Patent Publication Number: US-2022221198-A1

Title: Asynchronous drive of cryocooling systems for low temperature applications

Description:
BACKGROUND 
     The subject disclosure relates to cryogenic environments, and more specifically, to techniques of facilitating mechanical vibration management for cryogenic environments. 
     SUMMARY 
     The following presents a summary to provide a basic understanding of one or more embodiments of the invention. This summary is not intended to identify key or critical elements, or delineate any scope of the particular embodiments or any scope of the claims. Its sole purpose is to present concepts in a simplified form as a prelude to the more detailed description that is presented later. In one or more embodiments described herein, systems, devices, computer-implemented methods, and/or computer program products that facilitate mechanical vibration management for cryogenic environments are described. 
     According to an embodiment, a system can comprise a processor that executes computer executable components stored in memory. The computer executable components can comprise a linearization component and a drive component. The linearization component can translate data indicative of a nonlinear drive signal into a linear drive signal. The drive component can dynamically control operation of a compressor of a cryocooler using the linear drive signal. The cryocooler can provide cooling capacity for a cryogenic environment. 
     According to another embodiment, a computer-implemented method can comprise translating, by a system operatively coupled to a processor, data indicative of a nonlinear drive signal into a linear drive signal. The computer-implemented method can further comprise dynamically controlling, by the system, operation of a compressor of a cryocooler using the linear drive signal. The cryocooler can provide cooling capacity for a cryogenic environment. 
     According to another embodiment, a computer program product can comprise a computer readable storage medium having program instructions embodied therewith. The program instructions are executable by a processor to cause the processor to perform operations. The operations can include translate, by the processor, data indicative of a nonlinear drive signal into a linear drive signal. The operations can further include dynamically control, by the processor, operation of a compressor of a cryocooler using the linear drive signal. The cryocooler can provide cooling capacity for a cryogenic environment. 
    
    
     
       DESCRIPTION OF THE DRAWINGS 
         FIG. 1  illustrates a block diagram of an example, non-limiting system that can facilitate mechanical vibration management for cryogenic environments, in accordance with one or more embodiments described herein. 
         FIG. 2  illustrates an example, non-limiting cryostat, in accordance with one or more embodiments described herein. 
         FIG. 3  illustrates an example, non-limiting isometric view depicting multiple pulse tube systems coupled with the cryostat of  FIG. 2 , in accordance with one or more embodiments described herein. 
         FIG. 4  illustrates an example, non-limiting pulse tube system, in accordance with one or more embodiments described herein. 
         FIG. 5  illustrates an example, non-limiting graph depicting a non-linear drive signal. 
         FIG. 6  illustrates an example, non-limiting graph depicting mechanical vibrations generated by a cryocooler driven by a non-linear drive signal. 
         FIG. 7  illustrates an example, non-limiting graph depicting amplitude spectral density versus frequency. 
         FIG. 8  illustrates an example, non-limiting graph depicting a linear drive signal, in accordance with one or more embodiments described herein. 
         FIG. 9  illustrates an example, non-limiting graph depicting in-phase linear drive signals, in accordance with one or more embodiments described herein. 
         FIG. 10  illustrates an example, non-limiting graph depicting out-of-phase linear drive signals, in accordance with one or more embodiments described herein. 
         FIG. 11  illustrates an example, non-limiting graph depicting relative phase shifts between multiple linear drive signals, in accordance with one or more embodiments described herein. 
         FIG. 12  illustrates an example, non-limiting graph depicting temperature of a Mixing Chamber stage versus time, in accordance with one or more embodiments described herein. 
         FIG. 13  illustrates a block diagram of an example, non-limiting system that can facilitate mechanical vibration management for cryogenic environments, in accordance with one or more embodiments described herein. 
         FIG. 14  illustrates a flow diagram of an example, non-limiting computer-implemented method of facilitating mechanical vibration management for cryogenic environments, in accordance with one or more embodiments described herein. 
         FIG. 15  illustrates a block diagram of an example, non-limiting operating environment in which one or more embodiments described herein can be facilitated. 
     
    
    
     DETAILED DESCRIPTION 
     The following detailed description is merely illustrative and is not intended to limit embodiments and/or application or uses of embodiments. Furthermore, there is no intention to be bound by any expressed or implied information presented in the preceding Background or Summary sections, or in the Detailed Description section. 
     One or more embodiments are now described with reference to the drawings, wherein like referenced numerals are used to refer to like elements throughout. In the following description, for purposes of explanation, numerous specific details are set forth in order to provide a more thorough understanding of the one or more embodiments. It is evident, however, in various cases, that the one or more embodiments can be practiced without these specific details. 
       FIG. 1  illustrates a block diagram of an example, non-limiting system  100  that can facilitate mechanical vibration management for cryogenic environments, in accordance with one or more embodiments described herein. System  100  includes memory  110  for storing computer-executable components and one or more processors  120  operably coupled via one or more communication busses  130  to memory  110  for executing the computer-executable components stored in memory  110 . As shown in  FIG. 1 , the computer-executable components can include linearization component  140  and drive component  150 . 
     Linearization component  140  can translate data indicative of a nonlinear drive signal into a linear drive signal. For example, linearization component  140  can receive a nonlinear drive signal and convert the nonlinear drive signal into a linear drive signal. Drive component  150  can dynamically control operation of a compressor of a cryocooler using the linear drive signal. The cryocooler can provide cooling capacity for a cryogenic environment. In an embodiment, the cryocooler can be a regenerative cryocooler. In an embodiment, the cryocooler can be a Stirling cryocooler, a pulse tube cryocooler, and/or a Gifford McMahon cryocooler. In an embodiment, drive component  150  can modify the linear drive signal to terminate operation of the compressor when an operational state of the cryocooler transitions from a healthy operational state to a failing operational state. 
     In an embodiment, the computer-executable components stored in memory  110  can further include asynchronization component  160  and monitor component  170 . Asynchronization component  160  can modify a phase of the linear drive signal relative to a corresponding phase of a drive signal associated with an additional cryocooler based on a feedback signal. The feedback signal can be generated using sensor data indicative of mechanical vibrations associated with the cryogenic environment. The drive signal can control operation of a corresponding compressor of the additional cryocooler that provides cooling capacity for the cryogenic environment. In an embodiment, asynchronization component  160  can modify the phase of the linear drive signal to facilitate asynchronous operation of the compressor and the corresponding compressor. 
     Monitor component  170  can generate a feedback signal using sensor data indicative of mechanical vibrations associated with the cryogenic environment. In an embodiment, monitor component  170  can identify an operational state of the cryocooler by evaluating an operational parameter of the cryocooler. In an embodiment, the operational parameter can include: a low-pressure level of a coolant medium, a high-pressure level of the coolant medium, a pressure differential, a compressor temperature, a cold head temperature, a cold head vibration level, or a combination thereof. The functionality of the computer-executable components utilized by the embodiments will be covered in greater detail below. 
       FIG. 2  illustrates an example, non-limiting cryostat  200 , in accordance with one or more embodiments described herein. As shown in  FIG. 2 , cryostat  200  comprises an outer vacuum chamber  210  formed by a sidewall  220  intervening between a top plate  230  and a bottom plate  240 . In operation, outer vacuum chamber  210  can maintain a pressure differential between an ambient environment  250  of outer vacuum chamber  210  and an interior  260  of outer vacuum chamber  210 . Cryostat  200  further comprises a plurality of thermal stages (or stages)  270  disposed within interior  260  that are each mechanically coupled to top plate  230 . The plurality of stages  270  includes: stage  271 , stage  273 , stage  275 , stage  277 , and stage  279 . Each stage among the plurality of stages  270  can be associated with a different temperature. For example, stage  271  can be a 50-kelvin (50-K) stage that is associated with a temperature of 50 kelvin (K), stage  273  can be a 4-kelvin (4-K) stage that is associated with a temperature of 4 K, stage  275  can be associated with a temperature of 700 millikelvin (mK), stage  277  can be associated with a temperature of 100 mK, and stage  279  can be associated with a temperature of 10 mK. Each stage among the plurality of stages  270  is spatially isolated from other stages of the plurality of stages  270  by a plurality of support rods (e.g., support rods  272  and  274 ). In an embodiment, stage  275  can be a Still stage, stage  277  can be a Cold Plate stage, and stage  279  can be a Mixing Chamber stage. 
       FIG. 3  illustrates an example, non-limiting isometric view  300  depicting multiple pulse tube systems  310  coupled with the cryostat  200  of  FIG. 2 , in accordance with one or more embodiments described herein. As shown by  FIG. 3 , each pulse tube system  310  includes a pair of buffer volumes  312  and a motor head  314  positioned on a frame structure  320  providing mechanical support to cryostat  200 . Each pulse tube system  310  further includes a pulse tube head  316  positioned on top plate  230  of cryostat  200 . One skilled in the art will recognize that each pulse tube system  310  can be coupled with a compressor (not shown) to form a cryocooler providing cooling capacity for cryostat  200 . In an embodiment, the cryocooler can be a regenerative cryocooler. In an embodiment, the cryocooler can be a Stirling cryocooler, a pulse tube cryocooler, and/or a Gifford McMahon cryocooler. 
       FIG. 4  illustrates an example, non-limiting pulse tube system  400 , in accordance with one or more embodiments described herein. As shown by  FIG. 4 , pulse tube system  400  comprises a high-pressure inlet  412 , a low-pressure inlet  414 , a motor head  420 , a motor line  430 , a top plate flange  440 , a 50-K stage flange  450 , a 4-K stage flange  460 , and buffer volumes  470 . High-pressure inlet  412  and low-pressure inlet  414  can couple pulse tube system  400  to an outlet port and an inlet port of a compressor, respectively. High-pressure inlet  412  and low-pressure inlet  414  can couple a rotary valve of motor head  420  with the outlet and inlet ports of the compressor, respectively. Top plate flange  440  can couple to a top plate of an outer vacuum chamber at room temperature. For example, top plate flange  440  can couple to top plate  230  of outer vacuum chamber  210 . 50-K stage flange  450  and 4-K stage flange  460  can each couple to thermal stages of a cryostat enclosed within the outer vacuum chamber. For example, 50-K stage flange  450  and 4-K stage flange  460  can couple to stages  271  and  273  of cryostat  200 , respectively. 
     In operation, high-pressure coolant medium can be supplied to a high-pressure inlet  412  and low-pressure coolant medium can be pumped from a low-pressure inlet  414  responsive to a drive signal that the compressor receives at an input to control operation of the compressor. Example coolant mediums can include helium, hydrogen, nitrogen, and the like. A rotary valve of motor head  420  alternatively connects a low-pressure coolant medium from top plate flange  440  (and buffer volumes  470 ) to an inlet port of a compressor via low-pressure inlet  414  and a high-pressure coolant medium from an outlet port of the compressor to top plate flange  440  via high-pressure inlet  412 . As such, the rotary valve can generate an oscillating compression-expansion cycle of the coolant medium that facilitates reducing a temperature of 50-K stage  450  and 4-K stage flange  460 . 
     To that end, high-pressure coolant medium from the rotary valve of motor head  420  flows towards 50-K stage flange  450  and 4-K stage flange  460 . 50-K stage flange  450  and 4-K flange stage  460  facilitate heat exchange between the high-pressure coolant medium and the respective thermal stages. The high-pressure coolant medium transitions to low-pressure coolant medium via expansion. Heat from the respective thermal stages can be transferred with the low-pressure coolant medium as that coolant medium flows towards buffer volumes  470 . By transferring heat away from the respective thermal stages, a reduction of temperature can occur at each thermal stage. The low-pressure coolant medium collected in buffer volumes  470  flows toward the inlet port of the compressor via the rotary valve of motor head  420  and low-pressure inlet  414  to close a cycle of the coolant medium between pulse tube system  400  and the compressor. 
     Operation of some compressors can be controlled by non-linear drive signals as input.  FIG. 5  illustrates an example, non-limiting graph  500  depicting a non-linear drive signal  510 . As shown by  FIG. 5 , non-linear drive signal  510  can transition between a first amplitude level  520  and a second amplitude level  530  at each transition time. Responsive to receiving drive signal  510  at first amplitude level  520 , a compressor can supply high-pressure coolant medium to a high-pressure inlet (e.g., high-pressure inlet  412 ) of a pulse tube system. Responsive to receiving drive signal  510  at second amplitude level  530 , a compressor can pump low-pressure coolant medium from a low-pressure inlet (e.g., low-pressure inlet  414 ) of the pulse tube system. 
     As discussed above with respect to  FIG. 4 , coolant medium is alternatively transferred between a motor head and a top plate flange of the pulse tube system via a motor line coupling the motor head and the top plate flange by operation of a rotary valve within the motor head. In particular, the rotary valve alternately connects the top plate flange and/or associated buffer volumes with the high-pressure and low-pressure inlets to facilitate a flow of the coolant medium towards (at a high-pressure) and from (at a low-pressure) the top plate flange, respectively. Oscillating pressures in the coolant medium transferred between the motor head and the top plate flange via the motor line can generate low frequency pressure waves within the motor line. Such low frequency pressure waves within the motor line can impart low frequency mechanical vibrations on the top plate flange that can transfer to thermal stages of a cryostat via flanges (e.g., 50-K stage flange  450  and 4-K stage flange  460 ) of the pulse tube system that couple with the thermal stages to facilitate heat exchange. 
       FIG. 6  illustrates an example, non-limiting graph  600  depicting mechanical vibrations generated by a cryocooler driven by a non-linear drive signal (e.g., non-linear drive signal  510  of  FIG. 5 ). As shown by graph  600 , such mechanical vibrations can include a fundamental frequency component  610  centered at approximately 1 Hertz (Hz) and various harmonic components (e.g., harmonic components  620  and  630 ). 
       FIG. 7  illustrates an example, non-limiting graph  700  depicting amplitude spectral density versus frequency. As shown by graph  700 , such mechanical vibrations can persist without regard to whether a pulse tube system is operational. For example, waveform  710  corresponds to mechanical vibrations associated with a non-operational pulse tube system and waveform  720  corresponds to an operational pulse tube system. 
     In accordance with various embodiments disclosed herein, operation of a compressor associated with a cryocooler can be controlled using linear drive signals as input.  FIG. 8  illustrates an example, non-limiting graph  800  depicting a linear drive signal  810 . As shown by  FIG. 8 , non-linear drive signal  810  can transition between a first amplitude level  820  and a second amplitude level  830  at each transition time. Responsive to receiving drive signal  810  at first amplitude level  820 , a compressor can supply high-pressure coolant medium to a high-pressure inlet (e.g., high-pressure inlet  412 ) of a pulse tube system. Responsive to receiving drive signal  810  at second amplitude level  830 , a compressor can pump low-pressure coolant medium from a low-pressure inlet (e.g., low-pressure inlet  414 ) of the pulse tube system. 
     A comparison between  FIGS. 5 and 8  illustrates an aspect of how linear drive signals can facilitate mitigating mechanical vibrations generated by a cryocooler by reducing a frequency of pressure waves within a motor line of a pulse tube system. For example,  FIG. 5  shows that non-linear drive signal  500  can abruptly transition from a second amplitude level  530  to a first amplitude level  520  at transition time t 2 . In this example, a compressor receiving non-linear drive signal  500  as input can abruptly transition from pumping low-pressure coolant medium from a low-pressure inlet of a pulse tube system to supplying high-pressure coolant medium to a high-pressure inlet of the pulse tube system. As such, oscillating pressures in the coolant medium transferred between a motor head and a top plate flange of the pulse tube system via a motor line can generate pressure waves within the motor line. Those pressure waves within the motor line can have a frequency that is associated with a rate at which the compressor switches from pumping low-pressure coolant medium from the low-pressure inlet to supplying high-pressure coolant medium to the high-pressure inlet. The pressure waves within the motor line can impart mechanical vibrations on the top plate flange that can transfer to thermal stages of a cryostat. Such mechanical vibrations can have a frequency that corresponds to the frequency of the pressure waves. 
     In contrast, a compressor receiving linear drive signal  800  as input can gradually switches from pumping low-pressure coolant medium from a low-pressure inlet to supplying high-pressure coolant medium to a high-pressure inlet. For example,  FIG. 8  shows that linear drive signal  800  can steadily transition from a second amplitude level  830  to a first amplitude level  820  over a duration defined by transition time t 1  and transition time t 2 . In this example, a compressor receiving linear drive signal  800  as input can gradually transition from pumping low-pressure coolant medium from a low-pressure inlet of a pulse tube system to supplying high-pressure coolant medium to a high-pressure inlet of the pulse tube system over the duration defined by transition time t 1  and transition time t 2 . That gradual transition can facilitate dampening pressure waves within the motor line. As such, that gradual transition can facilitate mitigating mechanical vibrations that such pressure waves impart on the top plate flange that can transfer to thermal stages of a cryostat. 
     As discussed above with respect to  FIG. 3 , multiple pulse tube systems can be coupled with a cryostat. Each pulse tube system can be coupled with a compressor to form a cryocooler providing cooling capacity for the cryostat. Operation of each cryocooler can involve oscillating pressures in a coolant medium that generate pressure waves within a motor line of a given pulse tube system. As such, each cryocooler can represent a distinct source of mechanical vibrations imparted on thermal stages of the cryostat. Various embodiments disclosed herein can facilitate management of mechanical vibrations generated by multiple cryocoolers providing cooling capacity to a cryostat by modifying relative phases of linear drive signals. To that end, relative phases of linear drive signals controlling respective compressors of the multiple cryocoolers can be modified to facilitate asynchronous operation of those compressors. 
       FIG. 9  illustrates an example, non-limiting graph  900  depicting in-phase linear drive signals, in accordance with one or more embodiments described herein. In  FIG. 9 , linear drive signal  910  can control operation of a first compressor associated with a cryocooler and linear drive signal  920  can control operation of a second compressor associated with the cryostat. As shown by  FIG. 9 , linear drive signals  910  and  920  are in-phase. Accordingly, linear drive signals  910  and  920  can facilitate synchronous operation of the first and second compressors. By operating synchronously, the first and second compressors can synchronously impart mechanical vibrations on thermal stages of the cryostat. 
     A magnitude of the synchronously imparted mechanical vibrations can be greater than a sum of the respective magnitudes of mechanical vibrations imparted by the first and second compressors. One aspect of that additional mechanical vibration magnitude realized by synchronously operating the first and second compressors relates to constructive interference. For example, the first and second compressors can be construed as a common vibrational source from the perspective of the cryostat. That common vibrational source would be driven by a linear drive signal  930  having a greater amplitude than the respective amplitudes of linear drive signals  910  and  920  combined. That greater amplitude of linear drive signal  930  results from constructive interference created by virtue of linear drive signals  910  and  920  being in-phase. The greater amplitude of the linear drive signal  930  driving the common vibrational source can correspond with a higher magnitude of mechanical vibrations imparted on the cryostat. 
       FIG. 10  illustrates an example, non-limiting graph  1000  depicting out-of-phase linear drive signals, in accordance with one or more embodiments described herein. In  FIG. 10 , linear drive signal  1010  can control operation of a first compressor associated with a cryocooler and linear drive signal  1020  can control operation of a second compressor associated with the cryostat. As shown by  FIG. 10 , linear drive signals  1010  and  1020  are out-of-phase by 180 degrees. Accordingly, linear drive signals  1010  and  1020  can facilitate asynchronous operation of the first and second compressors. By operating asynchronously, the first and second compressors can asynchronously impart mechanical vibrations on thermal stages of the cryostat. 
     A magnitude of the asynchronously imparted mechanical vibrations can be less than a sum of the respective magnitudes of mechanical vibrations imparted by the first and second compressors. One aspect of that reduced mechanical vibration magnitude realized by asynchronously operating the first and second compressors relates to destructive interference. For example, the first and second compressors can be construed as a common vibrational source from the perspective of the cryostat. That common vibrational source would be driven by a linear drive signal  1030  having a lower amplitude than the respective amplitudes of linear drive signals  1010  and  1020  combined. That lower amplitude of linear drive signal  1030  results from destructive interference created by virtue of linear drive signals  1010  and  1020  out-of-phase by 180 degrees. The lower amplitude of the linear drive signal  1030  driving the common vibrational source can correspond with a lower magnitude of mechanical vibrations imparted on the cryostat. 
       FIG. 11  illustrates an example, non-limiting graph  1100  depicting relative phase shifts between multiple linear drive signals, in accordance with one or more embodiments described herein. In particular, line  1110  corresponds to a phase of a first linear drive signal, line  1120  corresponds to a phase of a second linear drive signal, and line  1130  corresponds to a phase of a third linear drive signal. 
       FIG. 12  illustrates an example, non-limiting graph  1200  depicting temperature of a Mixing Chamber stage versus time, in accordance with one or more embodiments described herein. Graph  1200  shows that controlling compressor operation using linear drive signals can facilitate improving a stability of the temperature of the Mixing Chamber stage than can be achieved using non-linear drive signals. 
       FIG. 13  illustrates a block diagram of an example, non-limiting system  1300  that can facilitate mechanical vibration management for cryogenic environments, in accordance with one or more embodiments described herein. System  1300  includes controller  1310 , cryocooler  1330 , cryocooler  1340 , and cryocooler  1350 . Cryocoolers  1330 ,  1340 , and  1350  can each provide cooling capacity for a cryogenic environment (e.g., cryostat  200  of  FIGS. 2-3 ). To that end, a pulse tube system of each regenerative cryocooler can be coupled to the cryogenic environment. For example, pulse tube systems  1334 ,  1344 , and/or  1354  can each be coupled to the cryogenic environment as illustrated in  FIG. 3 . In an embodiment, pulse tube systems  1334 ,  1344 , and/or  1354  can be implemented using pulse tube system  400  of  FIG. 4 . In an embodiment, cryocoolers  1330 ,  1340 , and/or  1350  can be a regenerative cryocooler. In an embodiment, cryocoolers  1330 ,  1340 , and/or  1350  can be a Stirling cryocooler, a pulse tube cryocooler, and/or a Gifford McMahon cryocooler. 
     Each cryocooler can include a compressor that supplies high-pressure coolant medium to a high-pressure inlet (e.g., high-pressure inlet  412  of  FIG. 4 ) of a corresponding pulse tube system and pumps low-pressure coolant medium from a low-pressure inlet (e.g., low-pressure inlet  414 ) responsive to a drive signal. For example, compressor  1332  can exchange a coolant medium with pulse tube system  1334 , compressor  1342  can exchange a coolant medium with pulse tube system  1344 , and compressor  1352  can exchange a coolant medium with pulse tube system  1354 . Each compressor can receive a corresponding drive signal from controller  1310  via a network  1320  that communicatively couples controller  1310  with each compressor. 
     In operation, controller  1310  can centrally orchestrate (or manage) operation of cryocoolers  1330 ,  1340 , and  1350  using linear drive signals that dynamically control operation of each respective compressor. By centrally orchestrating operation of each cryocooler, controller  1310  can facilitate reducing mechanical vibrations associated with the cryogenic environment. Centrally orchestrating operation of each cryocooler can include controller  1310  identifying (e.g., with monitor component  170 ) an operational state of each cryocooler. 
     Controller  1310  can identify the operational state of each cryocooler by evaluating one or more operational parameters of each cryocooler. Example operational parameters can include a low-pressure level of a coolant medium, a high-pressure level of the coolant medium, a pressure differential, a compressor temperature, a cold head temperature, a cold head vibration level, or a combination thereof. In an embodiment, controller  1310  can receive data indicative of the one or more operational parameters of each cryocooler via network  1320 . Controller  1310  can evaluate the one or more operational parameters using a predefined threshold value and/or a predefined tolerance range for that threshold value for each operational parameter. 
     If such evaluation determines that the one or more operational parameters for a given cryocooler each satisfy a corresponding predefined threshold value and/or a corresponding predefined tolerance range for that threshold value, controller  1310  can identify an operational state of the given cryocooler as being a healthy operational state. When controller  1310  identifies the given cryocooler as being in the healthy operational state, controller  1310  can permit a respective compressor of the given cryocooler to continue operation. 
     If such evaluation determines that, at least, one operational parameter among the one or more operational parameters for a given cryocooler fails to satisfy a corresponding predefined threshold value and/or a corresponding predefined tolerance range for that threshold value, controller  1310  can identify an operational state of the given cryocooler as being a failing operational state. When controller  1310  identifies the given cryocooler as being in the failing operational state, controller  1310  can modify a linear drive signal of a respective compressor of the given cryocooler to terminate operation of that compressor. 
     By way of example, at a first time, controller  1310  can evaluate respective operational parameters of cryocoolers  1330 ,  1340 , and  1350 . Through such evaluation at the first time, controller  1310  can identify cryocoolers  1330 ,  1340 , and  1350  as each being in a healthy operational state. Accordingly, at the first time, controller  1310  can permit respective compressors of cryocoolers  1330 ,  1340 , and  1350  to continue operation. At a second time after the first time, controller  1310  can again evaluate respective operational parameters of cryocoolers  1330 ,  1340 , and  1350 . Through such evaluation at the second time, controller  1310  can identify cryocoolers  1330  and  1350  as each being in a healthy operational state. Accordingly, at the second time, controller  1310  can permit compressors  1332  and  1352  of cryocoolers  1330  and  1350 , respectively, to continue operation. However, controller  1310  can determine that cryocooler  1340  has transitioned from a healthy operational state to a failing operational state from that evaluation at the second time. As such, controller  1310  can modify a linear drive signal of compressor  1342  to terminate operation of compressor  1342  at the second time. For example, controller  1310  can modify the linear drive signal of compressor  1342  to an amplitude value that causes compressor  1342  to cease exchanging a coolant medium with pulse tube system  1344 . 
       FIG. 14  illustrates a flow diagram of an example, non-limiting computer-implemented method  1400  of facilitating mechanical vibration management for cryogenic environments, in accordance with one or more embodiments described herein. Repetitive description of like elements employed in other embodiments described herein is omitted for sake of brevity. At  1410 , the computer-implemented method  1400  can comprise translating (e.g., with linearization component  140 ), by a system operatively coupled to a processor, data indicative of a nonlinear drive signal into a linear drive signal. At  1420 , the computer-implemented method  1400  can comprise dynamically controlling, by the system (e.g., with drive component  150 ), operation of a compressor of a cryocooler using the linear drive signal. The cryocooler can provide cooling capacity for a cryogenic environment. In an embodiment, the cryocooler can be a regenerative cryocooler. In an embodiment, the cryocooler can be a Stirling cryocooler, a pulse tube cryocooler, and/or a Gifford McMahon cryocooler. 
     In an embodiment, the computer-implemented method  1400  can further comprise: modifying, by the system (e.g., with asynchronization component  160 ), a phase of the linear drive signal relative to a corresponding phase of a drive signal associated with an additional cryocooler based on a feedback signal generated using sensor data indicative of mechanical vibrations associated with the cryogenic environment. The drive signal can control operation of a corresponding compressor of the additional cryocooler that provides cooling capacity for the cryogenic environment. In an embodiment, modifying the phase of the linear drive signal can facilitate asynchronous operation of the compressor and the corresponding compressor. In an embodiment, modifying the phase of the linear drive signal can facilitate management of mechanical vibrations generated by the cryocooler. 
     In an embodiment, the computer-implemented method  1400  can further comprise: generating, by the system (e.g., with monitor component  170 ), a feedback signal using sensor data indicative of mechanical vibrations associated with the cryogenic environment. In an embodiment, the computer-implemented method  1400  can further comprise: identifying, by the system (e.g., with monitor component  170 ), an operational state of the cryocooler by evaluating an operational parameter of the cryocooler. In an embodiment, the operational parameter can include: a low-pressure level of a coolant medium, a high-pressure level of the coolant medium, a pressure differential, a compressor temperature, a cold head temperature, a cold head vibration level, or a combination thereof. 
     In an embodiment, the computer-implemented method  1400  can further comprise: modifying, by the system (e.g., with drive component  150 ), the linear drive signal to terminate operation of the compressor when an operational state of the cryocooler transitions from a healthy operational state to a failing operational state. 
     In order to provide a context for the various aspects of the disclosed subject matter,  FIG. 15  as well as the following discussion are intended to provide a general description of a suitable environment in which the various aspects of the disclosed subject matter can be implemented.  FIG. 15  illustrates a suitable operating environment  1500  for implementing various aspects of this disclosure can also include a computer  1512 . The computer  1512  can also include a processing unit  1514 , a system memory  1516 , and a system bus  1518 . The system bus  1518  couples system components including, but not limited to, the system memory  1516  to the processing unit  1514 . The processing unit  1514  can be any of various available processors. Dual microprocessors and other multiprocessor architectures also can be employed as the processing unit  1514 . The system bus  1518  can be any of several types of bus structure(s) including the memory bus or memory controller, a peripheral bus or external bus, and/or a local bus using any variety of available bus architectures including, but not limited to, Industrial Standard Architecture (ISA), Micro-Channel Architecture (MSA), Extended ISA (EISA), Intelligent Drive Electronics (IDE), VESA Local Bus (VLB), Peripheral Component Interconnect (PCI), Card Bus, Universal Serial Bus (USB), Advanced Graphics Port (AGP), Firewire (IEEE 1094), and Small Computer Systems Interface (SCSI). The system memory  1516  can also include volatile memory  1520  and nonvolatile memory  1522 . The basic input/output system (BIOS), containing the basic routines to transfer information between elements within the computer  1512 , such as during start-up, is stored in nonvolatile memory  1522 . By way of illustration, and not limitation, nonvolatile memory  1522  can include read only memory (ROM), programmable ROM (PROM), electrically programmable ROM (EPROM), electrically erasable programmable ROM (EEPROM), flash memory, or nonvolatile random-access memory (RAM) (e.g., ferroelectric RAM (FeRAM). Volatile memory  1520  can also include random access memory (RAM), which acts as external cache memory. By way of illustration and not limitation, RAM is available in many forms such as static RAM (SRAM), dynamic RAM (DRAM), synchronous DRAM (SDRAM), double data rate SDRAM (DDR SDRAM), enhanced SDRAM (ESDRAM), Synchlink DRAM (SLDRAM), direct Rambus RAM (DRRAM), direct Rambus dynamic RAM (DRDRAM), and Rambus dynamic RAM. 
     Computer  1512  can also include removable/non-removable, volatile/non-volatile computer storage media.  FIG. 15  illustrates, for example, a disk storage  1524 . Disk storage  1524  can also include, but is not limited to, devices like a magnetic disk drive, floppy disk drive, tape drive, Jaz drive, Zip drive, LS-100 drive, flash memory card, or memory stick. The disk storage  1524  also can include storage media separately or in combination with other storage media including, but not limited to, an optical disk drive such as a compact disk ROM device (CD-ROM), CD recordable drive (CD-R Drive), CD rewritable drive (CD-RW Drive) or a digital versatile disk ROM drive (DVD-ROM). To facilitate connection of the disk storage  1524  to the system bus  1518 , a removable or non-removable interface is typically used, such as interface  1526 .  FIG. 15  also depicts software that acts as an intermediary between users and the basic computer resources described in the suitable operating environment  1500 . Such software can also include, for example, an operating system  1528 . Operating system  1528 , which can be stored on disk storage  1524 , acts to control and allocate resources of the computer  1512 . System applications  1530  take advantage of the management of resources by operating system  1528  through program modules  1532  and program data  1534 , e.g., stored either in system memory  1516  or on disk storage  1524 . It is to be appreciated that this disclosure can be implemented with various operating systems or combinations of operating systems. A user enters commands or information into the computer  1512  through input device(s)  1536 . Input devices  1536  include, but are not limited to, a pointing device such as a mouse, trackball, stylus, touch pad, keyboard, microphone, joystick, game pad, satellite dish, scanner, TV tuner card, digital camera, digital video camera, web camera, and the like. These and other input devices connect to the processing unit  1514  through the system bus  1518  via interface port(s)  1538 . Interface port(s)  1538  include, for example, a serial port, a parallel port, a game port, and a universal serial bus (USB). Output device(s)  1540  use some of the same type of ports as input device(s)  1536 . Thus, for example, a USB port can be used to provide input to computer  1512 , and to output information from computer  1512  to an output device  1540 . Output adapter  1542  is provided to illustrate that there are some output devices  1540  like monitors, speakers, and printers, among other output devices  1540 , which require special adapters. The output adapters  1542  include, by way of illustration and not limitation, video and sound cards that provide a means of connection between the output device  1540  and the system bus  1518 . It can be noted that other devices and/or systems of devices provide both input and output capabilities such as remote computer(s)  1544 . 
     Computer  1412  can operate in a networked environment using logical connections to one or more remote computers, such as remote computer(s)  1544 . The remote computer(s)  1544  can be a computer, a server, a router, a network PC, a workstation, a microprocessor-based appliance, a peer device or other common network node and the like, and typically can also include many or the elements described relative to computer  1512 . For purposes of brevity, only a memory storage device  1546  is illustrated with remote computer(s)  1544 . Remote computer(s)  1544  is logically connected to computer  1512  through a network interface  1548  and then physically connected via communication connection  1550 . Network interface  1548  encompasses wire and/or wireless communication networks such as local-area networks (LAN), wide-area networks (WAN), cellular networks, etc. LAN technologies include Fiber Distributed Data Interface (FDDI), Copper Distributed Data Interface (CDDI), Ethernet, Token Ring and the like. WAN technologies include, but are not limited to, point-to-point links, circuit switching networks like Integrated Services Digital Networks (ISDN) and variations thereon, packet switching networks, and Digital Subscriber Lines (DSL). Communication connection(s)  1550  refers to the hardware/software employed to connect the network interface  1548  to the system bus  1518 . While communication connection  1550  is shown for illustrative clarity inside computer  1512 , it can also be external to computer  1512 . The hardware/software for connection to the network interface  1548  can also include, for exemplary purposes only, internal and external technologies such as, modems including regular telephone grade modems, cable modems and DSL modems, ISDN adapters, and Ethernet cards. 
     The present invention may be a system, a method, an apparatus and/or a computer program product at any possible technical detail level of integration. The computer program product can include a computer readable storage medium (or media) having computer readable program instructions thereon for causing a processor to carry out aspects of the present invention. The computer readable storage medium can be a tangible device that can retain and store instructions for use by an instruction execution device. The computer readable storage medium can be, for example, but is not limited to, an electronic storage device, a magnetic storage device, an optical storage device, an electromagnetic storage device, a semiconductor storage device, or any suitable combination of the foregoing. A non-exhaustive list of more specific examples of the computer readable storage medium can also include the following: a portable computer diskette, a hard disk, a random access memory (RAM), a read-only memory (ROM), an erasable programmable read-only memory (EPROM or Flash memory), a static random access memory (SRAM), a portable compact disc read-only memory (CD-ROM), a digital versatile disk (DVD), a memory stick, a floppy disk, a mechanically encoded device such as punch-cards or raised structures in a groove having instructions recorded thereon, and any suitable combination of the foregoing. A computer readable storage medium, as used herein, is not to be construed as being transitory signals per se, such as radio waves or other freely propagating electromagnetic waves, electromagnetic waves propagating through a waveguide or other transmission media (e.g., light pulses passing through a fiber-optic cable), or electrical signals transmitted through a wire. 
     Computer readable program instructions described herein can be downloaded to respective computing/processing devices from a computer readable storage medium or to an external computer or external storage device via a network, for example, the Internet, a local area network, a wide area network and/or a wireless network. The network can comprise copper transmission cables, optical transmission fibers, wireless transmission, routers, firewalls, switches, gateway computers and/or edge servers. A network adapter card or network interface in each computing/processing device receives computer readable program instructions from the network and forwards the computer readable program instructions for storage in a computer readable storage medium within the respective computing/processing device. Computer readable program instructions for carrying out operations of the present invention can be assembler instructions, instruction-set-architecture (ISA) instructions, machine instructions, machine dependent instructions, microcode, firmware instructions, state-setting data, configuration data for integrated circuitry, or either source code or object code written in any combination of one or more programming languages, including an object oriented programming language such as Smalltalk, C++, or the like, and procedural programming languages, such as the “C” programming language or similar programming languages. The computer readable program instructions can execute entirely on the user&#39;s computer, partly on the user&#39;s computer, as a stand-alone software package, partly on the user&#39;s computer and partly on a remote computer or entirely on the remote computer or server. In the latter scenario, the remote computer can be connected to the user&#39;s computer through any type of network, including a local area network (LAN) or a wide area network (WAN), or the connection can be made to an external computer (for example, through the Internet using an Internet Service Provider). In some embodiments, electronic circuitry including, for example, programmable logic circuitry, field-programmable gate arrays (FPGA), or programmable logic arrays (PLA) can execute the computer readable program instructions by utilizing state information of the computer readable program instructions to personalize the electronic circuitry, in order to perform aspects of the present invention. 
     Aspects of the present invention are described herein with reference to flowchart illustrations and/or block diagrams of methods, apparatus (systems), and computer program products according to embodiments of the invention. It will be understood that each block of the flowchart illustrations and/or block diagrams, and combinations of blocks in the flowchart illustrations and/or block diagrams, can be implemented by computer readable program instructions. These computer readable program instructions can be provided to a processor of a general purpose computer, special purpose computer, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, create means for implementing the functions/acts specified in the flowchart and/or block diagram block or blocks. These computer readable program instructions can also be stored in a computer readable storage medium that can direct a computer, a programmable data processing apparatus, and/or other devices to function in a particular manner, such that the computer readable storage medium having instructions stored therein comprises an article of manufacture including instructions which implement aspects of the function/act specified in the flowchart and/or block diagram block or blocks. The computer readable program instructions can also be loaded onto a computer, other programmable data processing apparatus, or other device to cause a series of operational acts to be performed on the computer, other programmable apparatus or other device to produce a computer implemented process, such that the instructions which execute on the computer, other programmable apparatus, or other device implement the functions/acts specified in the flowchart and/or block diagram block or blocks. 
     The flowchart and block diagrams in the Figures illustrate the architecture, functionality, and operation of possible implementations of systems, methods, and computer program products according to various embodiments of the present invention. In this regard, each block in the flowchart or block diagrams can represent a module, segment, or portion of instructions, which comprises one or more executable instructions for implementing the specified logical function(s). In some alternative implementations, the functions noted in the blocks can occur out of the order noted in the Figures. For example, two blocks shown in succession can, in fact, be executed substantially concurrently, or the blocks can sometimes be executed in the reverse order, depending upon the functionality involved. It will also be noted that each block of the block diagrams and/or flowchart illustration, and combinations of blocks in the block diagrams and/or flowchart illustration, can be implemented by special purpose hardware-based systems that perform the specified functions or acts or carry out combinations of special purpose hardware and computer instructions. 
     While the subject matter has been described above in the general context of computer-executable instructions of a computer program product that runs on a computer and/or computers, those skilled in the art will recognize that this disclosure also can or can be implemented in combination with other program modules. Generally, program modules include routines, programs, components, data structures, etc. that perform particular tasks and/or implement particular abstract data types. Moreover, those skilled in the art will appreciate that the inventive computer-implemented methods can be practiced with other computer system configurations, including single-processor or multiprocessor computer systems, mini-computing devices, mainframe computers, as well as computers, hand-held computing devices (e.g., PDA, phone), microprocessor-based or programmable consumer or industrial electronics, and the like. The illustrated aspects can also be practiced in distributed computing environments in which tasks are performed by remote processing devices that are linked through a communications network. However, some, if not all aspects of this disclosure can be practiced on stand-alone computers. In a distributed computing environment, program modules can be located in both local and remote memory storage devices. For example, in one or more embodiments, computer executable components can be executed from memory that can include or be comprised of one or more distributed memory units. As used herein, the term “memory” and “memory unit” are interchangeable. Further, one or more embodiments described herein can execute code of the computer executable components in a distributed manner, e.g., multiple processors combining or working cooperatively to execute code from one or more distributed memory units. As used herein, the term “memory” can encompass a single memory or memory unit at one location or multiple memories or memory units at one or more locations. 
     As used in this application, the terms “component,” “system,” “platform,” “interface,” and the like, can refer to and/or can include a computer-related entity or an entity related to an operational machine with one or more specific functionalities. The entities disclosed herein can be either hardware, a combination of hardware and software, software, or software in execution. For example, a component can be, but is not limited to being, a process running on a processor, a processor, an object, an executable, a thread of execution, a program, and/or a computer. By way of illustration, both an application running on a server and the server can be a component. One or more components can reside within a process and/or thread of execution and a component can be localized on one computer and/or distributed between two or more computers. In another example, respective components can execute from various computer readable media having various data structures stored thereon. The components can communicate via local and/or remote processes such as in accordance with a signal having one or more data packets (e.g., data from one component interacting with another component in a local system, distributed system, and/or across a network such as the Internet with other systems via the signal). As another example, a component can be an apparatus with specific functionality provided by mechanical parts operated by electric or electronic circuitry, which is operated by a software or firmware application executed by a processor. In such a case, the processor can be internal or external to the apparatus and can execute at least a part of the software or firmware application. As yet another example, a component can be an apparatus that provides specific functionality through electronic components without mechanical parts, wherein the electronic components can include a processor or other means to execute software or firmware that confers at least in part the functionality of the electronic components. In an aspect, a component can emulate an electronic component via a virtual machine, e.g., within a cloud computing system. 
     In addition, the term “or” is intended to mean an inclusive “or” rather than an exclusive “or.” That is, unless specified otherwise, or clear from context, “X employs A or B” is intended to mean any of the natural inclusive permutations. That is, if X employs A; X employs B; or X employs both A and B, then “X employs A or B” is satisfied under any of the foregoing instances. Moreover, articles “a” and “an” as used in the subject specification and annexed drawings should generally be construed to mean “one or more” unless specified otherwise or clear from context to be directed to a singular form. As used herein, the terms “example” and/or “exemplary” are utilized to mean serving as an example, instance, or illustration. For the avoidance of doubt, the subject matter disclosed herein is not limited by such examples. In addition, any aspect or design described herein as an “example” and/or “exemplary” is not necessarily to be construed as preferred or advantageous over other aspects or designs, nor is it meant to preclude equivalent exemplary structures and techniques known to those of ordinary skill in the art. 
     As it is employed in the subject specification, the term “processor” can refer to substantially any computing processing unit or device comprising, but not limited to, single-core processors; single-processors with software multithread execution capability; multi-core processors; multi-core processors with software multithread execution capability; multi-core processors with hardware multithread technology; parallel platforms; and parallel platforms with distributed shared memory. Additionally, a processor can refer to an integrated circuit, an application specific integrated circuit (ASIC), a digital signal processor (DSP), a field programmable gate array (FPGA), a programmable logic controller (PLC), a complex programmable logic device (CPLD), a discrete gate or transistor logic, discrete hardware components, or any combination thereof designed to perform the functions described herein. Further, processors can exploit nano-scale architectures such as, but not limited to, molecular and quantum-dot based transistors, switches and gates, in order to optimize space usage or enhance performance of user equipment. A processor can also be implemented as a combination of computing processing units. In this disclosure, terms such as “store,” “storage,” “data store,” data storage,” “database,” and substantially any other information storage component relevant to operation and functionality of a component are utilized to refer to “memory components,” entities embodied in a “memory,” or components comprising a memory. It is to be appreciated that memory and/or memory components described herein can be either volatile memory or nonvolatile memory, or can include both volatile and nonvolatile memory. By way of illustration, and not limitation, nonvolatile memory can include read only memory (ROM), programmable ROM (PROM), electrically programmable ROM (EPROM), electrically erasable ROM (EEPROM), flash memory, or nonvolatile random access memory (RAM) (e.g., ferroelectric RAM (FeRAM). Volatile memory can include RAM, which can act as external cache memory, for example. By way of illustration and not limitation, RAM is available in many forms such as synchronous RAM (SRAM), dynamic RAM (DRAM), synchronous DRAM (SDRAM), double data rate SDRAM (DDR SDRAM), enhanced SDRAM (ESDRAM), Synchlink DRAM (SLDRAM), direct Rambus RAM (DRRAM), direct Rambus dynamic RAM (DRDRAM), and Rambus dynamic RAM (RDRAM). Additionally, the disclosed memory components of systems or computer-implemented methods herein are intended to include, without being limited to including, these and any other suitable types of memory. 
     What has been described above include mere examples of systems and computer-implemented methods. It is, of course, not possible to describe every conceivable combination of components or computer-implemented methods for purposes of describing this disclosure, but one of ordinary skill in the art can recognize that many further combinations and permutations of this disclosure are possible. Furthermore, to the extent that the terms “includes,” “has,” “possesses,” and the like are used in the detailed description, claims, appendices and drawings such terms are intended to be inclusive in a manner similar to the term “comprising” as “comprising” is interpreted when employed as a transitional word in a claim. 
     The descriptions of the various embodiments have been presented for purposes of illustration, but are not intended to be exhaustive or limited to the embodiments disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the described embodiments. The terminology used herein was chosen to best explain the principles of the embodiments, the practical application or technical improvement over technologies found in the marketplace, or to enable others of ordinary skill in the art to understand the embodiments disclosed herein.