wire, and said cathode 14 is charged negatively with respect to the diode anode 23 so the diode 11 operates under what is known as space charge limited conditions, where the voltage on the anode 23 is not sulficiently positive to attract all the electrons emitted by the cathode 14, and there is a considerable relatively stationary space charge surrounding the cathode.
- the triode anode 15, having a slot 24 therein is made negative with respect to the diode anode 23, having a slot 25 therein.
- Triode anode 15 and diode anode 23 are placed in close proximity, and slot 24 and slot 25 are placed so that substantially all of the ions leaving triode 10 through slot 24 can enter diode 11 through slot 25.
- Slots 24 and 25 each have an area which is relatively small compared to the total area of the anodes 15 and 23 respectively.
- the envelope of the device is mechanically connected to the system in which the pressure is to be measured, and some of the residual gas molecules will be in the volume of the triode when the pressures in the system and in the gauge become equalized.
- the electrons emitted by the triode cathode are accelerated towards the positive grid, and some of the electrons will collide with gas molecules, thus ionizing them. These positively charged ions are then attracted to the triode anode, and most of them are neutralized by the negative charge thereon.
- the diode anode 23 is of the proper amplitude and polarity to slow 'down the ions but not great enough to prevent the ions from entering the volume of the diode.
- the anode voltage and the cathode heating current are so proportioned to cause the diode to o'p erate in the space-charged limited manner.
- the anode voltage is not high enough to attract all of the elections which are emitted by the cathode, so electron clOud forms as a sheath iiiqi i a the cathode. Becauseof the density of the electron cloud, the voltage in the densest, portion will be more negative thari the cathode. This poteiitial vs, radius distribution is shown in Fig.
- V is the anode voltag'e'in the diode
- Vc is the cathode voltage in the diode
- R5 is the anode radius
- the cathode is con sidered to be at the origin.
- point is at the,l otential m nimum, arid this minimum is below the eatho'de potential.
- the ions enter the diode, they are drawn to the poteiit ia'l minimum. Because of the inertia of the ions, they will overshoot the potential IfilIiil'Illll'il before they lose all of their kinetic energy.
- H I I The potential applied between the t'riode anode and the diode anode 23 is of the proper polarity to slow down the ions and the proper amplitude to allow the ions to enter, but to keep as many asvpossible from overshooting the potential minimum sufficiently to strike the diode anode 23. This potential would not be necessary if the ions do not have very large energy.
- the ions will be accelerated back towardsthe potential minimum and again inertia will make them overshoot.
- the ions will tend to oscillate about the potential minimum iintil they are neutralized by an electron in theelectron cloud, or until they drift axially out o'f the electron cloud. 7
- the change in plate current, resulting from the entralization of part of the space charge by the ions from the triode is a measure of the degree or vacuum in the it .i i
- the end plates on the diode serve to make it indie difiicult for the ions to leave the diode section after ehter'ing'. Thus they can be reionized again and again by the electrons in the diode, and contribute even more effectively to space charge neutralization. It has been found tha't leaving the end plates unconnected results in better operation;
- This improved ionization gauge ean be operated in several ways:
- the diode cathode would be used as the electron source, the grid would be used normally, and the cold triode cathode would behsd as the anode; This would give greater sensitivity than a.
- the device may be operated in the improved manner, with the triode connected as an ordinary ion gauge, and the diode operated as a space charge limited diode.
- the diode filament can be used for adsorption and flashing, and the triode can be used as an ordinary ionization gauge to measure the pull ballisticallyl b.
- the trio'de can be used to pump gas ions into the diode so less time is requiredfor the cold diode filament to adsorb a measurable quantity of gas, then the diode filament is flashed, and the triode is used tomeasu re the resulting pull ballistically. This will give reater sensitivity than a. p
- the triod'elfilament can be used to adsorb the gas
- Fig. 4 is a modification of the improved ionization gauge in which another diode 17 comprising cathode 18 and anode 19 has been added, said diode 17 being substantially electrically and mechanically similar to diode ll eiiceptthat aiiode 19 does not contain a slot correia qf ilot in1 a q' 2 59 e i I he adva nt ag'es ofthe modifications of Fig. 4 ean best be achieved by usiii'g a cricuit such as in Fig.
- Resistor 2 1 is adjusted s8 meter 20 readszero when no ions areeritering diode 11;
- the meter readihg' on meter can be callibrated in terms of i acuur n of the system being measured. 7 p I
- the main advantage of using the bridge circuit of Fig. 5 for the r neasurement of the anode currerit of diode 11 is that most of the randonivariations' in the anode current of diodell are balaneed out by similar variations in the anode cur rentof diode 17 Such random variations as filament temperatureand anode voltage thus will have little or no el fect ori the reading.
- Air ioriiz'atio'rrtype ya cuitim gauge comprising an envelope conta'ifiing a' gafsj the pressure of which is to be measured, a first spaee, dis 'charge device within said ehvi pe comprising a' holiow' anode member with an aperture the wall thereof, an'd a cathode and control grid within said member, means coupled to said discharge device for iiidihiai'i'iih said grid at a, positive potential respect to said cathode and said cathode at a; positive potential with resp'eettdsaid anode, a second space discharge device within said envelope adjacent saidfirst dis charg efi device eonip 'sing a hollow second anode V erribe'r with an aperture ulcerhe wall thereof, and a cathode withinsaid se'c' drhember', said second member beinlgf spaeed fr oni s
- An ionizatioii gauge comprising a tubee'nvelop'e containing a gas thelpressure of which to be measured; a first space discharge d eyi'ce wit n said envelope eof L prising a hdllow first anode jenjt" havingfa' restricted opening in' a'wall" thereof, a cathode disposed within said element and a: e i i' iee ede disposed within said element; a seeoh'd space die char'gedevi'cewithin said enve rape a'd'jac'en't saidfifirsji d schh 'gg" dev c comprising a hollow second anode element a restricted opening in a wall thereof eatl i ode disposedwithin said second element; said second element being disposed with its restricted opening adjacent the restricted opening in said first member.
- An ionization gauge comprising an envelope containing a gas the pressure of which is to be measured, a first space discharge device within said envelope comprising a hollow, substantially cylindrical first anode element having a longitudinal slot therein, a first filament within said element disposed on the longitudinal axis thereof, and a grid within said element concentric with said filament; and a second space discharge device within said envelope adjacent said first discharge device comprising a hollow, substantially cylindrical second anode element having a longitudinal slot therein and a second filament within said second element disposed on the longitudinal axis of said second element, said second element being disposed with the slot therein adjacent and substantially parallel to the slot in said first element.
- An ionization gauge comprising an envelope containing a gas the pressure of which is to be measured; a first space discharge device within said envelope comprising a hollow, substantially cylindrical first anode element having a longitudinal slot therein, a first cathode within said element disposed on the longitudinal axis thereof and a grid within said element concentric with said cathode; a second space discharge device within said envelope adjacent said first device comprising a hollow, substantially cylindrical second anode element having a longitudinal slot therein and a second cathode within said second element disposed on the longitudinal axis thereof, said second element being disposed with the slot therein adjacent and substantially parallel to the slot in said first element; and a third space discharge device within said envelope adjacent said first device comprising an unslotted, hollow, substantially cylindrical third anode element, and a third cathode within said third element disposed on the longitudinal axis thereof, said third element being disposed with its longitudinal axis substantially parallel to that of said first element.
Description
Oct. 25, 1955 J. ROTHSTEIN HIGH SENSITIVITY IONIZATION GAUGE Filed Aug. 4, 1952 INVENTOR.
JEROME ROTHSTEIN BY a A -r roam/5y FIG.5
United States Patent Ofiice Patented Oct. 25, 1955 HIGH SENSITIVITY IONIZATION GAUGE 7 Jerome Rothsteiu, Belmar, N. J., assignor to the United States of America as represented by the Secretary of the Army I The invention described herein may be manufactured and used by or for the Government for governmental purposes, without the payment of any royalty thereon.
This invention relates to an electron discharge device for measuring low pressures in vacuum systems by the measurement of ionization of the residual gas molecules by electrons emitted from the cathode of the device.
The usual ionization type of vacuum gauge is constructed as a normal triode, with a plate and grid and a hot cathode within said plate and grid. In operation, the grid is charged positively, and the anode is charged negatively with respect to the cathode. The envelope is connected to the system in which the pressure is to be measured, and the cathode is heated to emit electrons. The electrons are accelerated toward the grid, and collide with the residual gas molecules thus ionizing them. The positively charged ions are then attracted to the negative anode, where they are neutralized. The ion current to the anode is thus a measure of the number of residual gas molecules and thus of the pressure in the system. This type of vacuum gauge will measure down to about mm. of mercury. This lower limit is due to the fact that at these low pressures the electrons accelerated by the positive grid strike the grid with sutficient energy to generate soft X-rays, which in turn strike the anode, because the anode almost completely surrounds the grid, and these X-rays cause emission of photoelectrons from the anode which are collected by the grid. This electron current from the anode becomes of sufficient magnitude to mask the ion current to the anode at about 10-" mm. of mercury.
A modification of this standard type of vacuum gauge, the Bayard-Alpert Gauge, uses a fine wire anode, a cylindrical grid surrounding the anode, and a cathode outside of the grid. The operation is the same, but by making the anode small, a much smaller fraction of the X-rays strike the anode, so the photocurrent is much less. This simple modification enables measurements down to about 10 mm. of mercury.
The triode ionization type gauge can be used with the flash filament technique to extend the lower limit of measurement. The filament is cleaned of adsorbed gas, then allowed to remain cold on the vacuum to be measured. Residual gas is adsorbed on the filament over a period of time, after which the filament is quickly heated to incandescence, or flashed. The high temperature drives oil the adsorbed gases, giving a puff of gas which is measured ballistically by the ionization gauge in the usual manner. The greater the degree of vacuum, the longer it takes to adsorb a measurable quantity of gas.
The limitation of the standard ionization vacuum gauge and its modifications is the photocurrent from the anode caused by the soft X-rays generated by the electrons striking the grid at high velocity, and, in the case of the flash filament technique, the time required for the cold filament to adsorb a measurable quantity of gas becomes prohibitively long for very low pressures.
Therefore, it is an object of this invention to provide an 2 ionization type vacuum gauge in which the soft X-rays generated have substantially no efiect on the gauge reading.
' A further object is to provide an ionization type vacuum gauge which is capable of measuring pressures much lower than other vacuum gauges.
Another object is to providea vacuum gauge capable o measuring routinely down to l0 mm. of mercury, and perhaps lower under ideal conditions.
' .Another object is to provide a vacuum gauge capable of operating as a conventional, Bayard-Alpert, or improved ionization vacuum gauge, depending on the pres sure range,and on the connections and potentials applied.
Another object is to provide a vacuum gauge capable of operation with the flash filament technique with materially shortened adsorption time.
These and further objects of this invention will become apparent from the following specification taken in connection with the claims and drawings.
Fig. l is a perspective view partly cut away of a preferred embodiment of the invention.
Fig. 2 is a top view of Fig. l and includes a schematic representation of the applied potentials.
Fig. 3 is the voltage distance relationship in the diode when the gauge is operated in the improved manner.
Fig. 4 is a top view of a modification of Fig. 1.
Fig. 5 is a circuit used with the modification of Fig. 4.
Referring now to the accompanying drawings, there is shown in Fig. 1 a preferred embodiment of the improved ionization gauge comprising an envelope 9 in which 10 is a triode section in which 12 is a cathode, which is heated (heater source not shown) to emit electrons, consisting preferably of a strand of pure tungsten wire, and said cathode 12 is charged positively with respect to the triode anode 15 and said cathode 12 is charged negatively with respect to the triode grid 13. Diode 11 also has its cathode 14 heated (heater source not shown) to emit electrons, and also consists preferably of a strand of pure tungsten wire, and said cathode 14 is charged negatively with respect to the diode anode 23 so the diode 11 operates under what is known as space charge limited conditions, where the voltage on the anode 23 is not sulficiently positive to attract all the electrons emitted by the cathode 14, and there is a considerable relatively stationary space charge surrounding the cathode. The triode anode 15, having a slot 24 therein is made negative with respect to the diode anode 23, having a slot 25 therein. Triode anode 15 and diode anode 23 are placed in close proximity, and slot 24 and slot 25 are placed so that substantially all of the ions leaving triode 10 through slot 24 can enter diode 11 through slot 25. Slots 24 and 25 each have an area which is relatively small compared to the total area of the anodes 15 and 23 respectively.
The envelope of the device is mechanically connected to the system in which the pressure is to be measured, and some of the residual gas molecules will be in the volume of the triode when the pressures in the system and in the gauge become equalized. The electrons emitted by the triode cathode are accelerated towards the positive grid, and some of the electrons will collide with gas molecules, thus ionizing them. These positively charged ions are then attracted to the triode anode, and most of them are neutralized by the negative charge thereon. However, a fraction of the ions approximately equal to the ratio of slot area to triode anode area will be traveling in a path that will cause them to go through the slot 24 in the triode anode 15, and enter the volume of the diode 11 through the slot 25 in the diode anode 23.
The voltage applied between the triode anode 15 and.
the diode anode 23 is of the proper amplitude and polarity to slow 'down the ions but not great enough to prevent the ions from entering the volume of the diode.
In the diode, the anode voltage and the cathode heating current are so proportioned to cause the diode to o'p erate in the space-charged limited manner. In this mode of operation, the anode voltage is not high enough to attract all of the elections which are emitted by the cathode, so electron clOud forms as a sheath iiiqi i a the cathode. Becauseof the density of the electron cloud, the voltage in the densest, portion will be more negative thari the cathode. This poteiitial vs, radius distribution is shown in Fig. 3, where V is the anode voltag'e'in the diode, Vc is the cathode voltage in the diode, R5 is the anode radius, and the cathode is con sidered to be at the origin. Thus, in Fig. 3, point is at the,l otential m nimum, arid this minimum is below the eatho'de potential. v
Wheii the ions enter the diode, they are drawn to the poteiit ia'l minimum. Because of the inertia of the ions, they will overshoot the potential IfilIiil'Illll'il before they lose all of their kinetic energy. H I I The potential applied between the t'riode anode and the diode anode 23 is of the proper polarity to slow down the ions and the proper amplitude to allow the ions to enter, but to keep as many asvpossible from overshooting the potential minimum sufficiently to strike the diode anode 23. This potential would not be necessary if the ions do not have very large energy.
Then the ions will be accelerated back towardsthe potential minimum and again inertia will make them overshoot. Thus, the ions will tend to oscillate about the potential minimum iintil they are neutralized by an electron in theelectron cloud, or until they drift axially out o'f the electron cloud. 7
While an ion is in the vicinity of the potential minimum, it will neutralize some of the electron space charge, Because an ion has a much larger mass and a much lower velocity than an electron for the same energy, it will neutralize many electrons, as each electron would only be in the field of each ion for a very short time. As man'y a's' 70,000 extra electrons can flow to the plate as a result of the entry of a single positive ioii.
The change in plate current, resulting from the entralization of part of the space charge by the ions from the triode is a measure of the degree or vacuum in the it .i i
The end plates on the diode serve to make it indie difiicult for the ions to leave the diode section after ehter'ing'. Thus they can be reionized again and again by the electrons in the diode, and contribute even more effectively to space charge neutralization. It has been found tha't leaving the end plates unconnected results in better operation;
This improved ionization gauge ean be operated in several ways:
a. As a conventional ionization gauge, the triode alone would be used.
b. a Bayard-Alpert gauge, the diode cathode would be used as the electron source, the grid would be used normally, andthe cold triode cathode would behsd as the anode; This would give greater sensitivity than a.
c; The device may be operated in the improved manner, with the triode connected as an ordinary ion gauge, and the diode operated as a space charge limited diode.
The following adaptations of the flash filament techniques; are possible:
al The diode filament can be used for adsorption and flashing, and the triode can be used as an ordinary ionization gauge to measure the pull ballisticallyl b. The trio'de can be used to pump gas ions into the diode so less time is requiredfor the cold diode filament to adsorb a measurable quantity of gas, then the diode filament is flashed, and the triode is used tomeasu re the resulting pull ballistically. This will give reater sensitivity than a. p
.- The triod'elfilament can be used to adsorb the gas,
arid the pull released on flashing can be measured bal- 4 listically in the diode. This method would be more sensitlVe than "a 01 "[7.
The soft X-rays which limit the degree of vacuum which may be measured with conventional gauges do not affect this gauge for three reasons:
1. Only a small fraction of the X-rays generated at the triode grid pass through the slot into the diode.
2. The photo-electrons which are emitted from the diode anode because of the X-rays fallingon it are recollected by the diode anode, and so do not afllect the external diode current. V
3. The photoelectrons which, are emitted from the diode cathode because of the X-rays falling on it are merely added to the thermionically emitted electrons in thespace charge and so cause negligible external eifect.
Fig. 4 is a modification of the improved ionization gauge in which another diode 17 comprising cathode 18 and anode 19 has been added, said diode 17 being substantially electrically and mechanically similar to diode ll eiiceptthat aiiode 19 does not contain a slot correia qf ilot in1 a q' 2 59 e i I he adva nt ag'es ofthe modifications of Fig. 4 ean best be achieved by usiii'g a cricuit such as in Fig. 5, which has a meter 26, variable resistor 21, a suitable source of current 2}, s' ieh as' a'; battery, aiid diodes 11 and 17 as pr eviously referred to, which can beused for the measure- I'iieiit of the anode current change in diode 11. Since dio'des 1' l and l7 are similar, the anode currents of each should be very nearly equal. Resistor 2 1 is adjusted s8 meter 20 readszero when no ions areeritering diode 11; Thusgwhen the anode cuirei t of diode 11 increases, the meter readihg' on meter can be callibrated in terms of i acuur n of the system being measured. 7 p I The main advantage of using the bridge circuit of Fig. 5 for the r neasurement of the anode currerit of diode 11 is that most of the randonivariations' in the anode current of diodell are balaneed out by similar variations in the anode cur rentof diode 17 Such random variations as filament temperatureand anode voltage thus will have little or no el fect ori the reading.
What isjua iiai is; v
1: Air ioriiz'atio'rrtype ya cuitim gauge comprising an envelope conta'ifiing a' gafsj the pressure of which is to be measured, a first spaee, dis 'charge device within said ehvi pe comprising a' holiow' anode member with an aperture the wall thereof, an'd a cathode and control grid within said member, means coupled to said discharge device for iiidihiai'i'iih said grid at a, positive potential respect to said cathode and said cathode at a; positive potential with resp'eettdsaid anode, a second space discharge device within said envelope adjacent saidfirst dis charg efi device eonip 'sing a hollow second anode V erribe'r with an aperture irithe wall thereof, and a cathode withinsaid se'c' drhember', said second member beinlgf spaeed fr oni sa d first member a'nd being disposed with the aperture thereof facing t'he aperture of said first member, means coupled to said second space discharge del licei fOr applyiriga potential difference between the cathode and anode thereof to cause spaceon thereof and fo'ir maintaining said charge limited o'pe d v secorid anode member at ajpo'sitive'p'otential with respect to said first anode member, and means in circuit with said second space discharge device for measuring the current t heretlirough; V H
2. An ionizatioii gauge comprising a tubee'nvelop'e containing a gas thelpressure of which to be measured; a first space discharge d eyi'ce wit n said envelope eof L prising a hdllow first anode jenjt" havingfa' restricted opening in' a'wall" thereof, a cathode disposed within said element and a: e i i' iee ede disposed within said element; a seeoh'd space die char'gedevi'cewithin said enve rape a'd'jac'en't saidfifirsji d schh 'gg" dev c comprising a hollow second anode element a restricted opening in a wall thereof eatl i ode disposedwithin said second element; said second element being disposed with its restricted opening adjacent the restricted opening in said first member.
3. An ionization gauge as set forth in claim 2, further including a third space discharge device within said envelope adjacent said first space discharge device comprising a hollow third anode element having continuous walls and a cathode disposed within said third element.
4. An ionization gauge as set forth in claim 3, including means for applying a potential difference between the cathode and anode of each of said second and third space discharge devices, respectively, to cause space-charge limited operation of said devices, a bridge circuit, said second and third discharge devices being connected in series with opposite arms of said circuit, means for equalizing the current flow through said second and third discharge devices thereby balancing said bridge circuit, means connected across said bridge circuit for indicating a condition of unbalance thereof, means for heating the cathode of said first discharge device, and means for maintaining the control electrode of said first discharge device at a positive potential with respect to its cathode, the cathode of said first discharge device at a positive potential with respect to its anode element, and said last named anode element at a negative potential with respect to said second anode element.
5. An ionization gauge comprising an envelope containing a gas the pressure of which is to be measured, a first space discharge device within said envelope comprising a hollow, substantially cylindrical first anode element having a longitudinal slot therein, a first filament within said element disposed on the longitudinal axis thereof, and a grid within said element concentric with said filament; and a second space discharge device within said envelope adjacent said first discharge device comprising a hollow, substantially cylindrical second anode element having a longitudinal slot therein and a second filament within said second element disposed on the longitudinal axis of said second element, said second element being disposed with the slot therein adjacent and substantially parallel to the slot in said first element.
6. An ionization gauge as set forth in claim 5, further including a conductive member covering and spaced from each end of said second element.
7. An ionization gauge as set forth in claim 5, including means for heating said first and second filaments, means coupled to said first discharge device for maintaining its grid at a positive potential with respect to its filament and its filament at a positive potential with respect to its anode element, means coupled to said second discharge device for applying a potential difference between the filament and anode element thereof to cause space-charge limited operating thereof, and for maintaining said second member at a positive potential with respect to said first member, and means in circuit with said second discharge device for measuring the current therethrough.
8. An ionization gauge as set forth in claim 5, including means for heating said second filament, said first filament being maintained cold, means for maintaining said grid at a positive potential with respect to said second filament and said second filament at a positive potential with respect to said first filament, and means in circuit with said first and second filaments for measuring the space current therebetween.
9. An ionization gauge as set forth in claim 5, including means for heating said first filament, means for maintaining said grid at a positive potential with respect to said first filament and said first filament at a positive potential with respect to said first element, means for flashing said second filament comprising means for quickly heating said second filament from cold condition to incandescence, and means in circuit with said first discharge device for measuring the change in current therethrough due to said flashing of said second filament.
10. An ionization gauge comprising an envelope containing a gas the pressure of which is to be measured; a first space discharge device within said envelope comprising a hollow, substantially cylindrical first anode element having a longitudinal slot therein, a first cathode within said element disposed on the longitudinal axis thereof and a grid within said element concentric with said cathode; a second space discharge device within said envelope adjacent said first device comprising a hollow, substantially cylindrical second anode element having a longitudinal slot therein and a second cathode within said second element disposed on the longitudinal axis thereof, said second element being disposed with the slot therein adjacent and substantially parallel to the slot in said first element; and a third space discharge device within said envelope adjacent said first device comprising an unslotted, hollow, substantially cylindrical third anode element, and a third cathode within said third element disposed on the longitudinal axis thereof, said third element being disposed with its longitudinal axis substantially parallel to that of said first element.
11. An ionization gauge as set forth in claim 10, further including a bridge circuit having four arms, said second and third devices being in series with the first and fourth arms of said bridge, respectively, means in at least a third arm of said bridge for varying the impedance thereof, a source of potential to cause space-current limited operation of said second and third devices connected across said bridge from the junction of the first and fourth arms thereof to the junction of the second and third arms thereof, a meter for indicating unbalance of said bridge connected between the junction of the first and second arms thereof and the junction of the third and fourth arms thereof, means for heating the cathode of said first device, and means for maintaining the grid at a positive potential with respect to said first cathode, said first cathode at a positive potential with respect to said first element, and said first element at a negative potential with respect to said second element.
References Cited in the file of this patent UNITED STATES PATENTS 1,566,279 King Dec. 22, 1925 1,871,443 Berthold Aug. 16,1932 1,925,558 Foster Sept. 5,1933 2,243,902 Guntherschulze June 3, 1941
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US302640A US2721972A (en) | 1952-08-04 | 1952-08-04 | High sensitivity ionization gauge |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US302640A US2721972A (en) | 1952-08-04 | 1952-08-04 | High sensitivity ionization gauge |
Publications (1)
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US2721972A true US2721972A (en) | 1955-10-25 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US302640A Expired - Lifetime US2721972A (en) | 1952-08-04 | 1952-08-04 | High sensitivity ionization gauge |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3138736A (en) * | 1960-04-16 | 1964-06-23 | United Aircraft Corp | Electron beam generator system |
US3267326A (en) * | 1963-09-05 | 1966-08-16 | Varian Associates | Vacuum gauge |
US3986111A (en) * | 1974-12-24 | 1976-10-12 | The United States Of America As Represented By The Secretary Of The Navy | Inverted voltage Gerdien Condenser |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1566279A (en) * | 1921-01-10 | 1925-12-22 | Western Electric Co | Gas-pressure control |
US1871443A (en) * | 1924-10-06 | 1932-08-16 | Westinghouse Electric & Mfg Co | Space current device |
US1925558A (en) * | 1925-01-08 | 1933-09-05 | Rca Corp | Rectifying device |
US2243902A (en) * | 1939-02-03 | 1941-06-03 | Hermes Patentverwertungs Gmbh | Gas filled electron tube |
-
1952
- 1952-08-04 US US302640A patent/US2721972A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1566279A (en) * | 1921-01-10 | 1925-12-22 | Western Electric Co | Gas-pressure control |
US1871443A (en) * | 1924-10-06 | 1932-08-16 | Westinghouse Electric & Mfg Co | Space current device |
US1925558A (en) * | 1925-01-08 | 1933-09-05 | Rca Corp | Rectifying device |
US2243902A (en) * | 1939-02-03 | 1941-06-03 | Hermes Patentverwertungs Gmbh | Gas filled electron tube |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3138736A (en) * | 1960-04-16 | 1964-06-23 | United Aircraft Corp | Electron beam generator system |
US3267326A (en) * | 1963-09-05 | 1966-08-16 | Varian Associates | Vacuum gauge |
US3986111A (en) * | 1974-12-24 | 1976-10-12 | The United States Of America As Represented By The Secretary Of The Navy | Inverted voltage Gerdien Condenser |
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