US3144200A - Process and device for cryogenic adsorption pumping - Google Patents

Process and device for cryogenic adsorption pumping Download PDF

Info

Publication number
US3144200A
US3144200A US231311A US23131162A US3144200A US 3144200 A US3144200 A US 3144200A US 231311 A US231311 A US 231311A US 23131162 A US23131162 A US 23131162A US 3144200 A US3144200 A US 3144200A
Authority
US
United States
Prior art keywords
gas
chamber
pumping
hydrogen gas
approximately
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
US231311A
Inventor
Clyde E Taylor
Angus L Hunt
John E Omohundro
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US231311A priority Critical patent/US3144200A/en
Application granted granted Critical
Publication of US3144200A publication Critical patent/US3144200A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B37/00Pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B25/00 - F04B35/00
    • F04B37/06Pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B25/00 - F04B35/00 for evacuating by thermal means
    • F04B37/08Pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B25/00 - F04B35/00 for evacuating by thermal means by condensing or freezing, e.g. cryogenic pumps

Definitions

  • the present invention relates to vacuum pumping and, more particularly, to a process and device capable of pumping hydrogen gas at a high rate.
  • the device comprises an adsorption element having a thermally conducting surface within a vacuum chamber, means for evacuating said chamber, to high vacuum-of the order of mm. Hg, means for cooling the aforementioned surface to about 11 Kelvin and means for the alternate introduction of either hydrogen or a substrate gas into said chamber.
  • a major difiiculty is that if access to the interior is not to be severely restricted, demountable vacuum seals, commonly with metal or Teflon gaskets, must be used on the vacuum ports. Demountable seals often fail under hightemperature treatment. Further, thermal treatment of large structures requires very exact mechanical design clue to the expansions and contractions of the structures resulting from the aforementioned thermal treatment.
  • a problem that pertains more specifically to the area of plasma research is the maintenance of ultra-high vacuum conditions in these large metal vacuum systems under an appreciable hydrogen or deuterium influx.
  • the present invention overcomes the above-mentioned difficulties in a unique manner, i.e., depositing a solidified layer of a substrate gas upon a cold surface located within an already evacuated chamber.
  • the system is then eapable of cryo-pumping hydrogen gas, in the ultra-high vacuum region, at high pumping speeds and in relatively large quantities by adsorption of the hydrogen gas on the solidified substrate surface.
  • the worth of this system is more readily apparent when considering the fact that the equilibrium vapor pressure of hydrogen gas is approximately 2 mm. Hg at approximately 11 K., a fact that, prior to the present invention, precluded the cryo-pumping of hydrogen gas at high vacuum pressures.
  • solidified gas films of A, N 0 E 0, N OQand CO have been individually used and hydrogen gas has been rapidly adsorbed at 11 Kelvin on all of them.
  • This pumping of hydrogen was done while the chamber was evacuated to the 10- mm. Hg pressure range, and it is to be noted that the vapor pressures of all of the above gases at 11 Kelvin are less than 10' mm. Hg. Indeed, the use of any gas whose vapor pressure at 11 Kelvin is less than the degree of vacuum desired is within the scope of the present invention.
  • the general pawn eters of the present invention comprises; the equilibrium vapor pressure, at the cryogenic temperature desired, of the gas to be pumped, the environmental vacuum pressure required, and the equilibrium vapor pressure, again at the cryogenic temperature desired, of the substrate gas. More particularly, the equilibrium vapor pressure of the substrate gas should be less than the environmental vacuum pressure.
  • the high vacuum chamber associated with a preferred embodiment of the present invention is constructed of aluminum alloy; the flanges common to this chamber being sealed with Teflon rings. While in general such a construction in the past has limited base pressures to 10- mm. Hg, it is possible through the use of the present invention to obtain and maintain pressures of approximately 10 mm. Hg while pumping hydrogen at a speed of 60,000 liters per second.
  • a cryogenic adsorption pump 11 comprising a vacuum chamber 12, an adsorption element 13 within said chamber, a helium refrigerator 14 for cooling element 13, conventional pump means 16 for evacuating said chamber, and a reservoir of substrate gas 17.
  • a preferred embodiment of pump 16 is an oil diffusion pump which is trapped with a liquid nitrogen trap of ultra-high vacuum design and is connected to the high vacuum chamber 12 through an all-metal valve 18 as is also shown schematically in the drawing.
  • helium coolant for adsorption element 13 is transferred from refrigerator 14 to the high vacuum chamber 12 through copper lines 19 which are insulated by a space which is evacuated by conventional means (not shown).
  • a preferred embodiment of adsorption element 13 is a copper cylinder with an interior winding of transfer lines 19.
  • Helium gas thermometer 21 monitors the temperature of this copper cylinder. Capillary tubing for this thermometer is brought out of this high vacuum chamber through the interior of transfer lines 19 to prevent any temperature transition regions which might establish high vapor pressure surfaces.
  • Vacuum chamber 12 could be used if adaptable to suitable cooling means.
  • oil diffusion pump 16 is connected to high vacuum chamber 12 through all metal valve 18, as shown schematically in the figure. Chamber 12 is then pumped down to about 10 mm. Hg by means of pump 16.
  • the surface of adsorption element 13 is cooled to about 11 Kel- 3 vin by helium refrigerator 14.
  • the helium coolant for cooling element 13 is transferred from refrigerator 14 to vacuum chamber 12 by means of transfer lines 19.
  • Cold transfer lines 19 enter high vacuum chamber 12 through flange 23 and are soldered to the interior of surface 13, thereby partially supporting said surface.
  • the pressure range within chamber 12 decreases to the 1() mm. Hg range. This pressure is indicated by ionization gauge 24 which extends into the evacuated space through a seal means.
  • the substrate gas is emitted from reservoir 17 through valve 26 and into chamber 12 where it forms a solidified gas film upon adsorption element 13.
  • gases have been used with the pump, supra, and of these gases CO and N have been selected as preferred substrates since they absorb 40% of the hydrogen molecules falling on them until approximately hydrogen molecules are absorbed per square centimeter of their surface. Because of the low vapor pressure of these preferred substrates at the low temperature of operation, the vacuum conditions within chamber 12 are not permanently impaired by their introduction. This is due to the virtually complete solidification of the substrate upon adsorption element 13. The system is now capable of pumping hydrogen gas at a high rate.
  • valve 27 is opened and hydrogen gas is thereby admitted to chamber 12.
  • the rate of pumping gradually decreases due to the saturation of the solidified substrate surface.
  • the pump is reactivated.
  • Reactivation of the pump is initiated as follows; thermally conducting surface 13 is increased in temperature to the order of Kelvin, i.e., between the hydrogen triple-point temperature and the normal boiling temperature. At this temperature the hydrogen gas vapor pressure increases to the extent that it is desorbed from adsorption element 13 and is slowly pumped out of chamber 12 by means of pump 16. The temperature of adsorption element 13 is again decreased to 11 Kelvin. This saturation and reactivation may be continued as a cycle without replacing the solidified substrate.
  • gas adsorption means disposed in an evacuated chamber and comprising (a) a surface cooled to a temperature of approximately 11 K., and I (b) a solidified layer of gas having a vapor pressure at approximately 11 K. less than the pressure of said evacuated chamber, said solidified layer being adhered to said surface.
  • hydrogen gas adsorption means disposed in an evacuated chamber and comprising (a) an adsorption element having a surface cooled to a temperature of approximately 11 K., and (b) a solidified layer of gas selected from the group ,4 consisting of gases whose vapor pressures at approximately 11 K. are less than approximately 10- mm. Hg, said solidified layer being adhered to said surface.
  • an adsorption element comprising (a) means defining a surface area
  • refrigeration means said refrigeration means being positioned in thermal communication with said surface so as to cool said surface to approximately 11 K.
  • the adsoprtion element according to claim 3 wherein said solidified layer of gas is selected from the group consisting of A, N 0 I1 0, N 0, and C0 5.
  • the adsorption element according to claim 3 wherein said adsorption element comprises a copper cylinder.
  • a cryogenic adsorption pump for hydrogen gas comprising (a) a vacuum chamber,
  • cryogenic adsorption pump according to claim 6 wherein the conventional pump means comprises a liquid nitrogen trapped oil diffusion pump of ultra-high vacuum design, said pump being in valved communication with said vacuum chamber.
  • cryogenic adsorption pump according to claim 6 wherein the cooling means comprises a helium refrigerator, said helium refrigerator being in thermal con duction relationship with the aforementioned adsorption element by means of cryogenic fluid transfer lines.
  • cryogenic adsorption pump according to claim 6 wherein the gas in said reservoir is selected from the group consisting of gases whose vapor pressures are less than l0 mm. Hg at approximately 11 K.
  • cryogenic adsorption pump according to claim 6 wherein the gas in said reservoir is selected from the group consisting of N 0 and CO 11.
  • the step comprising adsorbing the gas upon a surface cooled to cryogenic temperatures and upon which is adhered a solidified layer of gas selected from the group consisting of gases whose vapor pressures are less than the background pressure of the surrounding environment.
  • a process for pumping hydrogen gas comprising (at) introducing hydrogen gas into an evacuated chamber containing an adsorption element, the surface of which is cooled to 11 K. and upon which is adhered a solidified layer of gas selected from the group consisting of gases whose vapor pressures are less than 10- mm. Hg, and
  • the substrate gas is selected from the group consisting of A, N H O, N 0, CO

Description

Aug. 11, 1964 c. E. TAYLOR ETAL PROCESS AND DEVICE FOR CRYOGENIC ABSORPTION PUMPING Filed Oct. 17, 1962 RTO ONR m w Y OM U E m LH w B5 0 O V WM T mw m W N HWW United States Patent 3,144,200 PROCESS AND DEVICE FOR CRYOGENIC ABSORPTION PUMPING Clyde E. Taylor, Livermore, Angus L. Hunt, Alamo, and John E. Omohundro, San Jose, Calif, assiguors to the United States of America as represented by the United States Atomic Energy Commission Filed Oct. 17, 1962, Ser. No. 231,311 17 Claims. (Cl. 230-69) The present invention relates to vacuum pumping and, more particularly, to a process and device capable of pumping hydrogen gas at a high rate. In general, the device comprises an adsorption element having a thermally conducting surface within a vacuum chamber, means for evacuating said chamber, to high vacuum-of the order of mm. Hg, means for cooling the aforementioned surface to about 11 Kelvin and means for the alternate introduction of either hydrogen or a substrate gas into said chamber.
In the past, it has generally been considered necessary to bake large metal vacuum systems to at least 400 C. to reduce later degassing from the walls and to allow use of conventional pumping methods. However, there are several practical difficulties inherent to this high temperature treatment of these large metal vacuum systems, some of which are as follows:
A major difiiculty is that if access to the interior is not to be severely restricted, demountable vacuum seals, commonly with metal or Teflon gaskets, must be used on the vacuum ports. Demountable seals often fail under hightemperature treatment. Further, thermal treatment of large structures requires very exact mechanical design clue to the expansions and contractions of the structures resulting from the aforementioned thermal treatment.
A problem that pertains more specifically to the area of plasma research is the maintenance of ultra-high vacuum conditions in these large metal vacuum systems under an appreciable hydrogen or deuterium influx. Heretofore, attempts have been made to solve this particular problem through the prolonged operation of large and expensive diffusion pumps, but faster pumping rates are desired in the furtherance of the above-noted plasma research.
The present invention overcomes the above-mentioned difficulties in a unique manner, i.e., depositing a solidified layer of a substrate gas upon a cold surface located within an already evacuated chamber. The system is then eapable of cryo-pumping hydrogen gas, in the ultra-high vacuum region, at high pumping speeds and in relatively large quantities by adsorption of the hydrogen gas on the solidified substrate surface. The worth of this system is more readily apparent when considering the fact that the equilibrium vapor pressure of hydrogen gas is approximately 2 mm. Hg at approximately 11 K., a fact that, prior to the present invention, precluded the cryo-pumping of hydrogen gas at high vacuum pressures.
In a preferred embodiment of the present invention, solidified gas films of A, N 0 E 0, N OQand CO have been individually used and hydrogen gas has been rapidly adsorbed at 11 Kelvin on all of them. This pumping of hydrogen was done while the chamber was evacuated to the 10- mm. Hg pressure range, and it is to be noted that the vapor pressures of all of the above gases at 11 Kelvin are less than 10' mm. Hg. Indeed, the use of any gas whose vapor pressure at 11 Kelvin is less than the degree of vacuum desired is within the scope of the present invention.
It is to be noted that a preferred embodiment of the present invention pumps hydrogen gas at a very high rate. However, reduced to its simplest form, the general pawn eters of the present invention comprises; the equilibrium vapor pressure, at the cryogenic temperature desired, of the gas to be pumped, the environmental vacuum pressure required, and the equilibrium vapor pressure, again at the cryogenic temperature desired, of the substrate gas. More particularly, the equilibrium vapor pressure of the substrate gas should be less than the environmental vacuum pressure.
The high vacuum chamber associated with a preferred embodiment of the present invention is constructed of aluminum alloy; the flanges common to this chamber being sealed with Teflon rings. While in general such a construction in the past has limited base pressures to 10- mm. Hg, it is possible through the use of the present invention to obtain and maintain pressures of approximately 10 mm. Hg while pumping hydrogen at a speed of 60,000 liters per second.
It is a primary object of the present invention, therefore, to provide a cryogenic adsorption pump capable of pumping hydrogen gas.
It is a further object of the present invention to provide a process for pumping gas.
Other objects and advantages of the present invention will be more readily ascertained from an inspection of the following specification, taken in connection with the accompanying drawing, of which the single figure is an isometric, sectional view of the invention, while the features of novelty will be more distinctly pointed out in the appended claims. Referring to the drawing, there is shown a schematic presentation of a preferred embodiment of a cryogenic adsorption pump 11 comprising a vacuum chamber 12, an adsorption element 13 within said chamber, a helium refrigerator 14 for cooling element 13, conventional pump means 16 for evacuating said chamber, and a reservoir of substrate gas 17.
A preferred embodiment of pump 16 is an oil diffusion pump which is trapped with a liquid nitrogen trap of ultra-high vacuum design and is connected to the high vacuum chamber 12 through an all-metal valve 18 as is also shown schematically in the drawing. In this preferred embodiment helium coolant for adsorption element 13 is transferred from refrigerator 14 to the high vacuum chamber 12 through copper lines 19 which are insulated by a space which is evacuated by conventional means (not shown).
As shown in the drawing, a preferred embodiment of adsorption element 13 is a copper cylinder with an interior winding of transfer lines 19. Helium gas thermometer 21 monitors the temperature of this copper cylinder. Capillary tubing for this thermometer is brought out of this high vacuum chamber through the interior of transfer lines 19 to prevent any temperature transition regions which might establish high vapor pressure surfaces.
Although a copper cylinder is shown, it is to be understood that any object having a surface capable of being cooled to approximately 11 Kelvin would provide an adequate adsorption element. Indeed, the inner walls of Vacuum chamber 12 could be used if adaptable to suitable cooling means.
The process of operating the above apparatus to achieve high speed pumping of hydrogen and deuterium gases is also novel. In order that the process be better understood, reference is once more made to the drawing.
To initiate a preferred operation, oil diffusion pump 16 is connected to high vacuum chamber 12 through all metal valve 18, as shown schematically in the figure. Chamber 12 is then pumped down to about 10 mm. Hg by means of pump 16.
To continue the preferred operation (above), the surface of adsorption element 13 is cooled to about 11 Kel- 3 vin by helium refrigerator 14. The helium coolant for cooling element 13 is transferred from refrigerator 14 to vacuum chamber 12 by means of transfer lines 19. Cold transfer lines 19 enter high vacuum chamber 12 through flange 23 and are soldered to the interior of surface 13, thereby partially supporting said surface. As surface 13 is refrigerated to 11 Kelvin, the pressure range within chamber 12 decreases to the 1() mm. Hg range. This pressure is indicated by ionization gauge 24 which extends into the evacuated space through a seal means.
Then, the substrate gas is emitted from reservoir 17 through valve 26 and into chamber 12 where it forms a solidified gas film upon adsorption element 13. Various gases have been used with the pump, supra, and of these gases CO and N have been selected as preferred substrates since they absorb 40% of the hydrogen molecules falling on them until approximately hydrogen molecules are absorbed per square centimeter of their surface. Because of the low vapor pressure of these preferred substrates at the low temperature of operation, the vacuum conditions within chamber 12 are not permanently impaired by their introduction. This is due to the virtually complete solidification of the substrate upon adsorption element 13. The system is now capable of pumping hydrogen gas at a high rate.
At this time valve 27 is opened and hydrogen gas is thereby admitted to chamber 12. As this gas is admitted, the rate of pumping gradually decreases due to the saturation of the solidified substrate surface. When the pumping speed has decreased below a desired rate, as is evidenced by a higher reading on ion gauge 24, the pump is reactivated.
Reactivation of the pump is initiated as follows; thermally conducting surface 13 is increased in temperature to the order of Kelvin, i.e., between the hydrogen triple-point temperature and the normal boiling temperature. At this temperature the hydrogen gas vapor pressure increases to the extent that it is desorbed from adsorption element 13 and is slowly pumped out of chamber 12 by means of pump 16. The temperature of adsorption element 13 is again decreased to 11 Kelvin. This saturation and reactivation may be continued as a cycle without replacing the solidified substrate.
The above-mentioned steps, in combination, comprise a process whereby large quantities of hydrogen gas are pumped at high rates. Although hydrogen gas has been specified as the gas to be pumped, it will be apparent to those skilled in the art that many other gases with the notable exception of helium gas, can be likewise pumped through the use of the present process. This pumping of gases other than helium would merely entail an adjustment in parameters namely that of the substrate gas used.
While the present invention has been described in detail with respect to one embodiment thereof, it will be apparent that numerous modifications may be made Within the spirit and scope of the invention. It is therefore not desired to limit the invention to the exact details shown except insofar as they are'defined in the following claims.
What is claimed is: 1. In a cryogenic adsorption pump of the class described herein, gas adsorption means disposed in an evacuated chamber and comprising (a) a surface cooled to a temperature of approximately 11 K., and I (b) a solidified layer of gas having a vapor pressure at approximately 11 K. less than the pressure of said evacuated chamber, said solidified layer being adhered to said surface.
2. In a cryogenic adsorption pump for hydrogen gas of the class described herein, hydrogen gas adsorption means disposed in an evacuated chamber and comprising (a) an adsorption element having a surface cooled to a temperature of approximately 11 K., and (b) a solidified layer of gas selected from the group ,4 consisting of gases whose vapor pressures at approximately 11 K. are less than approximately 10- mm. Hg, said solidified layer being adhered to said surface.
3. In a cryogenic adsorption pump of the class described herein, an adsorption element comprising (a) means defining a surface area,
(b) refrigeration means, said refrigeration means being positioned in thermal communication with said surface so as to cool said surface to approximately 11 K., and
(c) a solidified layer of gas selected from the group consisting of gases whose vapor pressures at approximately 11 K. are less than the pressure of the environment Within which the adsorption element resides, said solidified layer being adhered to said surface area.
4. The adsoprtion element according to claim 3 wherein said solidified layer of gas is selected from the group consisting of A, N 0 I1 0, N 0, and C0 5. The adsorption element according to claim 3 wherein said adsorption element comprises a copper cylinder.
6. A cryogenic adsorption pump for hydrogen gas comprising (a) a vacuum chamber,
(b) conventional pump means in gas-tight communication with said vacuum chamber,
(0) an adsorption element positioned within said vacuum chamber,
(d) cooling means in thermal conduction relationship with said adsorption element,
(e) a reservoir of gas, the gas in said reservoir having a vapor pressure, when solidified upon said adsorption element, which is less than the pressure established in said vacuum chamber, said reservoir being in gastight communication with said vacuum chamber, and
(f) means for introducing hydrogen gas into said vacuum chamber. t
7. The cryogenic adsorption pump according to claim 6 wherein the conventional pump means comprises a liquid nitrogen trapped oil diffusion pump of ultra-high vacuum design, said pump being in valved communication with said vacuum chamber.
8. The cryogenic adsorption pump according to claim 6 wherein the cooling means comprises a helium refrigerator, said helium refrigerator being in thermal con duction relationship with the aforementioned adsorption element by means of cryogenic fluid transfer lines.
9. The cryogenic adsorption pump according to claim 6 wherein the gas in said reservoir is selected from the group consisting of gases whose vapor pressures are less than l0 mm. Hg at approximately 11 K.
10. The cryogenic adsorption pump according to claim 6 wherein the gas in said reservoir is selected from the group consisting of N 0 and CO 11. In a process for pumping gas, the step comprising adsorbing the gas upon a surface cooled to cryogenic temperatures and upon which is adhered a solidified layer of gas selected from the group consisting of gases whose vapor pressures are less than the background pressure of the surrounding environment.
12. In a process for pumping hydrogen gas, the steps comprising (at) introducing hydrogen gas into an evacuated chamber containing an adsorption element, the surface of which is cooled to 11 K. and upon which is adhered a solidified layer of gas selected from the group consisting of gases whose vapor pressures are less than 10- mm. Hg, and
(b) adsorbing said hydrogen gas upon said adsorption element.
13. In a process for pumping hydrogen gas, the steps comprising (a) evacuating a vacuum chamber,
(b) cooling a thermally conducting surface within said chamber,
(0) introducing an amount of substrate gas into said chamber such that the gas solidifies on the thermally conducting surface, and
(d) adsorbing the hydrogen gas to be pumped on said solidified substrate.
14. In a process for pumping hydrogen gas, the steps comprising (a) evacuating a vacuum chamber to a low pressure of approximately 10' mm. Hg, ([2) cooling a thermally conducting surface Within said chamber to a temperature of approximately 11 K.,
(c) introducing an amount of substrate gas selected from the group consisting of gases whose vapor pressures are less than 10* mm. Hg at 11 K. into said chamber,
(d) solidifying said substrate gas upon the aforementioned thermally conducting surface,
(e) introducing the hydrogen gas into the aforementioned vacuum chamber, and
(f) adsorbing said hydrogen gas upon the solidified layer of substrate gas.
15. In a process for pumping hydrogen gas according to claim 14 wherein the substrate gas is selected from the group consisting of A, N H O, N 0, CO
16. In a cyclic process for pumping hydrogen gas, the steps comprising (a) evacuating a vacuum chamber to a low pressure of the order of mm. Hg,
(b) cooling a thermal conducting surface within said chamber to a temperature of the order of 11 K.,
(c) introducing an amount of substrate gas selected (d) solidification of said substrate gas on the aforementioned thermally conducting surface,
(e) introducing the hydrogen gas into the aforementioned vacuum chamber,
(f) adsorbing said hydrogen gas upon the solidified layer of substrate gas,
(g) heating said thermally conducting surface within said chamber to approximately 15 K.,
(h) desorbing said pumped hydrogen gas from said solidified layer of substrate gas,
(i) removing said desorbed hydrogen gas by conventional pump means from said vacuum chamber, and
(j) recooling said thermally conducting surface to approximately 11 K.
17. In a process for adsorbing hydrogen gas, the steps comprising:
(a) evacuating a vacuum chamber to a low pressure of approximately 10- mm. Hg,
(b) cooling a thermally conducting surface within said chamber to a temperature of approximately 11 K.,
(c) introducing an amount of substrate gas of the class of gases having a vapor pressure less than 10- mm. Hg at approximately 11 K. into said vacuum chamber to solidify upon said thermally conducting surface, and
(d) exposing said solidified substrate gas to the hydrogen gas which is to be adsorbed, thereby adsorbing said hydrogen gas.
References Cited in the file of this patent UNITED STATES PATENTS 2,985,356 Beecher May 23, 1961

Claims (1)

1. IN A CRYOGENIC ADSORPTION PUMP OF THE CLASS DESCRIBED HEREIN, GAS ADSORPTION MEANS DISPOSED IN AN EVACUATED CHAMBER AND COMPRISING (A) A SURFACE COOLED TO A TEMPERATURE OF APPROXIMATELY 11*5., AND (B) A SOLIDIFIED LAYER OF GAS HAVING A VAPOR PRESSURE AT APPROXIMATELY 11*K. LESS THAN THE PRESSURE OF SAID EVACUATED CHAMBER, SAID SOLIDIFIED LAYER BEING ADHERED TO SAID SURFACE.
US231311A 1962-10-17 1962-10-17 Process and device for cryogenic adsorption pumping Expired - Lifetime US3144200A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US231311A US3144200A (en) 1962-10-17 1962-10-17 Process and device for cryogenic adsorption pumping

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US231311A US3144200A (en) 1962-10-17 1962-10-17 Process and device for cryogenic adsorption pumping

Publications (1)

Publication Number Publication Date
US3144200A true US3144200A (en) 1964-08-11

Family

ID=22868694

Family Applications (1)

Application Number Title Priority Date Filing Date
US231311A Expired - Lifetime US3144200A (en) 1962-10-17 1962-10-17 Process and device for cryogenic adsorption pumping

Country Status (1)

Country Link
US (1) US3144200A (en)

Cited By (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3263434A (en) * 1964-04-17 1966-08-02 Bendix Balzers Vacuum Inc High vacuum cryopumps
US3377495A (en) * 1965-06-17 1968-04-09 Varian Associates Glow discharge apparatus having a stacked array of magnets
US3396548A (en) * 1965-09-08 1968-08-13 Philips Corp Vacuum device
US3485054A (en) * 1966-10-27 1969-12-23 Cryogenic Technology Inc Rapid pump-down vacuum chambers incorporating cryopumps
US3502259A (en) * 1968-02-14 1970-03-24 Aero Vac Corp Stabilized ion-pumping system
US3662522A (en) * 1969-07-24 1972-05-16 Getters Spa Getter pump cartridge
US3791158A (en) * 1972-08-23 1974-02-12 Us Air Force Cryosorption pumping with frost sorbents
US4275566A (en) * 1980-04-01 1981-06-30 Pennwalt Corporation Cryopump apparatus
US4341079A (en) * 1980-04-01 1982-07-27 Cvi Incorporated Cryopump apparatus
USRE31665E (en) * 1980-04-01 1984-09-11 Cvi Incorporated Cryopump apparatus
US4474036A (en) * 1982-02-24 1984-10-02 U.S. Philips Corporation Infra-red radiation detectors
US4510760A (en) * 1984-03-02 1985-04-16 Messer Griesheim Industries, Inc. Compact integrated gas phase separator and subcooler and process
US4641499A (en) * 1985-02-14 1987-02-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Ten degree Kelvin hydride refrigerator
US4724677A (en) * 1986-10-09 1988-02-16 Foster Christopher A Continuous cryopump with a device for regenerating the cryosurface
US4785638A (en) * 1986-08-06 1988-11-22 SGS-Thompson Microelectronics S.p.A. Refrigerant fluid trap for vacuum evaporators for the deposit of thin metal films
EP0339047A4 (en) * 1986-12-29 1989-10-11 David A Hill Thermal cycle recirculating pump for isotope purifier.
US4976111A (en) * 1988-01-08 1990-12-11 Larin Marxen P Cryogenic condensation pump
US5079925A (en) * 1990-04-10 1992-01-14 Union Cagbide Canada Limited Cryogenic apparatus
US5123250A (en) * 1990-04-10 1992-06-23 Union Carbide Canada Limited Cryogenic apparatus
US5142874A (en) * 1990-04-10 1992-09-01 Union Carbide Canada Limited Cryogenic apparatus
US5303558A (en) * 1992-07-30 1994-04-19 Vlsi Technology, Inc. Thermal trap for gaseous materials
WO1996011739A1 (en) * 1994-10-13 1996-04-25 Advanced Technology Materials, Inc. Storage and delivery system for gaseous compounds
US5676735A (en) * 1996-10-31 1997-10-14 Advanced Technology Materials, Inc. Reclaiming system for gas recovery from decommissioned gas storage and dispensing vessels and recycle of recovered gas
US5704967A (en) * 1995-10-13 1998-01-06 Advanced Technology Materials, Inc. Fluid storage and delivery system comprising high work capacity physical sorbent
US5707424A (en) * 1994-10-13 1998-01-13 Advanced Technology Materials, Inc. Process system with integrated gas storage and delivery unit
US5851270A (en) * 1997-05-20 1998-12-22 Advanced Technology Materials, Inc. Low pressure gas source and dispensing apparatus with enhanced diffusive/extractive means
US5916245A (en) * 1996-05-20 1999-06-29 Advanced Technology Materials, Inc. High capacity gas storage and dispensing system
US5980608A (en) * 1998-01-07 1999-11-09 Advanced Technology Materials, Inc. Throughflow gas storage and dispensing system
US5985008A (en) * 1997-05-20 1999-11-16 Advanced Technology Materials, Inc. Sorbent-based fluid storage and dispensing system with high efficiency sorbent medium
US6019823A (en) * 1997-05-16 2000-02-01 Advanced Technology Materials, Inc. Sorbent-based fluid storage and dispensing vessel with replaceable sorbent cartridge members
US6027547A (en) * 1997-05-16 2000-02-22 Advanced Technology Materials, Inc. Fluid storage and dispensing vessel with modified high surface area solid as fluid storage medium
US6070576A (en) * 1998-06-02 2000-06-06 Advanced Technology Materials, Inc. Adsorbent-based storage and dispensing system
US6083298A (en) * 1994-10-13 2000-07-04 Advanced Technology Materials, Inc. Process for fabricating a sorbent-based gas storage and dispensing system, utilizing sorbent material pretreatment
US6132492A (en) * 1994-10-13 2000-10-17 Advanced Technology Materials, Inc. Sorbent-based gas storage and delivery system for dispensing of high-purity gas, and apparatus and process for manufacturing semiconductor devices, products and precursor structures utilizing same
US6204180B1 (en) 1997-05-16 2001-03-20 Advanced Technology Materials, Inc. Apparatus and process for manufacturing semiconductor devices, products and precursor structures utilizing sorbent-based fluid storage and dispensing system for reagent delivery
US6406519B1 (en) * 1998-03-27 2002-06-18 Advanced Technology Materials, Inc. Gas cabinet assembly comprising sorbent-based gas storage and delivery system
US6660063B2 (en) 1998-03-27 2003-12-09 Advanced Technology Materials, Inc Sorbent-based gas storage and delivery system
US20040118286A1 (en) * 2002-12-09 2004-06-24 Dennis Brestovansky Rectangular parallelepiped fluid storage and dispensing vessel
US20050188846A1 (en) * 2002-12-10 2005-09-01 Carruthers J. D. Gas storage and dispensing system with monolithic carbon adsorbent
US20060011064A1 (en) * 2002-12-10 2006-01-19 Carruthers J D Gas storage and dispensing system with monolithic carbon adsorbent
US20090272272A1 (en) * 2002-10-31 2009-11-05 Advanced Technology Materials, Inc. Semiconductor manufacturing facility utilizing exhaust recirculation
US8002880B2 (en) 2002-12-10 2011-08-23 Advanced Technology Materials, Inc. Gas storage and dispensing system with monolithic carbon adsorbent
US8679231B2 (en) 2011-01-19 2014-03-25 Advanced Technology Materials, Inc. PVDF pyrolyzate adsorbent and gas storage and dispensing system utilizing same
US9126139B2 (en) 2012-05-29 2015-09-08 Entegris, Inc. Carbon adsorbent for hydrogen sulfide removal from gases containing same, and regeneration of adsorbent

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2985356A (en) * 1958-12-04 1961-05-23 Nat Res Corp Pumping device

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2985356A (en) * 1958-12-04 1961-05-23 Nat Res Corp Pumping device

Cited By (65)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3263434A (en) * 1964-04-17 1966-08-02 Bendix Balzers Vacuum Inc High vacuum cryopumps
US3377495A (en) * 1965-06-17 1968-04-09 Varian Associates Glow discharge apparatus having a stacked array of magnets
US3396548A (en) * 1965-09-08 1968-08-13 Philips Corp Vacuum device
US3485054A (en) * 1966-10-27 1969-12-23 Cryogenic Technology Inc Rapid pump-down vacuum chambers incorporating cryopumps
US3502259A (en) * 1968-02-14 1970-03-24 Aero Vac Corp Stabilized ion-pumping system
US3662522A (en) * 1969-07-24 1972-05-16 Getters Spa Getter pump cartridge
US3791158A (en) * 1972-08-23 1974-02-12 Us Air Force Cryosorption pumping with frost sorbents
US4341079A (en) * 1980-04-01 1982-07-27 Cvi Incorporated Cryopump apparatus
US4275566A (en) * 1980-04-01 1981-06-30 Pennwalt Corporation Cryopump apparatus
USRE31665E (en) * 1980-04-01 1984-09-11 Cvi Incorporated Cryopump apparatus
US4474036A (en) * 1982-02-24 1984-10-02 U.S. Philips Corporation Infra-red radiation detectors
US4510760A (en) * 1984-03-02 1985-04-16 Messer Griesheim Industries, Inc. Compact integrated gas phase separator and subcooler and process
US4641499A (en) * 1985-02-14 1987-02-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Ten degree Kelvin hydride refrigerator
US4785638A (en) * 1986-08-06 1988-11-22 SGS-Thompson Microelectronics S.p.A. Refrigerant fluid trap for vacuum evaporators for the deposit of thin metal films
US4724677A (en) * 1986-10-09 1988-02-16 Foster Christopher A Continuous cryopump with a device for regenerating the cryosurface
EP0339047A4 (en) * 1986-12-29 1989-10-11 David A Hill Thermal cycle recirculating pump for isotope purifier.
EP0339047A1 (en) * 1986-12-29 1989-11-02 David A Hill Thermal cycle recirculating pump for isotope purifier.
US4976111A (en) * 1988-01-08 1990-12-11 Larin Marxen P Cryogenic condensation pump
US5079925A (en) * 1990-04-10 1992-01-14 Union Cagbide Canada Limited Cryogenic apparatus
US5123250A (en) * 1990-04-10 1992-06-23 Union Carbide Canada Limited Cryogenic apparatus
US5142874A (en) * 1990-04-10 1992-09-01 Union Carbide Canada Limited Cryogenic apparatus
US5303558A (en) * 1992-07-30 1994-04-19 Vlsi Technology, Inc. Thermal trap for gaseous materials
US5707424A (en) * 1994-10-13 1998-01-13 Advanced Technology Materials, Inc. Process system with integrated gas storage and delivery unit
US5935305A (en) * 1994-10-13 1999-08-10 Advanced Technology Materials, Inc. Storage and delivery system for gaseous compounds
US6125131A (en) * 1994-10-13 2000-09-26 Advanced Technology Materials, Inc. Laser system utilizing sorbent-based gas storage and delivery system
US5704965A (en) * 1994-10-13 1998-01-06 Advanced Technology Materials, Inc. Fluid storage and delivery system utilizing carbon sorbent medium
US5518528A (en) * 1994-10-13 1996-05-21 Advanced Technology Materials, Inc. Storage and delivery system for gaseous hydride, halide, and organometallic group V compounds
WO1996011739A1 (en) * 1994-10-13 1996-04-25 Advanced Technology Materials, Inc. Storage and delivery system for gaseous compounds
US6083298A (en) * 1994-10-13 2000-07-04 Advanced Technology Materials, Inc. Process for fabricating a sorbent-based gas storage and dispensing system, utilizing sorbent material pretreatment
US6132492A (en) * 1994-10-13 2000-10-17 Advanced Technology Materials, Inc. Sorbent-based gas storage and delivery system for dispensing of high-purity gas, and apparatus and process for manufacturing semiconductor devices, products and precursor structures utilizing same
US5704967A (en) * 1995-10-13 1998-01-06 Advanced Technology Materials, Inc. Fluid storage and delivery system comprising high work capacity physical sorbent
US5916245A (en) * 1996-05-20 1999-06-29 Advanced Technology Materials, Inc. High capacity gas storage and dispensing system
US5676735A (en) * 1996-10-31 1997-10-14 Advanced Technology Materials, Inc. Reclaiming system for gas recovery from decommissioned gas storage and dispensing vessels and recycle of recovered gas
US6204180B1 (en) 1997-05-16 2001-03-20 Advanced Technology Materials, Inc. Apparatus and process for manufacturing semiconductor devices, products and precursor structures utilizing sorbent-based fluid storage and dispensing system for reagent delivery
US6019823A (en) * 1997-05-16 2000-02-01 Advanced Technology Materials, Inc. Sorbent-based fluid storage and dispensing vessel with replaceable sorbent cartridge members
US6027547A (en) * 1997-05-16 2000-02-22 Advanced Technology Materials, Inc. Fluid storage and dispensing vessel with modified high surface area solid as fluid storage medium
US5985008A (en) * 1997-05-20 1999-11-16 Advanced Technology Materials, Inc. Sorbent-based fluid storage and dispensing system with high efficiency sorbent medium
US5851270A (en) * 1997-05-20 1998-12-22 Advanced Technology Materials, Inc. Low pressure gas source and dispensing apparatus with enhanced diffusive/extractive means
US5980608A (en) * 1998-01-07 1999-11-09 Advanced Technology Materials, Inc. Throughflow gas storage and dispensing system
US6406519B1 (en) * 1998-03-27 2002-06-18 Advanced Technology Materials, Inc. Gas cabinet assembly comprising sorbent-based gas storage and delivery system
US6540819B2 (en) * 1998-03-27 2003-04-01 Advanced Technology Materials, Inc. Gas cabinet assembly comprising sorbent-based gas storage and delivery system
US6660063B2 (en) 1998-03-27 2003-12-09 Advanced Technology Materials, Inc Sorbent-based gas storage and delivery system
US6070576A (en) * 1998-06-02 2000-06-06 Advanced Technology Materials, Inc. Adsorbent-based storage and dispensing system
US20090272272A1 (en) * 2002-10-31 2009-11-05 Advanced Technology Materials, Inc. Semiconductor manufacturing facility utilizing exhaust recirculation
US7857880B2 (en) 2002-10-31 2010-12-28 Advanced Technology Materials, Inc. Semiconductor manufacturing facility utilizing exhaust recirculation
US9636626B2 (en) 2002-12-09 2017-05-02 Entegris, Inc. Rectangular parallelepiped fluid storage and dispensing vessel
US6991671B2 (en) 2002-12-09 2006-01-31 Advanced Technology Materials, Inc. Rectangular parallelepiped fluid storage and dispensing vessel
US20060054018A1 (en) * 2002-12-09 2006-03-16 Dennis Brestovansky Rectangular parallelepiped fluid storage and dispensing vessel
US9062829B2 (en) 2002-12-09 2015-06-23 Entegris, Inc. Rectangular parallelepiped fluid storage and dispensing vessel
US8506689B2 (en) 2002-12-09 2013-08-13 Advanced Technology Mateials, Inc. Rectangular parallelepiped fluid storage and dispensing vessel
US7501010B2 (en) 2002-12-09 2009-03-10 Advanced Technology Materials, Inc. Rectangular parallelepiped fluid storage and dispending vessel
US7972421B2 (en) 2002-12-09 2011-07-05 Advanced Technology Materials, Inc. Rectangular parallelepiped fluid storage and dispensing vessel
US20040118286A1 (en) * 2002-12-09 2004-06-24 Dennis Brestovansky Rectangular parallelepiped fluid storage and dispensing vessel
US20050188846A1 (en) * 2002-12-10 2005-09-01 Carruthers J. D. Gas storage and dispensing system with monolithic carbon adsorbent
US8002880B2 (en) 2002-12-10 2011-08-23 Advanced Technology Materials, Inc. Gas storage and dispensing system with monolithic carbon adsorbent
US8282714B2 (en) 2002-12-10 2012-10-09 Advanced Technology Materials, Inc. Gas storage and dispensing system with monolithic carbon adsorbent
US7494530B2 (en) 2002-12-10 2009-02-24 Advanced Technology Materials, Inc. Gas storage and dispensing system with monolithic carbon adsorbent
US8858685B2 (en) 2002-12-10 2014-10-14 Advanced Technology Materials, Inc. Gas storage and dispensing system with monolithic carbon adsorbent
US7455719B2 (en) 2002-12-10 2008-11-25 Advanced Technology Materials, Inc. Gas storage and dispensing system with monolithic carbon adsorbent
US9518701B2 (en) 2002-12-10 2016-12-13 Entegris, Inc. Gas storage and dispensing system with monolithic carbon adsorbent
US20060011064A1 (en) * 2002-12-10 2006-01-19 Carruthers J D Gas storage and dispensing system with monolithic carbon adsorbent
US8679231B2 (en) 2011-01-19 2014-03-25 Advanced Technology Materials, Inc. PVDF pyrolyzate adsorbent and gas storage and dispensing system utilizing same
US9234628B2 (en) 2011-01-19 2016-01-12 Entegris, Inc. PVDF pyrolyzate adsorbent and gas storage and dispensing system utilizing same
US9468901B2 (en) 2011-01-19 2016-10-18 Entegris, Inc. PVDF pyrolyzate adsorbent and gas storage and dispensing system utilizing same
US9126139B2 (en) 2012-05-29 2015-09-08 Entegris, Inc. Carbon adsorbent for hydrogen sulfide removal from gases containing same, and regeneration of adsorbent

Similar Documents

Publication Publication Date Title
US3144200A (en) Process and device for cryogenic adsorption pumping
US3485054A (en) Rapid pump-down vacuum chambers incorporating cryopumps
US3137551A (en) Ultra high vacuum device
US3668881A (en) Adsorptive cryopumping method and apparatus
US3364654A (en) Ultrahigh vacuum pumping process and apparatus
US3992893A (en) Method for the production of superfluid helium under pressure at very low temperature and an apparatus for carrying out said method
Selzer et al. A superfluid plug for space
Benvenuti Characteristics, advantages, and possible applications of condensation cryopumping
US5014517A (en) Cryogenic sorption pump
US3525229A (en) On-off thermal switch for a cryopump
US3811794A (en) Ultrahigh vacuum sublimation pump
US3119243A (en) Vacuum device
Baechler Cryopumps for research and industry
CN110073135B (en) Method and device for establishing vacuum insulation under low temperature condition
US4716742A (en) Cryogenic system for radiation detectors
US3237419A (en) Method and device for attaining very low pressure
US4009585A (en) Method of producing vacuum in recipient and vacuum pump for effecting same
US3140820A (en) Method for maintaining very high vacuum in a system
JPH1047245A (en) Evacuating device
US3512369A (en) Ultrahigh-vacuum enclosure
JPS6314858A (en) Vacuum deposition device
US3126902A (en) Method and apparatus for producing high vacuum
SU781486A1 (en) Method of producing vacuum for heat insulation of "tube-in-tube"-type pipelines
Strang et al. Cryogenic pumping gas target system
JP3019471B2 (en) Cryopump