This invention relates to a pulse tube refrigerator/cryocooler apparatus and to a gas flow distribution device for use therewith.
The general function of a pulse tube cryocooler apparatus is well known to one skilled in the art, and generally includes the following features/components:
The function of the cryocooler is to provide cooling to a device, particularly cryogenic temperatures. The present invention has been devised to achieve temperatures lower than 80K.
According to a first aspect of the present invention, we provide a pulse tube refrigerator/cryocooler apparatus including:
According to a second aspect of the present invention, we provide a pulse tube refrigerator/cryocooler apparatus including:
According to a third aspect of the present invention, we provide a gas flow distribution device for use in a pulse tube refrigerator/cryocooler apparatus, including:
Further features of the various aspects of the invention are set out in the claims attached hereto.
Embodiments of the invention will now be described by way of example only with reference to the accompanying drawings, of which:
Referring to
The apparatus 10 also includes a regenerator device 14, a pulse tube 16 and a conduit (or inertance tube as it is often known in the art) 18. The regenerator device 14 in this example has a central opening which receives the pulse tube 16. Thus the two are co-axial with each other, with the pulse tube being fluidly connected to the regenerator 14 at their ends remote from the inertance tube 18. This end also supports a “cold end” part 25. The part 25 is the part of the apparatus 10 which is to be lowered to a temperature in the order of 80K during use, and is thus connectable to any further apparatus to be so cooled.
The inertance tube 18 is fluidly connected at one end to the pulse tube by the intermediary of an opening 40 in a gas flow distribution device 30 (discussed in more detail later) and at its opposite end to the internal volume of a container 20. The container 20 (which is often referred to in the art as a “reservoir”) provides a storage volume for the Helium gas and in hand with the inertance tube 18 provides the necessary phase shift between the mass flow rate and pressure of the cyclically moving gas in order to give rise to the cooling effect at the part 25, which effect is well known in the art.
Advantageously, the present invention is configured such that the cyclically moving gas enters/exits the regenerator 14 in a direction parallel to its elongate axis. In other words, the gas entering the inlet 12 passes through the gas flow distribution device 30 (discussed later) and into the regenerator 14, substantially evenly across its annular cross-section such that the gas moves in the axial direction of the regenerator 14. Such a configured flow of the cyclically moving gas ensures that minimal mixing of gas occurs which leads to improved efficiency of the apparatus 10.
As mentioned above, the apparatus 10 includes a gas flow distribution device 30 which distributes gas substantially evenly across and/or around the cross-sectional area of the regenerator 14. The gas flow distribution device (which can be seen better in
The gas flow distribution device 30 is preferably manufactured by a rapid prototyping technique, e.g. selective metal laser sintering, which enables complex gas flow paths to be provided between the inlet 32 and each of the respective outlets 34a to q. Other rapid prototyping techniques could be used.
The length of each of the gas flow paths between the inlet 32 and the respective outlet 34 are substantially identical to each other, which means that the gas flow distribution device 30 is configured such that the flow rate of gas exiting/entering one outlet 34 is substantially identical to all of the other outlets 34 during use. This substantially even distribution of the gas flow through the device 30 ensures substantially even distribution of the gas across the annular cross-sectional area of the regenerator 14. In hand with that, the smooth transition between each adjacent gas flow path portion, and the configured cross-sectional area thereof, ensures minimal pressure drop between the inlet 32 and each respective outlet 34. Thus, the pressure of the cyclically moving gas at each of the outlets 34 is substantially the same. Thus, the resistance to flow along the gas flow paths are substantially identical to each other.
As shown in the figures, the gas flow distribution device 30 includes a generally axially extending opening 40 which fluidly connects the pulse tube 16 to the inertance tube 18. The outlets 34 of the gas flow paths are positioned around the generally axially extending opening 40. In the present example there are 18 outlets 34, and thus they are each positioned at an angle of 20 degrees around the axis of the opening 40.
As can be seen from the figures, the end portion of each of the fourth gas flow path portions 39 is aligned substantially parallel with the axis of the regenerator, which means that the flow of the gas into the regenerator 14 is linearized with the axis of the regenerator 14.
In order to assist with this linearization of the gas into the regenerator 14, the apparatus 10 is also provided with a gas flow linearization device 50 which is positioned in between the gas flow distribution device 30 and the pulse tube/regenerator. The gas flow linearization device 50 fluidly connects to the outlets 34 of the gas flow distribution device 30. In more detail the gas flow linearization device 52 includes a plurality of first gas flow path channels 52 which are positioned substantially evenly around the periphery of the device 50 and which are aligned substantially parallel with each other. The first gas flow path channels 52 communicate with the outlets 34 from the device 30, at one end, and at an opposite end with the regenerator 14.
The device 50 also includes a plurality of second gas flow path channels 54 which are positioned inwardly towards the axis of the device 50. These channels 54 provide fluid communication between the opening 40 of the device 30 and the pulse tube 16.
The channels 52, 54 can take many forms, but it should be noted that in
Whilst in the present embodiment pulse tube 16 extends through an axially extending opening in the regenerator 14, it should be noted that the pulse tube and regenerator could, in alternative embodiments, be connected in end-to-end relationship, as is well known in the art of cryocoolers.
Referring to
In
It should be appreciated, however, that the cross-sectional shape of the inlet(s) and outlet(s) may be any desired shape, provided that the length of and/or resistance to flow along each of the plurality of gas flow paths are substantially identical to each other.
When used in this specification and claims, the terms “comprises” and “comprising” and variations thereof mean that the specified features, steps or integers are included. The terms are not to be interpreted to exclude the presence of other features, steps or components.
The features disclosed in the foregoing description, or the following claims, or the accompanying drawings, expressed in their specific forms or in terms of a means for performing the disclosed function, or a method or process for attaining the disclosed result, as appropriate, may, separately, or in any combination of such features, be utilised for realising the invention in diverse forms thereof.
Number | Date | Country | Kind |
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1302888.1 | Feb 2013 | GB | national |
Number | Name | Date | Kind |
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6196006 | Kawano | Mar 2001 | B1 |
20070157632 | Saito | Jul 2007 | A1 |
20090151364 | Dicken | Jun 2009 | A1 |
20120193216 | Endo | Aug 2012 | A1 |
Number | Date | Country |
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101852506 | Oct 2010 | CN |
102393096 | Oct 2010 | CN |
0803687 | Oct 1997 | EP |
2003166766 | Jun 2003 | JP |
2013044604 | Apr 2013 | WO |
Entry |
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UK Search Report of GB1302888.1 dated Oct. 25, 2013. |
Search Report from EP application No. GB1504768.1, dated Jul. 30, 2015. |
Number | Date | Country | |
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20140230457 A1 | Aug 2014 | US |