US3232031A - Diffusion pump cold trap - Google Patents

Diffusion pump cold trap Download PDF

Info

Publication number
US3232031A
US3232031A US219999A US21999962A US3232031A US 3232031 A US3232031 A US 3232031A US 219999 A US219999 A US 219999A US 21999962 A US21999962 A US 21999962A US 3232031 A US3232031 A US 3232031A
Authority
US
United States
Prior art keywords
chevron
annular
baffle
cold trap
disk
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
US219999A
Inventor
Jr John C Simons
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.)
National Research Corp
Original Assignee
Nat Res Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nat Res Corp filed Critical Nat Res Corp
Priority to US219999A priority Critical patent/US3232031A/en
Application granted granted Critical
Publication of US3232031A publication Critical patent/US3232031A/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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F9/00Diffusion pumps
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S55/00Gas separation
    • Y10S55/15Cold traps

Definitions

  • High vacuum lO to torr (mm. Hg abs). Very high vacuum 10 to 10- torr. Ultra high vacuum 10 torr audbelow.
  • the invention accordingly comprises the apparatus possessing the construction, combination of elements and arrangement of parts which are exemplified in the following detailed disclosure and the scope of the application of which will be indicated in the claims. d
  • FIG. 1 is a diagrammatic, schematic view of a preferred embodiment of the invention.
  • FIG. 2 is a partial section of a-detail ofthe apparatus indicated in FIG. 1. i
  • FIG. 1 there is shown a diffusion pump 10 with a vapor jet assembly 12 emitting streams of vapor, as indicated at 14, against the water-cooled wall 16 of the pump.
  • the vapor jet assembly is provided with a cold cap 18, in accordance with the teaching of the Power Patent 2,919,061, granted December 29, 1959.
  • This cold cap by eliminating the over-divergent portion of the vapor jet 14, cuts backstreaming by approximately 98%. Residual backstreaming and oil transport is completely eliminated by the novel cold trap described below.
  • the cold trap 30 comprises an oblate shell 32 for containing a cryogenic fluid such as liquid nitrogen and feed and return lines therefor, one of which is indicated at 33.
  • the oblate shell is surrounded by annular chevrons 34 and 36 which are connected to the shell by a plurality of ribs 33, selected for their high thermal conductivity.
  • the annular gap between the outermost chevron 36 and the wall 40 is bridged by an annular ring assembly 42 which is connected to both members 36 and 40.
  • the connection to wall40 is a vacuum-tight weld.
  • the connection to chevron 36 is structural; there are leakage paths. However, these are optically dense and. cryogenically cooled.
  • the ring 42 is of high thermal conductivity, as described below. 1
  • the backstreaming vapors from the pump 10. are confinedto'optically dense paths defined entirely by cryogenically-cooled bafiles. Creep along the wall is blocked by bafile 42;
  • the use of the cold cap for reducing the backstreaming problem by two orders of magnitude in the first instance makes this bafile practical for long term Without the cold cap an excessive amount of backstreaming vapor would be collected by trap 30, forming thick layers of ice (solidified oil).
  • a. cold cap For instance, a water-cooled bafiie or an elbow pipe could be interposed between the pump 19 and cryogenic, baffle 30.
  • the use of the cold cap is preferred since it avoids. the penalties in bulk, cost and loss of conductance presented by these additional bafiies.
  • the ring isdivided into two portions 44 and 46. to provide for assembly and disassembly.
  • the outer portion 44 is made of steel and the inner portion 46 of oxygen-free copper, a good thermal conductor.
  • the portions are welded or brazed to the wall 49 and outermost chevron; 36, respectively andwhen assembled, they are secured by annular clamping rings 43 and which are drilled and threaded to receive bolts 52. at a plurality of symmetrically spaced locations. For example, in a nominal 10-inch trap, 24 bolts would be provided.
  • the annular clamping rings are provided to prevent slight leakage pathsldue to buckling between bolts.
  • portion 46 A minimal amount of leakage is still possible between the portions, 44 and 46. However, this is, inhibited since portion 4.6 is atscryogenic temperature.
  • portion 46 and chevron 36, a plurality of spaced tack welds 54, is open to leakage. However this leakage path is defined by two cryogenically cooled members 46 and 36. There is suificient contact between members 46 and 36 to permit heat transfer by conduction.
  • the weld at the junction of wall 40 and member 44 is an annular vacuum-tight weld 56.
  • sential feature of the instant invention is the recognition that water cooling of wall 40, alone, does not solve the problem of backstre-aming and creeping along the wall in the ultra high vacuum range. Cryogenically cooled sur- 7 faces are necessary for this purpose.
  • the cold trap can be disassembled by removing bolts 52.
  • the reassembled trap can repeat its performance in preventing any backstreaming or creeping because of the novel design described above.
  • various types of cold traps can be modified to incorporate the principles of the instant invention.
  • the cooled surfaces could consist entirely of bafiies with no central shell containing coolant.
  • the cooling could he provided by separate pipes or thermoelectric means.
  • the present invention entails a recognition of the critical areas of vapor backstreaming and the extension of cryogenic cooling to those areas rather than an indiscriminate multiplication of baffling.
  • an improved cold trap comprising a vertically extending tubular wall, a bafiie assembly of radially spaced apart concentric annular chevron bafiies including an outermost chevron bafile and innermost chevron baflie located substantially in a horizontal plane, said chevron batfies being inclined with respect to the vertical axis of the cold trap and said horizontal plane to define at least one annular gas conductance path between adjacent chevron baffles, said gas conductance path being optically dense with respect to the inlet of the diffusion pump, said bafile assembly further comprising a central hollow shell located substantially in said horizontal plane and along the axis of the trap spaced from and encompassed by said innermost
  • the disk assembly consisting of inner and outer annular disks arranged horizontally and overlapping each other with the outer disk united at all points of its outer periphery to the vertically extending wall of said trap and the inner disk united to the outermost extending bafile at all points of the inner periphery of the inner disk to define a complete annular seal at the junction of said inner disk and outermost chevron bafile, and means constructed and arranged within said cold trap for clamping said disks together at their overlapping portions so that the supporting disk assembly presents an annular impenetrable barrier so that fluid flow through the cold trap is confined to said annular gas conductance paths.

Description

Feb. 1, 1966 J. c. SIMONS, JR
DIFFUSION PUMP COLD TRAP Filed Aug. 28, 1962 ULTRA-HIGH VACUUM CHAMBER FIG.
FIG. 2
3,232,031 DIFFUSION PUMP COLD TRAP John C. Simons, .lzu, Weston, Mass, assignor, by mesne assignments, to National Research Corporation, Cambridge, Mass, a corporation of Massachusetts Filed Aug. 28, 1962, Ser. No, 219,999 3 Claims. (Cl. 55-269) The present invention relates to the production of ultra;
high vacuum, as defined in the American Vacuum Society Standards:
High vacuum lO to torr (mm. Hg abs). Very high vacuum 10 to 10- torr. Ultra high vacuum 10 torr audbelow.
limits the ultimate vacuum which] the pumpican produce.
It is therefore the object of this invention to provide a pumping system, including a diffusion pump, which is arranged to limitbackstreaming and oil creep and make ultra high vacuum operation feasible.
Other objects of the inventionwill in part be obvious and will in partappear hereinafter.
The invention accordingly comprises the apparatus possessing the construction, combination of elements and arrangement of parts which are exemplified in the following detailed disclosure and the scope of the application of which will be indicated in the claims. d
For a fuller understanding of the nature and objects of the invention, reference should be had to thefollowirig detailed description" taken in connection, with the accompanying drawings wherein:
FIG. 1 is a diagrammatic, schematic view of a preferred embodiment of the invention; and
FIG. 2 is a partial section of a-detail ofthe apparatus indicated in FIG. 1. i
The phenomenon of backstreaining is generally attributed to back scatter of vapor phase oil molecules towards the pump inlet and re-evaporation of condensed oil from the pump wall near the inlet. Creeping of oil takes place due to capillary action of liquid phase pump oil and by successive re-evaporation and condensation of pump oil. Cryogenically cooled surfaces combat all these problems since they limit re-evaporation and liquid fiow along a surface. It is well known in the art to define the path of pumped gas by cryogenically cooled surfaces in an optically dense arrangement so that oil molecules traveling from the pump to the vacuum chamber will be trapped. The present invention entails a recognition of the importance of cooling all possible leakage paths and the location of those leakage paths.
Referring now to FIG. 1, there is shown a diffusion pump 10 with a vapor jet assembly 12 emitting streams of vapor, as indicated at 14, against the water-cooled wall 16 of the pump. The vapor jet assembly is provided with a cold cap 18, in accordance with the teaching of the Power Patent 2,919,061, granted December 29, 1959. This cold cap, by eliminating the over-divergent portion of the vapor jet 14, cuts backstreaming by approximately 98%. Residual backstreaming and oil transport is completely eliminated by the novel cold trap described below.
3,232,031 Patented Feb. 1, 1966 ice The pump is provided with an inlet flange 2t and sealmg means indicated as a single ring 22. It should be understood that it will often be necessary to turn to more complex sealing means such as double O-rings, refrigerated seals, and the like, which are known in the art.
The cold trap 30 comprises an oblate shell 32 for containing a cryogenic fluid such as liquid nitrogen and feed and return lines therefor, one of which is indicated at 33. The oblate shell is surrounded by annular chevrons 34 and 36 which are connected to the shell by a plurality of ribs 33, selected for their high thermal conductivity. The annular gap between the outermost chevron 36 and the wall 40; is bridged by an annular ring assembly 42 which is connected to both members 36 and 40. The connection to wall40 is a vacuum-tight weld. The connection to chevron 36 is structural; there are leakage paths. However, these are optically dense and. cryogenically cooled. The ring 42 is of high thermal conductivity, as described below. 1
Thus, the backstreaming vapors from the pump 10. are confinedto'optically dense paths defined entirely by cryogenically-cooled bafiles. Creep along the wall is blocked by bafile 42; The use of the cold cap for reducing the backstreaming problem by two orders of magnitude in the first instance makes this bafile practical for long term Without the cold cap an excessive amount of backstreaming vapor would be collected by trap 30, forming thick layers of ice (solidified oil). It should be understood however that other techniques for achieving a rough reduction in backstreaming may be employed in lieu of a. cold cap. For instance, a water-cooled bafiie or an elbow pipe could be interposed between the pump 19 and cryogenic, baffle 30. The use of the cold cap is preferred since it avoids. the penalties in bulk, cost and loss of conductance presented by these additional bafiies.
Referring now to FIG. 2, details of the ring 42 are shown. The ring isdivided into two portions 44 and 46. to provide for assembly and disassembly. The outer portion 44 is made of steel and the inner portion 46 of oxygen-free copper, a good thermal conductor. The portions are welded or brazed to the wall 49 and outermost chevron; 36, respectively andwhen assembled, they are secured by annular clamping rings 43 and which are drilled and threaded to receive bolts 52. at a plurality of symmetrically spaced locations. For example, in a nominal 10-inch trap, 24 bolts would be provided. The annular clamping rings are provided to prevent slight leakage pathsldue to buckling between bolts. A minimal amount of leakage is still possible between the portions, 44 and 46. However, this is, inhibited since portion 4.6 is atscryogenic temperature. The structural connection between portion 46 and chevron 36, a plurality of spaced tack welds 54, is open to leakage. However this leakage path is defined by two cryogenically cooled members 46 and 36. There is suificient contact between members 46 and 36 to permit heat transfer by conduction. The weld at the junction of wall 40 and member 44 is an annular vacuum-tight weld 56.
It will be noted that the cross-section dimensions of the ring 42 are small compared to the cryogenic shell 32 of FIG. 1. Thus heat transfer from the outer wall 41) does not stnain the capacity of the cryogenic cooling system. The relatively poor thermal conductivity of outer portion 44 also limits losses. However, water cooling of the wall 40 may be provided to limit this cooling loss. An .es-
sential feature of the instant invention is the recognition that water cooling of wall 40, alone, does not solve the problem of backstre-aming and creeping along the wall in the ultra high vacuum range. Cryogenically cooled sur- 7 faces are necessary for this purpose.
The cold trap can be disassembled by removing bolts 52. The reassembled trap can repeat its performance in preventing any backstreaming or creeping because of the novel design described above. It will now be appreciated that various types of cold traps can be modified to incorporate the principles of the instant invention. For instance, the cooled surfaces could consist entirely of bafiies with no central shell containing coolant. The cooling could he provided by separate pipes or thermoelectric means.
The design considerations must also take account of loss of conductance inherent in baffling. Thus, the present invention entails a recognition of the critical areas of vapor backstreaming and the extension of cryogenic cooling to those areas rather than an indiscriminate multiplication of baffling.
Since certain changes may be made in the above apparatus without departing from the scope of the invention herein involved, it is intended that all matter contained in the above description shall be interpreted as illustrative and not in a limiting sense.
What is claimed is:
1. In an ultrahigh vacuum pumping system comprising a vertically arranged tubular diffusion pump with its inlet end connected to a vacuum chamber via a tubular cold trap coaxially aligned with and mounted over the diffusion pump in end-to-end relation therewith and means for effecting a rough reduction in backstreaming from the diffusion pump an improved cold trap comprising a vertically extending tubular wall, a bafiie assembly of radially spaced apart concentric annular chevron bafiies including an outermost chevron bafile and innermost chevron baflie located substantially in a horizontal plane, said chevron batfies being inclined with respect to the vertical axis of the cold trap and said horizontal plane to define at least one annular gas conductance path between adjacent chevron baffles, said gas conductance path being optically dense with respect to the inlet of the diffusion pump, said bafile assembly further comprising a central hollow shell located substantially in said horizontal plane and along the axis of the trap spaced from and encompassed by said innermost chevron baflle so that it is surrounded by said annular chevron bafiles, the innermost chevron baffle and shell being constructed and arranged to define therebetween an annular gas conductance path which is optically dense with respect to the inlet of the diffusion pump, rib means constructed and arranged within said trap for transferring heat by conduction between said chev-rons and said shell, means for conducting cryogenic fluid to and from the interior of said shell, the cold trap further comprising an annular supporting disk assembly physically united at all points of its periphery to and extending substantially horizontally from the tubular vertically extending wall of said cold trap to the said bafiie assembly to support the bafile assembly from the wall,
the disk assembly consisting of inner and outer annular disks arranged horizontally and overlapping each other with the outer disk united at all points of its outer periphery to the vertically extending wall of said trap and the inner disk united to the outermost extending bafile at all points of the inner periphery of the inner disk to define a complete annular seal at the junction of said inner disk and outermost chevron bafile, and means constructed and arranged within said cold trap for clamping said disks together at their overlapping portions so that the supporting disk assembly presents an annular impenetrable barrier so that fluid flow through the cold trap is confined to said annular gas conductance paths.
2. The cold trap of claim 1 wherein the inner disk rests on top of the outer disk at the overlapping portion thereof and wherein the clamping means comprises a pair of rings bearing against the overlapped disks, said rings positioned one above and one below said disks, means constructed and arranged for forcing the rings toward each other.
3. The cold trap of claim 1 wherein the disks are constructed so that the inner disk is a more efficient thermal conductor than the outer disk.
References Cited by the Examiner UNITED STATES PATENTS 2,112,037 3/1938 Malter 23010l 2,125,910 8/ 1938 Gardner. 2,193,135 3/1940 Lamm 230--101 2,386,298 10/1945 Downing et a1. 230-101 2,397,591 4/1946 Becker 230101 2,703,673 3/1955 Winkler 230101 2,919,061 12/1959 Power 230l01 3,024,625 3/1962 Fraunhufer et a1. 230-101 X 3,075,689 l/1963 Stevenson 230l01 3,081,068 3/1963 Milleron --269 X 3,119,243 1/ 1964 Hnilicka et a1. 3,137,551 6/1964 Mark 55444 X FOREIGN PATENTS 1,028,734 4/ 1958 Germany. 1,037,644 8/ 8 Germany. 1,074,208 1/ 1960 Germany.
773,456 4/ 1957 Great Britain.
795,895 6/1958 Great Britain.
888,249 1/ 1962 Great Britain.
OTHER REFERENCES Ullman, Ralph L: A Large Metal System Permitting Low Base Pressures, University of California, Radiation Laboratory, Livermore Site, Livermore, California, Document No. UCRL-4972, October 4, 1957, 7 pages.
REUBEN FRIEDMAN, Primary Examiner.

Claims (1)

1. IN AN ULTRAHIGH VACUUM PUMPING SYSTEM COMPRISING A VERTICALLY ARRANGED TUBULAR DIFFUSION PUMP WITH ITS INLET END CONNECTED TO A VACUUM CHAMBER VIA A TUBULAR COLD TRAP COAXIALLY ALIGNED WITH AND MOUNTED OVER THE DIF FUSION PUMP IN END-TO-END RELATION HEREWITH AND MEANS FOR EFFECTING A ROUGH REDUCTION IN BACKSTEAMING FROM THE DIFFUSION PUMP AN IMPROVED COLD TRAP COMPRISING A VERTICALLY EXTENDING TUBULAR WALL, A BAFFLE ASSEMBLY OF RADIALLY SPACED APART CONCENTRIC ANNULAR CHEVRON BAFFLES INCLUDING AN OUTERMOST CHEVRON BAFFLE AND INNERMOST CHEVRON BAFFLE LOCATED SUBSTANTIALLY IN A HORIZONTAL PLANE, SAID CHEVRON BAFFLES BEING INCLINED WITH RESPECT TO THE VERTICAL AXIS OF THE COLD TRAP AND SAID HORIZONTAL PLANE TO DEFINE AT LEAST ONE ANNULAR GAS CONDUCTANCE PATH BETWEEN ADJACENT CHEVRON BAFFLES, SAID GAS CONDUCTANCE PATH BEING OPTICALLY DENSE WITH RESPECT TO THE INLET OF THE DIFFUSION PUMP, SAID BAFFLE ASSEMBLY FURTHER COMPRISING A CENTRAL HOLLOW SHELL LOCATED SUBSTANTIALLY IN SAID HORIZONTAL PLANE AND ALONG THE AXIS OF THE TRAP SPACED FROM AND ENCOMPASSED BY SAID INNERMOST CHEVRON BAFFLE SO THAT IT IS SURROUNDED BY SAID ANNULAR CHEVRON BAFFLES, THE INNERMOST CHEVRON BAFFLE AND SHELL BEING CONSTRUCTED AND ARRANGED TO DEFINE THEREBETWEEN AN ANNULAR GAS CONDUCTANCE PATH WHICH IS OPTICALLY DENSE WITH RESPECT TO THE INLET OF THE DIFFUSION PUMP, RIB MEANS CONSTRUCTED AND ARRANGED WITHIN SAID TRAP FOR TRANSFERRING HEAT BY CONDUCTION BETWEEN SAID CHEVRONS AND SAID SHELL, MEANS FOR CONDUCTING CRYOGENIC FLUID TO AND FROM THE INTERIOR OF SAID SHELL, THE COLD TRAP FURTHER COMPRISING AN ANNULAR SUPPORTING DISK ASSEMBLY PHYSICALLY UNITED AT ALL POINTS OF ITS PERIPHERY TO AND EXTENDING SUBSTANTIALLY HORIZONTALLY FROM THE TUBULAR VERTICALLY EXTENDING WALL OF SAID COLD TRAP TO THE SAID BAFFLE ASSEMBLY TO SUPPORT THE BAFFLE ASSEMBLY FROM THE WALL, THE DISK ASSEMBLY CONSISTING OF INNER AND OUTER ANNULAR DISK ARRANGED HORIZONTALLY AND OVERLAPPING EACH OTHER WITH THE OUTER DISK UNITED AT ALL POINTS OF ITS OUTER PERIPHERY TO THE VERTICALLY EXTENDING WALL OF SAID TRAP AND THE INNER DISK UNITED TO THE OUTERMOST EXTENDING BAFFLE AT ALL POINTS OF THE INNER PERIPHERY OF THE INNER DISK TO DEFINE A COMPLETE ANNULAR SEAL AT THE JUNCTION OF SAID INNER DISK AND OUTERMOST CHEVRON BAFFLE, AND MEANS CONSTRUCTED AND ARRANGED WITHIN SAID COLD TRAP FOR CLAMPING SAID DISK TOGETHER AT THEIR OVERLAPPING PORTIONS SO THAT THE SUPPORTING DISK ASSEMBLY PRESENT AN ANNULAR IMPENETRABLE BARRIER SO THAT FLUID FLOW THROUGH THE COLD TRAP IS CONFINED TO SAID ANNULAR GAS CONDUCTANCE PATHS.
US219999A 1962-08-28 1962-08-28 Diffusion pump cold trap Expired - Lifetime US3232031A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US219999A US3232031A (en) 1962-08-28 1962-08-28 Diffusion pump cold trap

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US219999A US3232031A (en) 1962-08-28 1962-08-28 Diffusion pump cold trap

Publications (1)

Publication Number Publication Date
US3232031A true US3232031A (en) 1966-02-01

Family

ID=22821623

Family Applications (1)

Application Number Title Priority Date Filing Date
US219999A Expired - Lifetime US3232031A (en) 1962-08-28 1962-08-28 Diffusion pump cold trap

Country Status (1)

Country Link
US (1) US3232031A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304731A (en) * 1964-03-13 1967-02-21 Granville Phillips Company High vacuum cold trap
US3410100A (en) * 1965-03-18 1968-11-12 Commerce Usa High-vacuum baffle using cooled, chevron-shaped members
US5537833A (en) * 1995-05-02 1996-07-23 Helix Technology Corporation Shielded cryogenic trap

Citations (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2112037A (en) * 1937-03-27 1938-03-22 Rca Corp Vacuum diffusion pump
US2125910A (en) * 1936-08-18 1938-08-09 Farnsworth Television Inc Vacuum valve
US2193135A (en) * 1938-01-22 1940-03-12 Asea Ab High vacuum vapor jet pump
US2386298A (en) * 1943-01-30 1945-10-09 Nat Res Corp Diffusion pump
US2397591A (en) * 1943-05-29 1946-04-02 Eitel Mccullough Inc Vacuum pump
US2703673A (en) * 1950-04-08 1955-03-08 Alois Vogt Vacuum pump
GB773456A (en) * 1954-04-29 1957-04-24 Philips Electrical Ind Ltd Improvements in or relating to vapour traps for use with diffusion pumps
DE1028734B (en) * 1957-02-09 1958-04-24 Leybolds Nachfolger E Device for preventing steam from flowing into high vacuum rooms
GB795895A (en) * 1956-01-25 1958-06-04 Edwards High Vacuum Company Improvements in or relating to vapour vacuum pumps
DE1037644B (en) * 1954-06-23 1958-08-28 Siemens Ag Vapor barrier for vacuum systems
US2919061A (en) * 1954-08-31 1959-12-29 Edwards High Vacuum Ltd Vapour vacuum pumps
DE1074208B (en) * 1960-01-28 TESLA närodni podnik, Prag-Hloubetin Vacuum gate valve with high pumping speed for oil diffusion pumps
GB888249A (en) * 1959-11-18 1962-01-31 Thomson Houston Comp Francaise Improvements relating to diffusion pumps
US3024625A (en) * 1956-06-08 1962-03-13 Jenaer Glaswerk Schott & Gen Cooling device for vacuum apparatus
US3075689A (en) * 1961-11-20 1963-01-29 Cons Vacuum Corp Vacuum pump
US3081068A (en) * 1959-10-16 1963-03-12 Milleron Norman Cold trap
US3119243A (en) * 1962-04-04 1964-01-28 Nat Res Corp Vacuum device
US3137551A (en) * 1959-10-02 1964-06-16 John T Mark Ultra high vacuum device

Patent Citations (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1074208B (en) * 1960-01-28 TESLA närodni podnik, Prag-Hloubetin Vacuum gate valve with high pumping speed for oil diffusion pumps
US2125910A (en) * 1936-08-18 1938-08-09 Farnsworth Television Inc Vacuum valve
US2112037A (en) * 1937-03-27 1938-03-22 Rca Corp Vacuum diffusion pump
US2193135A (en) * 1938-01-22 1940-03-12 Asea Ab High vacuum vapor jet pump
US2386298A (en) * 1943-01-30 1945-10-09 Nat Res Corp Diffusion pump
US2397591A (en) * 1943-05-29 1946-04-02 Eitel Mccullough Inc Vacuum pump
US2703673A (en) * 1950-04-08 1955-03-08 Alois Vogt Vacuum pump
GB773456A (en) * 1954-04-29 1957-04-24 Philips Electrical Ind Ltd Improvements in or relating to vapour traps for use with diffusion pumps
DE1037644B (en) * 1954-06-23 1958-08-28 Siemens Ag Vapor barrier for vacuum systems
US2919061A (en) * 1954-08-31 1959-12-29 Edwards High Vacuum Ltd Vapour vacuum pumps
GB795895A (en) * 1956-01-25 1958-06-04 Edwards High Vacuum Company Improvements in or relating to vapour vacuum pumps
US3024625A (en) * 1956-06-08 1962-03-13 Jenaer Glaswerk Schott & Gen Cooling device for vacuum apparatus
DE1028734B (en) * 1957-02-09 1958-04-24 Leybolds Nachfolger E Device for preventing steam from flowing into high vacuum rooms
US3137551A (en) * 1959-10-02 1964-06-16 John T Mark Ultra high vacuum device
US3081068A (en) * 1959-10-16 1963-03-12 Milleron Norman Cold trap
GB888249A (en) * 1959-11-18 1962-01-31 Thomson Houston Comp Francaise Improvements relating to diffusion pumps
US3075689A (en) * 1961-11-20 1963-01-29 Cons Vacuum Corp Vacuum pump
US3119243A (en) * 1962-04-04 1964-01-28 Nat Res Corp Vacuum device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3304731A (en) * 1964-03-13 1967-02-21 Granville Phillips Company High vacuum cold trap
US3410100A (en) * 1965-03-18 1968-11-12 Commerce Usa High-vacuum baffle using cooled, chevron-shaped members
US5537833A (en) * 1995-05-02 1996-07-23 Helix Technology Corporation Shielded cryogenic trap

Similar Documents

Publication Publication Date Title
US3137551A (en) Ultra high vacuum device
US3579998A (en) Cryogenic pumping device for the creation of very high vacua
US3068026A (en) Cryogenic fluid transfer line coupling
US3081068A (en) Cold trap
US4394344A (en) Heat pipes for use in a magnetic field
US3168819A (en) Vacuum system
EP0079960A1 (en) Improved cryopump.
US3579997A (en) Cryopumping installations with high flow-rates
US3122896A (en) Pump heat radiation shield
US4072025A (en) Regeneration-type cryopump
US5033756A (en) Wide temperature range seal for demountable joints
US3712074A (en) Cryogenic gas trap
US3232031A (en) Diffusion pump cold trap
US5537833A (en) Shielded cryogenic trap
US3572426A (en) Underwater heat exchange system
US3188785A (en) Vacuum cold trap
US3321927A (en) Spiral liquid cooled baffle for shielding diffusion pumps
US3129077A (en) Gas purifying apparatus
US3034319A (en) High-efficiency fluid transfer line coupling
US3119243A (en) Vacuum device
US3124443A (en) Gas fractionating system
US3194591A (en) Tube penetration for cryogenic shield
US4607491A (en) Cooling trap for vacuum
Mukherjee et al. Design and development of LN2 cooled cryopump for application in high heat flux test facility
RU2807139C1 (en) Cryogenic pipeline