This application is a § 371 of International PCT Application PCT/FR2017/050098, filed Jan. 17, 2017, which claims § 119(a) foreign priority to French patent application FR 1 650 962, filed Feb. 8, 2016.
The invention relates to a cryogenic refrigeration device.
The invention relates more particularly to a cryogenic refrigeration device comprising a working circuit intended to cool a working fluid circulating in said circuit, the working circuit comprising, arranged in series in a loop, a compression portion, a cooling portion, a portion with valve(s), an expansion portion and a reheating portion, in order to subject the working fluid to a recuperative working cycle comprising compression, then cooling, then expansion and then reheating to prepare for a new cycle.
The invention also relates to a cryogenic gas liquefaction unit comprising such a refrigeration device.
A concern for the constant improvement of existing cryogenic refrigerators or liquefaction units proposes to increase their service life, reduce the minimum operating temperature and increase their reliability. In particular, it is especially advantageous to eliminate maintenance operations and to phase out the use of oils.
A first known solution involves the use of a regenerative thermodynamic cycle of the Stirling or Pulse-Tube type. The disadvantages of these regenerative solutions are as follows. These devices have low performances at temperatures below 30K. This is associated with the low thermal capacity of the materials constituting the regenerator at this level of temperature. In addition, in these solutions, it is relatively difficult to connect the refrigerator thermally to the system to be cooled as well as to the heat removal system.
Another solution involves the use of a recuperative thermodynamic cycle of the reverse Brayton type based on a lubricated screw compressor, a counter-flow plate exchanger and a centripetal expansion turbine. This solution has the disadvantage, however, of using oil to cool and lubricate the compressor. This imposes the need for a cycle gas de-oiling operation after compression. In addition, the service life of this type of system is relatively short as a result of the compression technology used and as a result of the leaks at the level of the compressor. This technology also presents problems for the expansion of a diphasic fluid, and the energy efficiency is not optimal.
Yet another solution involves the use of a recuperative thermodynamic cycle of the reverse Turbo-Brayton type based on dry centrifugal compressors, a counter-flow plate exchanger and a centripetal expansion turbine (cf. FR2924205A1). This solution is poorly adapted to the low thermal inputs, however, as a result of the difficulty in miniaturizing the turbomachines that are utilized.
In addition, the rates of compression that are achievable at each stage of centrifugal compression is relatively low as a result of the low molar mass of the available gases at cryogenic temperature. The cost of manufacture of such turbomachines is relatively high, furthermore, and the centripetal machines that are utilized are poorly adapted for expanding a diphasic fluid.
One aim of the present invention is to address all or part of the shortcomings of the prior art mentioned above.
For this purpose, the device according to the invention, which is consistent, furthermore, with the generic definition provided by the above preamble, is essentially characterized in that the compression portion comprises at least one compressor with a linear piston driven by a linear motor, the expansion portion comprises at least one expander with a linear piston, the portion with valve(s) comprises at least one regulating valve of the linear type actuated by a linear motor and controlled in order to supply or extract the working fluid to or from the at least one piston expander.
Furthermore, embodiments of the invention may include one or a plurality of the following characterizing features
The invention exhibits numerous advantages in relation to the prior art, in particular
The invention also relates to a method for the refrigeration of a user device by means of such a cryogenic refrigeration device, in which the cooled working fluid is placed into thermal exchange with said user device.
The invention also relates to a liquefaction unit or a liquefaction method comprising or utilizing such a refrigeration device.
The invention may also relate to any alternative device or method comprising any combination of the characterizing features mentioned above or below.
Other features and advantages will become apparent from a perusal of the following description, given with reference to the figures, in which
The non-exhaustive illustrative embodiment illustrated in
The refrigeration device 100 preferably has as its aim to transfer heat from a cold source 13 at low temperature (via a thermal exchange with a device or a user 7 to be cooled) to a heat source 15 at a higher temperature (for example via a thermal exchange with a cooling device 5).
As illustrated in
The device may include all or part of the components described below.
The device comprises one or a plurality of linear motors 1 preferably using flexible bearings 2 (or gas or low-friction or magnetic bearings). The bearings represented by way of example in
The circuit comprises one or a plurality of piston compressors 3 arranged in series functioning preferably at ambient temperature and driven by the one or more linear motors 1. The piston compressor is in fact a piston compressor with linear displacement driven by a motor 1. The piston is coupled to a shaft that is displaced in translation according to an alternating movement via a motor, for example an electromagnetic motor, of which the alternating movement of translation of the integral shaft of the piston is driven by a system of magnetic coils (cooperating with magnets that are integral with the shaft or integral with a stator).
These piston compressors 3 utilize non-return valves 4 and 14, for example, in order to communicate with high-pressure lines 12 (to hold back the compressed fluid) and low-pressure lines 11 (to receive the expanded fluid for the purpose of re-compressing it). A plurality of non-return valve technologies are conceivable, for example reed valves. Of course, any other type of device making it possible to prevent the return of the compressed fluid in the opposite direction in the circuit may be envisaged.
The working circuit comprises one or a plurality of exchangers 5 provided in order to remove heat from the compressed gas to a heat source and arranged at the outlet of the one or more compressors 3. This cooling exchanger, for example, brings the working fluid into thermal exchange with a cooling heat transfer fluid 15.
At least one counter-flow heat exchanger 6 is then provided (downstream in the direction of circulation of the working fluid in the circuit on the high-pressure line 12). This heat exchanger 6 may separate the elements relatively at a high temperature from the elements at a relatively low temperature 6 of the circuit.
The circuit then comprises at least one valves 9 operating at low temperature (that is to say between 4 and 200 K). This valve 9 is provided in order to supply and extract the gas from a piston expander 10 situated downstream.
This valve 9 may be actuated by a linear motor 8 of equivalent technology to the technology of the compressor motor 1.
This valve 9 may be coupled equally to the motor 1 of the compressor 3 or to a separate motor. Likewise, the expander 10 may be coupled equally to the motor 1 of the compressor or to the motor 8 of the valve 9 or to a separate alternator (this linear alternator may be of equivalent technology to the technology of the motor 1 described above This alternator has a structure of the same type as the one or more motors of the compressor, for example, but utilized in an alternator mode. That is to say the piston is displaced by the fluid and produces energy).
This valve 9 is actuated preferably at the same frequency as the expander 10, although its movement is out of phase in relation to the expander 10 in such a way as to maximize the efficiency of the expander 10.
The one or more piston expanders 10 operate at low temperature and may or may not be connected mechanically to the motor 1 of the compressor.
The gas expanded by the expander 10 is returned to the compressor 3 via a low-pressure line 11 (through the valve 9). One or a plurality of heat exchangers 7 are provided in order to reheat the working fluid and thus to extract heat to the cold source 13. The expanded fluid passes in particular into the counter-flow exchanger 6 before returning into the compressor 3 (via the corresponding valve 4).
The operation of this refrigerator 100 may be the following. The working gas (helium in this example) in the gaseous phase (for example at 20° C.) is compressed on its way through the piston compressor 3 from a low pressure (for example 10 bar) to a high pressure (for example 18 bar).
The non-return valves 4, 14 are utilized to cause the compression chamber of the compressor to communicate alternately with the low-pressure line 11 and the high-pressure line 12.
The helium is reheated at the outlet of the compressor (for example to 110° C.). The helium is then cooled on its way through a first exchanger 5 with the help of a flow of water 15 (or any other appropriate cooling agent). The temperature of the helium is brought to 25° C.
The helium then passes through the counter-flow exchanger 6, where its temperature is lowered, for example to 79K. Downstream, the regulating valve 9 is utilized in order to cause the expansion chamber of the expander 10 to communicate alternately with the low-pressure line 11 and the high-pressure line 12.
The helium passes through the piston expander 10, where its temperature falls (for example to 67 K). This piston expander 10 is configured in particular in order to function with a diphasic or liquid fluid.
When the expander is coupled to the motor of the compressor, the expansion work of the expander 10 may be transferred via the common shaft of the linear motor 1 to the compressor 3.
The helium then passes through the reheat heat exchanger 7, where it cools the cold user device 13 (nitrogen in this example). The cooled gaseous nitrogen 13 is liquefied to saturation, for example by extracting heat from it.
The temperature of the helium is brought to 76 K, for example.
The helium then passes once more through the counter-flow exchanger 6, where it is reheated (for example to 20° C.).
The helium then returns into the compressor 3 in order to perform a new identical cycle via the valve 4.
The
The working gas (hydrogen), for example at 20° C. (in the gaseous phase), is compressed in two piston compressors 20 and 21 arranged in series.
At the outlet of each compressor 20, 21 (via a high-pressure line and a valve 14), the gas is cooled by a heat exchanger 22, 23. This hydrogen is then cooled on its way through a first counter-flow heat exchanger 24.
A part of the flow of cooled gas may be admitted in order to pass, via a derivation 15 comprising a first linear valve 9, through a first expander piston 25 in such a way as to extract heat from the hydrogen.
As noted above, this first piston expander 25 may be connected to the first compressor 20 via a linear motor (not depicted for the sake of simplification, but it may be of the same type as that described above). Likewise, the first expander may be coupled to a separate motor (alternator)).
The first control valve 9 upstream of the first expander 25 is actuated preferably via a linear motor (not depicted for the sake of simplification, but it may be of the same type as that described above).
The hydrogen (expanded or otherwise) may then be cooled on its way through a second counter-flow exchanger 26 and, if necessary, on its way through a third counter-flow exchanger 27. This hydrogen that has been expanded in the first expander 25 may be returned directly to the first compressor 20 (via the one or more counter-flow heat exchangers 24, 26. That is to say the hydrogen that has been expanded in the first expander 25 may be returned to the compressors without being subjected to a second expansion or cooling.
Downstream of the derivation 15, the remaining hydrogen is then expanded in a second linear expander 28 (via a linear control valve 9). The second expander 28 is preferably of the diphasic piston type in order to extract heat from the hydrogen for the purpose of liquefying it partially. This second piston expander 28 may be connected mechanically (coupled) to the second compressor 21 (via a linear motor not depicted for the sake of simplification as previously) or to a separate alternator.
The second control valve 9 situated upstream of the second expander 28 may also be actuated by a linear motor (not depicted for the sake of simplification).
The control valves 9 controlling the circulation of the fluid between the expanders 25, 28 and the compressors 20 may be actuated, if necessary, by one and the same common actuator.
The diphasic mixture obtained after passage into the second expander 28 may then be delivered to a cryogenic separator 29. The gaseous phase of the hydrogen is returned to the first compressor 20 through the counter-flow exchangers 27, 26, 24.
The resulting liquid phase may be delivered to a final user through a line 30 provided for this purpose. The circuit may include an inlet 31 for the supply of working fluid (for example upstream of the first compressor 20) in order to compensate for the sampling of liquid.
Of course, the working fluid used may be any fluid other than helium or hydrogen, for example nitrogen, methane, neon, oxygen or argon.
The working circuit may thus be of the open or closed type.
Of course, the invention is not limited to the examples of cycles and circuits illustrated in
While the invention has been described in conjunction with specific embodiments thereof, it is evident that many alternatives, modifications, and variations will be apparent to those skilled in the art in light of the foregoing description. Accordingly, it is intended to embrace all such alternatives, modifications, and variations as fall within the spirit and broad scope of the appended claims. The present invention may suitably comprise, consist or consist essentially of the elements disclosed and may be practiced in the absence of an element not disclosed. Furthermore, if there is language referring to order, such as first and second, it should be understood in an exemplary sense and not in a limiting sense. For example, it can be recognized by those skilled in the art that certain steps can be combined into a single step.
The singular forms “a”, “an” and “the” include plural referents, unless the context dearly dictates otherwise.
“Comprising” in a claim is an open transitional term which means the subsequently identified claim elements are a nonexclusive listing i.e. anything else may be additionally included and remain within the scope of “comprising.” “Comprising” is defined herein as necessarily encompassing the more limited transitional terms “consisting essentially of” and “consisting of”; “comprising” may therefore be replaced by “consisting essentially of” or “consisting of” and remain within the expressly defined scope of “comprising”.
“Providing” in a claim is defined to mean furnishing, supplying, making available, or preparing something. The step may be performed by any actor in the absence of express language in the claim to the contrary.
Optional or optionally means that the subsequently described event or circumstances may or may not occur. The description includes instances where the event or circumstance occurs and instances where it does not occur.
Ranges may be expressed herein as from about one particular value, and/or to about another particular value. When such a range is expressed, it is to be understood that another embodiment is from the one particular value and/or to the other particular value, along with all combinations within said range.
All references identified herein are each hereby incorporated by reference into this application in their entireties, as well as for the specific information for which each is cited.
Number | Date | Country | Kind |
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1650962 | Feb 2016 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FR2017/050098 | 1/17/2017 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2017/137674 | 8/17/2017 | WO | A |
Number | Name | Date | Kind |
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4267701 | Toscano | May 1981 | A |
5205134 | Gistau-Baguer | Apr 1993 | A |
5799867 | Misawa | Sep 1998 | A |
20120174610 | Takayama | Jul 2012 | A1 |
20130305751 | Gomes | Nov 2013 | A1 |
20150052887 | Dadd | Feb 2015 | A1 |
20150369528 | Lee | Dec 2015 | A1 |
Number | Date | Country |
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2 084 109 | Dec 1971 | FR |
2 924 205 | May 2009 | FR |
1 305 506 | Apr 1987 | SU |
Entry |
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FR2084109 Translation (Year: 1971). |
International Search Report and Written Opinion for PCT/FR2017/050098, dated May 18, 2017. |
French Search Report and Written Opinion for FR 1 650 962, dated Oct. 28, 2016. |
Number | Date | Country | |
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20190063791 A1 | Feb 2019 | US |