FIELD OF THE INVENTION
The subject matter of this invention relates refrigeration and power generators. More particularly, the subject matter of this invention relates to devices and methods of making active heat exchanger electrocaloric refrigerators and pyroelectric energy generators.
BACKGROUND OF THE INVENTION
Currently, the great majority of devices for near room-temperature refrigeration and air conditioning are based on vapor compression technology. In some small niche applications, solid state thermoelectric devices are used. While the solid state thermoelectric devices are much less efficient than vapor compression devices, they are compact and without moving parts or fluids. Both of these technologies are mature and are unlikely to improve much in the foreseeable future. There have been small efforts to develop electrocaloric or magnetocaloric refrigerators, but practical and economic obstacles have prevented their use in practical coolers. Early attempts by Radebaugh et al. (Radebaugh, R; Lawless, W N; Siegwarth, J D; Morrow, A J Cryogenics, Vol. 19, No. 4, pp. 187-208, 1979) and Hadni (Hadni, A J. PHYS. E: SCI. INSTR., Vol. 14, No. 11, pp. 1233-1240, 1981) to develop a cryogenic electrocaloric refrigerator were unsuccessful because the electric fields needed for the required temperature swings were larger than the breakdown fields.
Furthermore, most of the effort in directly extracting electrical energy from heat utilizes some type of thermoelectric material. The thermoelectric approach has been vigorously pursued for decades with modest, incremental success. However, no major breakthroughs have occurred. Pyroelectric energy conversion has been examined for many years, but little progress has been made in developing practical systems. The most efficient systems that have been investigated use the “Olsen cycle”, which involves regenerators and requires moving parts and fluid flow, as described by Lang & Muensit, Appl. Phys. A, 85, 125-134 (2005). Additionally, because this conventional pyroelectric approach uses a single material to span the entire temperature range, the pyroelectric coefficient is well below its maximum value over much of this range.
Hence, there is a need for a new refrigeration device which is more efficient, versatile, and economical than conventional vapor compression refrigerators and a new pyroelectric approach to extract power.
SUMMARY OF THE INVENTION
In accordance with various embodiments, there is an active heat exchanger device including a first single-layer heat engine having a first side configured to be in contact with a first reservoir and a second side configured to be in contact with a second reservoir, wherein the first single-layer heat engine can include a first active layer disposed between a first liquid crystal thermal switch and a second liquid crystal thermal switch. The device can also include a second single-layer heat engine having a first side configured to be in contact with the first reservoir and a second side configured to be in contact with a third reservoir, wherein the second single-layer heat engine can include a second active layer disposed between a third liquid crystal thermal switch and a fourth liquid crystal thermal switch. The device can further include a channel disposed between the first single-layer heat engine and the second single-layer heat engine, the channel configured to transport the fluid from a first end to a second end and one or more power supplies configured to apply voltages to the first, the second, the third, and the fourth liquid crystal thermal switch and the first and the second active layer to create a first temperature difference between the first side and the second side of the first single-layer heat engine, a second temperature difference between the first side and the second side of the second single-layer heat engine, and a third temperature difference between the first end and the second end of the channel.
According to various embodiments, there is a method of cooling a fluid. The method can include creating a first temperature difference between a first side and a second side of a first single-layer heat engine, the first side configured to be in contact with a first reservoir and the second side configured to be in contact with a second reservoir, the first reservoir comprising a fluid, wherein the first single-layer heat engine comprises a first electrocaloric layer disposed between a first liquid crystal thermal switch and a second liquid crystal thermal switch. The method can also include creating a second temperature difference between a first side and a second side of a second single-layer heat engine, the first side configured to be in contact with the first reservoir and the second side configured to be in contact with a third reservoir, wherein the second single-layer heat engine comprises a second electrocaloric layer disposed between a third liquid crystal thermal switch and a fourth liquid crystal thermal switch. The method can further include creating a third temperature difference between a first end and a second end of a channel by flowing the fluid through the channel, such that the fluid enters through the first end of the channel and exits through the second end of the channel, wherein the channel is disposed between the first single-layer heat engine and the second single-layer heat engine.
According to various embodiments, there is a method of extracting electrical power in a pyroelectric energy generator. The method can include extracting electrical energy from a first single-layer heat engine by creating a first temperature difference between a first side and a second side of the first single-layer heat engine, the first side configured to be in contact with a first reservoir and the second side configured to be in contact with a second reservoir, the first reservoir comprising a fluid, wherein the first single-layer heat engine comprises a first pyroelectric layer disposed between a first liquid crystal thermal switch and a second liquid crystal thermal switch. The method can also include extracting electrical energy from a first single-layer heat engine by creating a second temperature difference between a first side and a second side of a second single-layer heat engine, the first side configured to be in contact with the first reservoir and the second side configured to be in contact with a third reservoir, wherein the second single-layer heat engine comprises a second pyroelectric layer disposed between a third liquid crystal thermal switch and a fourth liquid crystal thermal switch. The method can further include extracting electrical energy from a first single-layer heat engine by creating a third temperature difference between a first end and a second end of a channel by flowing the fluid through the channel, such that the fluid enters through the first end of the channel and exits through the second end of the channel, wherein the channel is disposed between the first single-layer heat engine and the second single-layer heat engine.
Additional objects and advantages of the invention will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention. The objects and advantages of the invention will be realized and attained by means of the elements and combinations particularly pointed out in the appended claims.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention, as claimed.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1A schematically illustrates an exemplary device, according to various embodiments of the present teachings.
FIG. 1B schematically illustrates an exemplary active layer of the device shown in FIG. 1A, according to various embodiments of the present teachings.
FIGS. 2A-2C show schematic illustration of an exemplary thermal switch, in accordance with various embodiments.
FIG. 3 shows a schematic illustration of an exemplary device with a single active layer sandwiched between two thermal switches, in accordance with various embodiments.
FIG. 4 shows a Carnot cycle in the temperature-entropy plane for an exemplary electrocaloric cooling device as shown in FIG. 3, in accordance with the present teachings.
FIG. 5 shows a Carnot cycle in the displacement-electric field plane for the exemplary electrocaloric cooling device shown in FIG. 3, in accordance with the present teachings.
FIG. 6A shows heat flow during the warm isothermal phase of the Carnot cycle shown in FIG. 4 for the exemplary electrocaloric cooling device shown in FIG. 3, according to various embodiments of the present teachings.
FIG. 6B shows heat flow during the cool isothermal phase of the Carnot cycle shown in FIG. 4 for the exemplary electrocaloric cooling device shown in FIG. 3, according to various embodiments of the present teachings.
FIG. 7 shows operation of an exemplary multilayer electrocaloric cooling device, in accordance with various embodiments of the present teachings.
FIG. 8 shows a Carnot cycle in the temperature-entropy plane for an exemplary pyroelectric energy generator as shown in FIG. 3, in accordance with the present teachings.
FIG. 9 shows a Carnot cycle in the displacement-electric field plane for an exemplary pyroelectric energy generator as shown in FIG. 3, in accordance with the present teachings.
FIG. 10A shows heat flow during the warm isothermal phase of the Carnot cycle shown in FIG. 8 for the exemplary pyroelectric energy generator shown in FIG. 3, according to various embodiments of the present teachings.
FIG. 10B shows heat flow during the cool isothermal phase of the Carnot cycle shown in FIG. 8 for the exemplary pyroelectric energy generator shown in FIG. 3, according to various embodiments of the present teachings.
FIG. 11 shows operation of an exemplary multilayer pyroelectric generator, in accordance with various embodiments of the present teachings.
FIG. 12 shows a schematic illustration of a cross sectional view of an exemplary active heat exchanger device, in accordance with various embodiments of the present teachings.
FIG. 13 shows a schematic illustration of a cross sectional view of another exemplary active heat exchanger device, in accordance with various embodiments of the present teachings.
DESCRIPTION OF THE EMBODIMENTS
Reference will now be made in detail to the present embodiments, examples of which are illustrated in the accompanying drawings. Wherever possible, the same reference numbers will be used throughout the drawings to refer to the same or like parts.
Notwithstanding that the numerical ranges and parameters setting forth the broad scope of the invention are approximations, the numerical values set forth in the specific examples are reported as precisely as possible. Any numerical value, however, inherently contains certain errors necessarily resulting from the standard deviation found in their respective testing measurements. Moreover, all ranges disclosed herein are to be understood to encompass any and all sub-ranges subsumed therein. For example, a range of “less than 10” can include any and all sub-ranges between (and including) the minimum value of zero and the maximum value of 10, that is, any and all sub-ranges having a minimum value of equal to or greater than zero and a maximum value of equal to or less than 10, e.g., 1 to 5. In certain cases, the numerical values as stated for the parameter can take on negative values. In this case, the example value of range stated as “less that 10” can assume negative values, e.g. −1, −2, −3, −10, −20, −30, etc.
FIG. 1A schematically illustrates an exemplary device 100, according to various embodiments of the present teachings. The device 100 can include a first reservoir 110 at a first temperature T1 and a second reservoir 115 at a second temperature T2, wherein the first temperature T1 is lower than the second temperature T2. Depending upon the application in which the device 100 is used, the first reservoir 110 and the second reservoir 115 can be, but is not limited to, one or more of ambient air, a storage unit of a refrigerator, one or more electronic components of an electronic device, an electronic device, a furnace, a radiator of an automobile, an exhaust system of an automobile, a human body, and any other suitable heat sink. The device 100 can also include a plurality of liquid crystal thermal switches 140 disposed between the first reservoir 110 and the second reservoir 115. The device 100 can further include one or more active layers 130 disposed between the first reservoir 110 and the second reservoir 115, such that each of the one or more active layers 130 can be sandwiched between two liquid crystal thermal switches 140. FIG. 1B schematically illustrates another embodiment, wherein each of the one or more active layers 130 can further include a stack of alternating thin active layers 132 and electrode layers 134, such that each of the thin active layer 132 is disposed between two electrode layers 134. The device 100 can further include one or more power supplies 150 to apply voltage to one or more of the liquid crystal thermal switches 140 and the active layers 130.
In various embodiments, each of the plurality of liquid crystal thermal switches 140 can include a thin layer 144 of liquid crystal sandwiched between two metal layers 142, 146, as shown in FIG. 1A. FIGS. 2A-2C show another exemplary thermal switch 240 in accordance with various embodiments of the present teachings. The thermal switch 240 can include a first metal layer 244 and a first insulating layer 221 disposed over the first metal layer 246, wherein the first insulating layer 221 can include one or more pairs of first interdigitated electrodes 248 on a first surface 223. In various embodiments, each of the one or more pairs of first interdigitated electrodes 248 can include a plurality of first electrodes 249, as shown in FIG. 2B. The thermal switch 240 can also include a second insulating substrate 222 including a second pair of interdigitated electrodes 248 on a second surface 225. Each of the one or more pairs of second interdigitated electrodes 248 can have a structure as shown in FIG. 2B. The thermal switch 240 can further include a thin layer 244 of liquid crystal 245 disposed between the first surface 223 of the first insulating substrate 221 and the second surface 225 of the second insulating substrate 222, wherein the liquid crystal 245 can have anisotropic thermal conductivity. As used herein, the term “anisotropic thermal conductivity” means different thermal conductivities in the direction perpendicular and parallel to the director 247 of the liquid crystal 245. The ratio of these thermal conductivities has been measured and can be larger than about 3. The thermal switch 240 can also include a second metal layer 246 disposed over the second insulating layer 222, as shown in FIG. 2A. FIG. 2A shows the open state where the thermal conductivity across the thin layer 244 of the liquid crystal 245 is low. FIG. 2C shows the closed state, where the thermal conductivity across the thin layer 244 of liquid crystal 245 is high.
Exemplary liquid crystal can include, but are not limited to ZL1-2806 and MLC-2011 (Merck, Japan). In some embodiments, the thin layer 144 of liquid crystal can include a plurality of carbon nanotubes. While not intending to be bound by any specific theory, it is believed that the addition of carbon nanotubes can further enhance the anisotropy of the thermal conductivity of the thin layer 130 of liquid crystal 132.
In various embodiments, each of the one or more active layers 130 and the liquid crystal thermal switches 140, 240 can have a thickness from about 10 μm to about 100 μm. In certain embodiments, as shown in FIG. 1B, each of the thin active layers 132 can have a thickness from about 0.01 μm to about 5 μm and in some cases from about 0.1 μm to about 1 μm. In some embodiments, the device 100 can have tens of layers, depending upon the temperature difference between the first and the second reservoirs 110, 115. In other embodiments, the device 100 can have a thickness on the order of millimeters. FIG. 3 shows another embodiment, where the device 300 can include only one active layer 330 between the first reservoir 310 and the second reservoir 315, such that the active layer 330 can be sandwiched between the two liquid crystal thermal switches 340, 340′.
In certain embodiments, each of the one or more active layers 130 can include an electrocaloric layer and the device 100 can be an electrocaloric cooling device. Exemplary electrocaloric materials include, but are not limited to, PbZrxTi(1-x)O3 (PZT), poly(vinylidene fluoride) (PVDF), poly(vinylidene fluoride-trifluoroethylene) [P(VDF-TrFE)], and ferroelectric liquid crystals. The principle physical mechanism in the electrocaloric cooling device 100 in accordance with the present teachings is the electrocaloric effect in which application of an electrical potential across an electrocaloric material changes its temperature. The exemplary electrocaloric cooling device 100 overcomes previous disadvantages by making use of thin film technologies and by utilizing a thin film thermal switch. Since, heat flow is very rapid in thin films, effective refrigeration can be achieved through rapid voltage cycling of the electrocaloric material and through rapid operation of the heat switch, allowing significant fractions of Carnot efficiency with less than perfect materials. Larger temperature drops can be achieved by stacking several structures.
In various embodiments, there can be a food storage unit including the electrocaloric cooling device 100. In other embodiments, there can be an air conditioning unit including the electrocaloric cooling device 100. The air conditioning unit can be used in, for example, buildings and automobiles. In some other embodiments, there can be an electronic device including the electrocaloric cooling device 100 for cooling individual electronic components. In various embodiments, the electrocaloric cooling device 100 can be well suited for portable applications because of its compactness and ruggedness.
According to various embodiments, there is a method of driving heat flow from the first reservoir 110, 310 to the second reservoir 115, 315 in the electrocaloric cooling device 100, 300, using the Carnot cycle 400, shown in FIG. 4. For simplicity, an electrocaloric cooling device 300 including a single stack of electrocaloric layer 330 disposed between the first thermal switch 340 and the second thermal switch 340′, is shown in FIG. 3 and will be used for discussion of the method of operation. The Carnot cycle 400 shown in FIG. 4 is in the temperature-entropy plane, while FIG. 5 shows a Carnot cycle in the displacement-electric field plane. In various embodiments, the method of driving heat flow from the first reservoir 110, 310 to the second reservoir 115, 315 in the electrocaloric cooling device 100, 300, using the Carnot cycle 400 can include a first isothermal step (a) of closing the second liquid crystal thermal switch 340′ adjacent to the second reservoir 315 at a temperature T2, opening the first liquid crystal thermal switch 340 on the other side of the electrocaloric layer 330 and adjacent to the first reservoir 310 at a temperature T1 to transfer heat from the electrocaloric layer 330 at a temperature T3 to the second reservoir at the temperature T2, wherein T3 is greater than T2 and T2 is greater than T1. The isothermal step (a) can also include keeping the temperature of the electrocaloric layer 330 constant at T3 by increasing the electric field across the electrocaloric layer 330. The Carnot cycle 400 can further include the adiabatic step (b) of opening both the first and the second liquid crystal thermal switches 340, 340′ and changing the temperature of the electrocaloric layer 330 from T3 to T4 (T4 being less than T1) by decreasing the electric field across the electrocaloric layer 330. The third step (c) of the Carnot cycle 400 can include closing the first liquid crystal thermal switch 340 adjacent to the first reservoir 310 at the temperature T1 and opening the second liquid crystal thermal switch adjacent to the second reservoir 315 at a temperature T2, to extract heat from the first reservoir 310 at the temperature T1 to the electrocaloric layer 330 at T4 because T1>T4. The isothermal step can also include keeping the temperature of the electrocaloric layer 330 constant at T4 by decreasing the electric field across the electrocaloric layer 330. The Carnot cycle 400 can also include another adiabatic step (d) of opening both the first and the second liquid crystal thermal switches 340, 340′ and increasing the temperature of the electrocaloric layer from T4 to T3 by increasing the electric field across the electrocaloric layer 330. The steps a-d, can be repeated, as desired, across each stack of alternating electrocaloric layers 130, 330 and liquid crystal thermal switches 140, 340, 340′ of the multilayer stack of the electrocaloric cooling device 100, 300. The Carnot cycle 400 can be effectively used with the multilayer stack of the electrocaloric cooling device 100 because the temperature spanned by each layer of the electrocaloric cooling device 100 can be less than about 10° C. The four steps of the Carnot cycle 400 shown in FIG. 4 can be repeated across each stack of alternating electrocaloric layers 130 and liquid crystal thermal switches 140 of the multilayer stack. As the voltage across each electrocaloric layer 130 is changed, the electrocaloric layer 130 heats or cools from its average value. By opening and closing the liquid crystal thermal switches at the appropriate time, the heat can be forced to flow from the cold reservoir at T1 to the warm reservoir at T2.
FIGS. 6A and 6B illustrate the heat flow in a single electrocaloric layer 330 during the warm and cool isothermal phases of the Carnot cycle shown in FIG. 4. The relative thickness of the arrow indicates the magnitude of the heat flow through liquid crystal thermal switches 340, 340′. In the “closed” state, the liquid crystal thermal switches 340, 340′ can have high thermal conductivity Khigh, and in the open state they can have low thermal conductivity Klow. In various embodiments, the ratio Khigh/Kb, can be greater that 3. The larger the ratio Khigh/Klow, the lower the entropy generating heat leakage through the “open’ liquid crystal thermal switches 340, 340′ and the greater the efficiency with which the electrocaloric refrigerator 300 can extract heat from the cold reservoir 310.
FIG. 7 illustrates operation of an exemplary multilayer electrocaloric cooling device 700, in accordance with various embodiments of the present teachings. To effectively use a stack of electrocaloric layers 730 in a heat engine such as, electrocaloric cooling device 700, the thermal connections between the electrocaloric layers 730 has to be opened and closed appropriately as the electrocaloric layers 730 are heated or cooled. The multilayer electrocaloric cooling device 700 can operate in a “bucket brigade” mode, rhythmically passing heat between adjacent electrocaloric layers 730. Thermal switches 740 on both sides of each of the electrocaloric layers 730 can control the heat flow. The top panel in FIG. 7 is a schematic of a thin-film electrocaloric cooling device 700 with four electrocaloric layers 730. The electrocaloric layers 730 can be connected to the hot and cold ends of the device 700 and to each other by thermal switches 740. The bottom panel shows the temperature profiles of the device 700 during two phases of operation when it is functioning as a refrigerator. During Phase 1 for the electrocaloric cooling device 700, the voltages across the electrocaloric layers 730 can be adjusted so that the first and third layers are cool relative to their average temperatures and the second and fourth are relatively warm. The thermal switches 740 can be adjusted so that the net heat flows are to the right from the cold reservoir 710 to the first electrocaloric layer, from the second layer to the third, and from the fourth layer to the hot reservoir 715. During the Phase 2, the voltages are adjusted such that electrocaloric layers 730 one and three are relatively warm and the electrocaloric layers 730 two and four are cooler. The thermal switches 740 are reversed so that the heat continues to flow towards the right (from electrocaloric layer 730 one to two and from electrocaloric layer 730 three to four). The shaded regions show the temperature range through which the electrocaloric material shifts between Phases 1 and 2.
Referring back to FIG. 4, this figure shows the thermodynamic cycle of a single layer of electrocaloric material of an electrocaloric cooling device in the temperature entropy plane. Two dashed curves of constant electric field are shown to indicate how the applied electric field changes around the cycle. Each electrocaloric layer 130, 330730 undergoes a Carnot cycle. A changing electric field drives the vertical, adiabatic legs (b) and (d) of the cycle. A combination of heat flows and changing electric field maintains constant temperature in the horizontal isothermal legs (a) and (c). The efficiency of an actual thin-film heat engine/electrocaloric cooling device is lower than the Carnot value because of entropy generation from heat flows though the thermal switches and because of hysteresis in the electrocaloric material.
Furthermore, if the electrocaloric layer 130, 330, 730 comprises a multilayer structure 130B shown in FIG. 1B, wherein many sub-micron layers 132 can be separated by electrodes 134, the diffusion time can be made long relative to the response time of the thermal switches and large electric fields can be produced with low voltages.
The electrocaloric cooling devices 100 according to the present teachings can be thin, efficient devices that can function in a large array of novel situations. Furthermore, the materials used in the electrocaloric refrigerators can be relatively inexpensive and the growth techniques are simple and are well established in the prior art; these devices can be economically produced in large volumes and may prove to be more economical than vapor compression devices. The efficiency of the electrocaloric cooling devices can exceed those of vapor compression devices, depending on the performance of the liquid crystal thermal switches.
Referring back to the device 100, shown in FIG. 1, each of the one or more active layers 130 can include a pyroelectric layer and the device 100 can be a pyroelectric energy generator. Exemplary pyroelectric materials include, but are not limited to, PbZrxTi(1-x)O3 (PZT), poly(vinylidene fluoride) (PVDF), poly(vinylidene fluoride-trifluoroethylene) [P(VDF-TrFE)], and ferroelectric liquid crystals. The principle physical mechanism in the exemplary pyroelectric energy generator 100 in accordance with the present teachings is the pyroelectric effect in which a change in temperature of the pyroelectric material results in a generation of an electrical potential. The pyroelectric effect is opposite of the electrocaloric effect, where an applied voltage can reversibly change the temperature of the pyroelectric/electrocaloric material. The exemplary pyroelectric energy generator 100 can use stacks of thin films of pyroelectric material 130 separated by liquid-crystal thermal switches 140 to generate electric energy from the heat flow from a hot medium 115 to a cool one 110. As the liquid-crystal thermal switches 140 open and close, heat flows into and out of each thin layer 130 of pyroelectric material. By appropriately adjusting the phase and amplitude of the voltages across each layer, electric power can be efficiently extracted through Carnot cycle.
In various embodiments, there can be an automobile including the pyroelectric energy generator 100 for extracting electrical energy from a surface that can be at a temperature different from its surrounding environment. In some embodiments, the surface can be a radiator. In other embodiments, the surface can be an exhaust system. In some embodiments, there is a furnace including the pyroelectric energy generator 100 for extracting electrical energy from its surface that is at a temperature different from its surrounding environment. In other embodiments, either the first reservoir 110 or the second reservoir 120 of the exemplary pyroelectric energy generator 100 can include a human body.
According to various embodiments, there is a method of extracting electrical power in the pyroelectric energy generator 100, 300 using the Carnot cycle 800, shown in FIG. 8. For simplicity, a pyroelectric generator 300 including a single stack of pyroelectric layer 330 disposed between the first thermal switch 340 and the second thermal switch 340′, as shown in FIG. 3 will be used for discussion of the method of extracting electrical power. The Carnot cycle 700 shown in FIG. 8 is in the temperature-entropy plane and in FIG. 9 is in the displacement-electric field plane. The method of extracting electrical power in the pyroelectric energy generator 100 using the Carnot cycle 800 can include the first isothermal step (a) of closing the second liquid crystal thermal switch 340′ adjacent to the second reservoir 315 at the temperature T2 and opening the first liquid crystal thermal switch 340 adjacent to the first reservoir 310 at a temperature T1 on the other side to the pyroelectric layer 330 to transfer heat from the second reservoir 315 at T2 to the pyroelectric layer 330 at a temperature T3 (T3<T2). The isothermal step (a) can also include maintaining the temperature of the pyroelectric layer 330 constant at T3 by decreasing the applied electric field. The Carnot cycle 800 can also include an adiabatic step (b) of opening both the first and the second liquid crystal thermal switches 340, 340′ and changing the temperature of the pyroelectric layer 330 from T4 to T3 by decreasing the applied electric field on the pyroelectric layer 330, wherein T4<T1. The Carnot cycle 800 can further include a step (c) of closing the first liquid crystal thermal switch 340 and opening the second liquid crystal thermal switch 340′, such that heat is transferred from the first reservoir 310 at the temperature T1 to the pyroelectric layer 330 at temperature T4 (T4 being less than T1). The isothermal step (c) can further include keeping the temperature of the pyroelectric layer constant at T4, by extracting electrical power from the pyroelectric layer 330. The Carnot cycle 800 can also include step (d) of opening both the first and the second liquid crystal thermal switches 340, 340′ to induce a temperature change of the pyroelectric layer from T4 to T3 and extracting electrical power from the pyroelectric layer 330. The steps a-d can be repeated as desired, across each stack of alternating pyroelectric layers 130, 330 and liquid crystal thermal switches 140, 340, 340′ of the multilayer stack. Furthermore, by appropriately adjusting the heat flow with thermal switches 140 and the temperature of the pyroelectric layers 130 with applied voltages, each pyroelectric layer 130 can closely approximate the rectangular Carnot heat cycle 700 in the temperature-entropy plane as shown in FIG. 8. This cycle maximizes the electrical power that can be extracted for a given heat flow. Each of the one or more pyroelectric layers 130 in the pyroelectric energy generator 100 can operate in a narrow temperature range. In various embodiments, the composition of each pyroelectric layer 130 can be further adjusted to tune its Curie temperature to further optimize the pyroelectric and electrocaloric effects for its operation.
FIGS. 10A and 10B illustrate the heat flow in a single pyroelectric layer 130 during the warm and cool isothermal phases of the Carnot cycle 800 shown in FIG. 8. The relative thickness of the arrow indicates the magnitude of the heat flow through liquid crystal thermal switches 140. In the “closed” state, the liquid crystal thermal switches 140 can have high thermal conductivity Khigh, and in the open state they can have low thermal conductivity Klow. In various embodiments, the ratio Khigh/Klow can be greater that about 3. The larger the ratio, the lower the entropy generating heat leakage through the “open’ switches and the greater the efficiency with which the pyroelectric energy generator 100 can generate electrical power.
FIG. 11 illustrates operation of an exemplary multilayer pyroelectric energy generator 1100, in accordance with various embodiments of the present teachings. To effectively use a stack of pyroelectric layers 1130 in a heat engine such as, the pyroelectric energy generator 1100, the thermal connections between the pyroelectric layers 1130 has to be opened and closed appropriately as the pyroelectric layers 1130 are heated or cooled. The multilayer pyroelectric energy generator 1100 can operate in a “bucket brigade” mode, rhythmically passing heat between adjacent pyroelectric layers 1130. Thermal switches 1140 on both sides of each of the pyroelectric layers 1130 can control the heat flow. The top panel in FIG. 11 is a schematic of a pyroelectric energy generator 1100 with four pyroelectric layers 1130. The pyroelectric layers 1130 are connected to the hot and cold ends of the device 1100 and to each other by thermal switches 1140. The bottom panel shows the temperature profiles of the pyroelectric energy generator 1100 during two phases of operation. When the thin-film heat engine operates as a pyroelectric energy generator 1100, the heat flow is from the hot reservoir 1115 to the cold reservoir 1110 (to the left) and electrical power is extracted. The sequence of voltage and heat switch changes is similar to that of the electrocaloric cooling device 700 cycle described earlier. The important difference is that in the pyroelectric energy generator 1100, there is a net flow of heat into the pyroelectric material when it is hot and out of this material when it is cool, the reverse of what happens in the electrocaloric cooling device 700.
The pyroelectric generators according to the present teachings can be thin, flat devices that can be attached to a large variety of hot surfaces to salvage electrical power. Furthermore, the materials used in the pyroelectric generators can be relatively inexpensive and the growth techniques are simple and are well established in the prior art. Hence, pyroelectric generators provide a cost effective approach to salvaging electric power from heat that would otherwise be wasted.
According to various embodiments, there is a method of forming a device 100. The method can include providing a first reservoir 110 at a first temperature T1 and providing a second reservoir 115 at a second temperature T2, wherein the first temperature T1 is less than the second temperature T2. The method can also include forming a multilayer stack of alternating one or more electrocaloric layers 130 and liquid crystal thermal switches 140 between the first reservoir 110 and the second reservoir 115, such that each of the one or more active layers 130 is sandwiched between two liquid crystal thermal switches 140. The method of forming a device 100 can further include providing one or more power supplies 150 to apply voltage to the plurality of liquid crystal thermal switches 140 and the one or more active layers 130.
In some embodiments, the step of forming a multilayer stack of alternating one or more active layers 130 and liquid crystal thermal switches 140 can include forming a first layer 142 of metal, forming a thin layer of liquid crystal over the first layer of metal, forming a second layer 146 of metal over the thin layer 144 of liquid crystal, forming an active layer 130 over the second layer 146 of metal and repeating the above mentioned steps to form the multilayer stack of alternating one or more active layers 130 and liquid crystal thermal switches 140. In some embodiments, the step of forming a thin layer of liquid crystal can further include adding a plurality of carbon nanotubes to the thin layer of liquid crystal. In certain embodiments, the step of forming an active layer 130, 130B over the second layer 146 of metal further include forming a first thin active layer 132 over a first thin electrode layer 134, as shown in FIG. 1B, forming a second thin electrode layer 134 over the first thin active layer 132, and so on to form the active layer 130B including a multilayer stack of alternating thin active layers 132 and electrode layers 134.
In other embodiments, the step of forming a multilayer stack of alternating one or more active layers 130, 230 and liquid crystal thermal switches 140, 240 can include forming a first layer 142, 242 of metal and providing a first insulating layer 221 over the first layer 242 of metal. In various embodiments, the first insulating layer 221 can include one or more pairs of first interdigitated electrodes 248 on a first surface 223 of the first insulating layer 221 on a side opposite the first layer 242 of metal, wherein each of the one or more pairs of first interdigitated electrodes 248 can include a plurality of first electrodes 249. The method can also include forming a thin layer 244 of liquid crystal 245 over the first surface 223 of the first insulating layer 221 and providing a second insulating layer 222 over the thin layer, 244 of liquid crystal 245, such that a second surface 225 of the second insulating layer 222 is disposed over the thin layer 244 of liquid crystal 245. In some embodiments, the step of forming a thin layer 144,244 of liquid crystal can further include adding a plurality of carbon nanotubes to the thin layer 144,244 of liquid crystal 245. In various embodiments, the second insulating layer 222 can include one or more pairs of second interdigitated electrodes 248′ on the second surface 225 of the second insulating layer 222. In various embodiments, each of the one or more pairs of second interdigitated electrodes 248′ can include a plurality of second electrodes 249′ having similar arrangement as that of first electrodes 249 shown in FIG. 2B. The method can further include forming a second layer 246 of metal over the second insulating layer 222 on a side opposite the second surface 222, forming an active layer 130 over the second layer 146, 246 of metal, and repeating the above steps, as desired, to form the multilayer stack 100 of alternating one or more active layers 130 and liquid crystal thermal switches 140, 240, as shown in FIG. 1.
Referring back to the method of forming a device 100, the step of forming one or more multilayer stacks of alternating active layers 130 and liquid crystal thermal switches 140 between the first reservoir 110 and the second reservoir 115 can include forming one or more multilayer stacks of alternating electrocaloric layers 130 and liquid crystal thermal switches 140 between the first reservoir 110 and the second reservoir 115. The device 100, including the electrocaloric layer can be an electrocaloric cooling device.
Referring back to the method of forming a device 100, the step of forming one or more multilayer stacks of alternating active layers 130 and liquid crystal thermal switches 140 between the first reservoir 110 and the second reservoir 115 can include forming one or more multilayer stacks of alternating pyroelectric layers 130 and liquid crystal thermal switches 140 between the first reservoir 110 and the second reservoir 115. The device 100, including the pyroelectric layer can be a pyroelectric energy generator.
FIG. 12 shows an exemplary active heat exchanger device 1200 in accordance with various embodiments of the present teachings. The exemplary active heat exchanger device 1200 can include a first single-layer heat engine 1265 having a first side 1261 configured to be in contact with a first reservoir 1210 and a second side 1262 configured to be in contact with a second reservoir 1215. In various embodiments, the first reservoir 1210 can include a fluid. Any suitable liquid or gas can be used as the fluid. Exemplary fluids include, but are not limited to, air, water, glycols, mixture of water and glycol. In various embodiments, the first single-layer heat engine 1265 can include a first active layer 1230 disposed between a first liquid crystal thermal switch 1240 disposed adjacent to the first reservoir 1210 and a second liquid crystal thermal switch 1240′ disposed adjacent to the second reservoir 1215. The exemplary active heat exchanger device 1200 can also include a second single-layer heat engine 1265′ having a first side 1261′ in contact with the first reservoir 1210 and a second side 1262′ in contact with a third reservoir 1215′. In various embodiments, the second single-layer heat engine 1265′ can include a second active layer 1230′ disposed between a third liquid crystal thermal switch 1240″ disposed adjacent to the first reservoir 1210 and a fourth liquid crystal thermal switch 1240′ disposed adjacent to the third reservoir 1215′.
The exemplary active heat exchanger device 1200 can further include a channel 1275 disposed between the first single-layer heat engine 1265 and the second single-layer heat engine 1265′, the channel 1275 configured to transport the fluid from a first end 1271 of the channel 1275 to a second end 1272 of the channel 1275 and one or more power supplies (not shown) configured to apply voltages to the first, the second, the third, and the fourth liquid crystal thermal switches 1240, 1240′, 1240″,1240″ and the first and the second active layers 1230, 1230′ to create a first temperature difference between the first side 1261 and the second side 1262 of the first single-layer heat engine 1265, a second temperature difference between the first side 1261′ and the second side 1262′ of the second single-layer heat engine 1265′, and a third temperature difference between the first end 1271 of the channel 1275 and the second end 1272 of the channel 1275. The channel 1275 can have any suitable shape such as planar and cylindrical.
In various embodiments, each of the first, the second, the third, and the fourth liquid crystal thermal switches 1240, 1240′, 1240″, 1240′″ can include a thin layer of liquid crystal sandwiched between two metal layers, as described earlier and shown in FIGS. 2A-2B. In some embodiments, the thin layer of liquid crystal can include carbon nanotubes. In some embodiments, each of the first and the second active layers 1230, 1230′ can further include a stack of alternating thin active layers and electrode layers, such that each of the thin active layer can be disposed between two electrode layers, as described earlier and shown in FIG. 1B.
In some embodiments, the first and the second active layer 1230, 1230′ can include an electrocaloric material and the active heat exchanger device 1200 can be an electrocaloric cooling device. In various embodiments, there can be a food storage unit including the electrocaloric cooling device 1200. In other embodiments, there can be an air conditioning unit including the electrocaloric cooling device 1200. The air conditioning unit can be used in, for example, buildings and automobiles. In some other embodiments, there can be an electronic device including the electrocaloric cooling device 1200 for cooling individual electronic components. In various embodiments, the electrocaloric cooling device 1200 can be well suited for portable applications because of its compactness and ruggedness.
According to various embodiments, there is a method of cooling a fluid, the method can include providing an electrocaloric cooling device, such as the exemplary active heat exchanger device 1200 shown in FIG. 12. In the electrocaloric device, the active layer can include any suitable electrocaloric material. The method can include creating a first temperature difference (ΔT1n=|T2,1−T1,1| or |T2,n−T1,n|) between the first side 1261 and the second side 1262 of the first single-layer heat engine 1265 and a second temperature difference (ΔT2n=|T′2,1−T1,1| or |T′2,n−T1,n|) between the first side 1261′ and the second side 1262′ of the second single-layer heat engine 1265′, such that heat flows from the fluid 1210 to the second 1215 and the third reservoir 1215′. The two dashed lines 12011, and 1201n each represent a single-layer heat engine and a plurality of single-layer heat engines between them, each operated by a, such as the Carnot cycle 400 shown in FIG. 4. The method can further include flowing the fluid 1210 through the channel 1275 such that the fluid 1210 enters through the first end 1271 and exits through the second end 1272, such that the flowing fluid can create a third temperature difference (ΔT3n=|T1,n−T1,1|) between the first end 1271 and the second end 1272 of the channel 1275.
In various embodiments, the step of creating a first temperature difference (ΔT1n=|T2,n−T1,n|) between the first side 1261 and the second side 1262 of the first single-layer heat engine 1265 can include a step (a) of closing the second liquid crystal thermal switch 1240′ adjacent to the second reservoir 1215 at a second set of temperatures T2,i (where i=1−n) and opening the first liquid crystal thermal switch 1240 adjacent to the first reservoir 1210 at a first set of temperatures T1,i, thereby transferring heat from the first electrocaloric layer 1230 at a third set of temperatures T3,i to the second reservoir 1215 at temperature T2,i and keeping the temperature of the first electrocaloric layer 1230 constant at T3,i by increasing the electric field across the first electrocaloric layer 1230, wherein T3,i is greater than T2,i and T2,i is greater than T1,i. The method can include a step (b) of opening both the first and the second liquid crystal thermal switches 1240, 1240′ and changing the temperature of the first electrocaloric layer 1230 from T3,i to T4,i by decreasing the electric field across the first electrocaloric layer 1230, wherein T4,i is less than T1,i and a step (c) of closing the first liquid crystal thermal switch 1240 and opening the second liquid crystal thermal switch 1240′, to extract heat from the first reservoir 1210 at T1,i to the first electrocaloric layer 1230 at T4,i and keeping the temperature of the first electrocaloric layer 1230 constant at T4,i by decreasing the electric field across the first electrocaloric layer 1230. The method can also include a step (d) of opening both the first and the second liquid crystal thermal switches 1240, 1240′ and increasing the temperature of the electrocaloric layer 1230 from T4,i to T3,i by increasing the electric field across the first electrocaloric layer 1230. The steps a-d as described here are shown in FIG. 4 and the steps a-d can be repeated as desired, across the first electrocaloric layer 1230 and the first and second liquid crystal thermal switches 1240, 1240′ of the first single-layer heat engine 1265. As a result of flowing fluid the fluid at the second end 1271 can be a lower temperature than the fluid at the first end 1271. In various embodiments, the third temperature difference (ΔT3n=|T1,n−T1,1|) can be many times the first and the second temperature difference (ΔT1n, ΔT2n). The third temperature difference (ΔT3n=|T1,n−T1,1|) depends upon the various factors such as, the rate of flow of fluid, the length of the single layer heat engines and the first and the second temperature differences.
Referring back to FIG. 12, the first and the second active layer 1230, 1230′ can include a pyroelectric material and the active heat exchanger device 1200 can be a pyroelectric energy generator. In various embodiments, there can be an automobile including the pyroelectric energy generator 1200 for extracting electrical energy from a surface that can be at a temperature different from its surrounding environment. In some embodiments, the surface can be a radiator. In other embodiments, the surface can be an exhaust system. In some embodiments, there is a furnace including the pyroelectric energy generator 1200 for extracting electrical energy from its surface that is at a temperature different from its surrounding environment.
In various embodiments, each single layer heat engine 1265, 1265′ of the pyroelectric generator 1200 can operate by a Carnot cycle for extracting electrical energy, such as, the Carnot cycle 800 shown in FIG. 8. The method for extracting electrical energy from the first single-layer heat engine 1265 can include a step (a) of closing the second liquid crystal thermal switch 1240′ adjacent to the second reservoir 1215 at a second set of temperatures T2,i and opening the first liquid crystal thermal switch 1240 adjacent to the first reservoir 1210 at a first set of temperatures T1,i (T1,i<T2,i), thereby transferring heat from the second reservoir 1215 to the first pyroelectric layer 1230 at a third set of temperatures T3,i (T3,i<T2,i) and extracting electrical power from the first pyroelectric layer 1230 by maintaining the temperature of the first pyroelectric layer 1230 constant at T3,i by decreasing the electric field across the first pyroelectric layer 1230. The method can include a step (b) of opening both the first and the second liquid crystal thermal switches 1240, 1240′ and changing the temperature of the first pyroelectric layer 1230 from T3,i to T4,i by decreasing the electric field across the first pyroelectric layer 1230 and extracting electrical power from the first pyroelectric layer 1230, wherein T1,i is less than The method can further include a step (c) of closing the first liquid crystal thermal switch 1240 and opening the second liquid crystal thermal switch 1240′, such that heat is transferred from the first reservoir 1210 at T1,i to the first pyroelectric layer 1230 at T4,i (T4,i<T1,i) and keeping the temperature of the first pyroelectric layer 1230 constant at T4,i by increasing the electric field across the electrocaloric layer 1230 and a step (d) of opening both the first and the second liquid crystal thermal switches 1240, 1240′ to induce a temperature change of the first pyroelectric layer 1230 from T4,i to T3,i. The steps a-d can be repeated as desired, across the first pyroelectric layer 1230 and the first and second liquid crystal thermal switches 1240, 1240′ of the first single-layer heat engine 1265. The second single-layer heat engine 1265′ can operate similar to the first single-layer heat engine 1265.
FIG. 13 shows another exemplary active heat exchanger device 1300 including a plurality of single-layer heat engines 13651, 13652, 13653, 13654, 13655 and a plurality of channels 13751, 13752, 13753, 13754, such that each of the plurality of single-layer heat engines 13651, 13652, 13653, 13654, 13655 is separated by at least one of the plurality of channels 13751, 13752, 13753, 13754. As shown in FIG. 13, the single-layer heat engines 13651 and 13652 can be separated by the channel 13751; the single-layer heat engines 13652 and 13653 can be separated by the channel 13752; the single-layer heat engines 13653 and 13654 can be separated by the channel 13753; and the single-layer heat engines 13655 and 13656 can be separated by the channel 13754. In some embodiments, each of the plurality of single-layer heat engines 13651, 13652, 13653, 13654, 13655 can include an electrocaloric material and in such a case, the active heat exchanger device 1300 can act as an electrocaloric cooling device. For the heat exchanger device 1300 to act as an electrocaloric cooling device, each of the plurality of single-layer heat engines 13651, 13652, 13653, 13654, 13655 can operate by a Carnot cycle, such as the Carnot cycle 400 shown in FIG. 4. Furthermore, the two dashed lines 13011, and 1301n each represent a single-layer heat engine and a plurality of single-layer heat engines between them, each operated by a Carnot cycle, such as the Carnot cycle 400 shown in FIG. 4. The electrocaloric cooling device can cool a fluid flowing through the plurality of channels 13751, 13752, 13753, 13754. In some embodiments, the plurality of channels 13751, 13752, 13753, 13754 can be connected to each other, such that the fluid in the first channel 13751 at a first set of temperatures T1,i exits from the first channel 13751 and enters the second channel 13752 at a temperature T3,i, such that T1,i<T3,i. Similarly, the fluid exiting from the second channel 13752 can enter the third channel 13753 at a fourth set of temperature T4,i, such that such that T4,i<T3,i, and so on thereby creating a first temperature difference (ΔT1i=|T2,i−T1,i|, |T3,i−T1,i|, |T4,i−T3,i|, |T5,i−T4,i|, where i=1−n). As a result the fluid exiting the fifth channel 13755 is at a much lower temperature than the fluid entering the first channel 13751. Also, depending upon various factors such as, the rate of flow of fluid, the length of the single layer heat engines and the first and the second temperature differences, a third temperature difference (ΔT3i=|T1,i−T1,i|, |T3,i−T3,i|, |T4,i−T4,i|, |T5,i−T5,i|, where i=1−n) can be created along the length of each of the plurality of channels 13751, 13752, 13753, 13754, which can be many times the first temperature difference (ΔT1i).
In various embodiments, each of the plurality of single-layer heat engines 13651, 13652, 13653, 13654, 13655 can include a pyroelectric material and in such a case, the active heat exchanger device 1300 can act as a pyroelectric energy generator. For the heat exchanger device 1300 to act as a pyroelectric energy generator, each of the plurality of single-layer heat engines 13651, 13652, 13653, 13654, 13655 can operate by a Carnot cycle, such as the Carnot cycle 800 shown in FIG. 8, similarly to the electrocaloric cooling device as described earlier.
While the invention has been illustrated respect to one or more implementations, alterations and/or modifications can be made to the illustrated examples without departing from the spirit and scope of the appended claims. In addition, while a particular feature of the invention may have been disclosed with respect to only one of several implementations, such feature may be combined with one or more other features of the other implementations as may be desired and advantageous for any given or particular function. Furthermore, to the extent that the terms “including”, “includes”, “having”, “has”, “with”, or variants thereof are used in either the detailed description and the claims, such terms are intended to be inclusive in a manner similar to the term “comprising.”
Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the invention being indicated by the following claims.
Patent Application
20100175392
