Cryocooler interface sleeve for a superconducting magnet and method of use

Information

  • Patent Grant
  • 6438967
  • Patent Number
    6,438,967
  • Date Filed
    Thursday, July 26, 2001
    23 years ago
  • Date Issued
    Tuesday, August 27, 2002
    22 years ago
Abstract
A method for cooling a superconducting device by using a sleeve assembly which thermally interconnects a two stage cryocooler with the device. In operation, the cryocooler is moveable relative to the sleeve assembly between a first configuration wherein the cryocooler is engaged with the sleeve assembly, and a second configuration wherein the cryocooler is disengaged from the sleeve assembly. The cryocooler is disposed in the sleeve assembly with the cooling element of the cryocooler positioned at a distance from the cylinder of the sleeve assembly to establish thermal communication therebetween. Also, the cooling probe of the cryocooler is in contact with the receptacle of the sleeve assembly and is urged against the receptacle to establish thermal communication therebetween. A bellows joins the cryocooler with the sleeve assembly to create an enclosed chamber therebetween and helium is pumped into the sleeve assembly to maintain an operational pressure in the sleeve assembly.
Description




FIELD OF THE INVENTION




The present invention pertains generally to coupling assemblies for thermally connecting a cryocooler with an apparatus that is to be cooled. More particularly, the present invention pertains to a method for cooling a superconducting device by using a sleeve assembly which thermally interconnects two stages of a cryocooler with two different components of a superconducting device simultaneously. The present invention particularly, though not exclusively, pertains to a method for using a sleeve assembly to thermally disconnect the pulse tube, two stage cryocooler from a superconducting device without compromising the thermal condition of the superconducting device.




BACKGROUND OF THE INVENTION




It is well known that superconductivity is accomplished at extremely low temperatures. Even the so-called high temperature superconductors require temperatures which are as low as approximately twenty degrees Kelvin. Other not-so-high temperature superconductors require temperatures which are as low as approximately four degrees Kelvin.




In any case, there are numerous specialized applications for using superconducting devices that require low temperatures. One specialized application, for example, involves medical diagnostic procedures using magnetic resonance imaging (MRI) techniques. When used for medical diagnosis, MRI techniques require the production of a very strong and substantially uniform magnetic field. If superconducting magnets are used to generate this strong magnetic field, some type of refrigeration apparatus will be required to attain the low operational temperatures that are necessary.




To attain the low operational temperatures that are necessary for a superconducting device, the refrigeration apparatus typically includes separate cryogenic units or cryocoolers that are thermally connected with the superconducting device. During operation of the superconducting device, such a connection is essential. There are times, however, when it is desirable for the cryocooler to be selectively disconnected or disengaged from the superconducting device. For example, during repair or routine maintenance of the cryocooler in a refrigeration apparatus, it is much easier to work on the cryocooler when it is disconnected from the superconducting device it has been cooling. Importantly, when so disengaged, the cryocooler can be warmed to room temperature for servicing. Any disengagement of the cryocooler from the superconducting device, however, must allow for a reengagement. Further, it is desirable that the superconducting device be held at a very low temperature during disengagement.




As it is known to persons skilled in the pertinent art, new generation cryocoolers, such as “Pulse Tubes”, cannot be “gutted” out and rebuilt as can the older generation cryocoolers. Instead, these pulse tube cryocoolers must either be entirely replaced or warmed to room temperature for servicing. It is, therefore, necessary for these new generation cryocoolers to use a refrigeration apparatus or a sleeve to cool a superconducting device. Because the entire pulse tube needs to be removed for servicing, the pulse tube cryocoolers cannot be directly and permanently bolted to the sleeve and, thus, the superconducting device. Further, the pulse tube internals cannot be removed independently as they can in many Gifford McMahon (GM) two stage cryocoolers.




For an effective thermal connection, it is known that the efficacy of heat transfer from one body to another body is dependent on several factors. More specifically, the amount of heat (Q) that is conductively transferred through a solid body or conductively transferred from one body to another body through a gas or liquid can be mathematically expressed as:







Q=k


(


A/L





T






In the above expression, k is the coefficient of thermal conductivity; A is the solid bodies cross-sectional area, or the surface area in contact between the two bodies for gas or liquid conduction; L is the solid bodies thermal length or the gap distance between the bodies; and ΔT is the temperature differential across the solid or between the two bodies. From this expression, it can be appreciated that in order to effectively cool one body (e.g. a superconducting device) with another body (e.g. a cryocooler) the transfer of heat, Q, must be accomplished. When the temperature differential between the bodies is desired to be very low, and for a given coefficient of thermal conductivity, it is necessary that the ratio of A/L be sufficiently high.




For any two separate bodies that are in contact with each other, even though they may be forced together under very high pressures, there will always be some average gap distance, L, between the interfacing cross-sectional surface areas of the bodies. For the case wherein there is a vacuum in the gaps, the gaps can create undesirable thermal insulators. Accordingly, it may be beneficial to have these gaps filled with a gas, such as helium. If this is done, heat transfer between the bodies in contact can result from a) solid conduction where there is actual contact between the bodies; b) molecular/gas conduction across the helium-filled gaps; and possibly c) liquid conduction in gaps where the gas has liquefied.




In light of the above, it is an object of the present invention to provide a method for cooling two components of a superconducting device by using a sleeve assembly that thermally interconnects two stages of a pulse tube cryocooler with the superconducting device. Another object of the present invention is to provide a method for cooling a superconducting device by using a sleeve assembly which allows the pulse tube, two stage cryocooler to be thermally disengaged from the superconducting device while the very low temperature of the superconducting device is substantially maintained. Still another object of the present invention is to provide a method for cooling a superconducting device which is effectively easy to implement and comparatively cost effective.




SUMMARY OF THE PREFERRED EMBODIMENTS




The present invention is directed to a method for cooling a superconducting device by using a sleeve assembly which thermally interconnects a pulse tube, two stage cryocooler with a superconducting device. For the present invention, the sleeve assembly has a heat transfer cylinder, a heat transfer receptacle and a midsection which interconnects the heat transfer cylinder with the heat transfer receptacle.




In more detail, the midsection of the sleeve assembly is hollow and elongated and defines a passageway between the heat transfer cylinder and the heat transfer receptacle. The heat transfer cylinder of the present invention is also hollow and is annular-shaped, having an inner surface and an outer surface. The heat transfer receptacle is formed with a recess and has an inner surface and an outer surface. Importantly, the inner surface of the heat transfer receptacle that defines the recess is tapered. Both the heat transfer cylinder and heat transfer receptacle are preferably made of copper, aluminum or any other high thermal conductivity material. Furthermore, the midsection of the sleeve assembly is preferably made of stainless steel or any other low thermal conductivity material known in the art.




The structure of the sleeve assembly is dimensioned for the engagement with a cryocooler which includes a cooling element and a tapered cooling probe. As contemplated for the present invention, the cryocooler is moveable relative to the sleeve assembly between a first configuration wherein the cryocooler is engaged with the sleeve assembly, and a second configuration wherein the cryocooler is disengaged from the sleeve assembly. Specifically, the two stages of the cryocooler will thermally engage and disengage with the two components of the superconducting device simultaneously through the sleeve assembly.




In operation, the sleeve assembly is engaged with the cryocooler when the cryocooler is juxtaposed with the sleeve assembly to establish thermal communication between the cryocooler and the superconducting device through the sleeve assembly. In more detail, when juxtaposed, the tapered cooling probe of the cryocooler is urged against the heat transfer receptacle of the sleeve assembly to establish thermal communication therebetween. As stated above, the inner surface of the heat transfer receptacle is tapered for mating engagement with the tapered cooling probe of the cryocooler. This engagement, however, will not be perfect. Always, there is an average gap distance between the inner surface of the heat transfer receptacle and the tapered cooling probe of the cryocooler. As contemplated for the present invention, this gap distance varies within the range between zero and approximately two thousandths of an inch (0-0.002 inches). Importantly, under these conditions, the gap ratio, A/L, in the above expression for Q will be in the range between approximately 10,000 in


2


/in to approximately 50,000 in


2


/in. Consequently, there can be effective heat flow, Q, even though the temperature differential, ΔT, between the heat transfer receptacle and the tapered cooling probe is small.




When the cryocooler is engaged with the sleeve assembly (first configuration), the cooling element of the cryocooler is positioned at a very small gap distance from the inner surface of the heat transfer cylinder. Importantly, this gap distance needs to be small enough to establish effective thermal communication between the cooling element and the heat transfer cylinder. For the present invention, this gap distance will vary within the range between approximately one thousandth of an inch to approximately five thousandths of an inch (0.001-0.005 inches). Although the gap ratio, A/L, in this case will be higher than it is for the receptacle/probe interface, there will still be effective heat flow, Q.




In order for the cryocooler and sleeve assembly to move between the first (engaged) and second (disengaged) configurations, an expandable bellows is provided which joins the heat transfer cylinder of the sleeve assembly with the room temperature section of the cryocooler and creates an enclosed chamber therebetween. In operation, the bellows allows the cryocooler to be separated from the sleeve assembly with a space therebetween which will maintain a gaseous thermal insulation between the cryocooler and the sleeve assembly. Stated another way, there will be sufficient thermal insulation between the sleeve assembly and the cryocooler to maintain the sleeve assembly at a substantially same low temperature when the cryocooler is disengaged from the sleeve assembly and is warmed to room temperature.




It is important for the sleeve assembly to maintain two substantially low temperatures for it to continually cool the two separate components of the superconducting device. To do this, the sleeve assembly of the present invention is operationally connected to the superconducting device by a proximal conductor and a distal conductor. In more detail, the proximal conductor is attached between the outer surface of the heat transfer cylinder and a thermal shield of the superconducting device to establish thermal communication therebetween. Further, the distal conductor is attached between the outer surface of the heat transfer receptacle and the superconducting wires of the superconducting device to establish thermal communication therebetween.




By way of a pipe, helium gas is pumped selectively into and from the chamber of the sleeve assembly. As contemplated for the present invention, the introduction of helium gas into the space between the cryocooler and the sleeve assembly will prevent a vacuum from forming when the cryocooler is disengaged and displaced from the sleeve assembly. Also, helium gas is useful to establish molecular conduction between the sleeve assembly and the cryocooler for an effective thermal connection therebetween when these two components are engaged with each other.











BRIEF DESCRIPTION OF THE DRAWINGS




The novel features of this invention, as well as the invention itself, both as to its structure and its operation, will be best understood from the accompanying drawings, taken in conjunction with the accompanying description, in which similar reference characters refer to similar parts, and in which:





FIG. 1

is a schematic, perspective view of the sleeve assembly of the present invention engaged with a pulse tube, two stage cryocooler and shown operationally connected to a superconducting device, with portions broken away for clarity;





FIG. 2

is a perspective exploded view showing the sleeve assembly of the present invention in its structural relationship with a pulse tube, two stage cryocooler;





FIG. 3A

is a cross-sectional view of the sleeve assembly and pulse tube, two stage cryocooler operationally engaged with each other as would be seen along the line


3





3


in

FIG. 1

; and





FIG. 3B

is a cross-sectional view of the sleeve assembly and pulse tube, two stage cryocooler as seen in

FIG. 3A

when they are operationally disengaged from each other for the purposes of servicing the cryocooler.











DESCRIPTION OF THE PREFERRED EMBODIMENT




Referring initially to

FIG. 1

, a cooling system according to the present invention is shown and generally designated


10


. More specifically, the cooling system


10


includes a sleeve assembly


12


which thermally interconnects a pulse tube, two stage cryocooler


14


with a superconducting device


16


. As also shown, a helium source


18


is connected via a pipe


19


to the sleeve assembly


12


. As intended for the present invention, the sleeve assembly


12


is an easily operated means for thermally connecting and disconnecting the cryocooler


14


from the superconducting device


16


.




As shown in

FIG. 2

, the pulse tube, two stage cryocooler


14


has a valve motor body


17


having a first stage


20


(first cryocooler station) aligned with a second stage


22


(second cryocooler station). A cooling element


24


is disposed between the stages


20


and


22


and is in thermal communication with the first stage


20


. As shown, a tapered cooling probe


26


extends from the second stage


22


and is in thermal communication with the second stage


22


. As intended for the present invention, the second stage


22


maintains a temperature of approximately four degrees Kelvin (4° K) and cools the tapered cooling probe


26


to that same low temperature. Further, the first stage


20


maintains a temperature of approximately forty degrees Kelvin (40° K) and cools the cooling element


24


to that same temperature. Preferably, the cooling element


24


and the tapered cooling probe


26


of the cryocooler


14


can be both made of copper, aluminum or any other known high thermal conductivity material. A bellows


28


having a flange


29


is shown attached, with the flange


29


, to the cryocooler


14


. The pipe


19


that interconnects the helium source


18


with the sleeve assembly


12


is attached through the bellows flange


29


as shown in FIG.


1


.




Still referring to

FIG. 2

, it will be seen that the sleeve assembly


12


includes a heat transfer receptacle


30


, a heat transfer cylinder


32


and a midsection


34


which interconnects the heat transfer receptacle


30


with the heat transfer cylinder


32


. It is important for the heat transfer receptacle


30


to be dimensioned to receive the tapered cooling probe


26


of the cryocooler


14


. Similarly, the heat transfer cylinder


32


is dimensioned to receive the cooling element


24


of the cryocooler


14


. The details of the structure of the sleeve assembly


12


can perhaps be best seen in

FIGS. 3A and 3B

.




In

FIGS. 3A and 3B

, the heat transfer receptacle


30


of the sleeve assembly


12


is formed with a recess


36


and has an inner surface


38


and an outer surface


40


. Importantly, the inner surface


38


of the heat transfer receptacle


30


that defines the recess


36


is tapered. As also shown in

FIGS. 3A and 3B

, the midsection


34


of the sleeve assembly


12


is hollow and elongated and defines a passageway


42


between the heat transfer receptacle


30


and the heat transfer cylinder


32


. The heat transfer cylinder


32


is also hollow and is annular-shaped, having an inner surface


44


and an outer surface


46


. Preferably, the heat transfer receptacle


30


and the heat transfer cylinder


32


can be made of copper, aluminum or any other high thermal conductivity material. The midsection


34


of the sleeve assembly


12


can be made of stainless steel or any other low thermal conductivity material.




Referring back to

FIG. 1

, the sleeve assembly


12


is shown connected to two components of the superconducting device


16


by a proximal conductor


52


and a distal conductor


54


. In more detail, the proximal conductor


52


has a first end


56


and a second end


58


and the distal conductor


54


also has a first end


62


and a second end


64


. The first end


56


of the proximal conductor


52


is attached to the outer surface


46


of the heat transfer cylinder


32


and the second end


58


is attached to the thermal shield


60


of the superconducting device


16


as shown in FIG.


1


. Similarly, the first end


62


of the distal conductor


54


is attached to the outer surface


40


of the heat transfer receptacle


30


and the second end


64


is attached to the wire


68


of the superconducting device


16


as shown in FIG.


1


.




As shown in

FIG. 3A

, the flange


29


of expandable bellows


28


joins the room temperature flange


66


of cryocooler


14


with the heat transfer cylinder


32


of the sleeve assembly


12


by any means known in the art. With this interconnection, an enclosed chamber


50


is created between the sleeve assembly


12


and the cryocooler


14


. (see FIG.


3


B). Also, an elongated, thin stainless steel tube


48


is disposed between the bellows


28


and the heat transfer cylinder


32


. Helium gas is pumped from the helium source


18


through the bellows flange


29


and into the chamber


50


. Importantly, the bellows


28


, with the helium gas present in the chamber


50


, creates an air-lock seal between the sleeve assembly


12


and the cryocooler


14


to isolate the external environment from the superconducting device


16


.




The cooperation of the sleeve assembly


12


of the present invention and the cryocooler


14


can perhaps be best appreciated by cross referencing

FIGS. 3A and 3B

. Specifically, the cryocooler


14


is moveable relative to the sleeve assembly


12


between a first configuration wherein the cryocooler


14


is engaged with the sleeve assembly


12


(

FIG. 3A

) and a second configuration wherein the cryocooler


14


is disengaged with the sleeve assembly


12


(FIG.


3


B). Importantly, the first stage


20


and the second stage


22


of the cryocooler


14


engage and disengage simultaneously with the sleeve assembly


12


. It is to be appreciated that when the cryocooler


14


is engaged with the sleeve assembly


12


, the area to gap distance ratio, A/L, is very big. Specifically, when there is an engagement, the A/L is typically in the range between approximately 10,000 in


2


/in to approximately 50,000 in


2


/in and, thus, there is a very small temperature differential ΔT. When the cryocooler


14


is disengaged from the sleeve assembly


12


, the A/L will be in the range between approximately 10 in


2


/in to approximately 50 in


2


/in. In this case where A/L is small, the ΔT is very big and, as a result, the transfer of heat, Q, is effectively not accomplished.





FIG. 3A

shows the tapered cooling probe


26


of the cryocooler


14


urged against the recess


36


of the heat transfer receptacle


30


to establish thermal communication therebetween. As mentioned above, the heat transfer receptacle


30


is tapered for mating engagement with the tapered cooling probe


26


with a gap distance


70


between all of their respective interfacing surfaces. In general, this gap distance


70


between the tapered cooling probe


26


and the inner surface


38


of the heat transfer receptacle


30


may vary within a range between zero and approximately two thousandths of an inch (0-0.002 inches). Importantly, helium molecular/gas or liquid conduction is established through gap distance


70


.

FIG. 3A

also shows the cooling element


24


of the cryocooler


14


positioned at a very small gap distance


72


from the inner surface


44


of the heat transfer cylinder


32


. It is important for this gap distance


72


to be small enough to establish effective molecular/gas conduction through helium gas between the cooling element


24


and the heat transfer cylinder


32


. On the other hand, there needs to be sufficient gap distance


72


for the cooling element


24


to be inserted into the heat transfer cylinder


32


. As contemplated for the present invention, this gap distance


72


will vary within a range between approximately one thousandth of an inch to approximately five thousandths of an inch (0.001-0.005 inches).





FIG. 3B

shows the cryocooler


14


disengaged with the sleeve assembly


12


. The bellows


28


allows the cryocooler


14


to be separated from the sleeve assembly


12


. There will be sufficient thermal insulation between the sleeve assembly


12


and the cryocooler


14


to maintain the sleeve assembly


12


at a substantially same low temperature when the cryocooler


14


is disengaged with the sleeve assembly


12


. Meanwhile, the sleeve assembly


12


will remain in thermal communication with the superconducting device


16


.




Operation




In the operation of the sleeve assembly


12


of the present invention, reference is first made to

FIG. 2

wherein the pulse tube, two stage cryocooler


14


is shown being disposed the sleeve assembly


12


. In more detail, as shown in

FIG. 3B

, the tapered cooling probe


26


of the cryocooler


14


is passed through the passageway


42


of the sleeve assembly


12


and is inserted into the recess


36


of the heat transfer receptacle


30


as shown in FIG.


3


A. The cryocooler


14


is placed in the sleeve assembly


12


and is bolted to the bellows flange


29


. When the tapered cooling probe


26


contacts the heat transfer receptacle


30


, the second stage


22


of the cryocooler


14


is disposed in the passageway


42


of the sleeve assembly


12


. Furthermore, the cooling element


24


of the cryocooler


14


is disposed in the heat transfer cylinder


32


of the sleeve assembly


12


. Importantly, when the cryocooler


14


is engaged with the sleeve assembly


12


, the A/L is very big. Specifically, A/L is typically in the range between approximately 10,000 in


2


/in to approximately 50,000 in


2


/in and therefore, the temperature differential, ΔT, between the cryocooler


14


and the sleeve assembly


12


, is very small.




As shown in

FIG. 1

, the superconducting device


16


is in thermal communication with the sleeve assembly


12


which, in turn, is in thermal communication with the cryocooler


14


. Stated differently, thermal communication is established between the cryocooler


14


and the superconducting device


16


through the sleeve assembly


12


. In more detail, via the distal conductor


54


, the tapered cooling probe


26


will cool the wire


68


of the superconducting device


16


to approximately four degrees Kelvin (4° K). Similarly, via the proximal conductor


52


, the cooling element


24


of the cryocooler


14


will cool the thermal shield


60


of the superconducting device


16


to approximately forty degrees Kelvin (40° K).




During the engagement or disengagement of the cryocooler


14


with the sleeve assembly


12


, helium gas is pumped into the sleeve assembly


12


to establish molecular conduction between the cryocooler


14


and the sleeve assembly


12


. Importantly, helium gas allows the three orders in magnitude difference in the A/L to act like a switch. This switch operation, therefore, allows for the engaging and disengaging between the cryocooler


14


and the sleeve assembly


12


, as desired. Helium gas will also maintain an operational pressure between the sleeve assembly


12


and the cryocooler


14


as the cryocooler


14


moves between the first and second configurations.




To disengage the cryocooler


14


from the sleeve assembly


12


and to disconnect thermal communication therebetween, the cryocooler


14


is lifted from the sleeve assembly


12


by any mechanical means known in the art. The cryocooler


14


, however, is not removed from the sleeve assembly


12


. Instead, the cryocooler


14


is lifted just enough to thermally disconnect the cryocooler


14


from the sleeve assembly


12


. It is important to note that when the cryocooler


14


is lifted from the sleeve assembly


12


, the first stage


20


and the second stage


22


are simultaneously disengaged from their respective positions in the sleeve assembly


12


, which, in turn, are simultaneously disengaged with their respective thermal communication with the superconducting device


16


.




Upon thermal disengagement between the cryocooler


14


and the sleeve assembly, it is important to appreciate that the A/L between the two bodies becomes very small. Specifically, A/L is in the range between approximately 10 in


2


/in to approximately 50 in


2


/in. As a result, ΔT is very big, and the transfer of heat is relatively insignificant.




As indicated above, the bellows


28


interconnects the cryocooler


14


with the sleeve assembly


12


to create a chamber


50


therebetween. Other than the bellows


28


, there is no other mechanical connection between the sleeve assembly


12


and the cryocooler


14


. Importantly, when the cryocooler


14


is disengaged from the sleeve assembly


12


, A/L goes from being very large (approximately 10,000 in


2


/in-approximately 50,000 in


2


/in) to very small (approximately 10 in


2


/in-approximately 50 in


2


/in). As a result of this, thermal isolation is create. Furthermore, the bellows


28


maintains sufficient thermal insulation between the cryocooler


14


and the sleeve assembly


12


for the sleeve assembly


12


to maintain its substantially same low temperature.




Upon thermal disconnection between the cryocooler


14


and the sleeve assembly


12


, the cryocooler


14


is warmed to room temperature for servicing. Meanwhile, the sleeve assembly


12


will remain in thermal communication with the superconducting device


16


. Importantly, the superconducting device


16


will tend to maintain its cold temperature during disengagement (i.e. 4° Kelvin for the superconducting wires and 40° K for the thermal shield).




When the cryocooler


14


is disengaged from the sleeve assembly


12


for servicing, the cryocooler


14


will tend to expand as it is warmed to room temperature. It is, therefore, necessary to recool the cryocooler


14


prior to reengaging the cryocooler


14


with the sleeve assembly


12


in order for the cryocooler


14


to fit into the sleeve assembly


12


. To do this, the stages


20


and


22


of the cryocooler


14


will cool the tapered cooling probe


26


and the cooling element


24


respectively and to their respective low temperatures. The cooled cryocooler


14


is then reengaged with the sleeve assembly


12


to establish thermal communication therebetween.




While the particular Cryocooler Interface Sleeve for a Superconducting Magnet and Method of Use as herein shown and disclosed in detail is fully capable of obtaining the objects and providing the advantages herein before stated, it is to be understood that it is merely illustrative of the presently preferred embodiments of the invention and that no limitations are intended to the details of construction or design herein shown other than as described in the appended claims.



Claims
  • 1. A method for cooling portions of a superconducting device to temperatures below approximately six degrees Kelvin, said method comprising the steps of:providing a cryocooler; joining said cryocooler with a sleeve to create an enclosed chamber therebetween; connecting said superconducting device with said sleeve for heat transfer therebetween; and selectively juxtaposing said cryocooler with said sleeve to establish thermal communication between said cryocooler and said superconducting device through said sleeve, via a conductor interconnecting said sleeve to said superconducting device.
  • 2. A method as recited in claim 1 further comprising the step of pumping helium selectively into and from said chamber to maintain an operational pressure in said chamber and establish molecular conduction between said cryocooler and said sleeve.
  • 3. A method as recited in claim 1 wherein said sleeve comprises a cylinder, a receptacle and a wall interconnecting said cylinder and said receptacle.
  • 4. A method as recited in claim 3 wherein said cylinder and said receptacle are made of copper and said wall is made of stainless steel.
  • 5. A method as recited in claim 3 wherein said juxtaposing step further comprises the steps of:positioning a cooling element of said cryocooler at a first distance from said cylinder of said sleeve; and urging a cooling probe of said cryocooler against said receptacle of said sleeve with a second distance therebetween.
  • 6. A method as recited in claim 1 wherein said connecting step between said sleeve and said superconducting device is accomplished with a first conductor being attached to an outer surface of said cylinder and a second conductor being attached to an outer surface of said receptacle, and wherein each said conductor is attached to said superconducting device.
  • 7. A method as recited in claim 1 wherein said joining step is accomplished using a bellows attached between said cylinder of said sleeve and said cryocooler to create said chamber.
  • 8. A method as recited in claim 5 wherein said first distance between said cooling element and said cylinder is in a range between approximately one thousandth of an inch to approximately five thousandths of an inch (0.001-0.005 inches) and further wherein said second distance between said cooling probe and said receptacle varies within a range between zero and approximately two thousandths of an inch (0-0.002 inches).
  • 9. A method as recited in claim 1 wherein said cryocooler is a pulse tube, two stage cryocooler.
  • 10. A method for cooling a superconducting device comprising the steps of:providing a cooling means formed with a probe; connecting a receptacle in thermal communication with said superconducting device via a conductor; selectively juxtaposing said probe of said cooling means with said receptacle to establish thermal communication therebetween to draw heat from said superconducting device, through said conductor and said receptacle, and into said cooling means to cool said superconducting device; and maintaining a thermal insulation between said receptacle and said cooling means whenever said cooling means is distanced from said probe.
  • 11. A method as recited in claim 10 wherein said receptacle is tapered for mating engagement with said probe of said cooling means and further wherein said probe is substantially in contact with said receptacle.
  • 12. A method as recited in claim 10 wherein said connecting step is accomplished with a first conductor having a first end and a second end and further wherein said first end is attached to said receptacle and said second end is attached to said superconducting device to establish thermal communication therebetween.
  • 13. A method as recited in claim 10 further comprising the steps of:interconnecting a cylinder to said receptacle by a wall therebetween to define a sleeve, said sleeve having a chamber therein; linking said cylinder in thermal communication with said superconducting device; and selectively disposing a cooling element of said cooling means in said cylinder to establish thermal communication therebetween to draw heat from said superconducting device, through said cylinder, and into said cooling means to cool said superconducting device.
  • 14. A method as recited in claim 13 further comprising the step of pumping helium selectively into and from said chamber to maintain an operational pressure in said chamber and establish molecular conduction between said cooling means and said sleeve.
  • 15. A method as recited in claim 13 wherein said cooling element is disposed at a distance from said cylinder, said distance being in a range between approximately one thousandth of an inch to approximately five thousandths of an inch (0.001-0.005 inches).
  • 16. A method as recited in claim 13 wherein said linking step is accomplished with a second conductor having a first end and a second end and further wherein said first end is attached to said cylinder and said second end is attached to said superconducting device to establish thermal communication therebetween.
  • 17. A method for cooling a superconducting device which comprises the steps of:providing a pulse tube, two stage cryocooler having a cooling element and a tapered cooling probe; connecting said superconducting device with a sleeve for heat transfer therebetween, said sleeve having a receptacle, a cylinder and a wall interconnecting said receptacle and said cylinder; joining said sleeve with said cryocooler to create an enclosed chamber therebetween; pumping helium selectively into and from said chamber to maintain an operational pressure in said chamber and establish molecular conduction and to maintain pressure balance between said sleeve and said cryocooler; and selectively moving said cryocooler relative to said sleeve between a first configuration wherein said sleeve is engaged with said cryocooler, where said tapered cooling probe is urged against said receptacle to establish thermal communication therebetween and said cooling element is positioned in said cylinder to establish thermal communication therebetween, and a second configuration wherein said cryocooler is disengaged from said sleeve.
  • 18. A method as recited in claim 17 wherein said joining step is accomplished using a bellows attached between said cylinder of said sleeve and said cryocooler to maintain thermal insulation therebetween when said sleeve is in said second configuration.
  • 19. A method as recited in claim 17 wherein said receptacle is tapered for mating engagement with said tapered cooling probe of said cryocooler and further wherein said tapered cooling probe is substantially in contact with said receptacle when said sleeve is in said first configuration.
  • 20. A method as recited in claim 17 wherein said cooling element of said cryocooler is positioned at a distance from said cylinder when said sleeve is in said first configuration and further wherein said distance is in a range between approximately one thousandth of an inch to approximately five thousandths of an inch (0.001-0.005 inches).
Parent Case Info

This application is a continuation of application Ser. No. 09/881,642 filed Jun. 13, 2001, which is currently pending. The contents of application Ser. No. 09/881,642 are incorporated herein by reference.

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4344302 Jarrett et al. Aug 1982 A
4501131 Gaskin et al. Feb 1985 A
5386870 Nieman et al. Feb 1995 A
5680768 Rattray et al. Oct 1997 A
6029458 Eckels Feb 2000 A
6038867 Einzinger et al. Mar 2000 A
6256999 Chase Jul 2001 B1
6305174 Binneberg et al. Oct 2001 B1
Continuations (1)
Number Date Country
Parent 09/881642 Jun 2001 US
Child 09/915916 US