Thermoacoustic electric generator system

A thermoacoustic electric generator system includes: a thermoacoustic engine provided in an annular tube; a turbine provided in a branched tube and rotating when receiving acoustic energy, which is generated by thermoacoustic oscillation of working gas in the thermoacoustic engine; and a generator for converting kinetic energy, which is generated by rotation of the turbine, to electric energy. The turbine is provided at a specified position that belongs to a region between a first position and a second position in each region of the branched tube, the first position being an intermediate position between one end and the other end, and the second position being an intermediate position between the first position and the other end.

TECHNICAL FIELD

The invention relates to a thermoacoustic electric generator system for generating electric energy using a thermoacoustic engine that induces thermoacoustic oscillation of working gas.

BACKGROUND ART

Conventionally, efficient energy use has been promoted in various industrial fields. However, a rate of exhaust heat, which is exhausted and wasted from facilities such as factories and vehicles, for example, still remains high. Thus, a technique of efficiently collecting thermal energy has been desired. In the earnest investigation into this technique, the present inventor has focused his attention on use of a thermoacoustic engine capable of inducing thermoacoustic oscillation of working gas. One example of a system (hereinafter also referred to as a “thermoacoustic electric generator system”) that generates electric energy using this thermoacoustic engine has been disclosed in PCT/JP/2012-081193.

The thermoacoustic engine used in this thermoacoustic electric generator system includes: a stack configured by including plural channels; a hot heat exchanger provided at one end of each of the channels in the stack; and a cold heat exchanger provided at the other end of each of the channels in the stack. This thermoacoustic engine induces thermoacoustic oscillation of working gas, which is enclosed in a tube, through generation of a temperature gradient between both of the ends of the channel in the stack, and thus can generate acoustic energy. Furthermore, this thermoacoustic electric generator system is configured to include a linear generator in a branched tube, which is branched from an annular tube, drive this generator using the acoustic energy generated in the thermoacoustic engine, and thereby generate electric energy.

SUMMARY OF THE INVENTION

As described above, the linear generator is used to generate the electric energy using the thermoacoustic oscillation of the working gas, which is generated in the thermoacoustic engine. However, use of the linear generator is disadvantageous in terms of cost because this linear generator itself is expensive. Thus, the present inventor performed the earnest investigation into a technique of arranging a turbine in a branched tube and using a turbine-type generator that generates the electric energy using kinetic energy during actuation of this turbine. As a result of the investigation, it was successfully found out that mere provision of the turbine in the branched tube did not always allow driving of the generator and that, in order to reliably drive the generator, an installment position of the turbine in the branched tube was extremely important.

The invention has been made in view of the above points, and one of purposes of the invention is to provide an effective technique of reliably driving a turbine-type generator in a thermoacoustic electric generator system that generates electric energy using thermoacoustic oscillation of working gas generated in a thermoacoustic engine.

In order to achieve the above purpose, a thermoacoustic electric generator system (100) according to the invention includes a tube component (101), a thermoacoustic engine (110), a turbine (140), and a generator (150). The tube component (101) includes: an annular tube (102) configured to be annular; and a branched tube (103) branched from the annular tube (102), extending lengthwise from one end (103a), which is located at a branched point from the annular tube (102), to the other end (103b), and communicating with the annular tube (102), and specified working gas is enclosed in both of the annular tube (102) and the branched tube (103). The thermoacoustic engine (110) includes: a stack (111) incorporated in an inside of the annular tube (102) in the tube component (101) and having plural channels (111c), each of which extends in a tube longitudinal direction; and heat exchangers (112,113) exchanging heat with the working gas such that a temperature gradient is generated between both ends of each of the plural channels (111c) in the stack (111), so as to cause thermoacoustic oscillation of the working gas. The turbine (140) is provided in the branched tube (103) of the tube component (101) and rotates when receiving a sound wave, which is generated by the thermoacoustic oscillation of the working gas in the thermoacoustic engines (110). A generator (150) fulfills a function of converting kinetic energy generated by rotation of the turbine (140) to electric energy. The turbine (140) is provided at a specified position that belongs to a region between a first position (P3) and a second position (P4) in each region of the branched tube (103) in the tube component (101), the first position (P3) being an intermediate position between the one end (103a) and the other end (103b), and the second position (P4) being an intermediate position between the first position (P3) and the other end (103b).

In regard to the thermoacoustic electric generator system of this configuration, according to the examination by the present inventor, it has been found out that the region in the branched tube of the tube component is effective in the continuous and reliable rotation of the turbine as being a region where flow velocity amplitude of the working gas (displacement per unit time of the working gas in the tube longitudinal direction) is relatively large, and realizes favorable energy efficiency as being a region where a vibration starting temperature of the thermoacoustic engine (a temperature at which the thermoacoustic oscillation of the working gas actually starts being induced) is relatively low. Accordingly, when the turbine is installed at the specified position belonging to the region, the generator can reliably be driven to generate the electric energy, and an energy efficient state can be realized in terms of the generation of the electric energy.

In the thermoacoustic electric generator system (100) of the above configuration, at the other end (103b), the branched tube (103) of the tube component (101) preferably includes an energy extraction section (160) for extracting the acoustic energy, which is generated by the thermoacoustic oscillation of the working gas, to an outside thereof, and the energy extraction section (160) is preferably constructed of a speaker-type generator or a linear generator capable of outputting electrical energy when receiving pressure vibration in a tube longitudinal direction of the branched tube (103).

In the thermoacoustic electric generator system of this configuration, according to the examination by the present inventor, it has been found out that the other end of the branched tube in the tube component is a position at which pressure amplitude (a magnitude of a pressure fluctuation, that is, fluctuation width between a maximum value and a minimum value of the pressure) of the working gas becomes the largest in each of the regions of the branched tube and is an appropriate position for driving of the speaker-type generator or the linear generator. Accordingly, when the generator that is the speaker-type generator or the linear generator is provided at the other end of the branched tube, the acoustic energy, which cannot be fully collected by a turbine-type generator can be collected as the electrical energy.

Note that, in the above description, in order to facilitate understanding of the invention, components of the invention that correspond to those of the embodiment are denoted by the reference signs used in the embodiment in parentheses. However, each of the components of the invention is not limited to that in the embodiment defined by the reference sign.

As it has been described so far, according to the invention, the turbine-type generator can reliably be driven in the thermoacoustic electric generator system that generates the electric energy using the thermoacoustic oscillation of the working gas generated in the thermoacoustic engine.

MODES FOR CARRYING OUT THE INVENTION

A detailed description will hereinafter be made on one embodiment of the invention with reference to the drawings. Note that, in said drawings, in regard to each component of the same element that is denoted by the same reference sign for the description, a reference sign thereof for the description is omitted when necessary.

As shown inFIG. 1, a thermoacoustic electric generator system100includes a tube component101that is configured by including metallic tubes. This tube component101is configured by including: an annular tube102as an annular (loop) tube portion; and a branched tube103that is branched from the annular tube102and, an internal space of which communicates with an internal space of the annular tube102. This tube component101corresponds to the “tube component” of the invention. In addition, the annular tube102and the branched tube103respectively correspond to the “annular tube” and the “branched tube” of the invention. Note that the annular tube102of the tube component101only needs to be annular, and any of various shapes such as a circle, an oval, and a polygon can be adopted as a shape thereof in a side view.

The branched tube103has one end103aas a branched point that is branched from the annular tube102, and is a tube portion that extends lengthwise from this one end103ato the other end103b. The branched tube103is closed at the other end103bby an energy extraction section160, and specified working gas (helium in this embodiment) is thereby enclosed under a specified pressure in both of the annular tube102and the branched tube103. Note that, instead of or in addition to helium, nitrogen, argon, mixed gas of helium and argon, air, or the like can be used as the working gas.

The annular tube102of the tube component101is provided with three thermoacoustic engines (also referred to as “motors”)110that are connected in series. These three thermoacoustic engines110constitute a so-called “multistage thermoacoustic engine”. Each of the thermoacoustic engines110includes: a stack111incorporated in an inside of the annular tube102; a hot heat exchanger112arranged to oppose one end111aas a high-temperature section of the stack111; and a cold heat exchanger113arranged to oppose the other end111bas a normal-temperature section (or a low-temperature section) of the stack111. The thermoacoustic engine110herein corresponds to the “thermoacoustic engine” of the invention. Note that the number of installment of this thermoacoustic engine110is not limited to three, and another number of the installment can be selected when necessary.

As shown inFIG. 2, each of the stack111is configured as a structure having plural channels111cthat extend in parallel with each other from the one end111ato the other end111balong a tube longitudinal direction (a tube extending direction) of the annular tube102. When a specified temperature gradient is generated between the one end111aand the other end111bof this stack111, the working gas in the annular tube102becomes unstable to induce thermoacoustic oscillation thereof. In this way, oscillatory waves (also referred to as “sound waves”, a “vibration flow”, or a “work flow”) are produced by vertical waves that vibrate in parallel with an advancing direction of the working gas, and such oscillatory waves transfer from the inside of the annular tube102to an inside of the branched tube103. As this stack111, a honeycomb structure made of ceramics, a structure in which thin mesh sheets made of stainless steel are stacked in parallel at fine pitches, a nonwoven fabric-like material made of metallic fiber, or the like can typically be used. This stack111corresponds to the “stack” of the invention.

Each of the hot heat exchangers112is connected to a heating source120. The heating source120fulfills a function of supplying a heating medium such as hot air or hot water to each of the hot heat exchangers112. Each of the hot heat exchangers112is configured as a heat exchanger for heating that includes: a passage112a, through which the relatively high-temperature heating medium flows; and a passage (not shown), through which the relatively low-temperature working gas flows, and that can move heat from the heating medium to the working gas through heat exchange between the heating medium and the working gas. In this way, the working gas situated around the one end111aof each of the stack111is heated by the heating medium supplied from the heating source120to each of the hot heat exchangers112.

Each of the cold heat exchangers113is connected to a cooling source130. The cooling source130fulfills a function of supplying a cooling medium such as cold wind, cold water, or atmospheric air to each of the cold heat exchangers113. Each of the cold heat exchangers113is configured as a heat exchanger for cooling that includes: a passage113a, through which the relatively low-temperature cooling medium flows; and a passage (not shown), through which the relatively high-temperature working gas flows, and that can move the heat from the working gas to the cooling medium through the heat exchange between the working gas and the cooling medium. In this way, the working gas situated around the other end111bof each of the stack111is cooled by the cooling medium supplied from the cooling source130to each of the cold heat exchangers113.

The specified temperature gradient is generated between the one end111aand the other end111bof each of the stack111through cooperation of a heating effect by the above hot heat exchanger112and a cooling effect by the above cold heat exchanger113. The hot heat exchanger112and the cold heat exchanger113described above serve as the heat exchanger that exchanges the heat with the working gas such that the temperature gradient is generated between both ends of each of the plural channels111cin each of the stack111in order to induce the thermoacoustic oscillation of the working gas enclosed in the tube component101. These hot heat exchanger112and cold heat exchanger113constitute the “heat exchanger” of the invention.

Returning toFIG. 1, the branched tube103includes: a first tube section104that extends linearly between the annular tube102and a turbine140; a second tube section105that extends linearly on an opposite side of the turbine140from the annular tube102; and a crank tube section106that is bent in a crank shape to couple the first tube section104and the second tube section105.

Although details will be described below, the turbine140is configured to communicate with the inside of the branched tube103and fulfills a function to convert acoustic energy (also referred to as “vibration energy”), which is generated by the oscillatory waves of the working gas flowing through the branched tube103, to mechanical rotational energy. That is, this turbine140is provided in the branched tube103and rotates when receiving the acoustic energy, which is generated by the thermoacoustic oscillation of the working gas in the thermoacoustic engines110. A generator150that converts kinetic energy (the rotational energy) by the rotation of this turbine140to electric energy is connected to the turbine140. The turbine140and the generator150herein respectively correspond to the “turbine” and the “generator” of the invention. These turbine140and generator150constitute a turbine-type generator that is driven by the turbine to generate the electric energy.

The other end103bof the branched tube103, that is, a tube end on an opposite side from the turbine140of tube ends on both sides of the second tube section105is provided with the energy extraction section160that extracts the acoustic energy of the working gas from the branched tube103to an outside of the tube. This energy extraction section160corresponds to the “energy extraction section” of the invention. In this embodiment, as this energy extraction section160, a speaker-type generator capable of receiving pressure vibrations in the tube longitudinal direction of the branched tube103and outputting electrical energy (the electric energy) is used. This speaker-type generator uses a reverse phenomenon of a normal speaker that converts the electrical energy to vibrations of air or the like, and is configured to output the electrical energy by receiving a vibration flow of the working gas.

As shown inFIG. 3, the turbine140, which constitutes the turbine generator, includes a turbine housing141, a turbine rotational shaft144, and a turbine blade145. The turbine housing141is a portion that accommodates a part of the turbine rotational shaft144and the turbine blade145and that constitutes a part of the branched tube103, and communicates with both of the second tube section105and the crank tube section106in the branched tube103. The turbine rotational shaft144is configured as a cylindrical member that is supported via bearings142,143in a manner capable of rotating axially. This turbine rotational shaft144extends lengthwise in the tube longitudinal direction from one end144a, which is located in the turbine housing141, that is, in the branched tube103, to the other end144bby penetrating a tube wall of the crank tube section106from the inside to the outside of the branched tube103. This turbine rotational shaft144is coupled to the turbine blade145and serves as a rotation center of this turbine blade145.

The turbine blade145is provided in the branched tube103(the crank tube section106), receives the acoustic energy generated by the thermoacoustic oscillation of the working gas in the thermoacoustic engines110, and rotates by an effect of an impulsive force thereof. This turbine blade145includes: a toric rotor blade section146fixed to the turbine rotational shaft144; toric fixed blade sections147that interpose the rotor blade section146therebetween and are arranged on both sides thereof; and a cone section148provided on an opposite side of each of the fixed blade sections147from the rotor blade section146. This turbine blade145is configured as a rotary vane including the rotor blade section146that integrally rotates with the turbine rotational shaft144. Accordingly, the turbine140, which has the turbine blade145, is also referred to as an “impulsive turbine”.

The fixed blade section147does not rotate even when the rotor blade section146rotates. As shown inFIG. 4, in this fixed blade section147, plural blades147athat extend in a radial direction are arranged at constant intervals in a circumferential direction, and a circulation space, in which the working gas can circulate, is formed between two each of these plural blades147a.

With reference toFIG. 3andFIG. 4, the cone section148has a conical shape, an outer diameter of which is gradually reduced as separating from the corresponding fixed blade section147, an outer surface thereof constitutes an inclined surface148athat is inclined to an axis of the turbine rotational shaft144. The inclined surface148aof the cone section148fulfills a function of smoothly introducing the oscillatory wave of the working gas toward the fixed blade section147. According to this cone section148, the oscillatory wave of the working gas can be introduced into the fixed blade section147at a specified entry angle θ (an acute angle defined by the inclined surface148a, which is inclined along the outer surface of the cone section148, and the axis of the turbine rotational shaft144).

The turbine blade145configured as above is a so-called “bidirectional turbine blade” and, as shown inFIG. 5, is configured that, in either of cases where the working gas flows in a first direction indicated by an arrow D1and the working gas flows in a second direction (a reverse direction of the first direction) indicated by an arrow D2, the working gas flows into the rotor blade section146through the circulation space of the fixed blade section147and that the rotor blade section146thereby rotates in the specified one direction.

Returning toFIG. 3, the generator150, which constitutes the turbine generator, is provided on the outside of the branched tube103in the tube component101, is coupled to the turbine rotational shaft144of the turbine140, and fulfills a function of converting the rotational energy of the turbine blade145to the electric energy. This generator150includes a generator housing151. This generator housing151includes: a first housing section152that is joined to the crank tube section106by welding; and a second housing section153that is attached to the first housing section152via a bolt member154.

In this generator housing151, when the second housing section153is attached to the first housing section152, an accommodation space151afor accommodating an electric motor156as a component of the generator150in an airtight state is formed. The first housing section152is provided with a communication hole152afor communicating the accommodation space151awith the inside of the crank tube section106in the branched tube103.

In the turbine140, a portion of the turbine rotational shaft144that is located on the outside of the branched tube103is introduced into the accommodation space151athrough the communication hole152aof the generator housing151, and the other end144bis coupled to a motor shaft154aof the electric motor156by a coupling section155. That is, the turbine blade145of the turbine140is coupled to the generator150via the turbine rotational shaft144. According to this generator150, in the case where the turbine rotational shaft144rotates axially due to mechanical rotary motion of the turbine140, a motor shaft154arotates due to the rotary motion of this turbine rotational shaft144, and the electric motor156thereby generates electricity. In this case, the electric motor156fulfills a function as a substantial generator.

While a part of the turbine rotational shaft144in the turbine140extends from the inside to the outside of the branched tube103, the extended portion is accommodated in a tightly sealed state in the accommodation space151aof the generator housing151. As a result, the entire turbine rotational shaft144is placed in a tightly sealed region from the inside of the branched tube103to the accommodation space151aof the generator housing151. Accordingly, a dedicated shaft seal structure to the turbine rotational shaft144does not have to be provided, and thus a structure related to the turbine rotational shaft144can be simplified.

The above coupling section155can easily detach the generator150from the turbine140when necessary by canceling coupling between the other end144bof the turbine rotational shaft144and a motor shaft156aof the electric motor156. As described above, in the turbine140of this embodiment, the turbine rotational shaft144extends from the inside to the outside of the branched tube103. In this way, in a state of being arranged on the outside of the branched tube103, the generator150can be coupled to the other end144bof the turbine rotational shaft144. In this case, as a result of facilitated detachment of the generator150from the turbine140, maintainability of the generator150is improved. In addition, according to the above coupling section155, the other end144bof the turbine rotational shaft144is coupled to a motor shaft of another motor instead of the electric motor156. Thus, the electric motor (the generator) that is coupled to the turbine140can be replaced with an optimum motor in accordance with capacity and the like of the turbine140. In this way, electric energy generation capacity of the turbine generator can easily be changed.

Next, a description will be made on an operation of the thermoacoustic electric generator system100with the above configuration on the basis of the above description.

As shown inFIG. 1, in each of the thermoacoustic engines110, when the one end111aof the stack111is heated by the hot heat exchanger112, and the other end111bof the stack111is cooled by the cold heat exchanger113, a temperature difference occurs between the one end111aas a high-temperature side region and the other end111bas a low-temperature side region in the stack111. Due to this temperature difference, the oscillatory wave is primarily generated from the thermoacoustic oscillation of the working gas in each of the stack111. The acoustic energy E (the vibration energy) of this oscillatory wave (the sound wave) is transferred from the annular tube102of the tube component101to the turbine140through the branched tube103, and is further transferred to the energy extraction section160. In this case, the branched tube103is configured as a resonance tube (a wave guide tube) for guiding the acoustic energy E of the working gas that is generated in the thermoacoustic engines110. The acoustic energy E is partially extracted by the turbine140as energy extraction means and converted to the electrical energy (the electric energy) by the generator150, which is connected to said turbine140, and is also partially extracted by the speaker-type generator of the energy extraction section160and converted to the electrical energy (the electric energy).

By the way, in the thermoacoustic electric generator system100of the above configuration, mere provision of the turbine140in the branched tube103does not always allow driving of the generator150, and in order to reliably drive the generator150, an installment position of the turbine140in the branched tube103is extremely important. As a result of the earnest investigation in the installment position of the turbine140in the branched tube103, the present inventor has found an effective turbine installment position for reliable driving of the generator150(more specifically, a preferred installment position of the turbine blade145, which rotates by receiving the acoustic energy, in the turbine140). A description will hereinafter be made on a measurement method implemented by the present inventor to obtain this finding and a measurement result thereof with reference toFIG. 6toFIG. 8.

As shown inFIG. 6, of each region of the branched tube103whose tube length (a distance between the one end103ato the other end103b) was L, measurement points, at which measurement to define the preferred installment position of the turbine140was made, were respectively set at five positions P1to P5as shown in a lower section of the drawing. Note that thisFIG. 6schematically shows a state where the branched tube103inFIG. 1extends linearly. Of each portion of the branched tube103, the position P1is a position corresponding to the one end103aon the annular tube102side. Of each of the portions of the branched tube103, the position P2is a position that moves from the one end103ato the other end103bside by one-fourth of length of the tube length L ((¼)L). Of each of the portions of the branched tube103, the position P3is a position that moves from the one end103ato the other end103bside by two-fourth of length of the tube length L (( 2/4)L). Of each of the portions of the branched tube103, the position P4is a position that moves from the one end103ato the other end103bside by three-fourth of length of the tube length L ((¾)L). Of each of the portions of the branched tube103, the position P5is a position that moves from the one end103ato the other end103bside by four-fourth of length of the tube length L ((4/4)L), that is, a position corresponding to the other end103b.

In first measurement, in a pre-installment state where the turbine140was not installed in the branched tube103, the pressure amplitude and the flow velocity amplitude were measured by a two-sensor method (a method making pressure measurement at two positions) at each of the five positions P1to P5in this branched tube103. The “pressure amplitude” described herein is represented as a magnitude of a pressure fluctuation at a point at a time when the oscillatory wave generated by the thermoacoustic oscillation of the working gas is generated in the inside of the branched tube103(fluctuation width between a maximum value and a minimum value of the pressure). In addition, the “flow velocity amplitude” described herein is represented as displacement per unit time of the working gas in the tube longitudinal direction in the inside of the branched tube103.

Furthermore, in second measurement, a vibration starting temperature of the thermoacoustic engine110in a state where the turbine140was actually installed at each of the five positions P1to P5in the branched tube103was measured by a temperature sensor. The “vibration starting temperature” described herein is represented as a temperature at which the thermoacoustic oscillation of the working gas actually starts being induced in the thermoacoustic engine110(a minimum value of the temperature at which the thermoacoustic oscillation of the working gas is induced).

As shown inFIG. 7, the following measurement result (hereinafter, also referred to as a “first measurement result”) was obtained; according to the first measurement, while the pressure amplitude became the largest at the position P1and the position P5and became the smallest at the position P3, the flow velocity amplitude became the smallest at the position P1and the position P5and became the largest at the position P3. In addition, even when an absolute value of the tube length L was changed, a similar tendency to this measurement result, that is, that the pressure amplitude became the smallest and the flow velocity amplitude became the largest at the position P3was confirmed.

As shown inFIG. 8, the following measurement result (hereinafter, also referred to as a “second measurement result”) was obtained; according to the second measurement, the vibration starting temperature of the thermoacoustic engine110became the highest at 270° C. at the position P1, became the second highest at 200° C. at the position P2, became 190° C. at the position P5, and became the lowest at 120° C. at the position P3and the position P4. In addition, even when the absolute value of the tube length L was changed, a similar tendency to this measurement result, that is, that the vibration starting temperature became the lowest at the position P3and the position P4was confirmed.

In a case based on the first measurement result and the second measurement result as described above, the present inventor determined that a position belonging to a region from the position P3to the position P4was the preferred installment position of the turbine140. When a specific description is made on a basis of this determination, in order to make the turbine blade145of the turbine140continuously and reliably rotate, a region where the flow velocity amplitude is relatively large (a region from the position P2to the position P4) is preferred, and, of the region, the position P3, at which the flow velocity amplitude is the largest, is the most advantageous. Meanwhile, in order to actuate the thermoacoustic engine110under an energy efficient condition, a region where the vibration starting temperature is the lowest (the region from the position P3to the position P4) is advantageous. Here, the position P3is an intermediate position between the one end103aand the other end103bin each of the regions of the branched tube103(the position moved from the one end103ato the other end103bside by half the length of the tube length L) and corresponds to the “first position” of the invention. In addition, the position P4is an intermediate position between the position P3and the other end103b(the position P5) in each of the regions of the branched tube103(the position moved from the position P3to the other end103bside by one-fourth of length of the tube length L) and corresponds to the “second position” of the invention.

Accordingly, it can be determined that, when the turbine-type generator is used to generate the electric energy, a specified position is preferably defined from the plural positions belonging to the region from the position P3to the position P4, which is the region where both of the first measurement result and the second measurement result are satisfied, and the turbine140is preferably installed at this specified position. When the turbine140is installed on the basis of this determination result, the generator150can be reliably driven to generate the electric energy, and an energy efficient state can be realized in terms of the generation of the electric energy. Such an approach is effective as a design assist method for the thermoacoustic electric generator system, in which designing thereof is assisted by defining the turbine installment position of the turbine140in the branched tube103.

Furthermore, in a case based on the first measurement result, the other end103b(the position P5) of the branched tube103, at which the energy extraction section160is installed, is the position at which the pressure amplitude of the working gas becomes the largest of each of the regions of the branched tube103, and, as this energy extraction section160, use of the speaker-type generator that is actuated by receiving the pressure vibration in the tube longitudinal direction is advantageous. In this way, the acoustic energy E, which cannot fully be collected by the turbine-type generator150, can be collected as the electrical energy. Note that, as the energy extraction section160, a known linear generator can be used instead of the speaker-type generator. Also, in a case of using the linear generator, similar to the case of using the speaker-type generator, the electrical energy can be output by receiving the pressure vibration in the tube longitudinal direction of the branched tube103.

The invention is not only limited to the above typical embodiment, and various applications and modifications thereof can be considered without departing from the purpose of the invention. For example, each of the following embodiments, for which the above embodiment is applied, can also be implemented.

The description has been made on the case where the two heat exchangers (the hot heat exchanger112and the cold heat exchanger113) are provided for the stack111in order to generate the specified temperature gradient between the one end111aand the other end111bof the stack111in the thermoacoustic engine110of the above embodiment. However, as long as the above temperature gradient can be realized in the invention, either one heat exchanger of the hot heat exchanger112and the cold heat exchanger113can be removed.

In the above embodiment, the description has been made on the case where the generator150is installed on the outside of the branched tube103. However, the invention can also adopt a structure in which the generator150is installed with the turbine140in the inside of the branched tube103when necessary.

In the above embodiment, the description has been made on the case where the energy extraction section160is installed at the other end103bof the branched tube103. However, in the invention, instead of this energy extraction section160, a vibration absorbing material (sponge, urethane, or the like) that can absorb the vibration of the working gas may be installed.

In a case based on the above embodiment or any of various modified examples, the invention can adopt the following aspects.

The invention can adopt an aspect of

a design assist method of a thermoacoustic electric generator system including:

“a tube component that is configured by including: an annular tube configured to be annular; and a branched tube branched from the annular tube, extending lengthwise from one end, which is located at a branched point from the annular tube, to the other end, and communicating with the annular tube and, in which specified working gas is enclosed in both of the annular tube and the branched tube;

a thermoacoustic engine that includes: a stack incorporated in an inside of the annular tube in the tube component and having plural channels, each of which extends in a tube longitudinal direction; and a heat exchanger exchanging heat with the working gas such that a temperature gradient is generated between both ends of each of the plural channels in the stack, so as to cause thermoacoustic oscillation of the working gas;

a turbine provided in the branched tube of the tube component and rotating when receiving acoustic energy, which is generated by thermoacoustic oscillation of the working gas in the thermoacoustic engines; and

a generator for converting kinetic energy generated by rotation of the turbine to electric energy,

the design assist method assisting designing thereof by defining a turbine installment position of the turbine in the branched tube of the tube component, in which

in a pre-installment state of the turbine, flow velocity amplitude as displacement per unit time of the working gas in a tube longitudinal direction in an inside of the branched tube is measured, and a region where the measured flow velocity amplitude is relatively large in each region of the branched tube is defined as the turbine installment position.”

REFERENCE SINGS LIST