U.S. patent number 3,882,687 [Application Number 05/435,856] was granted by the patent office on 1975-05-13 for method of and apparatus for the cooling of an object.
This patent grant is currently assigned to Linde Aktiengesellschaft. Invention is credited to Stefan Asztalos, Reinhard Glatthaar, Rudolf Kneuer, Alfred Stephan.
United States Patent |
3,882,687 |
Asztalos , et al. |
May 13, 1975 |
Method of and apparatus for the cooling of an object
Abstract
An object, such as a superconductive magnet or a super-conductor
cable in a housing or cryostat, is cooled with a cryogenic fluid
passed continuously from one vessel into the housing or cryostat
and then conducted after expansion into a second vessel where part
of the cryogenic liquid is converted to vapor by expansion. A
vapor/liquid separation is carried out in the second vessel and the
liquid phase is delivered to a third vessel serving as a storage
reservoir and intermittently connected to the first vessel to
return liquid coolant thereto. During the accumulation of liquid in
the third vessel, both the second and third vessels are maintained
at a pressure lower than that in the first vessel, the pressure
difference driving the liquid coolant through the housing or
cryostat.
Inventors: |
Asztalos; Stefan (Munich,
DT), Kneuer; Rudolf (Walchstadt, Icking,
DT), Stephan; Alfred (Munich, DT),
Glatthaar; Reinhard (Munich, DT) |
Assignee: |
Linde Aktiengesellschaft
(Wiesbaden, DT)
|
Family
ID: |
5869964 |
Appl.
No.: |
05/435,856 |
Filed: |
January 23, 1974 |
Foreign Application Priority Data
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|
|
|
|
Jan 25, 1973 [DT] |
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2303663 |
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Current U.S.
Class: |
62/50.5; 62/50.7;
62/51.1; 62/376; 62/512; 505/897; 505/899; 62/64 |
Current CPC
Class: |
F25D
3/10 (20130101); Y10S 505/899 (20130101); Y10S
505/897 (20130101) |
Current International
Class: |
F25D
3/10 (20060101); F25J 1/00 (20060101); F25d
017/02 () |
Field of
Search: |
;62/45,50-55,467,512,514,62,64,376,218 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Perlin; Meyer
Assistant Examiner: Capossela; Ronald C.
Attorney, Agent or Firm: Ross; Karl F. Dubno; Herbert
Claims
We claim:
1. A method of cooling an object to be maintained at a cryogenic
temperature comprising the steps of: continuously feeding a liquid
cryogen from a supply vessel to said object; maintaining a pressure
in said vessel sufficient to displace said liquid cryogen to said
object; expanding liquid cryogen upon its passage to said object to
form a vapor/liquid phase mixture of the liquid cryogen; separating
said phase mixture into a liquid phase and a vapor phase in a
second vessel; transferring the liquid phase from said second
vessel directly to a third storage vessel; and at least
intermittently feeding said liquid cryogen from said storage vessel
to said supply vessel upon the liquid level in said storage vessel
attaining a predetermined height and at substantially the pressure
in said supply vessel.
2. The method defined in claim 1 wherein a first valve is provided
between said storage vessel and said supply vessel and a second
valve is provided between said second vessel and said storage
vessel, said method further comprising the step of controlling said
valves in response to the liquid level in said storage vessel.
3. The method defined in claim 1, further comprising the step of
super-cooling the liquid cryogen from said supply vessel prior to
its use to cool said object in heat exchange with the expanded
cryogen.
4. The method defined in claim 1, further comprising the step of
shielding the liquid cryogen in contact with said object with the
expanded cryogen.
5. The method defined in claim 1, further comprising the step of
shielding the liquid cryogen between said supply vessel and said
object with the expanded cryogen.
6. The method defined in claim 1 wherein a radiation shield is
provided around said object, said method further comprising the
step of cooling said radiation shield with the vapor phase
separated from said liquid phase.
7. An apparatus for cooling an object, comprising a supply vessel
for a liquid cryogen; conduit means connecting said supply vessel
with said object; an expansion valve receiving liquid cryogen from
said object; a second vessel communicating with said expansion
valve and receiving a vapor-liquid phase mixture of said cryogen
therefrom; a storage vessel connected to said supply vessel for
delivering liquid cryogen thereto; and means connecting said second
vessel to said storage vessel for delivering said liquid cryogen to
said storage vessel upon its separation from the vapor phase of
said mixture in response to the liquid level in said storage
vessel.
8. The apparatus defined in claim 7 further comprising a heat
exchanger having a first section traversed by the liquid cryogen
between said supply vessel and said object and a second section
traversed by a vapor-liquid phase mixture from said expansion valve
for super-cooling the liquid cryogen prior to the use thereof to
cool said object.
9. The apparatus defined in claim 7, further comprising a radiation
shield surrounding said object and means for passing the
vapor-liquid phase mixture formed upon expansion of said liquid
cryogen in said expansion valve into heat exchanging relation with
said radiation shield.
10. An apparatus for cooling an object, comprising a supply vessel
for a liquid cryogen; conduit means connecting said supply vessel
with said object; an expansion valve receiving liquid cryogen from
said object; a second vessel communicating with said expansion
valve and receiving a vapor-liquid phase mixture of said cryogen
therefrom; a storage vessel connected to said supply vessel for
delivering liquid cryogen thereto; and means connecting said second
vessel to said storage vessel for delivering said liquid cryogen to
said storage vessel upon its separation from the vapor phase of
said mixture a valve being provided between said second vessel and
said third vessel and another valve being provided between said
second vessel and said storage vessel and another valve being
provided between said storage vessel and said supply vessel, said
apparatus further comprising a liquid level sensor in said storage
vessel for controlling said valves.
11. The apparatus defined in claim 10 wherein a pressure control
device is provided for regulating the relative pressures in said
vessels above that in said supply vessel to displace liquid cryogen
from said storage vessel to said supply vessel.
12. The apparatus defined in claim 10 wherein said conduit means
comprises a central passage traversed by the liquid cryogen and a
plurality of annular passages surrounding said central passage, at
least one of said annular passages being connected to one of said
vessels for passage of cryogenic fluid therethrough.
Description
FIELD OF THE INVENTION
Our present invention relates to a method of and an apparatus for
the cooling of an object such as a superconductive magnet or a
superconductive cable in a housing or cryostat with a liquid
coolant, e.g. liquid helium.
BACKGROUND OF THE INVENTION
The deep cooling of objects has been found to be especially
advantageous in recent years for the cooling of conductors in
electrical systems, the conductivity of a conductor increasing as
its temperature is reduced in the great majority of cases. The
development of superconductive materials has caused increasing
interest in cooling systems adapted to reach superconductive
temperatures, i.e. temperatures of 14.degree.k or below and in the
handling of cryogenic liquids, i.e. liquefied gases capable of
reaching these low temperatures.
Superconductors are used, for example, in magnets of particle
accelerators and other systems in which high magnetic field
strengths must be developed and an increasing cross-section of the
conductor cannot be tolerated either because of high cost or other
factors. Moreover, superconductors are used in cables for the
transmission of large currents over both small and large
distances.
A typical cryogenic-liquid-cooled cable may comprise a plurality of
coaxial ducts in which the superconductor is received in the inner
duct and an outer space is evacuated and/or provided with so-called
superinsulation composed of alternating layers of fiberous material
and reflective foil. The cryogenic liquid or cryogen is caused to
flow through the innermost duct in direct contact or
heat-exchanging relation with the superconductor.
Superconductor magnets are often enclosed in highly insulated
housings or cryostats to which the superconductive liquid is
admitted.
In a conventional process for the cooling of objects enclosed in a
housing, e.g. a duct or cryostat, it has been the practice to
supply liquid helium from a first storage vessel to the housing and
to conduct the liquid after it has traversed the housing into a
second storage vessel. A pressure differential, produced by some
pressure buildup means, is maintained across the vessels to obtain
the driving pressure necessary to displace the liquid from the
first vessel to the housing and thence to the second vessel. When
the first vessel is emptied, the pressure differential is reversed
and the liquid now collected in the second vessel is displaced by
the opposite pressure differential through the housing and into the
first vessel in the opposite direction.
The disadvantage of this system is that the housing cannot be
supplied for prolonged periods continuously with the cryogenic
liquid from one vessel and hence there are periods in which the
flow of the cryogen must be interrupted. This, of course, has the
disadvantage that uniform flow and cooling cannot be guaranteed and
that even brief interruptions in the continuity of coolant flow may
cause detrimental results when the cooled object is a
superconductive magnet or superconductive cable.
OBJECTS OF THE INVENTION
It is, therefore, the principal object of the present invention to
provide a process for the cooling of an object in a housing, e.g. a
superconductive magnet in the cryostat or a superconductive cable,
whereby the aforementioned disadvantages are obviated.
Another object of the invention is to provide an apparatus or
system for the cooling of objects with a liquid cryogen whereby the
continuity of flow to the cooled object from a supply vessel can be
maintained for much longer periods than heretofore.
Yet another object of the invention is to provide a method of an
apparatus for the continuous supply of a cryogen to and effective
cooling of an object to be cooled, especially a superconductive
system, for long periods and with a single supply vessel serving as
the source of the liquid cryogen to the housing of the object to be
cooled.
SUMMARY OF THE INVENTION
These objects and others which will become apparent hereinafter are
attained, in accordance with the present invention, in a method of
cooling an object in a housing, especially a superconductive magnet
or a superconductive cable, which comprises feeding a cryogenic
liquid from a first or supply vessel to the housing, collecting
cyrogenic liquid from said housing in a second vessel, expanding
the liquid in said second vessel to cool the liquid and separating
a vapor phase from the liquid phase of said second vessel, feeding
the liquid phase to a third storage vessel and at least
intermittently returning liquid from the storage vessel to the
supply vessel.
In other words, the present invention provides for expansion of the
liquid cryogen or coolant, after it has been used to cool the
object, thereby lowering the temperature of the liquid phase and
abstracting heat therefrom equivalent to the latent heat of
vaporization of the cryogen. Thereafter a phase separation is
carried out whereby the liquid component is collected in the third
or storage vessel and is resupplied to the first.
The system of the present invention is thus able to achieve, in a
simple manner, the aforestated object of permitting one-way,
continuous and long duration cooling of an object, e.g. a
superconductive system, with a liquid coolant or cryogen, e.g.
liquid helium.
The liquid coolant is displaced through the system under
appropriate driving pressures and thus, according to the present
invention, the pressure differential between the first and second
vessels is maintained at a level necessary to drive the liquid
cryogen from the first vessel through the cryostat or housing of
the object and into the second vessel.
During the accumulation of the liquid in the storage vessel, the
latter is maintained at the same pressure as the second vessel,
i.e. at a pressure lower than that in the first vessel. Even the
expansion step within the second vessel takes place to a pressure
below that in the first vessel.
As soon as the third or storage vessel is filled to a sufficient
degree with the liquid cryogen recovered from the first separation
in the second vessel, the connection between the second and third
vessels is closed with a valve and a valve between the third vessel
and the first or supply vessel is opened. The pressure is developed
in the third or storage vessel which is somewhat higher than the
pressure maintained in the first vessel to drive the liquid cryogen
into the latter.
When the third vessel is completely or partly emptied or discharges
into the first vessel, the valve between them is again closed and
simultaneously the second valve is opened so that the pressure in
the third vessel again assumes a level identical to that in the
second vessel and the liquid coolant can flow from the second
vessel to the third. Consequently, the second vessel serves for
temporary storage of the liquid phase only during the period in
which the third vessel is being discharged into the first.
The pressure differential required to drive the liquid from the
first vessel to the second and from the third vessel to the first
as described above can be generated by a pressure buildup means of
any conventional design.
An important feature of the present invention resides in the fact
that, during the two switch-over phases, i.e. the filling of the
third or storage vessel and the discharge of the storage vessel
into the supply vessel, the displacement of the liquid cryogen from
the first or supply vessel to housing of the object to be cooled is
neither influenced nor completely interrupted. The object to be
cooled is thus subjected to a continuous flow of the liquid cryogen
at a constant rate from a single supply vessel for long periods,
i.e. until all of the liquid cryogen has been converted into
vapor.
The method of the present invention has been found to be especially
advantageous, for the cooling of superconductive systems such as
conductive magnets, superconductive cables or the like.
According to another feature of the present invention the first
valve between the third (storage) and first (supply) vessels and
the second valve between the second (phase-separation and
liquid-collection) and third vessels can be controlled by a
liquid-level indicator, sensor or controller responsive to the
liquid level in the third or storage vessel and having upper and
lower threshold values.
As soon as the liquid level in the third or storage vessel reaches
the upper threshold valve, the level indicator or sensor generates
a first pulse to close the second valve and open the first valve
while energizing or operating the pressure control device for the
third vessel to bring the pressure entrainment to a level above
that in the first vessel. The pressure differential between the
third and first vessels can thus displace the accumulated liquid
cryogene and coolant into the first vessel.
Conversely, when the liquid-level senses a liquid level in the
third vessel which falls to the lower threshold value, a second
pulse is generated which once again closes the first valve and the
pressure-control device while opening the second valve. The liquid
cryogen or coolant then flows from the second vessel to the third
while the pressure in the latter vessel is reduced to that of the
second vessel; especially when the object to be cooled is a
super-conductive system it has been found to be advantageous to
pass the liquid coolant supplied to the object to be cooled in
indirect heat exchange with the oppositely flowing expanded
coolant, thereby super-cooling the oncoming coolant and insuring
that the liquid cryogen will maintain its liquid state as it
traverses the system to be cooled.
Furthermore, the coolant withdrawn from the system to be cooled may
advantageously be expanded and pass through separate cooling zones
to shield the liquid of the first or supply vessel from the input
of heat from the exterior. These separate cool zones may be
provided around the duct whereby the liquid cryogen is delivered to
the cryostat around the chambers of the cryostat traversed by the
liquid coolant and around the body of liquid cryogen maintained in
the supply vessel.
According to still another feature of the invention, radiation
shields preventing the loss of cold within the duct system and the
cryonate are cooled with cold coolant vapor from the second
vessel.
An apparatus for carrying out the method of the present invention
thus comprises three vessels whereby the third or storage vessel is
connected with the first by a duct and a first valve and the second
vessel is connected to the third by a duct and a second valve.
Preferably the third or storage vessel underlies the second or
phase-separation vessel (the latter is disposed above the third or
storage vessel) and suitable conduits, ducts or the like are
provided between the first or supply vessel and a cryostat
containing one or more objects to be cooled and between the
cryostat and the second vessel.
The duct means connecting the interior of the cryonate with the
second vessel is provided with an expansion valve.
Still another feature of the invention resides in the provision of
a level indicator in the third vessel having the upper and lower
threshold valves as described above whereby the valves are
automatically controlled in response to the level in the third or
storage vessel.
In accordance with another feature of the apparatus aspect of this
invention, all of the connecting ducts between the vessel and the
cryogen or the object to be cooled are formed as coaxial conduits
with a central passage and the coaxial annular passages surrounding
same. The central passage serves for the feed of the liquid cryogen
to the object to be cooled. The innermost or first annular passage
serves to conduct expanded cryogen or coolant from the object to be
cooled and the third annular passage forms a radiation shield and a
path for the vapor of the liquid cryogen between the second storage
vessel and a further radiation shield within the cryostat. The two
other annular passages, i.e. the second and fourth, are
evacuated.
Within the cryostat there is formed, a cooling zone immediately
surrounding the object to be cooled which is cooled by the expanded
coolant from this object for the supercooling of the incoming
liquid, the outflowing coolant is passed through a heat exchange
with one section traversed by the liquid cryogen from the supple
vessel and another section traversing by expanded cryogen from the
cooled object. Of course, while the system has been described for a
single object to be cooled, it may also be used to cool a number of
objects in parallel or in series with respect to the flow of the
liquid cryogen.
BRIEF DESCRIPTION OF THE DRAWING
The above and other objects, features and advantages of the present
invention will become more readily apparent from the following
description, reference being made to the accompanying drawing in
which the sole FIGURE is a flow diagram illustrating a system
according to the present invention.
SPECIFIC DESCRIPTION
The system illustrated in the drawing comprises a supply vessel 1
(first vessel), connected by a duct 2 to one section of a heat
exchanger 15 and then to the central passage 3 of a coaxial-conduit
system having four annular passages 11, 37, 30 and 38 surrounding
the central passage. The coaxial duct system may extend over long
distances and is represented generally by the numeral 12. From the
central passage the liquid cryogen is introduced at 4 into the
object 5 to be cooled in a cryostat represented generally at 20.
The object may be a superconductive magnet.
The supercooled liquid cryogen, somewhat heated to contact with the
object 5, is conducted away at 7 and enters an expansion valve 8 in
which the liquid cryogen is expanded to form a vapor-liquid mixture
which traverses a helical duct system 9 in heat exchanging relation
with a radiation shield directly surrounding the object 5 and
forming a cold zone therearound. The cooling avoided by the passage
of the mixture through the ducts 9 has been found to stabilize the
temperature of the space in which object 5 is disposed.
A duct 10 carries the two-phase mixture from the cold zone through
the first annular space 11 of the coaxial-duct system 12, through
another section of the heat exchanger 15 and, via line 13, to the
second or separation vessel 14.
The mixture of vapor and liquid phases is separated in vessel 14
and the liquid phase can be transferred via duct 15 and an
automatically controlled valve 16 to the third or storage vessel
17. The latter is connected by a duct 25 and a valve 24 to the
first vessel 1.
To create the displacement pressure driving the liquid from the
vessel 1 through the object 5 to be cooled and into the vessel 14,
we provide a pressure-generating device which comprises a duct 18
connected to a controlled-pressure valve 19 and a pressurized gas
source 6 which is also connected via line 22 and the
pressure-controlled valve 23 to the gas space of vessel 17.
A level sensor 21 responds to the liquid level in the storage
vessel 17 and has upper and lower thresholds represented by the
inlets 21a and 21b of the controller 21 whose outputs are applied
to the valves 16 and 24 and to the pressure-regulating valve 23
respectively.
The gas derived from the liquid/vapor separator 14 is fed by line
29 to the third annular passage 30 of the coaxial duct system 12
and then passes through tubes of a heat shield 32 surrounding the
heat shield 9 and enclosing the space in which the expansion valve
8 is provided. The latter heat shield 32 is endlosed in the
insulated walls of the cryogen 20 and delivers its vapor via line
34 to a condensing station or the like not shown.
The operation of the system will be more readily apparent with
reference to a specific example as given below.
Liquid helium at a pressure of about 1 - 8 atmospheres absolute and
a temperature of 4.9.degree.K passes from the first vessel 1 via
the line 2 through the heat exchanger 15, the central passage 3 of
the coaxial duct system 12 and by line 4 is admitted to the object
5 to be cooled, especially a conductive magnet.
In the heat exchanger 15 the liquid helium is supercooled to a
temperature of about 4.5.degree.K and the super-cooled liquid
helium is expanded at valve 8 to a pressure of 1.2 atmospheres
absolute before entering the cooling zone 9.
Within the cooling zone, the helium vapor liquid mixture passes in
counterflow to the liquid super-cooled helium at a temperature of
4.5.degree.K and thereby stabilizes the temperature within the
object 5.
The object is thus cooled with super-critical helium at a pressure
of about 1.8 atmospheres absolute and a temperature of about
4.5.degree.K.
From this second vessel 14, liquid helium is transferred to the
open valve (second valve) 16 into the third or storage vessel 17
which is at the same pressure as that of the phase-separation
vessel 14. A gravity transfer of the liquid takes place during this
period.
The latter pressures are about 1.2 atmospheres absolute and hence a
pressure differential of 0.6 atmospheres absolute is applied
between the first vessel 1 and the second vessel 14 to displace the
liquid helium.
As soon as the liquid level in the third vessel 17 reaches its
upper limits as defined by the inlet 21a, the level sensor 21
applies a signal which closes the second valve 16, opens the first
valve 24, and overlies upon the pressure controller 23 to raise the
pressure in the third vessel 17 above 1.8 atmospheres absolute,
e.g. to 2.0 atmospheres absolute. The liquid is driven out of the
storage vessel 17 into the supply vessel 1 and the flow of liquid
helium through the object 5 is not interrupted. Of course, vessel
14 remains under its original pressure 1.2 atmospheres absolute or
slowly increases in pressure, but well below 1.8 atmospheres
absolute.
As soon as the liquid level in the third vessel 17 falls to its
lower threshold value as sensed by the inlet 21b, the sensor 21
closes valve 24, opens valve 16 and restores the pressure control
23 to its original level while venting excess pressure and permits
the pressure to be repeated. The vapor of course is used to cool
the radiation shield 32. The passages 37 and 38 of the coaxial duct
system 12 are evacuated and the compartment e.g. 28, within the
cryogen 20 and the housing 36 surrounding the vessels 14, 17 and 1
can also be evacuated.
* * * * *