US3279214A - Pump - Google Patents

Pump Download PDF

Info

Publication number
US3279214A
US3279214A US39655664A US3279214A US 3279214 A US3279214 A US 3279214A US 39655664 A US39655664 A US 39655664A US 3279214 A US3279214 A US 3279214A
Authority
US
United States
Prior art keywords
header
tubing
coolant
cryopump
hollow
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
Inventor
Klipping Gustav
Mascher Werner
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.)
Max Planck Gesellschaft zur Foerderung der Wissenschaften eV
Original Assignee
Max Planck Gesellschaft zur Foerderung der Wissenschaften eV
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 Max Planck Gesellschaft zur Foerderung der Wissenschaften eV filed Critical Max Planck Gesellschaft zur Foerderung der Wissenschaften eV
Priority to DE1965M0077476 priority Critical patent/DE1300624B/en
Application granted granted Critical
Publication of US3279214A publication Critical patent/US3279214A/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
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C3/00Vessels not under pressure
    • F17C3/02Vessels not under pressure with provision for thermal insulation
    • F17C3/08Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
    • F17C3/085Cryostats
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/02Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using Joule-Thompson effect; using vortex effect
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0128Shape spherical or elliptical
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/0602Wall structures; Special features thereof
    • F17C2203/0612Wall structures
    • F17C2203/0626Multiple walls
    • F17C2203/0629Two walls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/04Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by other properties of handled fluid before transfer
    • F17C2223/042Localisation of the removal point
    • F17C2223/046Localisation of the removal point in the liquid
    • F17C2223/047Localisation of the removal point in the liquid with a dip tube

Definitions

  • the present invention relates to a device for producing a vacuum with the aid of a condensing element which is cooled to very low temperatures.
  • So-cal-led cryopumps are used in the art of vacuum engineering whenever high-speed suction is needed. If such high-speed suction is to remove hydrogen, the condensing elements have to be kept at temperatures below 42 K., this being the 4boiling point of liquid helium.
  • cryopumps have been used only for evacuating large receptacles, e.g., wind tunnels, and only for removing nitrogen or gases having higher boiling points.
  • Conventional cryopumps are connected directly with a refrigeration unit, and the condensing surfaces, which are usually :surrounded by a radiation protector cooled ⁇ by nitrogen, are cooled by means of cold helium gas which tlows under the inuence of pressure greater than atmospheric. This produces operating temperatures which are substantially above the boiling point of helium, namely, approximately l2 to 14 K.
  • cryopumps for evacuating hydrogen, because no existing cryopump has been known to operate at sufficiently low temperatures. But for many industrial and scientific purposes, there exists a need for a high-speed pump capable of drawing off hydrogen.
  • One example can be found in ultrahigh vacuum engineering where hydrogen often appears, in substantial quantities, as a residual gas.
  • Another example is in plasma physics where, particularly for nu clear experiments, extremely high vacuums and ⁇ very high rates of suction for hydrogen are needed.
  • the primary object ofthe present invention to provide a cryopump capable of drawing off, at very high speeds, hydrogen and other gases having low boiling points, and, with lthis object in view, the present invention resides, mainly, in a cryopump which comprises helical tubing forming a hollow cylinder, a hollow 4header arranged interiorly of the cylinder, conduit means serially connecting the tubing and the header, and means for circulating a coolant through the series-connection formed by the serially connected ⁇ tubing and header.
  • Ithe cryopump may further include a hollow protective member which is arranged between the cylindrical tubing and a main support on which the cryopump is mounted, this protective member being incorporated in the series-circuit such that the coolant iows therethrough after having passed through the header and tubing.
  • a hollow protective plate is mounted on the support plate and is arranged above the upper surface thereof.
  • the helical tubing forming the hollow cylinder is mounted on the protective plate and positioned above it, the axis of the cylindrical tubing being generally vertically oriented.
  • the header which is located interiorly of the cylinder, is in the form of a plate and is disposed generally at right angles to the cylinder axis, i ⁇ .e., generally horizontally.
  • the coolant is provided through a riser tube which comprises a valve and a throttling means and extends upwardly through the first-mentioned hollow tube.
  • This riser tube communicates at its top with the interior of the header plate and, besides the conduit means which connect the header and the helical tubing, there are the further conduit means which connect the tubing and the interior of the protective plate.
  • the cryopump also includes an exhaust tube which is in communication with the hollow protective plate and which extends through the second hollow tube passing through the support plate. It will thus be seen that the coolant introduced through the riser is made to circulate first through the h-ollow header, thereafter through the helical tubing, and thereafter through the protective plate, from which the spent coolant is drawn out through the exhaust tube.
  • FIGURE l is a sectional elevational view of a cryopump according to the present invention.
  • FIGURE 2 is a sectional elevational view of the cryopump according to FIGURE 1, taken in a plane at ⁇ right angles to the plane of FIGURE l and showing only icertain ⁇ ot the components.
  • FIGURE 3 is a sectional View through the hollow header plate taken on line 3-3 of FIGURE 2.
  • FIGURE 4 is a schematic diagram showing a chamber which is to be evacuated, within which chamber is arranged the cryopump according to the present invention.
  • FIGURE 4 shows the actual condensing components of the cryopump, as well as the supply reservoir for the liquid coolant, e.g., helium, and the vacuum pump by means of which the coolant is moved through the cryopump.
  • the liquid coolant e.g., helium
  • FIGURE 5 is a sectional view through the throttling means 35a of FIGURE 4.
  • FIGURE l shows the condensing element as comprising a support plate 1 which has set into it two hollow covering tubes 2 and 3 which are open at the it-op.
  • a tubular jacket 4 which, in turn, surrounds a vacuum riser tube 5, while the tube 3 has arranged within it an exhaust tube 6.
  • the covering tubes 2 and 3 for the jacket d and the exhaust .tube 6 are thus evacuated together with the chamber, receptacle or other space within which the cmdensing element is mounted by means of the support p ate ll.
  • the jacket 4 is surrounded, throughout a portion of its length, by a further tube 7 which protects the jacket 4 from radiation, this tube 7 being in heatexchange contact with the jacket 4.
  • an end piece 9 Arranged within the upper end of jacket 4t is an end piece 9, the same being provided with a bore 8 which is in communication with a number of tubes .l0 that are set into the end piece 9.
  • the other ends of the tubes 10 are in communication with a channel system 11 that is provided in a hollow plate or header 12..
  • the condensing element further comprises a biiilar helical tubing .14, forming, generally, a hollow cylinder, adjacent turns of the tubing 14 being in heat-exchange contact with each other.
  • the channeling L1 within the header 12 is connected with the tubing 14 by means of a spirally bent conduit 13 which itself is made of a poor conductor of heat.
  • the tubing 14 is connected, via a further spirally bent exhaust gas conduit d5, also made of a material which is a poor conductor of heat, with the interior of a generally plate-shaped hollow member 16, this plate 16 serving as a protective element against heat conduction and radiation.
  • the interior of the plate 16 is in communication, via the exhaust conduit tube 6, and
  • the actual condensing components, namely, 12, 14, of the condensing element are structurally attached to the protective plate 16 by means of mounting pins 18, the plate 16 being connected to the main support plate 1 by means of further pins 19.
  • the pins 18 and 19 are made of a material which is a poor conductor of heat.
  • the lower ends of the tube 2 and jacket 4 are set into a common end piece 21, the same being provided with a sealing gland or screw 22 by means of which the riser tube can be inserted gas-tightly into the jacket 4.
  • the protective tube 7 is in heat-exchange contact with the plate 16.
  • FIGURE 2 shows the disposition of the conduits 25 and 26 leading to the organs 23 and 24, respectively, these conduits 25 and 26 being likewise made of a poor conductor of heat.
  • the conduits 25 and 26 pass through vacuum packets 27 and 28, respectively, which are set into the support plate 1 and tare ending in anges 29 and 30, respectively, by means of which the vapor pressure thermometers are connected to the measuring and control system (FIGURE 4).
  • FIGURE 3 which shows the arrangement of the channel system 11 within the header 12, the coolant enters the channels at the points indicated at 31, flows therethrough in the direction shown by the arrows, and leaves the system at 32.
  • the channeling includes a number of radial branches, and since each of the several inlets of the header communicates with two adjacent radial channels and an outlet whereat two radial channels join, the coolant will be made to flow in counter-current ow through the header, thereby evenly to distribute the temperature throughout the header.
  • the inlets to the header are near the axis of the header, this axis being concentric with the axis of the cylinder formed by the helical tubing 14.
  • the cross section of the interior passage provided by the tubing 14 is greater than the cross section of the channeling in the header.
  • FIGURE 4 shows a receptacle 33 forming a chamber to be evacuated. Arranged within this chamber is the abovedescribed condensing element, of which the actual condensing components, namely, the header 12 and helical tubing ⁇ 14 are shown, as is the riser 5 whose lower end dips into a helium reservoir 34.
  • FIGURE 4 also shows a valve and a throttling means 35a, for controlling the helium ow through the riser 5.
  • the exhaust tube 6 is connected, via a control valve 36 and, if desired, a throttle valve 37, to a vacuum pump 38.
  • the control valve 36 is thermostatically operated by means of the vapor pressure thermometer 24.
  • FIGURE 4 shows pressure gauges 40 and 41 which are in communication with the vapor pressure thermometers 23, 24, respectively so that a temperature reading may be obtained. Further pressure gauges 42 and 43 are provided for measuring the pressure in the suction conduit connected to the exhaust tube 6. Finally, FIGURE 4 shows the interior of receptacle ⁇ 33 as being in communication, via a valve 44, with a suction stud 45 through which the chamber can be pre-evacuated, i.e., evacuated to a pressure which may be considered to be high as compared to the exceedingly low pressure to which the chamber is evacuated by means of the condensing element of the cryopump.
  • FIGURE 5 shows the throttling means 35a which is situated in riser 5.
  • the throttling means 35a is formed by a bundle of capillary tubes 46 which have a small diameter and different lengths and which are set into a base piece 47. Capillary tubes 46 and base piece 47 are arranged within riser tube 5. Valve 35 may be situated above or below this throttling means 35a.
  • the vacuum pump 38 sucks liquid helium out of the reservoir 34 through the riser 5 and into the condensing component 12 where it is vaporized under normal or reduced pressure so as to effect the desired cooling. More particularly, the coolant flows -through the riser 5, valve 35 and throttling means 35a, the bores 8 in the end piece 9, and the tubes 10, into the channels 11 in header 12. Thanks to the radial arrangement of the channels as shown in FIGURE 3, the coolant flows radially in countercurrent, as a result of which the temperature, as described above, is distributed evenly over the header 12.
  • the coolant leaves the header at the central outlet 32, from whence it ows through the connecting conduit 13, the bifilar tubing
  • the temperature of the components 12, 14 is regulated and maintained constant by means of the valve 35 in combination with the throttlings means 35a and the control valve 36 which, as explained above, is itself controlled by the vapor pressure thermometer 24.
  • the control valve 36 and valve 35 are open and coolant is sucked through the condensing components 12, 14, thereby cooling the same.
  • the headers temperature comes near 4.2 K.
  • the flow of liquid through riser 5 has to be reduced by partly closing valve 35, and the pressure within the header must be lowered to the desired low value corresponding to the desired header temperature below 4.2 K. This is done by means of the vacuum pump 38 which has a high suction rate.
  • the suction of the pump is reduced by means of the control valve 36 so that the desired temperature pressure relationship will be maintained. That means that during operation at a constant header temperature below 4.2 K. the ow of coolant is kept at a rather constant value given by the setting of valve ⁇ 35 and at the same time the desired low pressure is maintained constan-t by means of control valve 36.
  • the throttling means 35a helps to maintain the temperature at a constant value over long periods of time without having to correct the setting of valve 35. Without throttling means 35a it may happen that the temperature rises after some time of operation, so that valve 35 has to be adjusted ⁇ again and again.
  • control valve 36 is provided with a by-pass through which the pressure may be lowered to a value which is just short of the desired pressure for the desired corresponding temperature.
  • the control valve itself may then be used to obtain a ne, Vernier-type adjustment of the pressure and temperature relationship.
  • the temperature of the header may be reduced to below 4.2 K., while the temperature of the helical tubing 14 surrounding the hea-der 12 is kept to about 20 K.
  • the temperature of the helical tubing 14 may have different values for a given header temperature.
  • the temperature of the helical tubing depends on the flow of coolant, on the amount of cold that is needed to cool the header, and on the size of the outer surface of the helical tubing resp. on the amount of heat transferred to this outer surface by radiation.
  • the operation of the cryopump is most economical with a temperature of about 20 K. for the helical tubing 14, i.e. by means of measuring this temperature it is possible to control the operation with regard to economy.
  • the tubing 14 also serves so as partly to protect the header which is cooled to a temperature lower than that to which the helical tubing is cooled.
  • the protective member 16 which inhibits heat conduction and which acts as radiation protective shield for a portion of the header 12, can condense vapors which condense at still higher temperatures.
  • the coolant is made to flow through a series-connection which causes the liquid helium to iiow first through the hollow header 12, then through the helical tubing 14, and then through the protective plate 16, whereafter the spent coolant is drawn out of the cryopump, "by the vacuum pump 38, ultimately to be recovered in a manner known per se.
  • This utilizes the cold of the liquid helium to maximum advantage, in that the coolant first cools the header 12 to a temperature below 4.2 K., there to condense hydrogen.
  • the helical tubing 14 which serves to protect against radiation the coldest surface of the cryopump and which itself serves as the condensing surface for nitrogen and other gases having a boiling point higher than that of hydrogen is cooled to about 20 K.
  • the coolant cools the protective plate 16 as well as the lead-in conduit for the liquid coolant. In this way, the cryopump described above can be used to remove hydrogen alone or hydrogen as part of a mixture -containing other gases having higher boiling points.
  • the cryopump as a whole can easily be put into whatever space is to be evacuated. This means that the cryopump is versatile enough to allow it to be used wherever needed.
  • the coolant reservoir 34 per se is, for example, a conventional helium supply tank. Consequently, the cryopump is invulnerable tofbreakdown to which a liquefying system is susceptible. Furthermore, since the helium tank itself is under atmospheric pressure, the same can readily be replenished, so that the cryopump itself can be operated continuously, without it being necessary to interrupt operation for purposes of refilling the vessel. This means that the cryopumping can be carried on for indefinite periods of time.
  • cryopump one of the salient features of a cryopump according to the present invention is the fact that the coldest part of the pump, the hollow header 12, has in each case maximum size relative to the chosen dimensions of the cylindrical tubing 14 which is forming the radiation shield.
  • the tubing 14 may be constituted by a bilar winding and that the adjacent turns of the tubing are in good heatexchange contact with each other, the temperature dis tri'bution will be spread uniformly over the outer surface of the tubing 14.
  • thermometers 23 and 24 arranged, respectively, at the coldest surface, i.e., at the header 12, and at the point at which the coolant leaves the helical tubing 14, allow the operation of the cryopump to be regulated and to be monitored at all times.
  • cryopump is particularly troublefree and economical and needs little service thanks to the facts that a single coolant is circulated throughout the various serially connected parts to be cooled and that the temperature can be maintained automatically at a constant value.
  • a cryopump the combination which comprises: helical tubing forming a hollow cylinder; a hollow header in the form of a plate provi-ded with channeling therein arranged interiorly of said cylinder; conduit means serially connecting said tubing and said header; and means for circulating a coolant to the series-connection formed by said serially connected tubing and header.
  • tubing incorporates a plurality of turns which are closely adjacent to each other, the cross section of the interior passage provided ⁇ by said tubing being greater than the cross section of said channeling in said header.
  • a cryopump the combination which comprises: helical tubing forming a hollow cylinder; a hollow header arranged interiorly of said cylinder; conduit means serially connecting said tubing and said header; and means for circulating a coolant through the series-connection formed by said serially connected tubing and header, said header including a plate provided with channeling, said plate having a plurality of inlets with which said circulating means are in communication, sai-d channeling being provided, at ⁇ each of said inlets, with branches in consequence of which incoming coolant is made to iow through said header in a plurality of directions.
  • a cryopump the combination which comprises: helical tubing forming a hollow cylinder; a hollow header arranged interiorly of said cylinder; conduit means serially connecting said tubing and said header; and means for circulating a coolant through the series-connection formed by said serially connected tubing and header, said header including a plate provided with a plurality of channels which extend generally radially with respect to the axis of said hollow cylinder, said plate being provided with a plurality of inlet means each of which communicates with two adjacent radial channels, said header further comprising outlet means whereat two radial channels join, in consequence of which a coolant circulated through said header is made to tlow in counter-current flow thereby evenly to distribute the temperature throughout said header.
  • a cryopump the combination which comprises: a support; a hollow radiation and heat conduction protective plate mounted on said support; helical tubing forming a hollow cylinder and arranged on said protective plate, said tubing being positioned on that side of said plate which is opposite the side of said plate which faces said support, the axis of said cylinder being generally at right angles to said plate; a hollow header arranged interiorly of said cylinder; iirst conduit means serially connecting said header and said tubing; second conduit means serially connecting said tubing and said protective plate; and
  • said circulating means comprise a generally vertically oriented riser tube whose upper end is in communication with said header; a jacket surrounding said riser tube; and a further tube surrounding said jacket throughout at least a portion of its length for protecting the same against heat conduction and radiation, said further tube being in heatexchange contact with said jacket and with said protective plate.
  • said circulating means further comprise sealing means for securing said riser tube and said jacket to each other, and wherein said upper end of said riser tube is approximately at the same level as the upper end of said jacket.
  • a cryopump comprising, in combination: a generally horizontally oriented support plate; a first hollow tube extending through said support plate and opening at the upper surface of said support plate; a second hollow tube also extending through said support plate and opening at the upper surface thereof; a hollow protective plate mounted on said support plate and arranged above said upper surface thereof; helical tubing forming a hollow cylinder and mounted on said protective plate, said tubing being positioned above said protective plate, the axis of said cylinder being generally vertically oriented; a hollow header plate arranged interiorly of said cylinder and dis posed generally at right angles to said cylinder axis; a coolant riser tube comprising a valve and a throttling means and extending upwardly through said first hollow tube, Isaid riser tube communicating at its top with the interior of said header plate; first conduit means for placing said header plate in communication with said helical tubing; second conduit means for placing said helical tubing in communication with said hollow protective plate; and an exhaust tube in communication with said protective plate and
  • a reservoir for a liquid which boils at low temperature said reservoir being in communication with the lower end of said riser tube; and a vacuum pump in communication with said exhaust tube.
  • valve means arranged in the communication between said vacuum pump and said exhaust tube of said cryopump; and temperature sensitive means responsive to the temperature of said cryopump for controlling said valve means, thereby to regulate the temperature of said cryopump by means of regulating the pressure within the system.
  • valve means arranged in said riser tube for controlling the ow of coolant therethrough.
  • a cryopump the combination which comprises: bifilar helical tubing forming a hollow cylinder; a hollow header arranged interiorly of said cylinder; conduit means serially connecting said tubing and said header; and means for circulating a coolant through the series-connection formed by said serially connected tubing and header.
  • a cryopump the combination which comprises: helical tubing forming -a hollow cylinder, adjacent turns of said tubing being in heat-exchange contact with each other; a hollow header arranged interiorly of said cylinder; conduit means serially connecting said tubing and said header; and means for circulating a coolant through the series-connection formed by said serially connected tubing and header.

Description

Oct. 18, 1966 G. KLlPPxNG ETAL 3,279,214
PUMP
Filed Sept. 15, 1964 5 Sheets-Sheet 2 Fig.2
WERNER MAS HER BY ATTORNEYS Oct. 18, 1966 G. KLIPPING ETAL 3,279,214
' PUMP Filed Sept. l5, 1964 5 Sheets-Sheet 3 Jnvenors: GUSTAV KLIPPING WERNER MASCHER ATToRNEYs Oct. 18, 1966 G. KLIPPING ETAL 3,279,214
PUMP
Filed Sept. 15, 1964 5 Sheets-Sheet 4 Fig/1- vnu/UM i PUMP Invenors: GUSTAV KLIPPIN'G W RNER MASCHER ATTORNEYS Oct. 18, 1966 G. KLIPPING ETAL 3,279,214
PUMP
Filed Sept. 15, 1964 5 Sheets-Sheet 5 Fig.5
Jnvenors: GUSTAV KLIPPING WE RNE F? MASCH ER ATTORNEYS United States Patent O 3,279,214 PUMP Gustav Klipping, Berlin-Zehlendorf, and Werner Mascher,
Berlin-Steglitz, Germany, assignors to Max-Planclr-Gesellschaft zur Frderung der Wissenschaften, e. V., Gottingen, Germany Filed Sept. 15, 1964, Ser. No. 396,556
Claims priority, application Germany, Nov. 2, 1963,
20 Claims. (Cl. 62-55.5)
The present invention relates to a device for producing a vacuum with the aid of a condensing element which is cooled to very low temperatures.
So-cal-led cryopumps are used in the art of vacuum engineering whenever high-speed suction is needed. If such high-speed suction is to remove hydrogen, the condensing elements have to be kept at temperatures below 42 K., this being the 4boiling point of liquid helium.
Heretofore, cryopumps have been used only for evacuating large receptacles, e.g., wind tunnels, and only for removing nitrogen or gases having higher boiling points. Conventional cryopumps are connected directly with a refrigeration unit, and the condensing surfaces, which are usually :surrounded by a radiation protector cooled `by nitrogen, are cooled by means of cold helium gas which tlows under the inuence of pressure greater than atmospheric. This produces operating temperatures which are substantially above the boiling point of helium, namely, approximately l2 to 14 K.
It has up to now not been found possible to use cryopumps for evacuating hydrogen, because no existing cryopump has been known to operate at sufficiently low temperatures. But for many industrial and scientific purposes, there exists a need for a high-speed pump capable of drawing off hydrogen. One example can be found in ultrahigh vacuum engineering where hydrogen often appears, in substantial quantities, as a residual gas. Another example is in plasma physics where, particularly for nu clear experiments, extremely high vacuums and `very high rates of suction for hydrogen are needed.
It is, therefore, the primary object ofthe present invention to provide a cryopump capable of drawing off, at very high speeds, hydrogen and other gases having low boiling points, and, with lthis object in view, the present invention resides, mainly, in a cryopump which comprises helical tubing forming a hollow cylinder, a hollow 4header arranged interiorly of the cylinder, conduit means serially connecting the tubing and the header, and means for circulating a coolant through the series-connection formed by the serially connected `tubing and header. In a practical embodiment, Ithe cryopump may further include a hollow protective member which is arranged between the cylindrical tubing and a main support on which the cryopump is mounted, this protective member being incorporated in the series-circuit such that the coolant iows therethrough after having passed through the header and tubing.
More particularly, a cryopump according to the present invention comprises `a generally horizontally oriented support plate, a rst hollow tube extending through the sup port plate and opening at the upper surface of the support plate, and a second hollow tube also extending through the support plate and opening at the rupper surface thereof. A hollow protective plate is mounted on the support plate and is arranged above the upper surface thereof. The helical tubing forming the hollow cylinder is mounted on the protective plate and positioned above it, the axis of the cylindrical tubing being generally vertically oriented. The header, which is located interiorly of the cylinder, is in the form of a plate and is disposed generally at right angles to the cylinder axis, i`.e., generally horizontally.
3,279,2l4 Patented Uct. 18, lg
ICC
The coolant is provided through a riser tube which comprises a valve and a throttling means and extends upwardly through the first-mentioned hollow tube. This riser tube communicates at its top with the interior of the header plate and, besides the conduit means which connect the header and the helical tubing, there are the further conduit means which connect the tubing and the interior of the protective plate. The cryopump also includes an exhaust tube which is in communication with the hollow protective plate and which extends through the second hollow tube passing through the support plate. It will thus be seen that the coolant introduced through the riser is made to circulate first through the h-ollow header, thereafter through the helical tubing, and thereafter through the protective plate, from which the spent coolant is drawn out through the exhaust tube.
Additional objects and advantages of the present invention will become apparent upon consideration `of the following description when taken in conjunction with the accompanying drawings in which:
FIGURE l is a sectional elevational view of a cryopump according to the present invention.
FIGURE 2 is a sectional elevational view of the cryopump according to FIGURE 1, taken in a plane at `right angles to the plane of FIGURE l and showing only icertain `ot the components.
FIGURE 3 is a sectional View through the hollow header plate taken on line 3-3 of FIGURE 2.
FIGURE 4 is a schematic diagram showing a chamber which is to be evacuated, within which chamber is arranged the cryopump according to the present invention. FIGURE 4 shows the actual condensing components of the cryopump, as well as the supply reservoir for the liquid coolant, e.g., helium, and the vacuum pump by means of which the coolant is moved through the cryopump.
FIGURE 5 is a sectional view through the throttling means 35a of FIGURE 4.
Referring now to the drawings, FIGURE l shows the condensing element as comprising a support plate 1 which has set into it two hollow covering tubes 2 and 3 which are open at the it-op. Arranged within the tube 2 is a tubular jacket 4 which, in turn, surrounds a vacuum riser tube 5, while the tube 3 has arranged within it an exhaust tube 6.. The covering tubes 2 and 3 for the jacket d and the exhaust .tube 6 are thus evacuated together with the chamber, receptacle or other space within which the cmdensing element is mounted by means of the support p ate ll.
The jacket 4 is surrounded, throughout a portion of its length, by a further tube 7 which protects the jacket 4 from radiation, this tube 7 being in heatexchange contact with the jacket 4.
Arranged within the upper end of jacket 4t is an end piece 9, the same being provided with a bore 8 which is in communication with a number of tubes .l0 that are set into the end piece 9. The other ends of the tubes 10 are in communication with a channel system 11 that is provided in a hollow plate or header 12..
The condensing element further comprises a biiilar helical tubing .14, forming, generally, a hollow cylinder, adjacent turns of the tubing 14 being in heat-exchange contact with each other. The channeling L1 within the header 12 is connected with the tubing 14 by means of a spirally bent conduit 13 which itself is made of a poor conductor of heat. The tubing 14 is connected, via a further spirally bent exhaust gas conduit d5, also made of a material which is a poor conductor of heat, with the interior of a generally plate-shaped hollow member 16, this plate 16 serving as a protective element against heat conduction and radiation. The interior of the plate 16 is in communication, via the exhaust conduit tube 6, and
3 its end ange 17 as well as a control valve, with a vacuum pump (FIGURE 4).
The actual condensing components, namely, 12, 14, of the condensing element are structurally attached to the protective plate 16 by means of mounting pins 18, the plate 16 being connected to the main support plate 1 by means of further pins 19. The pins 18 and 19 are made of a material which is a poor conductor of heat. Also shown are ns 20, likewise made of a material which is a poor conductor of heat, which serve to position the header 12 centrally with respect to the bilar helical tubing 14.
The lower ends of the tube 2 and jacket 4 are set into a common end piece 21, the same being provided with a sealing gland or screw 22 by means of which the riser tube can be inserted gas-tightly into the jacket 4. The protective tube 7 is in heat-exchange contact with the plate 16.
A measuring organ 23 of a vapor pressure thermometer is set into the header 12, and a further measuring organ 24 of a further vapor pressure thermometer is attached to the outlet of the helical tubing 14. FIGURE 2 shows the disposition of the conduits 25 and 26 leading to the organs 23 and 24, respectively, these conduits 25 and 26 being likewise made of a poor conductor of heat. The conduits 25 and 26 pass through vacuum packets 27 and 28, respectively, which are set into the support plate 1 and tare ending in anges 29 and 30, respectively, by means of which the vapor pressure thermometers are connected to the measuring and control system (FIGURE 4).
As is apparent from FIGURE 3, which shows the arrangement of the channel system 11 within the header 12, the coolant enters the channels at the points indicated at 31, flows therethrough in the direction shown by the arrows, and leaves the system at 32. Inasmuch as the channeling includes a number of radial branches, and since each of the several inlets of the header communicates with two adjacent radial channels and an outlet whereat two radial channels join, the coolant will be made to flow in counter-current ow through the header, thereby evenly to distribute the temperature throughout the header. As shown in FIGURE 3, the inlets to the header are near the axis of the header, this axis being concentric with the axis of the cylinder formed by the helical tubing 14. Furthermore, the cross section of the interior passage provided by the tubing 14 is greater than the cross section of the channeling in the header.
FIGURE 4 shows a receptacle 33 forming a chamber to be evacuated. Arranged within this chamber is the abovedescribed condensing element, of which the actual condensing components, namely, the header 12 and helical tubing `14 are shown, as is the riser 5 whose lower end dips into a helium reservoir 34. FIGURE 4 also shows a valve and a throttling means 35a, for controlling the helium ow through the riser 5. The exhaust tube 6 is connected, via a control valve 36 and, if desired, a throttle valve 37, to a vacuum pump 38. The control valve 36 is thermostatically operated by means of the vapor pressure thermometer 24. The pressure side of vacuum pump 38 is connected, via a connecting flange 39, to the helium recovery system (not shown). FIGURE 4 also shows pressure gauges 40 and 41 which are in communication with the vapor pressure thermometers 23, 24, respectively so that a temperature reading may be obtained. Further pressure gauges 42 and 43 are provided for measuring the pressure in the suction conduit connected to the exhaust tube 6. Finally, FIGURE 4 shows the interior of receptacle `33 as being in communication, via a valve 44, with a suction stud 45 through which the chamber can be pre-evacuated, i.e., evacuated to a pressure which may be considered to be high as compared to the exceedingly low pressure to which the chamber is evacuated by means of the condensing element of the cryopump.
FIGURE 5 shows the throttling means 35a which is situated in riser 5. The throttling means 35a is formed by a bundle of capillary tubes 46 which have a small diameter and different lengths and which are set into a base piece 47. Capillary tubes 46 and base piece 47 are arranged within riser tube 5. Valve 35 may be situated above or below this throttling means 35a.
The above-described arrangement operates as follows:
The vacuum pump 38 sucks liquid helium out of the reservoir 34 through the riser 5 and into the condensing component 12 where it is vaporized under normal or reduced pressure so as to effect the desired cooling. More particularly, the coolant flows -through the riser 5, valve 35 and throttling means 35a, the bores 8 in the end piece 9, and the tubes 10, into the channels 11 in header 12. Thanks to the radial arrangement of the channels as shown in FIGURE 3, the coolant flows radially in countercurrent, as a result of which the temperature, as described above, is distributed evenly over the header 12. The coolant leaves the header at the central outlet 32, from whence it ows through the connecting conduit 13, the bifilar tubing |14, the connecting conduit 15, the protective member 16, the exhaust tube 6, the control valve 36, the throttle valve 37 and into the suction pump 38, and thence to the helium recovery system.
The temperature of the components 12, 14 is regulated and maintained constant by means of the valve 35 in combination with the throttlings means 35a and the control valve 36 which, as explained above, is itself controlled by the vapor pressure thermometer 24. At the start of the operation, the control valve 36 and valve 35 are open and coolant is sucked through the condensing components 12, 14, thereby cooling the same. As soon as the headers temperature comes near 4.2 K., the flow of liquid through riser 5 has to be reduced by partly closing valve 35, and the pressure within the header must be lowered to the desired low value corresponding to the desired header temperature below 4.2 K. This is done by means of the vacuum pump 38 which has a high suction rate. As soon as the desired pressure for such temperature is reached, the suction of the pump is reduced by means of the control valve 36 so that the desired temperature pressure relationship will be maintained. That means that during operation at a constant header temperature below 4.2 K. the ow of coolant is kept at a rather constant value given by the setting of valve `35 and at the same time the desired low pressure is maintained constan-t by means of control valve 36. To change the temperature of the condensing elements 12, 14 is is necessary to adjust valve 35 so as to obtain more or less `tlow of coolant, and to adjust valve 36 so as to maintain a lower or higher pressure Within the system. The throttling means 35a helps to maintain the temperature at a constant value over long periods of time without having to correct the setting of valve 35. Without throttling means 35a it may happen that the temperature rises after some time of operation, so that valve 35 has to be adjusted `again and again.
It has been found that temperature fluctuations may be kept very small if the control valve 36 is provided with a by-pass through which the pressure may be lowered to a value which is just short of the desired pressure for the desired corresponding temperature. The control valve itself may then be used to obtain a ne, Vernier-type adjustment of the pressure and temperature relationship.
It has been found that, by using the above-described condensing element, the temperature of the header may be reduced to below 4.2 K., while the temperature of the helical tubing 14 surrounding the hea-der 12 is kept to about 20 K. The temperature of the helical tubing 14 may have different values for a given header temperature. The temperature of the helical tubing depends on the flow of coolant, on the amount of cold that is needed to cool the header, and on the size of the outer surface of the helical tubing resp. on the amount of heat transferred to this outer surface by radiation. The operation of the cryopump is most economical with a temperature of about 20 K. for the helical tubing 14, i.e. by means of measuring this temperature it is possible to control the operation with regard to economy.
With the header at 42 K. and the `helical tubing at about 20 K. hydrogen will be condensed on the header while nitrogen and other gases having higher boiling points are condensed on the helical tubing. Here, the tubing 14 also serves so as partly to protect the header which is cooled to a temperature lower than that to which the helical tubing is cooled.
The protective member 16, which inhibits heat conduction and which acts as radiation protective shield for a portion of the header 12, can condense vapors which condense at still higher temperatures.
Thanks to the above arrangement, the coolant is made to flow through a series-connection which causes the liquid helium to iiow first through the hollow header 12, then through the helical tubing 14, and then through the protective plate 16, whereafter the spent coolant is drawn out of the cryopump, "by the vacuum pump 38, ultimately to be recovered in a manner known per se. This utilizes the cold of the liquid helium to maximum advantage, in that the coolant first cools the header 12 to a temperature below 4.2 K., there to condense hydrogen. Next, the helical tubing 14, which serves to protect against radiation the coldest surface of the cryopump and which itself serves as the condensing surface for nitrogen and other gases having a boiling point higher than that of hydrogen is cooled to about 20 K. Thirdly, the coolant cools the protective plate 16 as well as the lead-in conduit for the liquid coolant. In this way, the cryopump described above can be used to remove hydrogen alone or hydrogen as part of a mixture -containing other gases having higher boiling points.
A cryopump with a header diameter `of 76 mm., a helical tubing diameter of 98 mm., a helical tubing height of 100 min., a length of each channel in the header of about 75 mm., a cross section of each channel of 3 mm2 (i.e. cross section of all channels about 25 mm2), an inner cross section of the tube forming the helix of 33 mm?, a length of the tube forming the helix of 3600 mm., and a suction rate of the vacuum pump of 12 m.3/h. has for example a suction rate of 25001./sec. for hydrogen and at the same time 55001./sec. for nitrogen.
Thanks to the fact that the entire structure is mounted on a main support, i.e., the plate 1, the cryopump as a whole can easily be put into whatever space is to be evacuated. This means that the cryopump is versatile enough to allow it to be used wherever needed.
The coolant reservoir 34 per se is, for example, a conventional helium supply tank. Consequently, the cryopump is invulnerable tofbreakdown to which a liquefying system is susceptible. Furthermore, since the helium tank itself is under atmospheric pressure, the same can readily be replenished, so that the cryopump itself can be operated continuously, without it being necessary to interrupt operation for purposes of refilling the vessel. This means that the cryopumping can be carried on for indefinite periods of time.
It will also be seen from the above that one of the salient features of a cryopump according to the present invention is the fact that the coldest part of the pump, the hollow header 12, has in each case maximum size relative to the chosen dimensions of the cylindrical tubing 14 which is forming the radiation shield.
Also, thanks to the fact that, as described above, the tubing 14 may be constituted by a bilar winding and that the adjacent turns of the tubing are in good heatexchange contact with each other, the temperature dis tri'bution will be spread uniformly over the outer surface of the tubing 14.
Furthermore, the thermometers 23 and 24 arranged, respectively, at the coldest surface, i.e., at the header 12, and at the point at which the coolant leaves the helical tubing 14, allow the operation of the cryopump to be regulated and to be monitored at all times.
Furthermore, thanks to the fact that the protective tube 7 for the riser tube 5 is in good heat contact with the jacket 4- and the cooled protective plate 16, a minimum of heat is conveyed, via radiation and conduction, to the actual condensing surfaces of the cryopump.
Finally, the cryopump is particularly troublefree and economical and needs little service thanks to the facts that a single coolant is circulated throughout the various serially connected parts to be cooled and that the temperature can be maintained automatically at a constant value.
It will be understood that the above description of the present invention is susceptible to various modiiications, changes and adaptions, and the same are intended to be comprehended within the meaning and range of equivalents of the appended claims.
What is claimed is:
1. In a cryopump, the combination which comprises: helical tubing forming a hollow cylinder; a hollow header in the form of a plate provi-ded with channeling therein arranged interiorly of said cylinder; conduit means serially connecting said tubing and said header; and means for circulating a coolant to the series-connection formed by said serially connected tubing and header.
2. The combination deiined in claim 1 wherein said conduit means communicates with said header at a point near the axis of said cylinder.
3. The combination defined in cl-aim 1 wherein said conduit means serially connecting said tubing and said header are made of a material which is a poor conductor of heat.
4. The combination defined in claim 1 wherein said tubing incorporates a plurality of turns which are closely adjacent to each other, the cross section of the interior passage provided `by said tubing being greater than the cross section of said channeling in said header.
5. In a cryopump, the combination which comprises: helical tubing forming a hollow cylinder; a hollow header arranged interiorly of said cylinder; conduit means serially connecting said tubing and said header; and means for circulating a coolant through the series-connection formed by said serially connected tubing and header, said header including a plate provided with channeling, said plate having a plurality of inlets with which said circulating means are in communication, sai-d channeling being provided, at `each of said inlets, with branches in consequence of which incoming coolant is made to iow through said header in a plurality of directions.
6. In a cryopump, the combination which comprises: helical tubing forming a hollow cylinder; a hollow header arranged interiorly of said cylinder; conduit means serially connecting said tubing and said header; and means for circulating a coolant through the series-connection formed by said serially connected tubing and header, said header including a plate provided with a plurality of channels which extend generally radially with respect to the axis of said hollow cylinder, said plate being provided with a plurality of inlet means each of which communicates with two adjacent radial channels, said header further comprising outlet means whereat two radial channels join, in consequence of which a coolant circulated through said header is made to tlow in counter-current flow thereby evenly to distribute the temperature throughout said header.
7. In a cryopump, the combination which comprises: a support; a hollow radiation and heat conduction protective plate mounted on said support; helical tubing forming a hollow cylinder and arranged on said protective plate, said tubing being positioned on that side of said plate which is opposite the side of said plate which faces said support, the axis of said cylinder being generally at right angles to said plate; a hollow header arranged interiorly of said cylinder; iirst conduit means serially connecting said header and said tubing; second conduit means serially connecting said tubing and said protective plate; and
means for circulating a coolant through the series-connection formed by said serially-connected header, tubing and protective plate.
8. The combination defined in claim 7 wherein said circulating means supply coolant first to said header, in consequence of which the coolant traverses said protective plate after having flowed through said header and said helical tubing.
9. The combination defined in claim 8 wherein said first and second conduit means are made of a material which is a poor conductor of heat.
10. The combination defined in claim 8 wherein said circulating means comprise a generally vertically oriented riser tube whose upper end is in communication with said header; a jacket surrounding said riser tube; and a further tube surrounding said jacket throughout at least a portion of its length for protecting the same against heat conduction and radiation, said further tube being in heatexchange contact with said jacket and with said protective plate.
11. The combination defined in claim 10 wherein said circulating means further comprise sealing means for securing said riser tube and said jacket to each other, and wherein said upper end of said riser tube is approximately at the same level as the upper end of said jacket.
12. The combination defined in claim 7 wherein said protective plate is secured to said support by first pin means and said helical tubing is secured to said protective plate by second pin means, said pin means being made of a material which is a poor conductor of heat.
13. A cryopump comprising, in combination: a generally horizontally oriented support plate; a first hollow tube extending through said support plate and opening at the upper surface of said support plate; a second hollow tube also extending through said support plate and opening at the upper surface thereof; a hollow protective plate mounted on said support plate and arranged above said upper surface thereof; helical tubing forming a hollow cylinder and mounted on said protective plate, said tubing being positioned above said protective plate, the axis of said cylinder being generally vertically oriented; a hollow header plate arranged interiorly of said cylinder and dis posed generally at right angles to said cylinder axis; a coolant riser tube comprising a valve and a throttling means and extending upwardly through said first hollow tube, Isaid riser tube communicating at its top with the interior of said header plate; first conduit means for placing said header plate in communication with said helical tubing; second conduit means for placing said helical tubing in communication with said hollow protective plate; and an exhaust tube in communication with said protective plate and extending through said second hollow tube, in consequence of which coolant introduced into said riser tube is made to circulate first through said hollow header, thereafter through said helical tubing, and thereafter through said protective plate, whereafter the coolant ows through said exhaust tube.
14. In combination with a cryopump as defined in claim 13, a reservoir for a liquid which boils at low temperature, said reservoir being in communication with the lower end of said riser tube; and a vacuum pump in communication with said exhaust tube.
15. The combination defined in claim 14, further comprising valve means arranged in the communication between said vacuum pump and said exhaust tube of said cryopump; and temperature sensitive means responsive to the temperature of said cryopump for controlling said valve means, thereby to regulate the temperature of said cryopump by means of regulating the pressure within the system.
16. The 4combination defined in claim 14, further comprising valve means arranged in said riser tube for controlling the ow of coolant therethrough.
17. The combination defined in claim 14, further comprising a throttling means arranged within said riser tube for controlling the flow of coolant therethrough.
18. The combination defined in cl-aim 17, wherein said throttling means comprises a bundle of capillary tubes with small diameters and different lengths, this bundle being arranged within said riser tube.
19. In a cryopump, the combination which comprises: bifilar helical tubing forming a hollow cylinder; a hollow header arranged interiorly of said cylinder; conduit means serially connecting said tubing and said header; and means for circulating a coolant through the series-connection formed by said serially connected tubing and header.
20. In a cryopump, the combination which comprises: helical tubing forming -a hollow cylinder, adjacent turns of said tubing being in heat-exchange contact with each other; a hollow header arranged interiorly of said cylinder; conduit means serially connecting said tubing and said header; and means for circulating a coolant through the series-connection formed by said serially connected tubing and header.
References Cited by the Examiner UNITED sTATEs PATENTS 1,146,020 7/1915 Piace 62-45 x 1,976,688 10/1934 Danaetai 62-45X 3,166,915 1/1965 Klipping 62-52 3,195,322 7/1965 London 62-514 X OTHER REFERENCES Kaltetechnik, 13 Jahrgang, Helium Evaporator, published July 1961, pp. Z50-252.r
LLOYD L. KING, Przinaly Examiner.

Claims (1)

1. IN A CRYOPUMP, THE COMBINATION WHICH COMPRISES: HELICAL TUBING FORMING A HOLLOW CYLINDER; A HOLLOW HEADER IN THE FORM OF A PLATE PROVIDED WITH CHANNELING THEREIN ARRANGED INTERIORLY OF SAID CYLINDER; CONDUIT MEANS SERIALLY CONNECTING SAID TUBING AND SAID HEADER; AND MEANS FOR CIRCULATING A COOLANT TO THE SERIES-CONNECTION FORMED BY SAID SERIALLY CONNECTED TUBING AND HEADER.
US39655664 1963-11-02 1964-09-15 Pump Expired - Lifetime US3279214A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE1965M0077476 DE1300624B (en) 1964-09-15 1965-01-16 Pump capacitor for generating a vacuum with the help of a deep-freeze condensation element

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEM0058766 1963-11-02

Publications (1)

Publication Number Publication Date
US3279214A true US3279214A (en) 1966-10-18

Family

ID=7309325

Family Applications (1)

Application Number Title Priority Date Filing Date
US39655664 Expired - Lifetime US3279214A (en) 1963-11-02 1964-09-15 Pump

Country Status (2)

Country Link
US (1) US3279214A (en)
DE (1) DE1451092B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3396548A (en) * 1965-09-08 1968-08-13 Philips Corp Vacuum device
US3516429A (en) * 1967-04-12 1970-06-23 Sartorius Werke Gmbh System for automatic control of gas pressure
US3529429A (en) * 1968-10-16 1970-09-22 Us Air Force Transfer system for cryogenic liquids

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1146020A (en) * 1908-01-02 1915-07-13 American Air Liquefying Company Air liquefier and separator.
US1976688A (en) * 1932-04-19 1934-10-09 Linde Air Prod Co Container for liquefied gases
US3166915A (en) * 1961-03-01 1965-01-26 Max Planck Gesellschaft Cooling arrangement
US3195322A (en) * 1961-09-22 1965-07-20 Atomic Energy Authority Uk Refrigerator employing helium

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1146020A (en) * 1908-01-02 1915-07-13 American Air Liquefying Company Air liquefier and separator.
US1976688A (en) * 1932-04-19 1934-10-09 Linde Air Prod Co Container for liquefied gases
US3166915A (en) * 1961-03-01 1965-01-26 Max Planck Gesellschaft Cooling arrangement
US3195322A (en) * 1961-09-22 1965-07-20 Atomic Energy Authority Uk Refrigerator employing helium

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3396548A (en) * 1965-09-08 1968-08-13 Philips Corp Vacuum device
US3516429A (en) * 1967-04-12 1970-06-23 Sartorius Werke Gmbh System for automatic control of gas pressure
US3529429A (en) * 1968-10-16 1970-09-22 Us Air Force Transfer system for cryogenic liquids

Also Published As

Publication number Publication date
DE1451092A1 (en) 1969-03-13
DE1451092B2 (en) 1970-01-22

Similar Documents

Publication Publication Date Title
US3358472A (en) Method and device for cooling superconducting coils
US5862605A (en) Vaporizer apparatus
US4082967A (en) Uniformly-cooled superconducting rotor
US2909903A (en) Liquefaction of low-boiling gases
US4941527A (en) Heat pipe with temperature gradient
US3729946A (en) Cryogenic liquid handling system
KR100257146B1 (en) Liquid cryogen delivery system
CN111981724B (en) Cryogenic cooling system
US3620033A (en) Cryostat device
US3006157A (en) Cryogenic apparatus
US4204134A (en) Coolant loop for the rotor of a turbogenerator with a superconductive exciter winding
US3457730A (en) Throttling valve employing the joule-thomson effect
US5243826A (en) Method and apparatus for collecting liquid cryogen
US3279214A (en) Pump
US4672823A (en) Dilution cryostat
US3424230A (en) Cryogenic refrigeration device with temperature controlled diffuser
CA2513536A1 (en) A circulation type liquid helium recondensation device with a contaminant-purging function, a contaminant-purging method, and the refiners and transfer tubes used in the device
US3070968A (en) Liquid to gas conversion system
US4891951A (en) Refrigeration system
JPH0127669B2 (en)
US2968163A (en) Apparatus for storing and dispensing liquefied gases
US3797264A (en) Low-temperature pumping device
CA1199629A (en) Process for cooling and fluidizing
US2404010A (en) Refrigerating machine
US20210005366A1 (en) Cryogenic Analytical Systems and Methods