CROSS REFERENCE TO RELATED APPLICATIONS

This application claims the priority of U.S. Provisional Application Serial No. 63/064,528, filed on August 12, 2020, which is hereby incorporated herein by reference in its entirety.

FIELD OF THE INVENTION

This invention relates to an improved double-inlet valve for a Gifford-McMahon (GM) type pulse tube cryocooler that improves performance primarily by a favorable control of direct current (DC) flow.

BACKGROUND

The Gifford-McMahon (GM) type pulse tube refrigerator is a cryocooler, similar to GM refrigerators, which derives cooling from the compression of gas in a compressor connected to an expander by supply and return hoses. The expander cycles gas through inlet and outlet valves using a rotary valve commonly to a cold expansion space through a regenerator. A GM expander creates the cold expansion space by the reciprocation of a solid piston (a piston is often referred to as a displacer when the displaced volume above and below the piston are connected by a regenerator) in a cylinder while a pulse tube expander creates the cold expansion space by the reciprocation of a “gas piston.” Pulse tube refrigerators have no moving parts in their cold head, but rather an oscillating gas column within the pulse tube that functions as a compressible piston. The piston includes gas that stays in the pulse tube as it is pressurized and depressurized. The elimination of moving parts in the cold end of the pulse tube refrigerators allows a significant reduction of vibration, as well as greater reliability and lifetime. To reduce the vibration further, the rotary valve is typically connected to the expander by flexible hoses. Two stage GM type pulse tube refrigerators typically use oil lubricated compressors to compress helium and draw 5 to 15 kW, or more, of input power. Major applications today are cooling MRI (magnetic resonance imaging) and NMR (nuclear magnetic resonance imaging) magnets, where they cool heat shields at about 40 K and re-condense helium at around 4 K. They are also being used in the early development of quantum computers. These applications require low levels of vibration and low levels of electromagnetic interference (EMI). GM type pulse tube coolers have been developed in parallel with Stirling type pulse tube coolers which provide the pressure cycle to the regenerator and pulse tube directly from a reciprocating compressor piston. These are widely used in cooling infrared detectors near 70 K in ground and space based systems. They are typically much smaller, and run at much higher speeds e.g. 60 Hz vs. 1 to 2 Hz for GM type pulse tubes. Stirling type pulse tubes are more efficient than GM type pulse tubes because they recover much of the work of expansion but the means of controlling the flow between the warm end of the pulse tube and a buffer volume is different, and they are not as efficient at low temperatures.

W.E. Gifford who was a co-inventor of the GM cycle refrigerator also conceived of an expander that replaced the solid piston with a gas piston and called it a “pulse tube” refrigerator. This was first described in his U.S. Patent No. 3,237,421 (“the ‘421 patent”) which shows a pulse tube connected to valves like the earlier GM refrigerators. Early development of the pulse tube expander demonstrated that gas entering a vertically oriented tube at the bottom and flowing through a flow smoothing mesh created a stratified column of gas that got hot as it was compressed and pushed towards the top. The top of the tube had a copper cap that absorbed some of the heat so that when the gas flowed out of the tube and cooled as it expanded it cooled the flow smoother and adjacent copper in what is called the cold end. A significant improvement was made to the basic GM type pulse tube by Mikulin et al., as reported in 1984, by adding a buffer volume at the warm end of the pulse tube and flowing gas in and out through a throttle valve. This is now called a basic orifice type pulse tube or a single-inlet valve pulse tube. Subsequent development work has led to the design of several different means of throttling the flow that improve the performance of the pulse tube expander. Most Stirling type pulse tubes are of the single-inlet design.

For GM type pulse tubes it was found that the addition of a second orifice between the warm end of the pulse tube and the inlet to the regenerator improved the performance and made it possible to get below 4 K in a two stage pulse tube. This is now called a double-inlet pulse tube and the second throttling device is called a double-inlet valve. As was the case with the singleinlet valve taking on different forms, the double-inlet valve has taken on different forms. The present invention is a new double-inlet valve that has demonstrated improved performance.

U.S. patent No. 3,205,668 (“the ‘668 patent”) by Gifford describes a GM expander that has a solid piston having a stem attached to the warm end which drives the displacer up and down by cycling the pressure above the drive stem out of phase with the pressure cycle to the expansion space. Rotary valves are the most common means of cycling the pressures between high pressure Ph and low pressure Pl. One can think of the flow control at the warm end of a pulse tube as being optimized if the cold boundary of the gas piston follows essentially the same pattern as the cold end of the solid piston. A cycle with the expander described in the ‘668 patent starts with the displacer held down while the inlet valve opens and increases the pressure to Ph. The piston then moves up and at about ³ /4 of the way the inlet valve closes and the pressure drops as the piston moves to the top. The outlet valve then opens and the pressure drops to Pl. The piston then moves down and at about ³ /4 of the way the outlet valve closes and the pressure increases as the piston moves to the bottom. The area of the pressure-volume (P-V) is a measure of the refrigeration produced per cycle. The differences between a solid piston and a gas piston are numerous. They include 1) the length and stroke depend on the pressure ratio and how much gas is allowed to flow in and out of the cold end of the pulse tube, 2) an asymmetry in the valve timing and flow resistances can cause more gas to flow in or out of one end of the pulse tube each cycle than to flow out of or in, referred to as DC flow, and 3) it is very difficult to balance the flow in and out of the cold and warm ends simultaneously to establish a cold boundary, referred to as alternating current (AC) flow, that simulates the movement and the P-V relation of a solid piston. The Stirling cycle pulse tubes with a single-inlet valve avoid the first problem because the compressor piston has a fixed displacement, and it avoids the second problem because the same amount of gas flows out of the buffer volume as flows into it.

While this analogy of a gas piston with a solid piston provides a physical description of the process, it is more common to find the flow patterns described in terms of the phase relationship between the pressure cycle and the mass flow cycle. U.S. Patent application publication No. US 2011/0100022 (“the ‘022 publication”) by Yuan et al. has a good description of phase control devices for Stirling type single-inlet pulse tube cryocoolers. Figure 2 of the ‘022 publication shows resistive devices which are described as including an orifice, a short tube, and closely spaced plates. Figure 2 shows an inertance tube which is a long small diameter tube that acts as an inductance in an electrical analogy. Figure 8 of the ‘022 publication shows how these devices can be combined using an electrical circuit analogy to optimize the phase relationship between the pressure cycle and the mass flow cycle that provides the most cooling. Figure 7 of the ‘022 publication is a schematic of a single-inlet valve that is comprised of a resistive device in parallel with an inertance device. It is important to note that an inertance device is practical in a Stirling type pulse tube because it is operating at a high frequency. At the low frequencies of GM type pulse tubes only resistive devices are practical. It is also important to note that all of the devices described in the ‘022 publication have the same flow characteristics with flow in either direction.

Efforts to increase the cooling capacity of two-stage GM type coolers at 4K have included the development of the four-valve design. U.S. Patent No. 10,066,855 (“the ‘855 patent”) by Xu describes a four-valve pulse tube. This name derives from the phase shifting mechanism comprising a pair of inlet and outlet valves that connect to the warm end of the regenerator and a second pair of inlet and outlet valves that connect to the warm end of the pulse tube. The ‘855 patent describes flow control mechanisms to balance the flow of gas to second and third stage pulse tubes, each of which requires an additional pair of valves. The four-valve pulse tube does not use a buffer volume and present designs perform slightly better than present designs of doubleinlet pulse tubes. They are at a disadvantage that the void volume of the hoses reduces the pressure oscillation and performance however when the valve motor and rotary valve have to be separated from the regenerator. A double-inlet pulse tube only requires one hose between the valve assembly and the pulse tube/regenerator assembly, referred to as the cold end, while the four-valve pulse tube needs one hose to connect to the regenerator and smaller diameter hoses connected to the warm ends of each pulse tube in a multi-stage pulse tube. The improved performance of a doubleinlet pulse tube with the present invention makes it possible to get performance that is as good as a four-valve pulse tube in a unit with a remote valve assembly and a single connecting hose. A patent application for an improved connecting hose has recently been filed. This hose reduces the vibration transmitted to the cold head from the valve-motor assembly, and reduces the void volume resulting in improved efficiency.

Japanese (JP) Patent No. 3917123 by Ogura describes the use of a needle valve for the double-inlet valve and a replaceable bushing with a short hole through it for the first inlet valve. The short hole through the bushing has the same flow restriction in either direction for the same flow conditions, and it is a symmetric flow restrictor. The needle valve on the other hand, as it is depicted, has a port at the end that looks at the point of the needle and a port on the side that looks at the stem. As the flow restriction is different for flow at the same conditions in different directions, the flow restriction is asymmetric. The degree of asymmetry depends on a number of factors such as beveling the inlets to the ports, the length of the holes in the ports, etc. Improvements in phase shifting were made possible by simplifying the means of making adjustments.

In addition to optimizing the phase shifting mechanism that controls the P-V relationship in GM type pulse tubes operating near 4 K, it was also found to be important to control the DC flow. U.S. Patent No. 9,157,668 (“the ‘668 patent”) by Xu describes a double-inlet pulse tube to which a bleed line between a buffer volume and the compressor return line has been added. Figure 1 of the ‘668 patent shows the prior art basic double-inlet pulse tube and describes the flow pattern through the double-inlet valves as generating too much DC flow from the warm end to the cold end of the pulse tube. The bleed line from the buffer volume back to the return side of the compressor reduces the DC flow to a rate that optimizes the cooling. This has the disadvantage when the valve assembly is remote from the cold end of requiring an additional connecting line. A two stage double-inlet pulse tube has two tubes in parallel that extend from room temperature to first and second stage temperatures. The warm end of each connects to its own buffer volume and has its own double-inlet valves. The second stage regenerator is an extension of the first stage regenerator so the pressure drop through the first stage regenerator to the cold end of the first stage pulse tube is less than the pressure drop to the cold end of the second stage pulse tube. Optimizing the DC flow in a two stage pulse tube might require having an upward DC flow in the second stage and a downward DC flow in the first stage.

SUMMARY

The present invention is a double-inlet valve that has good AC flow characteristics and provides adjustability of the DC flow to increase the available cooling. It also only requires a single connecting hose between a remote valve assembly and the cold head.

The double-inlet valve comprises a fixed restrictor in parallel with an adjustable needle valve. The flow through the needle valve is asymmetric, that is there is more pressure drop when gas at a given condition enters one port compared to entering the other port. The fixed restrictor can be a short hole having the same symmetric pressure drop for flow in either direction or it can be a tapered hole that has asymmetric flow. This combination provides good AC flow characteristics and adjustability of the DC flow to increase the available cooling. It also only requires a single connecting hose between a remote valve assembly and the cold head.

These advantages and others are achieved by a GM type double-inlet pulse tube cryocooler system for providing cooling at cryogenic temperatures. The GM type double-inlet pulse tube cryocooler system comprises a compressor supplying gas at a supply pressure through a supply line and receiving gas at a return pressure through a return line, a valve assembly connected to the supply and return lines, and a pulse tube cold head connected to the valve assembly. The valve assembly cycles gas between the supply pressure and the return pressure to the pulse tube cold head through a connecting line. The pulse tube cold head comprises at least one regenerator having a warm end and a cold end, at least one pulse tube having a warm end and a cold end, at least one double-inlet valve, a buffer volume connected to the warm end of the pulse tube, a first line extending from the connecting line to the warm end of the regenerator and to the double-inlet valve, a second line connecting the cold end of the regenerator to the cold end of the pulse tube, and a third line from the warm end of the pulse tube to the double-inlet valve and to the buffer volume through a single-inlet valve.

BRIEF DESCRIPTION OF THE DRAWINGS

The drawing figures depict one or more implementations in accord with the present concepts, by way of example only, not by way of limitations. In the figures, like reference numerals refer to the same or similar elements.

FIG. 1 shows a schematic of a single stage GM type double-inlet pulse tube cryocooler system having a first embodiment of the double-inlet valve of the disclosed invention.

FIG. 2 shows a schematic of a single stage GM type double-inlet pulse tube cryocooler system having a second embodiment of the double-inlet valve of the disclosed invention.

FIG. 3 shows a schematic of a single stage GM type double-inlet pulse tube cryocooler system having a third embodiment of the double-inlet valve of the disclosed invention.

FIG. 4 shows a schematic of a two stage GM type double-inlet pulse tube cryocooler system having an embodiment of the double-inlet valve of the disclosed invention.

FIGS. 5A-5C show schematics of first, second and third embodiments of the double-inlet valves.

DETAILED DESCRIPTIONS

In this section, some embodiments of the invention will be described more fully with reference to the accompanying drawings, in which preferred embodiments of the invention are shown. This invention, however, may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will convey the scope of the invention to those skilled in the art. Like numbers refer to like elements throughout, and prime notation is used to indicate similar elements in alternative embodiments. Parts that are the same or similar in the drawings have the same numbers and descriptions are usually not repeated.

With reference to FIG. 1, shown is a schematic of a single stage GM type double-inlet pulse tube cryocooler system 100 having a first embodiment of the double-inlet valve la of the disclosed invention. With reference to FIG. 5A, shown is a schematic of the first embodiment of the double-inlet valve la. Double-inlet valve la is shown in context of the entire system. Referring to FIGS. 1 and 5A, the single stage GM type double-inlet pulse tube cryocooler system 100 includes a compressor 10, a valve assembly 12 including valves 12a and 12b, and a pulse tube cold head 101. Compressor 10 is connected to supply valve 12a, VI, through supply line Ila, and return valve 12b, V2, through return line 11b. Lines Ila and 11b are typically flexible metal hoses 5 to 20 meters long, and valves 12a and 12b are typically slots in a motor driven rotary valve rotating over ports in a stationary seat. Gas, usually helium, cycles in pressure between the supply and return pressures, typically 2.2 MPa and 0.6 MPa, as it flows through connecting line 13 to the warm end 16a of the regenerator 16 and the warm end of the pulse tube 17 through the doubleinlet valve la. The compressor 10 supplies gas at a supply pressure through a supply line Ila and receives gas at a return pressure through a return line 11b. The valves 12a and 12b are respectively connected to the supply line Ila and return line 11b that cycles gas between the supply pressure and the return pressure, through a connecting line 13, to a pulse tube cold head 101. Connecting line 13 can be a few millimeters long if valves 12a and 12b are integral to the pulse tube cold head 101 or it can be up to a meter long if the valves are remote.

The pulse tube cold head 101 includes a regenerator 16 having a warm end 16a and a cold end 16b, a pulse tube 17 having a warm flow smoother 17a at a warm end and a cold flow smoother 17b at a cold end, a line 18 connecting the regenerator cold end 16b of the regenerator 16 to the cold flow smoother 17b of the pulse tube 17, a line 7 extending from the connecting line 13 to the warm end 16a of the regenerator 16, lines 6a and 9a extending from the line 7 to a double-inlet valve la, a line 5 from the warm flow smoother 17a of the pulse tube 17 to a buffer volume 15 through a single-inlet valve 4, and lines 8a and 9b from the double-inlet valve la to the line 5 and to the warm flow smoother 17a of the pulse tube 17. Cycling flow continues to the warm end 16a of regenerator 16 through line 7, and continues to line 5 through double-inlet valve la. Line 5 connects at one end to the warm end of pulse tube 17 which contains warm flow smoother 17a, and at the other end to single-inlet valve 4 which in turn connects to buffer volume 15. The cold end 16b of regenerator 16 connects through line 18 to the cold end of pulse tube 17 which contains cold flow smoother 17b.

Referring to FIGS. 1 and 5A, double-inlet valve la includes fixed restrictor 3a and needle valve 2a which is adjustable for regulating the amount of the flow from both directions. The needle valve 2a and the fixed restrictor 3a are connected in parallel. The needle valve 2a includes a base

30 and a needle 31 extending from the base 30, both of which are disposed inside the cavity 32 formed in the needle valve 2a. Needle valve 2a includes needle end port 33 that is connected to line 7 through line 6a, and stem port 34 that is connected to the line 5 through line 8a. The needle

31 protrudes toward the needle end port 33 while the base 30 seals the cavity 32 so that a fluid flow path is formed between the needle end port 33 and stem port 34 through the cavity 32. Moving the needle 31 towards or away from the needle port 33 changes the opening of the flow channel, which changes the flow rates in both directions and the degree of asymmetry between the bidirectional flows. It is noted that the size and shape of the needle 31 and needle port 33 can be varied to change the flow rates in both directions and the degree of asymmetry of needle valve 2a, and thus the AC and DC flow characteristics.

The fixed restrictor 3a has a hole (flow path) 35a that is connected to line 9a, which is connected to the line 7, and line 9b which is connected to the line 5. The hole 35a may have the same cross-sectional area through the length of the hole, and consequently, flow through the restrictor 3a is symmetric. The symmetric flow means that gas flow in a direction has the same flow resistance as gas flow in the opposite direction. An asymmetric flow means that gas flow in a direction has a different flow resistances from gas flow in the opposite direction. In the asymmetric flow, flow resistance for gas flowing in a direction is greater or smaller than flow resistance for gas flowing in the opposite direction. The flow through needle valve 2a is asymmetric. Flow for gas entering the needle port 33 through line 6a is more restricted than flow for gas entering the stem port 34 through line 8a. Consequently, gas flow from the needle port 33 to the stem end port 34 has higher flow resistance than the gas flow from the stem port 34 to the needle port 33. In other words, flow in a direction from the needle 31 to the base 30 has a higher flow resistance than an opposite direction. With reference to FIG. 2, shown is a schematic of a single stage GM type double-inlet pulse tube cryocooler system 200, having a second embodiment of the double-inlet valve lb of the disclosed invention. With reference to FIG. 5B, shown is a schematic of the second embodiment of the double-inlet valve lb. Double-inlet valve lb differs from the double-inlet valve la in having needle valve 2b turned around so that the needle end port 33 connects to line 5 through line 6b and the stem port 34 connects to line 7 through line 8b. The hole 35a of the fixed restrictor 3a may have the same cross-sectional area through the length of the hole, and consequently, flow through the restrictor 3a is symmetric. The flow through needle valve 2b is asymmetric. Flow for gas entering the needle port 33 through line 6b is more restricted than flow for gas entering the stem port 34 through line 8b. Gas flow from the needle port 33 to the stem port 34 has higher flow resistance than the gas flow from the stem port 34 to the needle port 33.

The single stage GM type double-inlet pulse tube cryocooler system 200 includes a compressor 10, a valve assembly 12 including valves 12a and 12b, and a pulse tube cold head 201. The compressor 10 supplies gas at a supply pressure through a supply line Ila and receives gas at a return pressure through a return line 11b. The valves 12a and 12b are respectively connected to the supply line Ila and return line 11b that cycles gas between the supply pressure and the return pressure, through a connecting line 13, to a pulse tube cold head 201. The pulse tube cold head 201 includes a regenerator 16 having a warm end 16a and a cold end 16b, a pulse tube 17 having a warm flow smoother 17a at a warm end and a cold flow smoother 17b at a cold end, a line 18 connecting the regenerator cold end 16b to the cold flow smoother 17b of the pulse tube 17, a line 7 extending from the connecting line 13 to the warm end 16a of the regenerator 16, lines 8b and 9a extending from the line 7 to a double-inlet valve lb, a line 5 from the warm flow smoother 17a of the pulse tube 17 to a buffer volume 15 through a single-inlet valve 4, and lines 6b and 9b from the double-inlet valve lb to the line 5 and to the warm flow smoother 17a of the pulse tube 17.

With reference to FIG. 3, shown is a schematic of a single stage GM type double-inlet pulse tube cryocooler system 300, having a third embodiment of the double-inlet valve 1c of the disclosed invention. With reference to FIG. 5C, shown is a schematic of the third embodiment of the double-inlet valve 1c. Double-inlet valve 1c differs from la in having fixed restrictor 3b that has a tapered hole 35b which produces an asymmetric flow pattern. In this embodiment, the cross- sectional area of the hole 35b increases while proceeding from the connection point of the line 9a to the connection point of the line 9b. In this configuration, the fixed restrictor 3b has lower flow resistance in flow from the line 9a to the line 9b than flow in the opposite direction. It is understood that asymmetric restrictor 3b can be oriented in either direction in combination with adjustable restrictor 2a or 2b. For example, if the fixed restrictor 3b is combined with the needle valve 2b of the embodiment shown in FIG. 2, the cross-sectional area of the hole 35b may decrease while proceeding from the connection point of the line 9a to the connection point of the line 9b.

The single stage GM type double-inlet pulse tube cryocooler system 300 includes a compressor 10, a valve assembly 12 including valves 12a and 12b, and a pulse tube cold head 301. The compressor 10 supplies gas at a supply pressure through a supply line Ila and receives gas at a return pressure through a return line 11b. The valves 12a and 12b are respectively connected to the supply line Ila and return line 11b that cycles gas between the supply pressure and the return pressure, through a connecting line 13, to a pulse tube cold head 301. The pulse tube cold head 301 includes a regenerator 16 having a warm end 16a and a cold end 16b, a pulse tube 17 having a warm flow smoother 17a at a warm end and a cold flow smoother 17b at a cold end, a line 18 connecting the regenerator cold end 16b to the cold flow smoother 17b of the pulse tube 17, a line 7 extending from the connecting line 13 to the warm end 16a of the regenerator 16, lines 6a and 9a extending from the line 7 to a double-inlet valve 1c, a line 5 from the warm flow smoother 17a of the pulse tube 17 to a buffer volume 15 through a single-inlet valve 4, and lines 8a and 9b from the double-inlet valve 1c to the line 5 and to the warm flow smoother 17a of the pulse tube 17.

With reference to FIG. 4, shown is a schematic of a two stage GM type double-inlet pulse tube cryocooler system 400 which includes two pulse tubes 17 and 21. Double-inlet valve la is connected to first stage pulse tube system 17 and double-inlet valve Id is connected to second stage pulse tube 21. The double-inlet valve Id is equivalent to la in structures, but is arranged differently. Specifically, the double-inlet valves la and Id are arranged in a mirror symmetry with respect to the line 7. Cycling flow continues to the warm end 16a’ of first stage regenerator 16’ and to second stage regenerator 20 through line 7, and continues to line 5 through double-inlet valve la, and to line 5a through second stage double-inlet valve Id. Line 5 connects at one end to the warm end of first stage pulse tube 17 which contains warm flow smoother 17a, and at the other end to single-inlet valve 4 which in turn connects to buffer volume 15. Line 5a connects at one end to the warm end of the second stage pulse tube 21 which contains warm flow smoother 21a, and at the other end to single-inlet valve 4a which in turn connects to second stage buffer volume 15a As shown in FIG. 4, the two stage GM type double-inlet pulse tube cryocooler system 400 includes the second stage regenerator 20 as an extension of first stage regenerator 16’. The second stage pulse tube 21 is separated from first stage pulse tube 17, with the warm end at room temperature. The cold end 16b’ of first stage regenerator 16 connects through line 18 to the cold end of the first stage pulse tube 17 which contains cold flow smoother 17b. The cold end 20b of second stage regenerator 20 connects through line 22 to the cold end of the pulse tube 21 which has flow smoother 21b. The warm end of first stage pulse tube 17 has flow smoother 17a and connects to line 5, which connects to first double-inlet valve la and buffer volume 15 through single-inlet valve 4. The warm end of second stage pulse tube 21 has flow smoother 21a and connects to line 5a, which connects to double-inlet valve Id and buffer volume 15a through singleinlet valve 4a.

The two stage GM type double-inlet pulse tube cryocooler system 400 includes a compressor 10, a valve assembly 12 including valves 12a and 12b, and a pulse tube cold head 401. The compressor 10 supplies gas at a supply pressure through a supply line Ila and receives gas at a return pressure through a return line 11b. The valves 12a and 12b are respectively connected to the supply line Ila and return line 11b that cycles gas between the supply pressure and the return pressure, through a connecting line 13, to a pulse tube cold head 401. The pulse tube cold head 401 includes first stage regenerator 16’ having a warm end 16a’ and a cold end 16b’, second stage regenerator 20 attached to the cold end 16b’ of the first stage regenerator 16’ and having a cold end 20b, first stage pulse tube 17 having a warm flow smoother 17a at a warm end and a cold flow smoother 17b at a cold end, second stage pulse tube 21 having a warm flow smoother 21a at a warm end and a cold flow smoother 21b at a cold end, a line 18 connecting the regenerator cold end 16b’ to the cold flow smoother 17b of the pulse tube 17, a line 22 connecting the regenerator cold end 20b to the cold flow smoother 21b of the pulse tube 21, a line 7 extending from the connecting line 13 to the warm end 16a’ of the regenerator 16, lines 6a and 9a extending from the line 7 to double-inlet valves la, lines 6a’ and 9a’ extending from the line 7 to double-inlet valves Id, a line 5 from the warm flow smoother 17a of the pulse tube 17 to a buffer volume 15 through a single-inlet valve 4, and a line 5a from the warm flow smoother 21a of the pulse tube 21 to a buffer volume 15a through a single-inlet valve 4a, lines 8a and 9b from the double-inlet valve la to the line 5 and to the warm flow smoother 17a of the pulse tube 17, and lines 8a’ and 9b’ from the double-inlet valve Id to the line 5a and to the warm flow smoother 21a of the pulse tube 21. Double-inlet valve la has been found to give the best results for the present design. For other designs that have different pulse tube and regenerator sizes, double-inlet valves lb and 1c may be preferred. Double-inlet valve la or Id can be solely used on either the first or the second stage of the two stage GM type double-inlet pulse tube cold head 401, combined with a conventional double-inlet valve 2a on the other stage. The terms and descriptions used herein are set forth by way of illustration only and are not meant as limitations. Those skilled in the art will recognize that many variations are possible within the spirit and scope of the invention and the embodiments described herein.