EP0247935A1 - Zuleitungsverfahren für einen Joule-Thomson-Kühler und Kühlvorrichtung zu seiner Durchführung - Google Patents

Zuleitungsverfahren für einen Joule-Thomson-Kühler und Kühlvorrichtung zu seiner Durchführung Download PDF

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Publication number
EP0247935A1
EP0247935A1 EP87401167A EP87401167A EP0247935A1 EP 0247935 A1 EP0247935 A1 EP 0247935A1 EP 87401167 A EP87401167 A EP 87401167A EP 87401167 A EP87401167 A EP 87401167A EP 0247935 A1 EP0247935 A1 EP 0247935A1
Authority
EP
European Patent Office
Prior art keywords
working fluid
flow rate
orifice
fluid
cooling
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.)
Granted
Application number
EP87401167A
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English (en)
French (fr)
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EP0247935B1 (de
Inventor
Alain Faure
Serge Reale
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.)
Air Liquide SA
LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude
Original Assignee
Air Liquide SA
LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude
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 Air Liquide SA, LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude filed Critical Air Liquide SA
Publication of EP0247935A1 publication Critical patent/EP0247935A1/de
Application granted granted Critical
Publication of EP0247935B1 publication Critical patent/EP0247935B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/02—Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using Joule-Thompson effect; using vortex effect
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00—Gas cycle refrigeration machines
    • F25B2309/02—Gas cycle refrigeration machines using the Joule-Thompson effect
    • F25B2309/022—Gas cycle refrigeration machines using the Joule-Thompson effect characterised by the expansion element

Definitions

  • the present invention relates to a method for supplying a Joule-Thomson cooler comprising a high pressure line which ends in a pressure relief port, and a low pressure discharge circuit in heat exchange relation with the high line pressure and into which the expansion orifice opens, and more particularly to a method of the type in which the high pressure pipe is successively supplied with a starting fluid and then with a working fluid.
  • the object of the invention is to allow lower temperatures to be obtained in a very short time than has hitherto been possible.
  • the subject of the invention is a process of the aforementioned type, characterized in that the working fluid is used first at a high flow rate, then its flow rate is suddenly reduced to finish the cooling phase of the cooler .
  • the flow is reduced by masking the expansion orifice with a surface allowing a leakage passage to remain at the periphery of the orifice; - the flow rate of the working fluid is reduced in a ratio at least equal to 10; - We go from the starting fluid to the working fluid when the cooling speed provided by the first becomes lower than the cooling speed provided by the second.
  • the invention also relates to a cooling device intended to implement the method defined above.
  • This device of the type comprising a first source of starting fluid under a first high pressure, a second source of working fluid under a second high pressure, a Joule-Thomson cooler comprising a high pressure conduit which ends in a pressure relief port and a low pressure discharge circuit in heat exchange relationship with the high pressure pipe and into which the expansion orifice opens, and switching means for connecting the high pressure pipe first to the first source and then to the second source, is characterized in that it comprises throttling means for abruptly reducing the flow rate flowing in the high pressure pipe.
  • the throttling means comprise a shutter movable from a first position where the expansion orifice is free to a second position where this orifice is masked by a surface allowing the periphery of the orifice to be substituted an escape route.
  • the reservoir 1 shown in FIG. 1 is divided into two unequal chambers by a transverse partition 2: a downstream auxiliary chamber 3 containing a starting fluid with Joule-Thomson effect which is large but relatively not very volatile, for example argon, under a first high pressure which can be of the order of 700 bars, and an upstream main chamber 4 containing a more volatile working fluid and with a lesser Joule-Thomson effect, for example nitrogen, within one second high pressure at most equal to the first high pressure, for example of the order of 400 bars.
  • a transverse partition 2 a downstream auxiliary chamber 3 containing a starting fluid with Joule-Thomson effect which is large but relatively not very volatile, for example argon, under a first high pressure which can be of the order of 700 bars, and an upstream main chamber 4 containing a more volatile working fluid and with a lesser Joule-Thomson effect, for example nitrogen, within one second high pressure at most equal to the first high pressure, for example of the order of 400 bars.
  • the partition 2 is pierced with an orifice 5 masked by a piece of foil 6 applied to the front face of the partition.
  • From the downstream chamber 3 leaves an outlet pipe 9 provided with a stop valve 10 and on which is stuck, upstream of the valve 10, a pipe 11 for filling with argon itself provided with a valve stop 12.
  • the cooler shown in Figures 2 and 3 is of revolution about an axis X-X, assumed to be vertical for the convenience of the description, and comprises an inner tubular core 13 and a double outer shell 14 exposed under vacuum and forming Dewar.
  • An upper head 15 in the form of an inverted cup closes the upper end of the core 13 and of the annular space 16 between the core 13 and the casing 14; the space 16 however communicates with the surrounding atmosphere through a series of holes 17 passing through the head 15.
  • the internal diameters of the core 13 of the envelope 14 are approximately 2.5 mm and 5 mm respectively.
  • a sheath 18 is partially threaded and fixed in the lower end of the core 13.
  • the inner wall of the envelope 14 carries at its lower end a bottom 22 on which is fixed in heat exchange contact an element 23 to be cooled, which can be for example an infrared detector and which is located in space Dewar vacuum. Above the bottom 22 is thus defined a cooling chamber 24 which constitutes the coldest part of the device.
  • a rod 25 is slidably mounted inside the core 13.
  • This rod carries at its lower end a shutter needle 26 and, at its upper end, an electromagnet plunger 27.
  • the needle 26 slides with narrow adjustment in the sheath 19, that is to say with a clearance which, taking into account the coefficients of expansion, is, on the diameter , of the order of a few microns for the cold operating temperature of the cooler.
  • a clearance which, taking into account the coefficients of expansion, is, on the diameter , of the order of a few microns for the cold operating temperature of the cooler.
  • the needle is made of 100 C 6 steel and the sheath is made of bronze-beryllium, there will be a clearance, on the diameter, of 5 to 6 microns at room temperature, which corresponds to a clearance, on the diameter , from 2 to 3 microns at a cold temperature of the order of 80 to 90 K.
  • the plunger 27 slides in the head 15. Around the latter is arranged an electromagnet winding 28, the terminals 29, 30 of which are adapted to be connected to the terminals of a direct current source (not shown).
  • a spring 31 is compressed axially between the bottom of the head 15 and the plunger 27.
  • the rod 25 is guided on the one hand by the needle 26, on the other hand by the plunger 27.
  • a stop 32 for the plunger 27 is provided at the outlet of the head 15.
  • the cooler At rest, the cooler is in the state shown in Figure 3: the electromagnet is not supplied with electric current, so that the spring 31 is relaxed and pushes down the rod 27 to a stop position where the needle 26 closes the orifice 21 to the nearest sliding clearance (5 to 6 microns on the diameter since the device is at room temperature).
  • the valve 10 of the pipe 9 is opened, so that the argon under high pressure is sent into the pipe 19 and is expanded at high flow rate (for example 1000 to 1500 Nl / h) as the orifice 21.
  • high flow rate for example 1000 to 1500 Nl / h
  • the expanded and consequently cooled argon rises between the turns of the pipe 19 until it is discharged into the surrounding atmosphere through the orifices 17, cooling the high pressure argon.
  • the temperature prevailing in the chamber 24 decreases more and more.
  • the pressure drops in chamber 3 of the tank.
  • the pressure of chamber 3 is sufficiently lower than that of chamber 4 (400 bars in this example) to cause the rupture of the foil 6.
  • the nitrogen contained in chamber 4 then flushes out Almost instantaneously from the reservoir, the remainder of argon, then flows at a high flow rate (for example 600 to 800 Nl / h) in line 19 to relax as the orifice 21 passes.
  • a high flow rate for example 600 to 800 Nl / h
  • the electrical supply to the winding 28 is cut, for example by means of a timer, so that the spring 31 instantly returns the rod 25 to its initial position in FIG. 3: the needle 26 closes the orifice 21 and, being pushed laterally by the gas jet leaving this orifice, is at a distance j from the latter equal to the diametral clearance at low temperature, ie 2 to 3 microns with the values numbers indicated above.
  • the flow rate is thus suddenly reduced to a low value, preferably at least ten times lower than its previous value; the pressure drop of the low pressure circuit, which was of the order of a few bars, is reduced by the same amount, which makes it possible to obtain, in chamber 24, liquid nitrogen at a temperature close to the boiling point of nitrogen at atmospheric pressure, i.e. around 80 K.
  • FIG. 4 shows the variation of the temperature in the chamber 24 as a function of time.
  • cooling results solely from the expansion of the argon at high flow rates. As this gas has a significant Joule-Thomson effect, this cooling is very rapid.
  • This time can be chosen to abruptly decrease the nitrogen flow (time t2).
  • the final curve C3 of FIG. 4 is then obtained, which is parallel to the curve C4 corresponding to the case where the entire cooling operation is carried out with nitrogen at low flow rate.
  • This curve C3 is very satisfactory if it is desired to reach a final temperature of between 85 and 90 K. But to descend lower in temperature, it is preferable to allow the nitrogen to flow at a high rate until an instant t3 , posterior to t2, where a certain amount of nitrogen under a few bars has formed in the chamber 24 (point D of FIG. 4). In this case, the reduction in the nitrogen flow causes a very rapid vaporization of part of this liquid (flash effect), the temperature of which drops almost instantaneously in the vicinity of 80 K. We then obtain the final curve C5 of Figure 4.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
EP19870401167 1986-05-26 1987-05-25 Zuleitungsverfahren für einen Joule-Thomson-Kühler und Kühlvorrichtung zu seiner Durchführung Expired - Lifetime EP0247935B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8607449 1986-05-26
FR8607449A FR2599128A1 (fr) 1986-05-26 1986-05-26 Procede d'alimentation d'un refroidisseur joule-thomson et appareil de refroidissement pour sa mise en oeuvre

Publications (2)

Publication Number Publication Date
EP0247935A1 true EP0247935A1 (de) 1987-12-02
EP0247935B1 EP0247935B1 (de) 1990-04-25

Family

ID=9335590

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19870401167 Expired - Lifetime EP0247935B1 (de) 1986-05-26 1987-05-25 Zuleitungsverfahren für einen Joule-Thomson-Kühler und Kühlvorrichtung zu seiner Durchführung

Country Status (4)

Country Link
EP (1) EP0247935B1 (de)
DE (1) DE3762452D1 (de)
ES (1) ES2015309B3 (de)
FR (1) FR2599128A1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0945690A3 (de) * 1998-03-24 1999-11-24 Bodenseewerk Gerätetechnik GmbH Verfahren und Vorrichtung zum Kühlen von Bauteilen, insbesondere von Infrarot-Detektoren bei Suchköpfen
US11001500B2 (en) 2015-06-25 2021-05-11 Irbis Technology LLC Method, apparatus and system for producing granulated solid carbon dioxide

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2991633A (en) * 1958-03-17 1961-07-11 Itt Joule-thomson effect cooling system
US3095711A (en) * 1962-01-31 1963-07-02 Jr Howard P Wurtz Double cryostat
US3320755A (en) * 1965-11-08 1967-05-23 Air Prod & Chem Cryogenic refrigeration system
US3413819A (en) * 1966-05-09 1968-12-03 Hughes Aircraft Co Flow rate control for a joule-thomson refrigerator
US3415078A (en) * 1967-07-31 1968-12-10 Gen Dynamics Corp Infrared detector cooler
FR2095319A1 (fr) * 1970-06-17 1972-02-11 Hymatic Eng Co Ltd Appareils refrigerants cryogeniques
US3714796A (en) * 1970-07-30 1973-02-06 Air Prod & Chem Cryogenic refrigeration system with dual circuit heat exchanger
FR2176544A1 (de) * 1972-03-23 1973-11-02 Air Liquide
US3942010A (en) * 1966-05-09 1976-03-02 The United States Of America As Represented By The Secretary Of The Navy Joule-Thomson cryostat cooled infrared cell having a built-in thermostat sensing element
FR2322337A1 (fr) * 1975-08-26 1977-03-25 Air Liquide Dispositif d'alimentation de refrigerant d'un refrigerateur a circuit ouvert, et systeme de refrigeration comportant un tel dispositif
FR2417733A1 (fr) * 1978-02-17 1979-09-14 Deutsche Forsch Luft Raumfahrt Dispositif a vaporisation d'helium ii, utilise notamment pour porter des objets a tres basse temperature
EP0020111A2 (de) * 1979-05-23 1980-12-10 Air Products And Chemicals, Inc. Anordnung einer kryogenen Kühlvorrichtung und eines Isolierbehälters, und eine mit einer solchen Anordnung versehenen Anlage
GB2085139A (en) * 1980-10-10 1982-04-21 Hymatic Engineering The Co Ltd Cryogenic cooling apparatus
EP0084308A2 (de) * 1982-01-19 1983-07-27 Societe Anonyme De Telecommunications (S.A.T.) Regelvorrichtung für eine nach dem Joule-Thomson-Effekt arbeitende Kühleinrichtung

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE7626566U1 (de) * 1975-08-26 1977-02-03 L'air Liquide, S.A. Pour L'etude Et L'exploitation Des Procedes Georges Claude, Paris Vorrichtung zur speisung einer miniaturkaeltemaschine und kuehlvorrichtung

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2991633A (en) * 1958-03-17 1961-07-11 Itt Joule-thomson effect cooling system
US3095711A (en) * 1962-01-31 1963-07-02 Jr Howard P Wurtz Double cryostat
US3320755A (en) * 1965-11-08 1967-05-23 Air Prod & Chem Cryogenic refrigeration system
US3942010A (en) * 1966-05-09 1976-03-02 The United States Of America As Represented By The Secretary Of The Navy Joule-Thomson cryostat cooled infrared cell having a built-in thermostat sensing element
US3413819A (en) * 1966-05-09 1968-12-03 Hughes Aircraft Co Flow rate control for a joule-thomson refrigerator
US3415078A (en) * 1967-07-31 1968-12-10 Gen Dynamics Corp Infrared detector cooler
FR2095319A1 (fr) * 1970-06-17 1972-02-11 Hymatic Eng Co Ltd Appareils refrigerants cryogeniques
US3714796A (en) * 1970-07-30 1973-02-06 Air Prod & Chem Cryogenic refrigeration system with dual circuit heat exchanger
FR2176544A1 (de) * 1972-03-23 1973-11-02 Air Liquide
FR2322337A1 (fr) * 1975-08-26 1977-03-25 Air Liquide Dispositif d'alimentation de refrigerant d'un refrigerateur a circuit ouvert, et systeme de refrigeration comportant un tel dispositif
FR2417733A1 (fr) * 1978-02-17 1979-09-14 Deutsche Forsch Luft Raumfahrt Dispositif a vaporisation d'helium ii, utilise notamment pour porter des objets a tres basse temperature
EP0020111A2 (de) * 1979-05-23 1980-12-10 Air Products And Chemicals, Inc. Anordnung einer kryogenen Kühlvorrichtung und eines Isolierbehälters, und eine mit einer solchen Anordnung versehenen Anlage
GB2085139A (en) * 1980-10-10 1982-04-21 Hymatic Engineering The Co Ltd Cryogenic cooling apparatus
EP0084308A2 (de) * 1982-01-19 1983-07-27 Societe Anonyme De Telecommunications (S.A.T.) Regelvorrichtung für eine nach dem Joule-Thomson-Effekt arbeitende Kühleinrichtung

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0945690A3 (de) * 1998-03-24 1999-11-24 Bodenseewerk Gerätetechnik GmbH Verfahren und Vorrichtung zum Kühlen von Bauteilen, insbesondere von Infrarot-Detektoren bei Suchköpfen
US11001500B2 (en) 2015-06-25 2021-05-11 Irbis Technology LLC Method, apparatus and system for producing granulated solid carbon dioxide

Also Published As

Publication number Publication date
EP0247935B1 (de) 1990-04-25
FR2599128A1 (fr) 1987-11-27
ES2015309B3 (es) 1990-08-16
DE3762452D1 (de) 1990-05-31

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