Abstract:
A heat of fusion thermoelectric generator. A heat source is in thermal contact with a phase change material, wherein the heat source is capable of providing sufficient heat so as to be able to melt the phase change material. The phase change material is in thermal contact with a hot side heat sink. At least one thermoelectric module is disposed between and in thermal contact with the hot side heat sink and a cold side heat sink. Electric power is generated by the thermoelectric module from a temperature difference between the hot side heat sink and the cold side heat sink.

Description:
This invention relates to thermoelectric generators and in particular to backup thermoelectric generators. This invention was made with Government support under grant DAAE 30-00-C-1018 awarded by the Department of the Army. The Government has certain rights in this invention. 
    
    
     BACKGROUND OF THE INVENTION 
     A very large number of portable electronic devices are becoming available to people throughout the world. Better integrated circuits have greatly reduced the electric energy required to operate these devices and rechargeable batteries are available to power these devices. However, sometimes such recharging is inconvenient or impossible. 
     Thermoelectric generators are well known. These devices utilize the physics principal known as the Seebeck effect discovered in 1821. If two conductors of different materials such as copper and iron are joined at their ends forming two junctions, and one junction is held at a higher temperature than the other junction, a voltage difference will arise between the two junctions. Most thermoelectric generating devices currently in use today utilize semiconductor materials, such as bismuth telluride, which are good conductors of electricity but poor conductors of heat. These semiconductors are typically heavily doped to create an excess of electrons (n-type) or a deficiency of electrons (p-type). An n-type semiconductor will develop a negative charge on the cold side and a p-type semiconductor will develop a positive charge on the cold side. Since each element of a semiconductor thermoelectric device will produce only a few millivolts it is generally useful to arrange the elements in series so as to produce higher voltages. Several techniques have been developed for arranging the semiconductor elements in series in thermoelectric devices. One such method is to use a so-called eggcrate design where a small eggcrate-shaped structure made of insulating material separates the thermoelectric elements and permits the elements to be connected in series in an automated fabrication process to reduce the cost of fabricating these modules and improve reliability. Modules of this design are described in U.S. Pat. No. 5,892,656. That patent is incorporated herein by reference. Such modules (HZ-2) are commercially available from Hi-Z Corporation with offices in San Diego, Calif. The dimensions of the module are 1.15 inches×1.15 inches×.20 inch, and the module comprises a 14×14 array of thermoelectric elements. With a 200° C. (360° F.) temperature difference, it will deliver an open circuit voltage of 6.6 volts and has a design operating range of 2.5 to 4.5 volts with an energy conversion efficiency of 5 %. 
     The heat required to be removed from a material to produce a phase change from a liquid to a solid is called the heat of fusion or latent heat. One of the best known examples is water that requires a removal of 334 joules/gram (144 BTU/lb.) to make the phase changed from water to ice. This is a reversible process that the same amount of heat must be added to go from the solid to the liquid state as must be removed to go from the liquid to the solid state. 
     Gomez, U.S. Pat. No. 4,251,291 discloses an electric generation system in which solar energy irradiates upon a latent heat storage device to enable the heat to be stored at a relatively constant temperature to serve as the source of heat for a thermoelectric generator. The Gomez device has limited solar applications. 
     Rechargeable Batteries 
     It is known in the prior art to connect a rechargeable chemical battery to an electric circuit that is powering an electronic device. If the normal source of electricity fails, the charged chemical battery can provide electricity to the electronic device, for as long as the chemical battery is able to maintain its charge. However, there are significant problems with using a rechargeable chemical battery as a backup power source. For example, rechargeable chemical batteries tend to be very temperature sensitive and will operate poorly at high or low ambient temperatures. Also, rechargeable chemical batteries have a limited shelf life. For example, if left on the shelf too long the chemicals inside the battery can migrate causing battery degradation. Also, rechargeable chemical batteries can only be recharged a relatively small number of times before the battery is unable to hold any further charges. 
     What is needed is a more reliable backup source of energy. 
     SUMMARY OF THE INVENTION 
     The present invention provides a heat of fusion thermoelectric generator. A phase change material in the generator provides a thermal energy source and the thermal energy is converted into electric energy with a thermoelectric module. The phase change material is melted using an external source of energy. The phase change material is in thermal contact with a hot side heat sink. At least one thermoelectric module is disposed between and in thermal contact with the hot side heat sink and a cold side heat sink. Electric power is generated by the thermoelectric module from a temperature difference between the hot side heat sink and the cold side heat sink. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIG. 1 shows a preferred embodiment of the present invention. 
     FIG. 2 shows a preferred thermoelectric module. 
     FIGS. 3A-3C show a preferred embodiment of the heat source capsule. 
     FIGS. 4A-4C show another preferred embodiment of the heat source capsule. 
     FIG. 5 shows another preferred embodiment of the present invention. 
    
    
     DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS 
     Determination of a Preferred Compound with the Ideal Phase Change Range Different compounds were tested while searching for a compound that underwent a phase change at a temperature of interest to a BiTe thermoelectric generator. For a BiTe thermoelectric system, this temperature range is between approximately 250° C. and 350° C. It was also preferable to find a compound that was stable and had a relatively high heat of fusion to minimize the mass of material required to provide the desired thermoelectric output for the desired time (approx. 300 mW for approx. 4 hours). 
     Table A presents the results of the search for the compound in the 250° C.-350° C. range. This table presents the compound, its melting point, the heat of fusion, molecular weight, and a calculation of the mass of material required to produce 300 mW of output from a bismuth telluride thermoelectric system for a period of four hours (i.e., 1.2 watt-hours). 
     
       
         
               
               
               
               
               
             
               
               
               
               
               
             
           
               
                 TABLE A 
               
               
                   
               
               
                   
                   
                   
                   
                 Mass Required 
               
               
                   
                   
                 Heat 
                 Molecular 
                 for 1.2 
               
               
                   
                 Melting Point 
                 of Fusion 
                 Weight 
                 Watt-hours 
               
               
                 Compound 
                 (° C.) 
                 (Kcal/mol) 
                 (g/mole) 
                 (g) 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                 As 4 O 6   
                 278 
                 8.0 
                 395.68 
                 1,224.7 
               
               
                 Bi 
                 271.3 
                 2.6 
                 209.98 
                 1,990.3 
               
               
                 Bi 2 S 3   
                 310 
                 8.9 
                 117.8 
                 327.7 
               
               
                 C 5 OH 
                 315 
                 1.09 
                 149.91 
                 3,405.6 
               
               
                 CaCl 2  · H 2 O 
                 260 
                 6.8 
                 129 
                 469.7 
               
               
                 Cd(NO 3 ) 2   
                 350 
                 7.8 
                 236.41 
                 750.5 
               
               
                 FeCl 3   
                 304 
                 10.3 
                 162.21 
                 390.0 
               
               
                 HgCl 2   
                 277 
                 4.64 
                 271.52 
                 1449.0 
               
               
                 HgI 2   
                 259 
                 4.53 
                 454.45 
                 2,484.1 
               
               
                 KOH 
                 360.4 
                 2.06 
                 56.11 
                 674.5 
               
               
                 NaClO 3   
                 248-261 
                 5.4 
                 106.44 
                 488 
               
               
                 NaNO 2   
                 271 
                 11.4 
                 69 
                 149.9 
               
               
                 NaNO 3   
                 308 
                 3.6 
                 85.01 
                 584.7 
               
               
                 NaOH 
                 318.4 
                 1.58 
                 40 
                 626.9 
               
               
                 RbOH 
                 300 
                 1.62 
                 102.49 
                 1,566.6 
               
               
                 RbNO 3   
                 310 
                 1.34 
                 147.47 
                 2,725.1 
               
               
                 Tl 2 CO 3   
                 272 
                 4.4 
                 468.57 
                 2,236.9 
               
               
                 TeF 
                 327 
                 9.0 
                 223.38 
                 614.6 
               
               
                 TlF 
                 322 
                 3.3 
                 223.39 
                 1,676.2 
               
               
                 WBr 5   
                 276 
                 4.10 
                 583.37 
                 3,523.3 
               
               
                 WCl 5   
                 248 
                 4.9 
                 361.12 
                 1,825.3 
               
               
                 WCl 6   
                 275 
                 1.6 
                 396.57 
                 6,137.4 
               
               
                 ZuCl 2   
                 283 
                 2.45 
                 136.29 
                 1,377.5 
               
               
                   
               
             
          
         
       
     
     The mass calculation shown in Table A assumes a thermoelectric conversion efficiency of approximately 5% and approximately a 20% extraneous heat loss via heat transport through the insulation. These values are consistent with the operation of a bismuth telluride module with a 200° C. differential temperature across the module and a generator with an inert gas multi-foil insulation system similar to that shown in FIG.  1  and described below. 
     Based on the criteria described above and the results depicted in Table A, it was determined that a preferred phase change material would be sodium nitrite (NaNO 2 ). 149.9 grams of sodium nitrite at its phase change temperature of 271° C. will provide approximately 4 hours of 300 milliwatts of power (assuming a 200° C. temperature differential across module  8 ). 
     First Preferred Embodiment 
     A first preferred embodiment of the present invention is shown in FIG.  1 . The internal components of heat of fusion thermoelectric generator  1  are preferably contained within aluminum pressure shell  2 . In the first preferred embodiment, the diameter of pressure shell  2  is approximately 2.5 inches and its length is approximately 6 inches. Filled with approximately 150 grams of sodium nitrite (NaNO 2 ), thermoelectric generator  1  should weight approximately 0.75 pounds. The dimensions and weight of thermoelectric generator  1  make it pocket portable. 
     Heat source capsule  4  is a cylindrical container approximately 1.5 inches long. Stored inside of heat source capsule  4  are 150 grams of sodium nitrite (NaNO 2 ). The properties of sodium nitrite are disclosed in Table A. Heating coil  6  is wrapped around heat capsule  4 . Thermocouple  9  is attached to heat source capsule  4  and functions to sense the temperature of the sodium nitrite. Heat source capsule  4  is held against thermoelectric module  8  by four tie wires  10 , each of which is tensioned by Belleville spring stack and nut assembly  12 . Utilization of Belleville springs  12  will help minimize temperature drops at the thermal interfaces and will also allow the generator to withstand high shock loads. 
     Insulation 
     A multifoil type of thermal insulation system is located between heat source capsule  4  and pressure shell  2 . Two cylinders of aluminized Kapton® foils  14  (Kapton® is a trademark of Dupont Corp. and is used to describe a well-known polyimide material) provide radial insulation as shown. Likewise, aluminized Kapton® disks  16  and  18  form the axial insulation. The aluminized foils minimize radiation heat transfer since the foil surfaces are highly reflective and have low emissivity. 
     After the components have been installed inside pressure shell  2 , the void space within pressure shell  2  is evacuated and then backfilled with one atmosphere Xenon or another inert gas such as argon. Xenon is preferred because it has the lowest known thermal conductivity of any known gas. The chamber is then sealed via pinch off tube  20 . Protective cap  22  covers pinch off tube  20 . 
     It will be obvious to those skilled in the art that other insulation systems such as semi-rigid MIN-K or fibrous mineral insulation such as FIBERFRAX can also be used. (MIN-K is a registered trademark of the Johns-Manville Corporation with offices in New York, New York and refers generally to thermal insulation used particularly in high temperature applications. FIBERFRAX is a registered trademark of the Carborundum Corporation with offices in Cleveland, Ohio and refers generally to thermal insulation utilizing loose masses of refractory fibers.) These systems would require a back fill with a gas such as argon or nitrogen. In this embodiment, the size of pressure shell  2  may be slightly larger to achieve similar thermal performance. 
     Another insulation system that incorporates a larger number of reflecting foils than that shown in the preferred embodiment and that is used with an evacuated system could also be used to achieve the desired degree of thermal insulation. Such a system may be more efficient than that shown in the preferred embodiment, but it would likely be more expensive to produce and more prone to failure. 
     Operation of the First Preferred Embodiment 
     To melt the phase change material located in heat source capsule  4 , electric current is supplied to heating coil  6 . As shown in FIG. 1, electrical current from electric source  38  travels through plug 24 then through conductor 26 to heating coil 6. Thermocouple  9  senses the temperature of the phase change material inside heat source capsule  4 . In accordance with the phase change material&#39;s heat of fusion, the temperature sensed by thermocouple  9  will level off when the phase change material reaches its melting point. For sodium nitrite, the melting point is approximately 271° C. 
     In a preferred embodiment, controller  28  is programmed to trip switch  39  so that electricity from electric source  38  is cut-off, thereby deactivating heating coil  6  when the sensed temperature is greater than the preset value (i.e., slightly above the melting point). Likewise, when the sensed temperature is slightly below the melting point, controller  28  will close switch  39  and electricity will once again flow to heating coil  6 . For example, for sodium nitrite with a melting point of 271° C., heating coil 6 will deactivate at 275° C. and reactivate at 267° C. 
     Electricity Generation 
     As the phase change material inside heat source capsule  4  is heated, approximately 80% of the heat from heat source capsule  4  will pass through thermoelectric module  8 . Heat flowing through thermoelectric module  8  causes electric power to be produced. FIG. 2 shows a detailed top view of a preferred thermoelectric module  8  with electric leads  30  and  31 . In a preferred embodiment, thermoelectric module  8  is approximately 0.75 inches square and 0.4 inches thick. It contains a 10×10 array of N and P type bismuth telluride elements that are approximately 0.05 inches square and 0.357 inches long. A preferred thermoelectric module  8  will utilize the gapless eggcrate construction described in U.S. Pat. No. 5,892,656. The 10×10 array shown in FIG. 2 is similar to the 10×10 array described in the patent. It will produce 300 milliwatts of power and 1.65 Volts at matched load when subject to a differential temperature of 200° C. It should be noted that in the first preferred embodiment the design of thermoelectric module  8  was selected to match the voltage requirements of a light emitting diode (LED) and that the voltage can be altered to fit other applications by changing the number of series connected thermoelectric elements in the module. 
     Electricity generated by thermoelectric module  8  flows through output power wire  42 , through plug  24  and to electrically power device  44 . If electricity from electric source  38  is cut-off, either by controller  28  tripping switch  39  or due to failure of electric source  38 , electric power will continue to be supplied to electrically powered device  44  so long as there is a temperature differential across thermoelectric module  8 . 
     For example, assume sodium nitrite (NaNO 2 ) is the phase change compound inside heat source capsule  4 . As shown in Table A, the melting point of sodium nitrite is 271° C. In a preferred embodiment, the temperature of the sodium nitrite in a fully charged state is slightly greater than its melting point (for example, approximately 276° C.). Fully charged, the sodium nitrite is all liquid. After electricity has been removed from heating coil  6 , the temperature of the sodium nitrite will decrease reasonably rapidly until the phase change temperature of the compound is reached. The temperature of the compound will then remain constant (i.e., approximately 271° C.) until the entire compound has given up its heat of fusion and changed phase to a solid. The temperature will again decrease rapidly as the solid cools and gives up its heat capacity. As shown in Table A, approximately 150 grams of sodium nitrite at its phase change temperature of 271° C. will provide approximately 4 hours of 300 milliwatts of power (assuming a 200° C. temperature differential across module  8 ). 
     Heat Source Capsule 
     Metallic Clad Sheathed Heater 
     A preferred embodiment of heat source capsule  4  is shown in FIGS. 3A-3C. In this embodiment heating coil  6  (shown in FIG. 1) is a metallic clad sheathed heater  6 A brazed in a helical groove machined to the outside of heat source capsule  4 . In the first preferred embodiment, the two heating elements are contained in the same sheath. Therefore, only a single helix groove is required. Both external electrical connection connections to the heater (wires  42  and  43 ) are made at one end of heating coil  6 . The two heating elements are connected together inside the sheath at the other end of heating coil  6 . 
     Preferably, metallic clad sheathed heater  6  A is fabricated by first fitting an electric insulator (for example, MgO) over the two heating elements. The assembly is then fed into a metal sheath, and the entire assembly is then swaged to the desired dimension. Done properly, this will result in electric isolation of the two heating elements from the metal sheath and from each other while maintaining good heat transfer characteristics between the heating elements and the sheath. 
     Heat source capsule  4  contains solid metal heat transfer piece  50  that is positioned along its centerline and is attachable at end  51  to the hot side of a thermoelectric module. Preferably, heat transfer piece  50  is aluminum and is circular in cross section. Helical fin  52  aids in heat transfer from the phase change material to the heat transfer piece and is orientated in a perpendicular fashion to heat transfer piece  50 . Thermocouple  9  is fitted alongside heat transfer piece  5 . Thermoelectric module locating ears  54  aid in properly positioning the thermoelectric module next to heat transfer piece  50 . 
     Another preferred embodiment of heat source capsule  4  is shown in FIGS. 4A-4C. In this preferred embodiment, metallic clad sheathed heater  60  is inserted inside heat transfer piece  62 . Power leads  63  and  64  exit metallic clad sheathed heater  60 . Preferably, thermocouple  9  is placed off-center heat transfer piece  62 . 
     Another preferred embodiment of the present invention is shown in FIG.  5 . This embodiment is similar to the embodiment shown in FIGS. 4A-4C with the exception that thermocouple  9  is attached directly to the outside of heat source capsule  4 . 
     Advantages of the Present Invention 
     The present invention has several advantages. It has virtually an infinite shelf life. It can be recharged a very large number of times compared to a chemical rechargeable battery. It is unaffected by normal storage conditions. It can be charged rapidly. For example, with an electric source providing 500 watts to heating coil  6  (FIG.  1 ), 150 grams of sodium nitrite inside heat source capsule  4  should take approximately four to five minutes to melt and be ready for full power operations. Also, there is only a slight loss in peak power under high normal ambient operating temperatures (T approximately equal to 120° F.) and there is a slight increase in peak power at low ambient operating temperatures (T approximately equal to −40° F.). 
     A Preferred Application for the First Preferred Embodiment 
     One of ordinary skill in the art will recognize many possible applications for the first preferred embodiment. A preferred application for heat of fusion thermoelectric generator  1  shown in FIG. 1 is as a backup power source to provide electricity to illuminate the gun sight mechanism of a military weapons system. In this application, it is very important that the backup power source be rapidly rechargeable, reliable, and not subject in a major way to extremes of ambient temperature. 
     While the above description has dealt with preferred embodiments of the present invention, the reader should understand that many modifications could be made and still be within the scope of the invention. For example, although FIGS. 3A-3C showed metallic clad sheathed heater  6  A with two heating elements in the same sheath, those of ordinary skill in the art will recognize that it is possible to use a heater where there is just one heating element in the sheath. If a heater of this fashion is utilized, then a double helix groove would be machined to the outside of heat source capsule  4  so that both lead wire connections end up at the same end of heat source capsule  4 . This embodiment would require a circular groove at the opposite end of the helix to connect the two helix grooves in order to return the heater down the second helical to the starting end. Also, it will be obvious to those of ordinary skill in the art that there are many other ways of heating and melting the phase change material. For example, it would be possible to heat and melt the phase change material by utilizing a heat pipe, which is a solid metallic conductor. By conducting the heat from the heat source to the phase change material, the use of the heat pipe will allow the phase change material to be heated by sources other than electric. For example, an open fire, exhaust heat from an internal combustion engine, or other heat sources that are of sufficient temperature to melt the phase change material could heat the phase change material. Therefore, the attached claims and their legal equivalents should determine the scope of the invention.