1 Introduction

Concerns over environmental influence of hazardous refrigerants have impelled the researchers to searching and developing alternative cooling technologies as well as more environmentally friendly refrigerants. One of the most promising approaches in the class of new technologies is the thermoacoustic refrigeration [1, 2]. Thermoacoustic refrigerators are the machines which use sound to produce cooling power. They are mainly composed of an acoustic driver attached to an acoustic resonator which is filled with a working fluid and which encloses the heat exchangers and a stack. The thermal interaction between the acoustic waves that is sustained by the acoustic driver at a fundamental resonance frequency of the resonator with the stack material introduces an additional phase shift between the velocity and the temperature of the oscillating gas. This phase shift results in a longitudinal heat flux along the stack and enables transport heat from a cold to a hot reservoir, which is supplied to the cold end of the stack by the cold heat exchanger and is extracted from the hot end of the stack by the hot heat exchanger. A detailed explanation of the operating principles of the thermoacoustic devices is available in Swift review article [3].

Many prototypes of the thermoacoustic refrigerators have been developed since the success of the first cooler built by Hofler in 1986 [4]. The device driven by an acoustic driver at 500 Hz filled with the helium of 10 bar was capable of reaching 12% of a Carnot efficiency with an applied head load of 3 W. A thermoacoustic refrigerator called Space ThermoAcoustic Refrigerator (STAR) was designed and tested by Hofler and Atchley within the NASA’s space shuttle program [5]. In January 1992, the STAR was flown on the Space Shuttle Discovery (STS-42). The cooling capacity of this unit with working frequency of 400 Hz was 3 W at a temperature drop of 50 °C, which corresponded to the EERC of 16%. A thermoacoustic cooler constructed at Naval Postgraduate School in Monterey and supported by US Navy was installed on the ship USS Deyo (DD-989), where cooled ship’s electronic radar [6]. The device named Shipboard Electronics Thermoacoustic Chiller (SETAC) was operating with helium–argon mixture at 21 bar and provided nearly 420 W of cooling power. The overall energy efficiency ratio in relation to Carnot coefficient was only 8.5%. In 1996, the Office of Naval Research founded next project named TRITON, which aimed to develop a thermoacoustic chiller with cooling capacity of 10 kW [7]. The device constructed at Pennsylvania State University was completed in 2005 and reached to 19% of Carnot cycle energy efficiency ratio with helium–argon gas mixture at 30 bar [8]. In 2000, Adeff and Hofler built and tested a thermoacoustically driven thermoacoustic refrigerator powered by solar thermal energy [9]. The goal of the project was to construct a compact unit capable of producing five to ten watts of cooling power at 0 °C. An acoustic wave produced in the engine part of the system with a peak acoustic pressure amplitude of 4.3% allowed to achieve 2.5 W of cooling power at a cold temperature of 5 °C and a temperature span of 18 °C. A similar device powered also by solar radiation was built by Chen in his Ph.D. thesis [10]. The cooler equipped in a 2-dimensional solar tracking system produced 6.2 W of cooling power at 28.5 °C.

The efficiency of the thermoacoustic devices is still not yet competitive against commercial solutions. Thus, many efforts have been taken in order to improve the design and the performance of the thermoacoustic coolers. The studies focus on the theoretical analysis as well as on the experimental and concern the optimization of the geometric parameters (e.g. stack position, stack length, resonator length) or the operating parameters (e.g. frequency, mean pressure, temperature gradient) [11]. Wetzel and Herman [12] developed a design algorithm for the thermoacoustic refrigerators based on the simplified linear thermoacoustic model with the normalized equations of the enthalpy flux and the work flux. The algorithm, for example, allows to select an optimum stack position and length at given temperature difference between the heat exchangers to get the maximum performance of the stack. A similar approach was also proposed by Tijani et al. [13] or Babaei and Siddiqui [14]. New optimization procedures such as genetic algorithm [15], particle swarm optimization [16], teaching–learning-based optimization algorithm [17] and fruit fly optimization algorithm [18] were recently also introduced to the research area of thermoacoustics.

Most of the current experimental research has been done on the stack, where the thermoacoustic effect occurs. Tijani et al. [19] optimized the stack spacing for the maximum COP, the maximum cooling power and the lowest temperature. They found that the distance between the plates of about 2.5\(\delta_{k}\) was optimum for the cooling power, a distance of 4\(\delta_{k}\) gave the lowest temperature and a distance of 3\(\delta_{k}\) provided the highest performance. Similar dependence for the lowest temperature was also observed by Setiawan et al. [20]. Another experimental optimization of porosity was performed by Yahya et al. [21], Tasnim et al. [22], Hariharan et al. [23] or Alcock et al. [24]. The stack location in resonance tube was also extensively studied as well in [25,26,27,28]. As it was found, the optimum position depends on the stack length. However, most of the favourable positions in these works fell between λ/20 and λ/8 measured away from the pressure antinode. In [29], Tijani et al. showed, in turn, that the performance of the thermoacoustic refrigerator improves as the Prandtl number of the working fluid decreases. Rest of the experimental studies concern the optimization of the operating parameters. Wantha et al. in [30] proved that the optimal operating frequency of a standing-wave thermoacoustic refrigerator differs from the design based on the equation \(f = a/2L\), where \(L\) is the resonator length and \(a\) is the speed of sound. The influence of the operating frequency on the temperature difference created across the stack was also investigated in [31, 32], whereas, for example, in [33] the thermoacoustic refrigerator with the different stack geometry was examined under different cooling loads.

This work presents the design procedure of a small thermoacoustic refrigerator with the nominal cooling power of 10 W and with the temperature difference between the heat exchangers of 30 K. The procedure details are explained step by step with the justification for the choice of the design parameters. The simplified linear thermoacoustic model was applied to find the optimum length and position of the stack. The designed device was also checked and simulated in the DELTAEC program under various temperatures of the cold heat exchanger and drive ratios in terms of cooling power, EER and EERC coefficients.

2 Design of the thermoacoustic refrigerator

The performance of the simplest thermoacoustic refrigerator depends on the eighteen independent parameters, which can be categorized into three groups [12] (Table 1). First includes geometrical parameters such as stack spacing and plate thickness, stack position and length, and cross-sectional area of the stack. Second group refers to the material related variables which are thermophysical properties of the working fluid and the stack such as thermal conductivity or density. In the third group are design-related parameters like frequency, mean pressure and pressure amplitude, mean temperature and temperature difference along the stack and cooling capacity of the system. The number of these independent parameters can be reduced trough normalization. The equations for the enthalpy flux \(\left( {\dot{H}_{\text{n}} } \right)\) and the work flux \(\left( {\dot{W}_{\text{n}} } \right)\) consumed by the stack can be then written as [14]:

$$\dot{H}_{\text{n}} = - \frac{1}{8\gamma }\delta_{\text{kn}} \left( {\text{DR}} \right)^{2} \frac{{\sin \left( {2x_{\text{cn}} } \right)}}{{\left( {1 + Pr} \right)\varLambda }}\left[ {\varGamma \frac{{1 + \sqrt {Pr} + Pr}}{{1 + \sqrt {Pr} }} - \left( {1 + \sqrt {Pr} - \delta_{\text{vn}} } \right)} \right]$$
(1)
$$\dot{W}_{\text{n}} = \frac{1}{4\gamma }\delta_{\text{kn}} \left( {\text{DR}} \right)^{2} L_{\text{sn}} \left[ {{\text{BR}}\left( {\gamma - 1} \right)\cos^{2} \left( {x_{\text{cn}} } \right)\left( {\frac{\varGamma }{{\left( {1 + \sqrt {Pr} } \right)\varLambda }} - 1} \right) - \frac{{\sqrt {Pr} \sin^{2} \left( {x_{\text{cn}} } \right)}}{{{\text{BR}}\varLambda }}} \right]$$
(2)

where

$$\varGamma = \frac{{\nabla T_{\text{m}} }}{{\nabla T_{\text{crit}} }} = \frac{{\Delta T_{\text{mn}} \tan \left( {x_{\text{cn}} } \right)}}{{{\text{BR}}\left( {\gamma - 1} \right)L_{\text{sn}} }}$$
(3)
$$\varLambda = 1 - \delta_{\text{kn}} \sqrt {Pr} + \frac{1}{2}Pr\delta_{\text{kn}}^{2}$$
(4)
Table 1 Parameters describing the thermoacoustic core
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The normalized parameters from Eqs. (1)–(4) with an extra index \(n\) are shown in Table 2. The enthalpy flux \(\left( {\dot{H}_{\text{n}} } \right)\) is the sum of the work and the heat flux, and is constant, while the heat flux rises and the work flux drops. Using these principles, from Eqs. (1) and (2), the normalized cooling power can be expressed as:

Table 2 Normalized parameters
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$$\dot{Q}_{\text{Cn}} = \dot{H}_{\text{n}} + \dot{W}_{\text{n}}$$
(5)

The EER coefficient of the stack is thus given by:

$${\text{EER}}_{\text{s}} = \frac{{\dot{Q}_{\text{Cn}} }}{{\left| {\dot{W}_{\text{n}} } \right|}}$$
(6)

2.1 Working fluid

The working fluid for a thermoacoustic refrigerator should be characterized by high ratios of specific heats and low Prandtl numbers [34]. Therefore, the noble gases are recommended. Because of lower price in comparison with the other noble gases, the helium is chosen. Moreover, it has the highest sound velocity and thermal conductivity of all inert gases, which results in the higher cooling power and in the wider stack spacing, which in turn easier its construction.

2.2 Average pressure

The power density in a thermoacoustic refrigerator is proportional to the average pressure [3]. Thus, it is favourable to choose average pressure as large as possible. However, on the other hand there are factors that limit high pressure like the mechanical strength of the resonator and the effect of the pressure on the thermal penetration depth. High pressure requires a strong pressure vessel and very precise sealing, which very often lead to more expensive materials. High pressure also results in a small thermal penetration depth as it is inversely proportional to the square root of the average pressure. If the plate spacing is designed around the mean pressure, the problem can be countered by using very narrow gaps. However, the narrow gaps make the stack difficult to build with good precision. Thus, the choice of the average pressure must balance its influence on the power density, the resonator and the stack design. The average pressure of 10 bar is selected because combined with the frequency (Sect. 2.3) it allows to build a stack with reasonable size of the plate spacing and does not require any special material.

2.3 Frequency

The thermal penetration depth is inversely proportional to the square root of the frequency, so high resonance frequencies imply a narrow plate spacing. On the other hand, the power density in a thermoacoustic refrigerator is a linear function of the resonance frequency; therefore, high values are desired. The frequency also influences the length of the device as the resonator could be the quarter or the half-length of acoustic wave (Sect. 2.7); hence, low frequencies lead to long resonance tube. When the refrigerator is driven by a loudspeaker, the resonance frequency must also match the frequency response of the driver. Considering all these relationships, the frequency of 500 Hz is chosen as it allows to construct a compact device with the relatively wide plate spacing of the stack and enables to use a woofer as a sound source.

2.4 Drive ratio

The model of the thermoacoustic is based on the linear wave theory. In order to avoid the nonlinearities, the drive ratio should be smaller than 3% so that the acoustic Reynolds number and the Mach number would be smaller than 500 and 0.1, respectively [14]. The drive ratio should also be matched to the force of the acoustic driver. The drive ratios for the loudspeakers are on the order of a few per cent. To meet assumed cooling power without the need to drive the loudspeaker excessively hard, the drive ratio of 0.01 is selected.

2.5 Stack

The stack is the most important part of the thermoacoustic refrigerator, in which the heat-pumping process takes place. It should be made of a material characterized by a low thermal conductivity, which minimizes the losses caused by the ordinary heat conduction along the temperature gradient. The stack material should also have a heat capacity larger than the heat capacity of the working fluid, so that the temperature of the stack plates will stay steady [13]. The most commonly used effective material for the stack has been Mylar, as it has a low thermal conductivity and is produced in the wide range of thickness. For these reasons, this material is chosen for the stack.

There are many different stack geometries, such as parallel plates, circular pores, pin arrays and triangular pores. The main objective for the stack geometry is to increase the thermal boundary layer surrounding the solid wall where the thermoacoustic effect could occur [10]. Some of them are difficult to manufacture. Therefore, the stack geometry in the form of the parallel plates is selected. The optimal spacing between the plates for this type of the stack is between two and four thermal penetration depths [35]. The selection of helium as the working fluid, the average pressure of 10 bar and the frequency of 500 Hz determine the thermal penetration depth. Using the equation [2], we can obtain

$$\delta_{k} = \sqrt {2K/\left( {\omega \rho_{\text{m}} c_{\text{p}} } \right)}$$
(7)

where \(K\) is the thermal conductivity, \(\omega\) is the angular frequency, \(\rho_{\text{m}}\) is the density and \(c_{\text{p}}\) is the isobaric heat capacity; the thermal penetration depth for designing conditions is equal to 0.107 mm. Taking into account the above recommendations and simplicity of the fabrication, the plate spacing of 0.4 mm is selected.

The remaining parameters describing the stack, which are the stack centre position, stack length and stack cross-sectional area, will be chosen based on the optimization of the stack EERs (Eq. (6)). The calculations were done for eight stack centre positions, stack length varying from 30 to 160 mm and parameters presented in Table 3.

Table 3 Design parameters
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Figure 1 shows that the EERs for each stack centre position increases with the stack length, reaches maximum and then starts to decrease. The performance peak shifts towards shorter plates together with the decrease in the stack centre position. Generally, the highest values of EERs are achieved by the shortest stacks located closer to the sound source. These positions correspond nearly to a pressure antinode and a velocity node where a small viscous loss occurs.

Fig. 1
figure 1

EER of the stack versus the stack length for different stack centre positions measured from the sound source

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Taking into account described above relationships and for practical reasons, the length of 60 mm and the stack centre position at 120 mm away from the sound source are chosen. Among other configurations, these parameters show reasonable EERs of 1.45. They will also facilitate the construction of the device by leaving enough space between the acoustic driver and the stack for heat exchanger and measurement equipment installation. The dimensionless cooling power for chosen parameter is equal to 1.05 × 10−6. The required cooling power is assumed to be 10 W. Using the equation for normalized cooling power (Eq. (5)) and the equations for normalized enthalpy and work flux presented in Table 2, the inner diameter of the large tube of the resonator \(\left( {D_{1} } \right)\), which gives desired cooling power, should be of 108 mm.

2.6 Heat exchangers

The proper design of the heat exchangers is a critical task in thermoacoustics, as the literature contains very little guidance [14]. Swift in [3] proposed the optimum length of a heat exchanger, which should be equal to peak-to-peak gas displacement amplitude at the heat exchanger location. The displacement amplitude is equalled to [3]:

$$x_{1} = \frac{{p_{1} }}{{\omega \rho_{\text{m}} a}}\sin \left( {kx} \right)$$
(8)

where \(p_{1}\) is the pressure amplitude, \(\omega\) is the angular frequency, \(\rho_{\text{m}}\) is the density, \(a\) is the speed of sound, \(k\) is the wave number and \(x\) is the longitudinal coordinate. Using the above equation, designing conditions with the stack length and centre position the optimum length of the cold heat exchanger is about 1.8 mm. The length of the hot heat exchanger could be calculated in the same way. However, the hot heat exchanger has to reject more heat than the heat supplied by the cold heat exchanger, as it also removes acoustic power used for the thermoacoustic effect. Assuming that the heat transfer coefficient and the temperature difference between the solid plate and the working fluid are the same, the length of the hot heat exchanger could be set as a twice length of the cold heat exchanger (3.6 mm). In order not to disturb the parcel displacement between the heat exchanger and the stack, the plate spacing of the both heat exchangers is identical as for the stack (2y0 = 4 mm).

2.7 Resonator

The resonator length must match the resonance frequency of the system. In most cases, the resonance tubes are the quarter or the half-length of acoustic wave. The length of the resonator influences also the viscous and the thermal penetration losses. The total dissipated energy is proportional to the internal surface area of the resonator [3]. Hence, the quarter wave length resonator will dissipate half of energy dissipated in the half-length wave resonator. The shape of the resonator can be further optimized by minimizing its internal surface area. As it was shown by Hofler [4], this can be achieved by reducing the diameter of the resonance tube that is behind the stack and using a spherical bulb to simulate an open end. The total loss of energy has a minimum at about \(D_{2} /D_{1} = 0.54\) [13], where \(D_{2}\) is the diameter of the small tube and \(D_{1}\) is the diameter of the large tube containing the stack. Using this relationship, the inner diameter of the small tube should be of 58 mm.

The total length of the resonator is equalled to the sum of the lengths of the small diameter tube and the large diameter tube (Fig. 2) and is determined by earlier chosen operation frequency of 500 Hz. The length of each tube can be obtained considering the condition that at the junction of the small and the large diameter tubes the pressure and the volume flow rate have to be continuous. This implies also the same acoustic impedances at the connection of these tubes, which is reflected by the equation [13]:

$$\cot \left( {kx_{\text{con}} } \right) = \left( {\frac{{D_{1} }}{{D_{2} }}} \right)^{2} \tan \left( {k\left( {L_{\text{R}} - x_{\text{con}} } \right)} \right)$$
(9)

where \(k\) is the wave number, \(x_{\text{con}}\) is the longitudinal coordinate of the connection, \(L_{\text{R}}\) is the total length of the resonator, \(D_{1}\) is the diameter of the large tube and \(D_{2}\) is the diameter of the small tube (Fig. 2). The total length of the resonator after substitution of all necessary parameters in Eq. (9) is equalled to 322.6 mm. This value means that for the resonator with variable cross-sectional area its total length does not correspond to an integer number of the fundamental mode.

Fig. 2
figure 2

Schematic illustration of the device

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The buffer volume must have enough volume to simulate an open end. A spherical bulb firstly designed by Hofler [4] generates turbulence during the transition from the small diameter tube to the bulb. Tijani [36] proved that the minimal losses occur for the cone-shaped buffer volume with the half-angle of the cone of 9°. Therefore, a similar buffer tube with the volume of 2.5 L will be used. The volume determines the total length of the device \(\left( {L_{\text{T}} } \right)\) to be 636 mm with the buffer radius \(\left( R \right)\) of 68 mm (Fig. 2).

2.8 Acoustic driver

The total acoustic power \(\left( {\dot{W}_{\text{t}} } \right)\) that must be provided by the acoustic driver is the sum of the acoustic power used by stack \(\left( {\dot{W}_{\text{s}} } \right)\) to transfer heat and acoustic power dissipated in different parts of the device:

$$\dot{W}_{\text{t}} = \dot{W}_{\text{s}} + \dot{W}_{\text{che}} + \dot{W}_{\text{hhe}} + \dot{W}_{\text{res}}$$
(10)

The acoustic powers used by the stack, dissipated in the cold heat exchanger \(\left( {\dot{W}_{\text{che}} } \right)\) and in the hot heat exchanger \(\left( {\dot{W}_{\text{hhe}} } \right)\), are described by Eq. (2) and are equalled, respectively, to \(\dot{W}_{\text{s}} = 6.86\;{\text{W}}\), \(\dot{W}_{\text{che}} = 0.31\;{\text{W}}\), \(\dot{W}_{\text{hhe}} = 0.48\;{\text{W}}\). In the large diameter resonator, only the part of the tube does not contain any parts dissipating energy, and in the small diameter resonator, the energy is dissipated along all tube. In both cases, the amount of dissipated acoustic power can be estimated using the equation for normalized acoustic power dissipated in wavelength resonator with appropriate length’s coefficient for given tube [14]:

$$\Delta \dot{W}_{n} = - z\left[ {\left( {\frac{\pi }{8\gamma }\sqrt {Pr} {\text{DR}}^{2} \left( {\frac{{\delta_{k} }}{{R_{\text{hr}} }}} \right)} \right) - \left( {\frac{{\pi \left( {\gamma - 1} \right)}}{8\gamma }{\text{DR}}^{2} \left( {\frac{{\delta_{k} }}{{R_{\text{hr}} }}} \right)} \right)} \right]$$
(11)

where \(z\) is the length coefficient, \(\gamma\) is the ratio of isobaric to isochoric specific heats, \(Pr\) is the Prandtl number, \({\text{DR}}\) is the drive ratio, \(\delta_{k}\) is the thermal penetration depth and \(R_{\text{hr}}\) is the hydraulic radius. The total acoustic dissipated in resonator is \(\dot{W}_{\text{res}} = 0.11\;{\text{W}}\). Hence, the acoustic driver must deliver 7.76 W. The EER coefficient of the device described as the cooling power to the acoustic power delivered by the driver is 1.29. This coefficient does not include the efficiency of the driver; therefore, the final EER can be expected much smaller.

3 Simulation

The computer program Design Environment for Low-amplitude ThermoAcoustic Energy Conversion (DELTAEC) was used to simulate the designed device (Fig. 2). DELTAEC is the numerical tool developed by Los Alamos National Laboratory, which solves the one-dimensional wave equation in the gas based on the low-amplitude acoustic approximation in a geometry given by the user as a sequence of segments such as ducts, cones, stacks and heat exchangers [37]. The code uses a shooting method, by guessing and adjusting any unknown boundary conditions at the initial segment to achieve the desired boundary conditions elsewhere.

In the simulation, the volume flow amplitude, the mean temperature, the frequency and the heat removed from the hot heat exchanger were set as the guess parameters, and the real part of the inverse of the normalized specific impedance, the imaginary part of the inverse of the normalized specific impedance and the total energy flow determined at the final segment of the device were set as the target parameters as well as the temperature of the hot heat exchanger. The comparison between the results from design procedure and DELTAEC simulation is presented in Table 4. A good agreement can be observed. The small differences between these two ways are mainly due to assumptions that were made in the normalization of the thermoacoustic enthalpy flux and work flux.

Table 4 Comparison between results from design procedure and DELTAEC simulation
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Figures 3, 4 and 5 show the simulations results of the device for different temperatures of the cold heat exchanger \(\left( {T_{\text{che}} } \right)\) and drive ratios \(\left( {\text{DR}} \right)\). The temperature of the hot heat exchanger \(\left( {T_{\text{hhe}} } \right)\) and mean pressure \(\left( {p_{\text{m}} } \right)\) during the simulations was kept constant, respectively, at 300 K and 10 bar. The cooling power of the device increases with the increase in the drive ratio and with the increase in the cold heat exchanger temperature (Fig. 3). For high-temperature differences between the heat exchangers and for low drive ratios, the cooling power is nearly approaching zero. This is a consequence of the decrease in the critical temperature gradient (Eq. 3). The critical temperature gradient is a value for which the temperature change due to adiabatic compression and expansion matches the temperature change due to parcel motion of the working fluid along the stack plate [3]. The increase in the mean temperature gradient corresponds always to the increase in the temperature changes of the gas parcel caused by its displacement due to acoustic oscillation, what finally lead to the decrease in the heat flux. Below a certain ratio of the mean temperature gradient to the critical temperature gradient, a noxious effect starts to occur in which the acoustic energy is absorbed, and the heat is pumped from the hot to the cold heat exchanger (no cooling power). Further decrease in the cold heat exchanger temperature in simulation procedure would lead to such effect.

Fig. 3
figure 3

Cooling power of the device versus temperature of the cold heat exchanger for different drive ratios

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Fig. 4
figure 4

EER of the device versus temperature of the cold heat exchanger for different drive ratios

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Fig. 5
figure 5

EERC of the device versus temperature of the cold heat exchanger for different drive ratios

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The effects of the temperatures of the cold heat exchanger and drive ratios on the EER coefficient are shown in Fig. 4. The EER increases with the increase in the temperature of the cold heat exchanger and with the increase in the drive ratio. However, the influence of the drive ratio, especially for small temperature span along the stack, is not so significant. Such behaviour of EER is expected because as Eqs. (1) and (2) show, both the enthalpy and the work flux are proportional to the square of the drive ratio. For lower temperatures of the cold heat exchanger, the effect of the drive ratio is more observable. This is due to low cooling power for small acoustic pressure amplitude (Fig. 3).

The EER coefficient relative to Carnot coefficient shows a parabolic dependence for all drive ratios and temperatures of the cold heat exchangers (Fig. 5). The maximum values of EERC exist because, while EER rises almost linearly with the temperature (Fig. 4), the EERC of the Carnot cycle increases faster. Like the EER, the EERC increases with the increase in the drive ratio for high-temperature differences between the heat exchangers and is nearly similar for all drive ratios at small temperature differences. The peak of EERC shifts towards lower temperatures of the cold heat exchangers together with the increase in the drive ratio.

4 Conclusion

In this paper, the design procedure of a small capacity thermoacoustic refrigerator with the nominal cooling power of 10 W and with the temperature difference between the heat exchangers of 30 K is described. The design with the explanation of the choice of the design parameters is based on the dimensionless linear thermoacoustic model, which was used for the stack optimization. The algorithm was checked by the computer code DELTAEC, and a good agreement was achieved. The performance of the designed refrigerator under different temperatures of the cold heat exchanger and drive ratios was simulated in the program as well. The results show how sensitive on the change of the operational parameters the thermoacoustic refrigerator is. For example, an inappropriate temperature difference selection could lead to the change of the heat transport direction between the heat exchangers which will result in no cooling effect. It was also found that for analysed parameters the influence of the drive ratio on the EER and EERC coefficients especially for small temperature span, less than 15 K, is almost negligible.