SUPER CONDUCTING HEAT TRANSFER MEDIUM

Abstract: A superconducting heat transfer medium (6) that has three basic layers (20, 22, and 24), the first layer (20) being various combinations of metals and dichromate radical; the second layer (22) formed over the first layer (20) and being various combinations of metals such as cobalt, manganese, beryllium, strontium and the dichromate radical; and the third layer (24) formed over the second layer (22) and being various combinations of metal oxides, dichromates, monocrystalline silicon, strontium chromate, and beta -titanium. The three layers (20, 22 and 24) can be applied to a conduit (4) and then heat polarized to form a superconducting heat transfer device (2) that transfers heat without any net heat loss, or can be applied to a pair of plates having a small cavity relative to a large surface area to form a heat sink (18) that can immediately disperse heat from a heat source.

Description: SUPERCONDUCTING HEAT TRANSFER MEDIUM TECHNICAL FIELD The present invention relates generally to the field of heat transfer. More particularly, the present invention relates to a superconducting heat transfer medium which is disposed vvithin a conduit to rapidly and efficiently transfer heat. BACKGROUND ART Efficiently transporting heat from one location to another always has been a problem. Some applications, such as keeping a semiconductor chip cool, require rapid transfer and removal of heat, while other applications, such as dispersing heat from a furnace, require rapid transfer and retention of heat. Whether removing or retaining heat, the heat transfer conductivity of the material utilized limits the efficiency of the heat transfer. Further, when heat retention is desired, heat losses to the environment further reduce the efficiency of the heat transfer. For example, it is well known to utilize a heat pipe for heat transfer. The heat pipe operates on the principle of transferring heat through mass transfer of a fluid carrier contained therein and phase change of the carrier from the liquid state to the vapor state within a closed circuit pipe. Heat is absorbed at one end of the pipe by vaporization of the carrier and released at the other end by condensation of the carrier vapor. Although the heat pipe improves thermal transfer efficiency as compared to solid metal rods, the heat pipe requires the circulatory flow of the liquid/vapor carrier and is limited by the association temperatures of vaporization and condensation of the carrier. As a result, the heat pipe's axial heat conductive speed is further limited by the amount of latent heat of liquid vaporization and on the speed of circular transformation between liquid and vapor states. Further, the heat pipe is convectional in nature and suffers from thermal losses, thereby reducing the thermal efficiency. An improvement over the heat pipe, which is particularly useful with nuclear reactors, is described by Kurzweg in U.S. Patent Number 4,590,993 for a Heat Transfer Device For The Transport Of Large Conduction Flux Without Net Mass Transfer. This device has a pair of fluid reservoirs for positioning at respective locations of differing temperatures between which it is desired to transfer heat. A plurality of ducts having walls of a material which conducts heat connect the fluid reservoirs. Heat transfer fluid, preferably a liquid metal such as mercury, liquid hthium or liquid sodium, fills the reservoirs and ducts. Oscillatory axial movement of the liquid metal is created by a piston or a diaphragm within one of the reservoirs so that the extent of fluid movement is less than the duct length. This movement functions to alternately displace fluid within the one reservoir such that the liquid metal is caused to move axially in one direction through the ducts, and then to in effect draw heat transfer fluid back into the one reservoir such that heat transfer fluid moves in the opposite direction within the ducts. Thus, within the ducts, fluid oscillates in alternate axial directions at a predetermined frequency and with a predetermined tidal displacement or ampUtude. With this arrangement, large quantities of heat are transported axially along the ducts from the hotter reservoir and transferred into the walls of the ducts, provided the fluid is oscillated at sufficiently high frequency and with a sufficiently large tidal displacement. As the fluid oscillates in the return cycle to the hotter reservoir, cooler fluid from the opposite reservoir is pulled into the ducts and the heat then is transferred from the walls into the cooler fluid. Upon the subsequent oscillations, heat is transferred to the opposite reservoir from the hotter reservoir. However, as with the heat pipe, this device is limited in efficiency by the heat transfer conductivity of the materials comprising the reservoirs and ducts and by heat losses to the atmosphere. It is known to utilize radiators and heat sinks to remove excess heat generated in mechanical or electrical operations. Typically, a heat transferring fluid being circulated through a heat generating source absorbs some of the heat produced by the source. The fluid then is passed through tubes having heat exchange fins to absorb and radiate some of the heat carried by the fluid. Once cooled, the fluid is returned back to the heat generating source. Commonly, a fan is positioned to blow air over the fins so that energy from the heat sink radiates into the large volume of air passing over the fins. With this type of device, the efficiency of the heat transfer is again limited by the heat transfer conductivity of the materials comprising the radiator or the heat sink. Dickinson in U.S. Patent Number 5,542,471 describes a Heat Transfer Element Having Thermally Conductive Fibers that eliminates the need for heat transferring fluids. This device has longitudinally thermally conductive fibers extended between two substances that heat is to be transferred between in order to rmximize heat transfer. The fibers are comprised of graphite fibers in an epoxy resin matrix, graphite fibers cured from an organic matrix composite having graphite fibers in an organic resin matrix, graphite fibers in an aluminum matrix, graphite fibers in a copper matrix, or a ceramic matrix composite. In my People's Republic of China Patent Number 89108521.1, I disclosed an Inorganic Medium Thermal Conductive Device. This heat conducting device greatly improved the heat conductive abilities of materials over their conventional state. Experimentation has shown this device capable of transferring heat along a sealed metal shell having a partial vacuum therein at a rate of 5,000 meters per second. On the internal wall of the shell is a coating applied in three steps having a total optimum thickness of 0.012 to 0.013 millimeters. Of the total weight of the coating, strontium comprises 1.25%, beryllium comprises 1.38%, and sodium comprises 1.95%. This heat conducting device does not contain a heat generating powder and does not transfer heat nor prevent heat losses to the atmosphere in a superconductive manner as the present invention. BRIEF SUMMARY OF THE INVENTION It is generally accepted that when two substances having different temperatures are brought together, the temperature of the warmer substance decreases and the temperature of the cooler substance increases. As the heat travels along a heat conducting conduit from a warm end to a cool end, available heat is lost due to the heat conducting capacity of the conduit material, the process of warming the cooler portions of the conduit and thermal losses to the atmosphere. In accordance with the present invention and these contemplated problems which continue to exist in this field, one objective of this invention is to provide a superconducting heat transfer medium that is environmentally sound, rapidly conducts heat and preserves heat, in a highly efficient manner. Further, the present invention does not require a tightly controled process environment to produce. Another object of this invention is to provide a device that conducts heat with a heat preservation efficiency approaching 100 percent. Also, another object of this invention is to provide a method for denaturation of rhodium and radium carbonate. Yet another objective of this invention is to provide a process for making a device that transfers heat from a heat source from one point to another without any effective heat loss. Still yet, another object of this invention is to provide a heat sink utilizing the superconducting heat transfer medium that rapidly and efficiently disperses heat from a heat generating object. This invention accomplishes the above and other objectives and overcomes the disadvantages of the prior art by providing a superconducting heat transfer medium that is relatively inexpensive to prepare, simple in design and application, and easy to use. The medium is applied to the conduit in three basic layers. The first two layers are prepared from solutions which are exposed to the inner wall of the conduit. Initially, the first layer, which primarily comprises in ionic form various combinations of sodium, beryUium, a metal such as manganese or aluminum, calcium, boron, and dichromate radical, is absorbed into the inner waU of the conduit to a depth of 0.008 mm to 0.012 mm Subsequently, the second layer, which primarily comprises in ionic form various combinations of cobalt, manganese, beryUium, strontium, rhodium, copper, β-titanium, potassium, boron, calcium, a metal such as aluminum and the dichromate radical, bu ds on top of the first layer and actuaUy forms a film having a thickness of 0.008 mm to 0.012 mm over the inner waU of the conduit. FinaUy, the third layer is a powder comprising various combinations of rhodium oxide, potassium dichromate, radium oxide, sodium dichromate, suver dichromate, monocrystaUine sUicon, beryUium oxide, strontium chromate, boron oxide, β-titanium and a metal dichromate, such as manganese dichromate or aluminum dichromate, that evenly distributes itself across the inner waU. The three layers can be apphed to a conduit and then heat polarized to form a superconducting heat transfer device that transfers heat without any net heat loss, or can be apphed to a pair of plates having a smaU cavity relative to a large surface area to form a heat sink that can immediately disperse heat from a heat source. It is to be understood that the phraseology and terminology employed herein are for the purpose of description and should not be regarded as limiting. As such, those skiUed in the art wiU appreciate that the conception, upon which this disclosure is based, may readUy be utilized as a basis for the designing of other structures, methods, and systems for carrying out the several purposes of the present invention. It is important, therefore, that the claims be regarded as including such equivalent constructions insofar as they do not depart from the spirit and scope of the present invention. Other objects, advantages and capabilities of the invention wiU become apparent from the foUowing description taken in conjunction with the accompanying drawings showing the preferred embodiment of the invention. BRIEF DESCRIPTION OF THE DRAWINGS The invention wiU be better understood and the above objects as weU as objects other than those set forth above wiU become apparent when consideration is given to the foUowing detaUed description thereof. Such description makes reference to the annexed drawings wherein: Figure 1 is a pers ective view of a superconducting heat transfer device made in accordance with the present invention; Figure 2 is a cross- sectional view of the device of Figure 1; Figure 3 is a perspective view of a plug used with the device of Figure 1; Figure 4 is a perspective view of a heat sink made in accordance with the present invention; Figure 5 is a side elevation view of the heat sink of Figure 4; Figure 6 is a cross- sectional view of the heat sink of Figure 4; Figure 7 is an example testing apparatus for testing the superconducting heat transfer device; Figure 8 is the data from the results of Test No. 1 on a preferred embodiment of the present invention; Figure 9 is the data from the results of Test No. 2 on a preferred embodiment of the present invention; Figure 10 is the data from the results of Test No. 3 on a preferred embodiment of the present invention; and Figure 11 is the data from the results of Test No. 4 on a preferred embodiment of the present invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS For a fuUer understanding of the nature and desired objects of this invention, reference should be made to the foUowing detaUed description taken in connection with the accompanying drawings. Referring to the drawings, wherein like reference numerals designate corresponding parts throughout the several figures, reference is made first to Figures 1 and 2. A superconducting heat transfer device 2 comprising a carrier such as conduit 4 containing a superconducting heat transfer medium 6 is provided which can be placed within a cavity 8 of the conduit 4 without regard to the material comprising the conduit 4. WhUe the conduit 4 shown in Figure 1 is cylindrical in shape, the present invention envisions conduits in a variety of shapes and sizes. The resulting heat transfer capabUities of the medium 6 bearing conduit 4 are greatly enhanced without any subsequent thermal loss. If properly apphed within conduit 4, medium 6 actuaUy is catalyzed by heat to become a heat generator itself. Medium 6 is activated at a temperature of about 38 °C and can operate to a maximum temperature of about 1730 °C. Although not completely certain, it is beUeved that the thermal generating capabiUty of medium 6 is directly related to mass loss of medium 6 after activation. Because medium 6 is capable of immediately transferring heat through conduit 4 from a heat source (not shown), conduit 4 can be exposed to and operate within an environment having a source temperature far in excess of the melting temperature of the untreated material comprising conduit 4. It is additionaUy beUeved that during the initial stages of medium 6 activation, medium 6 reacts endothermicaUy. As a result, medium 6 can immediately absorb avaUable heat from the heat source and thereafter immediately transfer the heat throughout conduit 4. If the cubic volume of cavity 8 is smaU in relation to external surface 10 area of conduit 4, as shown in Figures 4 through 6, medium 6 absorbs heat to provide a heat sink 12 which immediately removes heat from the heat generating source. Heat radiation is directly related to heat capacity, the rate of heat conduction, and thermal conductivity. This, in other words, deteπnines the speed (rate) at which the volume (quantity) of heat can be transferred in each unit volume. If conduit 4 or carrier has a smaU cavity in relation to a large external surface 10 area, the carrier is more capable of distributing heat across the external surface 10. In appUcations where the temperature of the heat generating source does not exceed 38 °C, the medium 6 activation temperature, the heat is immediately absorbed and dispersed by medium 6. In cases where the heat generating source exceeds 38 °C, heat sink 12 is stiU highly effective because of the abiUty of medium 6 to rapidly transfer the heat to heat sink external surface 14 and be efficiently dispersed to the atmosphere by thermal radiation. Medium 6 is appUed in three basic layers, the first two of which are prepared from solutions. Each solution is exposed sequentaUy to an inner conduit surface 16 or an inner heat sink surface 18. InitiaUy, first layer 20 is absorbed into inner conduit surface 16 or heat sink surface 18. Subsequently, second layer 22 buUds on top of first layer 20 and actuaUy forms a film over inner conduit surface 16 or heat sink surface 18. FinaUy, third layer 24 is a powder that evenly distributes itself across inner conduit surface 16 or heat sink surface 18. Although reference is made to conduit 4 below in the discussion of medium 6, the appUcation of medium 6 within heat sink 12 is the same. First layer 20 is an anti-corrosion layer which prevents etching of inner conduit surface 16 and, in theory, causes a reaUgnment of the atomic structure of conduit 4 material so that heat is more readUy absorbed. A further function of first layer 20 is to prevent inner conduit surface 16 from producing oxides. For example, ferrous metals can be easUy oxidized when exposed to water molecules contained in the air. The oxidation of inner conduit surface 16 wUl cause corrosion and also create a heat resistance. As a result, there is an increased heat load wlule heat energy is transferred within conduit 4, thus causing an accumulation of heat energy inside conduit 4. Should this occur, the life span of medium 6 is decreased. Next, second layer 22, the active layer, prevents the production of elemental hydrogen and oxygen, thus restraining oxidation between oxygen atoms and the material of conduit 4 (or carrier). Also in theory, second layer 22 conducts heat across inner conduit surface 16 comparably to that of electricity being conducted along a wire. Experimentation has found that heat can be conducted by medium 6 at a rate of 15,000 meters per second, regardless of the heat conductivity coefficient of the material of the conduit. Second layer 22 also assists in accelerating molecular osculation and friction associated with third layer 24 to provide a heat transfer pathway for heat conduction. Third layer 24 is referred to, due to its color and appearance, as the "black powder" layer. It is beUeved third layer 24 generates heat once medium 6 is exposed to the minimum activation temperature of 38 °C. Upon activation of medium 6, the atoms of third layer 24, in concert with first layer 20 and second layer 22, begin to osciUate. As the heat source temperature increases, it is beUeved that frequency of osculation increases. It is beUeved that when the activating temperature reaches 200 °C, the frequency of osculation is 230 miUion times per second, and when the activating temperature is higher than 350 °C, the frequency can even reach 280 miUion times per second. TheoreticaUy, the higher the activating temperature, the higher the frequency of osculation. Therefore it is suspected that the higher the load, the higher the performance efficiency of the conduit. During the heat transfer process, there is neither phase transition nor mass transfer of medium 6. Experimentation has shown that a steel conduit 4 with medium 6 properly disposed therein has a thermal conductivity that is generaUy 20,000 times higher than the thermal conductivity of sUver, and can reach under laboratory conditions a thermal conductivity that is 30,000 times higher that the thermal conductivity of sUver. During use, after activation, medium 6 loses mass with use (decay caused by the conversion of mass into energy). As a result, medium 6 has a long, but limited useful life. Tests have shown that after 110,000 hours of continuous use, both the amount of medium 6 and the molecule vibration frequency remain the same as from the initial activation. However, at 120,000 hours of continuous use, the amount (mass) of medium 6 starts to decline at a rate of about 0.5% every 32 hours with the molecule vibration frequency significantly decreased by about 6%. After about 123,200 hours of continuous use, medium 6 became ineffective. It is beUeved that the aging is caused mainly by the decay, or conversion of mass into energy, of third layer 24. As is expected, lower working temperatures slow the decay of third layer 24. First layer 20 and second layer 22 have been determined to be used up at a rate of approximately 0.001 mm per 10,000 hours of use. To prepare first layer 20, a first layer solution is manufactured and thereafter appUed to inner conduit surface 16. A representative first layer solution is manufactured by the foUowing steps, preferably conducted in the order of Usting: (a) placing 100 ml of distilled water into an inert container such as glass or, preferably, ceramic; (b) dissolving and mixing between 2.0 and 5.0 grams of sodium peroxide into the water; (c) dissolving and mixing between 0.0 and 0.5 grams of sodium oxide into the solution of step (b); (d) dissolving and mixing between 0.0 and 0.5 grams of beryllium oxide into the solution of step (c); (e) dissolving and mixing between 0.3 and 2.0 grams of a metal dichromate such as aluminum dichromate or, preferably, magnesium dichromate into the solution of step (d); (f) dissolving and mixing between 0.0 and 3.5 grams of calcium dichromate into the solution of step (e); and (g) dissolving and mixing between 1.0 and 3.0 grams of boron oxide into the solution of step (f) to form the first layer solution. It is preferred for steps (a) through (g) to be conducted in the order Usted and under conditions having a temperature between 0 °C and 30 °C, preferably 5 °C to 8 °C, and a relative humidity of no greater that 40%. The steps for the addition of beryUium oxide and the metal dichromate can be reversed in order so that the metal dichromate is added to the first layer solution prior to the addition of beryUium oxide without causing negative effects. When medium 6 contains manganese sesquioxide, rhodium oxide or radium oxide, either sodium peroxide or sodium oxide may be eliminated, but the resulting heat transfer efficiency of medium 6 wUl be lower and the life span of medium 6 will be reduced by approximately 1 year. As to the reiriaining components of the first layer solution and subject to the above exceptions, each component should be added in the order presented. If the components of the first layer solution are combined in an order not consistent with the Usted sequence, the solution can become unstable and may result in a catastrophic reaction. Prior to manufacturing a solution for second layer 22 and compiling the compounds for third layer 24, rhodium and radium carbonate undergo a denaturation process. To denature 100 grams of rhodium powder, blend 2 grams of pure lead powder with the rhodium powder within a container and subsequently place the container with the rhodium and lead powders into an oven at a temperature of 850 °C to 900 °C for at least 4 hours to form rhodium oxide. Then separate the rhodium oxide from the lead. To denature 100 grams of radium carbonate powder, blend 11 grams of pure lead powder with the radium carbonate within a container and subsequently place the container with the radium carbonate and lead powders into an oven at a temperature of 750 °C to 800 °C for at least eight hours to form radium oxide. During experimentation, a platinum container was utilized in the denaturation process. The material comprising the container should be inert with respect to rhodium, rhodium oxide, radium carbonate, radium oxide, and lead. Lead utilized in the denaturation process preferably should be 99.9% pure and can be recycled for subsequent use in further like denaturation processes. Subsequent testing of medium 6 at a resting state and an active state with a PDM personal dosimeter resulted in no radioactive emissions of any kind detectable over background radiation. An isotope of titanium is utilized in medium 6. In some countries the isotope is known as B-type titanium, and in the United States of America, the isotope is known as β- titanium. Second layer 22 is derived from a solution that is appUed to inner conduit surface 16 over first layer 20. Siπήlar to the first layer solution, a representative second layer solution is manufactured by the foUowing steps, conducted preferably in the order of Usting: (a) placing 100 ml of twice-distUled water into an inert container such as glass or, preferably, ceramic; (b) dissolving and mixing between 0.2 and 0.5 grams of cobaltous oxide into the twice- distiUed water; (c) dissolving and mixing between 0.0 and 0.5 grams of manganese sesquioxide into the solution of step (b); (d) dissolving and mixing between 0.0 and 0.01 grams of beryUium oxide into the solution of step (c); (e) dissolving and mixing between 0.0 and 0.5 grams of strontium chromate into the solution of step (d); (f) dissolving and mixing between 0.0 and 0.5 grams of strontium carbonate into the solution of step (e); (g) dissolving and mixing between 0.0 and 0.2 grams of rhodium oxide into the solution of step (f); (h) dissolving and mixing between 0.0 and 0.8 grams of cupric oxide into the solution of step (g); (i) dissolving and mixing between 0.0 and 0.6 grams of β-titanium into the solution of step (h); (j) dissolving and mixing between 1.0 and 1.2 grams of potassium dichromate into the solution of step (i); (k) dissolving and mixing between 0.0 and 1.0 grams of boron oxide into the solution of step (j); (1) dissolving and mixing between 0.0 and 1.0 grams of calcium dichromate into the solution of step (k); and (m) dissolving and mixing between 0.0 and 2.0 grams of aluminum dichromate or, preferably, magnesium dichromate, into the solution of step (1) to form the second layer solution. It is preferred for the twice-distiUed water to have an electrical conductivity that approaches 0. The higher the electrical conductivity, the greater the problem of static electricity interfering with medium 6 and causing a reduction in the thermal conductive efficiency. The steps of (a) through (m) preferably are conducted under conditions having a temperature between 0 °C and 30 °C and a relative humidity of no greater than 40%. When medium 6 contains rhodium oxide or radium oxide, the amount of manganese sesquioxide may be reduced or eliminated; however, the life span of medium 6 wiU be reduced and the thermal conductive efficiency wiU be reduced by approximately 0.2%. GeneraUy, β-titanium may be added to the second layer solution at any step Usted above, except that it should not be added to the twice-distiUed water at step (b) or as the last component of the solution. Adding β-titanium at step (b) or as the last component of the solution can cause instabiUty of the second layer solution. The steps for adding manganese sesquioxide and beryUium oxide may be reversed in order so that beryUium oxide is added to the second layer solution prior to the addition of manganese sesquioxide. Likewise, the steps for adding potassium dichromate and calcium dichromate may be reversed in order so that calcium dichromate is added to the second layer solution prior to the addition of potassium dichromate. If the components of the second layer solution are combined in an order not consistent with the Usted sequence and the exceptions noted above, the solution can become unstable and may result in a catastrophic reaction. Prior to preparing third layer 24, silicon is treated by magnetic penetration. MonocrystaUine sUicon powder having a preferred purity of 99.999% is placed within a non-magnetic container and disposed within a magnetic resonator for at least 37 minutes, preferably 40 minutes to 45 minutes. The magnetic resonator utilized during experimentation was a 0.5 kilowatt, 220 volt and 50 hertz magnetic resonator. If the siUcon being used has a purity lower than 99.999%, the amount of siUcon needed in third layer 24 increases. The magnetic resonator is used to increase the atomic electron layer of the siUcon, which in turn, increases the speed that heat is conducted by medium 6. A representative powder of third layer 24 is manufactured by the foUowing steps, conducted preferably in the order of Usting: (a) placing between 0.0 and 1.75 grams of denatured rhodium oxide into an inert container such as glass or, preferably, ceramic; (b) blending between 0.3 and 2.6 grams of sodium dichromate with the rhodium oxide; (c) blending between 0.0 and 0.8 grams of potassium dichromate with the mixture of step (b); (d) blending between 0.0 and 3.1 grams of denatured radium oxide with the mixture of step (c); (e) blending between 0.1 and 0.4 grams of sUver dichromate with the mixture of step (d); (f) blending between 0.2 and 0.9 grams of the monocrystaUine siUcon powder treated by magnetic penetration with the mixture of step (e); (g) blending between 0.0 and 0.01 grams of beryUium oxide with the mixture of step (f); (h) blending between 0.0 and 0.1 grams of strontium chromate with the mixture of step (g); (i) blending between 0.0 and 0.1 grams of boron oxide with the mixture of step (h); (j) blending between 0.0 and 0.1 grams of sodium peroxide with the mixture of step (i); (k) blending between 0.0 and 1.25 grams of β-titanium with the mixture of step (j); and (1) blending between 0.0 and 0.2 grams of aluminum dichromate or, preferably, magnesium dichromate, into the mixture of step (k) to form the third layer powder. The powder for third layer 24 preferably should be blended at a temperature lower than about 25 °C. By blending at lower temperatures, the heat conducting efficiency of medium 6 improves. Further, the relative humidity should be below 40%. It is preferred for the relative humidity to be between 30% and 35%. GeneraUy, radium oxide and β- titanium may be added to the powder of third layer 24 at any step Usted above, except that neither one should be added to the powder as the first or last component. Adding either radium oxide or β-titanium as the first or last component of the powder can cause instab ity of medium 6 and may result in a catastrophic reaction. The steps for adding potassium dichromate and sUver dichromate may be reversed in order so that sUver dichromate is added to the powder of third layer 24 prior to the addition of potassium dichromate. Likewise, the steps for adding strontium chromate and beryllium oxide may be reversed in order so that beryUium oxide is added to the powder of third layer 24 prior to the addition of strontium chromate. If the components of the powder of third layer 24 are combined in an order not consistent with the Usted sequence and the exceptions noted above, medium 6 can become unstable and may result in a catastrophic reaction. The powder of third layer 24 may be stored for prolonged periods of time. To prevent degradation by Ught and humidity, the powder of third layer 24 should be stored in a dark, hermetic storage container made from an inert material, preferably glass. A moisture absorbing material also may be placed within the storage container so long as the moisture absorbing material is inert to and is not intermingled with the powder of third layer 24. Once the solutions for first layer 20 and second layer 22 and the powder of third layer 24 are prepared, the superconducting heat transfer device 2 can be fabricated. Conduit 4 can be any one of a variety of metaUic or non-metaUic materials; and in any event, should have very Uttle oxidation, preferably no oxidation, on inner conduit surface 16. It is recommended for conduit 4, particularly if conduit 4 is manufactured of a metal, to be clean, dry and free of any oxides or oxates. This can be accompUshed by convectional treating by, for example, sand blasting, weak acid washing, or weak base washing. Any materials used to clean and treat conduit 4 should be completely removed and inner conduit surface 16 also should be dry prior to adding medium 6 to conduit 4. AdditionaUy, the waU thickness of conduit 4 should be selected to take a wear rate of at least 0.1 mm per year into account. This wearing is caused by the osculation of third layer's 24 molecules. For steel, the waU thickness should be at least 3 mm. Obviously, softer materials need to be thicker. The conduit 4 may be of considerable length. In fact, it has been found that the performance efficiency of the conduit 4 increases with length. A representative superconducting heat transfer device 2 is manufactured utilizing the foUowing steps: (a) placing the first layer solution into a first layer solution container; (b) submerging conduit 4 having cavity 8 within the first layer solution such that the first layer solution fills cavity 8, conduit 4 preferably having a non-horizontal placement with lower end 26 disposed in a downward direction within the first layer solution, at a temperature between 0 °C and 30 °C for at least 8 hours so that the first layer solution can penetrate the waU of conduit 4 to a depth of between 0.008 mm and 0.012 mm; (c) drying conduit 4 naturaUy at ambient conditions to form first layer 20 within cavity 8; (d) placing the second layer solution into a second layer solution container; (e) submerging conduit 4 with first layer 20 within the second layer solution such that the second layer solution fitts cavity 8, conduit 4 preferably having a non- horizontal placement with lower end 26 disposed in a downward direction within the second layer solution at a temperature between 55 °C and 65 °C, preferably 60 °C, for at least 4 hours; (f) drying conduit 4 naturaUy at ambient conditions to form within cavity 8 a film of second layer 22 having a thickness between 0.008 mm and 0.012 mm; (g) welding an end cap 28 on the opposite end of conduit 8 from lower end 26 by a precision welding technique, preferably heU-arc welding done in the presence of heUum or argon; (h) welding an injection cap 30 having a bore 32 with a diameter between 2.4 mm and 3.5 mm, preferably 3.0 mm ; on lower end 26 preferably by the method utilized in step (g); (i) heating lower end 26 to a temperature not to exceed 120 °C, preferably to about 40 °C; (j) injecting the powder of third layer 24 through bore 32 in an amount of at least 1 cubic meter per 400,000 cubic meters of cavity 8 volume; (k) inserting plug 34, preferably conical- shaped and sohd, as shown in Figure 3, into bore 32; (1) heating lower end 26 to a temperature between 80 °C and 125 °C; (m) removing plug 34 from bore 32 for no more than about 3 seconds, preferably about 2 seconds, and reinserting plug 34 into bore 32; and (n) sealing plug 34 within bore 32, preferably by the welding method utilized in step (g), to form the superconducting heat transfer device 2. If the temperature of lower end 26 in step (i) exceeds 60 °C, lower end 26 should be aUowed to cool to at least 60 °C prior to injecting the powder of third layer 24 into cavity 8. By foUowing the steps above, lower end 26 becomes heat polarized. In other words, lower end 26 is polarized to receive heat from the heat source and transfer the heat away from lower end 26. The purpose of removing plug 34 from bore 32 in step (m) above is to release air and water molecules from cavity 8 of conduit 4 to the outside environment. A blue gas has been observed exiting bore 32 once plug 34 is removed. However, if a blue Ught is observed emitting from bore 32 prior to plug 34 being reinserted into bore 32, the powder of third layer 24 has escaped to the atmosphere and steps (j) through (m) need to be repeated. If step (j) can be accompUshed in a humidity free environment under a partial vacuum, steps (1) and (m) can be eliminated, but it is not recommended. Manganese sesquioxide, rhodium oxide, and radium oxide are not needed in aU appUcations of medium 6. These three components are used in medium 6 when the superconducting heat transfer device 2 is exposed to an environment of high pressure steam and conduit 4 is manufactured of high carbon steel. In this special case, high pressure is defined as being 0.92 miUion pascals or higher. Manganese sesquioxide, rhodium oxide, and radium oxide are not needed and may be eliminated from medium 6 when the use of the superconducting heat transfer device 2 is not in a high pressure steam environment, even if conduit 4 is made of high carbon steel. AdditionaUy, when manganese sesquioxide, rhodium oxide, and radium oxide are eliminated from medium 6, the powder of third layer 24 should be provided in an amount of 1 cubic meter of third layer powder per 200,000 cubic meters of cavity 8 volume. As disclosed above, heat sink 12 utilizes superconducting heat transfer medium 6. A representative heat sink 12 is manufactured utilizing the foUowing steps: (a) placing the first layer solution into a first layer solution container; (b) submerging first plate 36 and second plate 38 within the first layer solution such that the first layer solution covers at least one side of each of first plate 36 and second plate 38 at a temperature between 0 °C and 30 °C for at least 8 hours so that the first layer solution can penetrate the first layer solution covered side 40 to a depth between 0.008 mm and 0.012 nnn ; first plate 36 and second plate 38 having mating edges 42 and form a relatively smaU volume cavity 8 with respect to the surface area of first plate 36 and second plate 38 when first plate 36 and second plate 38 are placed together, and at least one of first plate 36 and second plate 38 has an opening 44 between 2.4 mm and 3.5 mrrv preferably 3.0 mm; (c) drying first plate 36 and second plate 38 naturaUy at ambient conditions to form first layer 20 on the first layer covered sides 40 of first plate 36 and second plate 38; (d) placing the second layer solution into a second layer solution container; (e) submerging first plate 36 and second plate 38 within the second layer solution such that the second layer solution contacts first layer 20 at a temperature between 55 °C and 65 °C, preferably 60 °C, for at least 4 hours; (f) drying first plate 36 and second plate 38 naturaUy at ambient conditions to form the film of second layer 22 having a thickness between 0.008 mm and 0.012 mm on first layer 20; (g) welding first plate 36 and second plate 38 together along mating edges 42 by a precision welding technique, preferably heU-arc welding done in the presence of hehum or argon, so that the first layer covered sides 40 face one another; (h) injecting the powder of third layer 24 into cavity 8 through opening 44 in an amount of at least 1 cubic meter per 400,000 cubic meters of cavity volume; and (i) sealing opening 44 preferably by the method utilized in step (g) to form heat sink 12. Heat sink 12 can be manufactured in the same manner as superconducting heat transfer device 2; that is, heat sink 12 may be heat polarized, but it is not necessary. Also, the steps calling for welding in the manufacture of superconducting heat transfer device 2 and heat sink 12 can be accompUshed by using glues, adhesives and/or epoxies, preferably heat tolerant glues, adhesives and epoxies. AdditionaUy, aU welding should be conducted to a depth of two-thirds of the thickness of conduit 4, end cap 28, injection cap 30, first plate 36 or second plate 38. After welding, a leakage test, such as the HeUum Vacuum Leakage Test, should be performed. AU materials comprising conduit 4, end cap 28, injection cap 30 and plug 34 of superconducting heat transfer device 2 or first plate 36 and second plate 38 of heat sink 12 should be compatible with one another. This prevents problems, particularly material fractures, associated with the different expansion/contraction rates of different materials used in combination and corrosion associated with anodic reactions. The material selected also should be compatible with and able to withstand the external environment in which superconducting heat transfer device 2 or heat sink 12 operates. For example, if superconducting heat transfer device 2 is operating in an acidic environment, the material should be resistant to the acid present. The invention wiU be better understood by reference to the foUowing Ulustrated examples. With respect to the above description then, it is to be realized that the optimum dimensional relationships for the parts of the invention, to include variations in size, materials, shape, form, function and manner of operation, assembly and use, are deemed readily apparent and obvious to on skiUed in the art, and aU equivalent relationships to those described in the specification are intended to be encompassed by the present invention. The super conducting heat transfer medium 6 can also conduct cold temperature transfer when a cold source is exposed to either end of the conduit 4. Cold temperatures have been successfuUy transferred across the conduit 4 when one end thereof came in contact with Uquid nitrogen having a temperature of -195 degrees C. The foUowing examples describe various compositions of first layer 20, second layer 22 and third layer 24 and are known to be useful in preparing superconducting heat transfer device 2 or heat sink 12. The components preferably are added to the respective layers 20, 22, 24 in the amounts Usted, in the order of Usting and in accordance with the respective steps described above. Example 1 For forming first layer 20, into 100 ml of distiUed water add 5.0 grams of sodium peroxide, 0.5 gram of sodium oxide, 2.0 grams of magnesium dichromate or aluminum dichromate, 2.5 grams of calcium dichromate and 3.0 grams of boron oxide. For forming second layer 22, into 100 ml of twice-distiUed water add 0.5 gram of cobaltous oxide, 0.5 gram of manganese sesquioxide, 0.5 gram of strontium carbonate, 0.2 gram of rhodium oxide, 0.8 gram of cupric oxide, 0.6 gram of β-titanium and 1.2 grams of potassium dichromate. For forming the powder of third layer 24, combine 1.75 grams of rhodium oxide, 1.25 grams of β-titanium, 3.1 grams of radium oxide, 2.6 grams of sodium dichromate, 0.4 gram of s ver dichromate and 0.9 gram of monocrystaUine siUcon powder. Example 2 For forming first layer 20, into 100 ml of distiUed water add 5.0 grams of sodium peroxide, 0.5 gram of beryUium oxide, 2.0 grams of magnesium dichromate, 2.0 grams of calcium dichromate and 3.0 grams of boron oxide. For forming second layer 22, into 100 ml of twice-distiUed water add 0.5 gram of cobaltous oxide, 0.5 gram of strontium chromate, 0.8 gram of cupric oxide, 0.6 gram of β- titanium and 1.2 grams of potassium dichromate. For forming the powder of third layer 24, combine 1.6 grams of sodium dichromate, 0.8 gram of potassium dichromate, 0.4 gram of sUver dichromate and 0.9 gram of monocrystaUine siUcon powder. Example 3 For forming first layer 20, into 100 ml of distiUed water add 5.0 grams of sodium peroxide, 0.5 gram of beryUium oxide, 2.0 grams of magnesium dichromate, 3.5 grams of calcium dichromate and 3.0 grams of boron oxide. For forming second layer 22, into 100 ml of twice- distiUed water add 0.5 gram of cobaltous oxide, 0.5 gram of strontium chromate, 0.8 gram of cupric oxide, 0.6 gram of β- titanium and 1.2 grams of potassium dichromate. For forming the powder of third layer 24, combine 1.6 grams of sodium dichromate, 0.8 gram of potassium dichromate, 0.6 gram of sUver dichromate and 0.9 gram of monocrystaUine siUcon powder. Example 4 For forming first layer 20, into 100 ml of distiUed water add 2.0 grams of sodium peroxide, 0.3 gram of beryUium oxide, 2.0 grams of magnesium dichromate, and 1.0 gram of boron oxide. For forming second layer 22, into 100 ml of twice-distiUed water add 0.5 gram of cobaltous oxide, 0.5 gram of strontium chromate, 0.4 gram of β-titanium and 1.0 gram of potassium dichromate. For forming the powder of third layer 24, combine 0.5 gram of sodium dichromate, 0.8 gram of potassium dichromate, 0.1 gram of sUver dichromate, 0.3 gram of monocrystaUine siUcon powder, 0.01 gram of beryUium oxide, 0.1 gram of strontium chromate, 0.1 gram of boron oxide and 0.1 gram of sodium peroxide. Example 5 For forming first layer 20, into 100 ml of distiUed water add 2.0 grams of sodium peroxide, 0.3 gram of beryUium oxide, 2.0 grams of magnesium dichromate and 1.0 gram of boron oxide. For forming second layer 22, into 100 ml of twice-dist led water add 0.3 gram of cobaltous oxide, 0.3 gram of strontium chromate, 1.0 gram of potassium dichromate and 1.0 gram of calcium dichromate. For forming the powder of third layer 24, combine 0.3 gram of sodium dichromate, 0.1 gram of sUver dichromate, 0.8 gram of potassium dichromate, 0.2 gram of monocrystaUine siUcon powder, 0.01 gram of beryUium oxide, 0.1 gram of strontium chromate, 0.1 gram of boron oxide, 0.2 gram of β-titanium and 0.1 gram of sodium peroxide. Example 6 For forming first layer 20, into 100 ml of distiUed water add 2.0 grams of sodium peroxide, 0.3 gram of magnesium dichromate, 1.0 gram of boron oxide and 1.0 gram of calcium dichromate. For forming second layer 22, into 100 ml of twice- distiUed water add 0.3 gram of cobaltous oxide, 0.01 gram of beryUium oxide, 1.0 gram of potassium dichromate, 1.0 gram of boron oxide and 2.0 grams of magnesium dichromate. For foirning the powder of third layer 24, combine 0.3 gram of sodium dichromate, 0.1 gram of sUver dichromate, 0.8 gram of potassium dichromate, 0.2 gram of monocrystaUine siUcon powder, 0.1 gram of strontium chromate, 0.01 gram of beryUium oxide, 0.1 gram of boron oxide, 0.1 gram of sodium peroxide, 0.2 gram of β-titanium and 0.2 gram of magnesium dichromate. Example 7 For forming first layer, into 100 ml of distiUed water add 2.0 grams of sodium peroxide, 0.3 gram of magnesium dichromate and 1.0 gram of boron oxide. For forming second layer 22, into 100 ml of twice- distiUed water add 0.2 gram of cobaltous oxide, 1.0 gram of calcium dichromate, 1.0 gram of potassium dichromate, 0.5 gram of boron oxide, 1.0 gram of magnesium dichromate and 0.01 gram of beryUium oxide. For forming the powder of third layer 24, combine 0.3 gram of sodium dichromate, 0.05 gram of suver dichromate, 0.8 gram of potassium dichromate, 0.2 gram of monocrystaUine siUcon powder, 0.1 gram of strontium chromate, 0.01 gram of beryUium oxide, 0.1 gram of boron oxide, 0.1 gram of sodium peroxide, 0.2 gram of β-titanium and 0.2 gram of magnesium dichromate. Experimental 1. Introduction Adding an appropriate quantity, on the order of several milligrams, of third layer 24 powder, which is an inorganic thermal superconductive medium to pipe, such as conduit 4, or flat interlayed piece, such as plates 36, 38, creates a superconductive device 2. For example, the addition of the third layer 24 powder into the cavity 6 of the conduit 6 or between the plates 36, 38 and then sealing the cavity 6 after subsequently eliminating the residual water and air upon heating, wUl create a thermal superconductive device 2. Subsequent test results prove that third layer 24 is a superconductive medium and that a heat conducting device made of third layer 24 is a thermal superconductive heat pipe. The fact that a convevtional heat pipe shares a simuar outside shape to a thermal superconductive heat pipe used to raise some misunderstandings. Therefore, it is necessary to give a brief description on the differences and simUarities of the two. A convectional heat pipe makes use of the technique of Uquids vaporizing upon absorbing great amounts of heat and vapors cooling upon emitting heat so as to bring the heat from the pipe's hot end to its cold end. The axial heat conducting velocity of the heat pipe depends on the value of the Uquid's vaporization potent heat and the circulation speed between two forms of Uquid and vapor. The axial heat conducting velocity of the heat pipe also is restrained by the type and quantity of the carrier material and the temperatures and pressures at which the heat pipe operates (it can not be too high). The present superconductive heat transfer device 2 is made of a thermal superconductive medium whose axial heat conduction is accompUshed by the thermal superconductive mediums' molecules high speed movement upon being heated and activated. The present superconductive heat transfer device's 2 heat conducting velocity is much higher than that of any metal bars or any convectional heat pipes of sirmlar size, whne its internal pressure is much lower than that of any convectional heat pipe of the same temperature. The appUcable upper temperature limit of the present superconductive thermal heat transfer device 2 is beyond the aUowed upper temperature limit of the conduit 4 material. The present superconductive thermal heat transfer device 2 can influence most if not aU categories of heat transfer, especiaUy on the heat utilization ratio. The present superconductive thermal heat transfer device 2 also is appUcable in the development and utilization of solar energy and geothermal energy, and for the recycling of lower energy level heat. 2. Testing Method And Principle The heat conducting velocity of a metal bar depends on the bar's heat conductivity, temperature gradient and the cross- sectional area orthogonal to the temperature gradient. Metals have higher heat conductivities than nonmetal soUds. Among metals, sUver has the highest heat conductivity of about 415 W/rnK. The present thermal superconductive heat transfer devices 2 are an entirely new development and there is no precedent on how to exemplify and test their properties. It would appear that using the measurements of their effective or apparent heat conductivities and axial and radial heat fluxes as an indication of their properties is scientific and logical. However, this does not change the fact that no precedent is avaUable on the measuring methods of heat conductivities of thermal superconductive devices. The testing method used to test the properties of the present superconductive thermal heat transfer devices 2 employed an upgrade Forbes Method, in which a thermal superconductive heat pipe was taken to be a semi-infinite rod. Given that the temperature of the rod's reference surface is T„ K, the temperature of a cross-section x meters away from the reference surface is T K, the temperature of the fluid (water) which is adjacent to the rod surface and which undergoes heat convection between itself and the rod is T t K, the heat conductivity of the rod is k W/mK, the convectional heat transfer coefficient of the surface is h W/m 2 K, the girth of the rod is P meters, and the cross- sectional area of the rod is f m 2 , the principal differential equation of heat transfer is d'Tldx* - (hp)/(kf)(T-T ∞ ) = 0 ( 1 ) This is a heterogeneous differential equation. Suppose Θ=T-T ∞ and Equation (1) then transforms into a homogeneous equation, by assuming m =hp/k£ we have d 2 θ/dx 2 - m 2 θ = 0 (2) For cylindrical objects, m 2 =4h/(kd o ), where do is the diameter of the cylindrical object. Suppose θ=θ 0 at x=0 (3) θ=0 at x=∞ (4) The solution that satisfies the above boundary conditions is θ=θ o ( - mx) (5) Under the boundary conduction defined by Equations (6) and (7) θ=θ 0 at x=0 (6) dθ/dx = 0 at x=L (7) then another solution of Equation (2) is θ/θo = Exp(mx){[l+Exp(2m(L-x))]/[l+Exp(2mL)]} (8) Since some experimental conditions may appear similar to that specified by Equations (6) and (7), and the value of the expression inside the { } is close to 1, therefore we have θ/θo- = Exp(mx) (9) which also is correct. The axial heat conducting velocity across the reference surface is Q x = -k^dθ/dx (10) From Equation (5), we can deduce the foUowing By substitution with Equation (6), we have Qo =kfmθ 0 (12) The speed of heat flux from rod to water is Q o = Vp'C p (T 0 -Ti) watts (13) where V=volume flow rate of water (m 3 /s) p=density of water (kg/m 3 ) C p =specific heat of water (J/kgK) T 0 =outlet temperature of water (K) Ti=inlet temperature of water (K) where L=length of the rod (meters) diameter of the rod (meters) h=convectional heat transfer coefficient (W/m 2 K) Upon having measured the above quantities, the effective heat conductivity of a thermal superconductive heat pipe can be calculated and the heat flux also can be calculated. 3. Testing Apparatus Based on the above mentioned testing principle and mathematical model, a testing apparatus, as shown in Figure 7, comprising the thermal heat conductive pipe 102, cooling water casing pipe 104, thermocouples 106, pressure gauge 108, water vapor heating chamber 110, condensed water coUector 112, and evacuation valve 114 was assembled. 4. Testing Results There are many advantages using saturated water vapor as the heat source to activate the thermal superconductive medium 24 inside the device 2. Saturated water vapor has a higher condensing heat transfer coefficient and the saturated water vapor comes into direct contact with the heated surface of the device 2 exclusive of contact heat resistance. Keeping the pressure of the saturated water vapor under control means keeping the heating temperature under control, and can provide the thermal superconductive heat transfer device 2 with a stable heat flux. After the flow rate and the inlet temperature of the cooling water is specified, the testing system wUl come into a stable equiUbrium. AU of the physical quantities that are measured are stable and weU repeatable. The foUowing chart Ulustrates four representative groups of measured results, and Figures 8-11 show these results graphicaUy. Results of Measurement No. Axial Heat Radial Heat Effective Heat k/k Ag Flux (W/m 2 ) Flux (W/m 2 ) Conductivity (W/mK) 1 8.618xl0 6 4.396xl0 4 1.969xl0 6 4.746xl0 : 2 8.363xl0 6 4.267xl0 4 3.183xl0 6 7.672xl0 : 3 8.260xl0 6 4.214xl0 4 2.624xl0 5 6.324xl0 : 4 8.83 lxlO 6 4.505xl0 4 3.235xl0 4 7.795xl0 : The temperature distribution curve, effective heat conductivity, convectional heat transfer coefficient of the pipe surface of the cooling segment, and heat conducting velocity were obtained under different cooling water flow rates. Although these values show certain differences, they indicate that the heat pipe is theπnaUy superconductive. Changes of cooling water flow rates causes changes in temperature distribution, but no changes in heat conducting velocity. This means that the heat conducting velocity in the heating segment has reached its upper limit. That the heat conducting area of the heating segment was designed not great enough was due to the underestimation of the heat conducting capabiUty of the heat pipe. Changes in temperature distribution brought changes in the value and sign of slope m in the conelation equation. That the convectional heat transfer coefficient was changed means that the effective heat conductivity also was changed. The thermal superconductivity of the heat pipe is confirmed by these changes. When m has a plus sign, the outlet temperature of the cooling water approaches the temperature at the base of the heat pipe (at x=0). A conventional heat exchanger can attain such a high heat transfer efficiency only under the condition of counter flow. If the cooling water flow rate is increased, then the outlet temperature of the cooling water approaches that at the other end (x=L). A conventional heat exchanger can reach such a great heat transfer efficiency only when the heat conducting area is infinite. Therefore, the foregoing, including the examples, is considered as iUustrative only of the principles of the invention. Further, various modifications may be made of the invention without departing from the scope and spirit thereof and it is desired, therefore, that only such limitations shah be placed thereon as are imposed by the prior art and which are set forth in the appended claims.

Claims: What is claimed is: 1. A superconducting heat transfer medium comprising: a first layer comprising at least one compound selected from the group consisting of sodium peroxide, sodium oxide, beryUium oxide, manganese sesquioxide, aluminum dichromate, calcium dichromate, boron oxide, dichromate radical, and combinations thereof; a second layer comprising at least one compound selected from the group consisting of cobaltous oxide, manganese sesquioxide, beryUium oxide, strontium chromate, strontium carbonate, rhodium oxide, cupric oxide, β-titanium, potassium dichromate, boron oxide, calcium dichromate, manganese dichromate, aluminum dichromate, dichromate radical, and combinations thereof; and a third layer comprising at least one compound selected from the group consisting of denatured rhodium oxide, potassium dichromate, denatured radium oxide, sodium dichromate, sUver dichromate, monocrystaUine siUcon, beryUium oxide, strontium chromate, boron oxide, sodium peroxide, β-titanium, a metal dichromate, and combinations thereof. 2. The superconducting heat transfer medium of Claim 1, wherein the first layer comprises beryUium oxide, a metal dichromate, calcium dichromate, and boron oxide. 3. The superconducting heat transfer medium of Claim 2, wherein the first layer further comprises a sodium compound selected from the group consisting of sodium peroxide and sodium oxide. 4. The superconducting heat transfer medium of Claim 3, wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate. 5. The superconducting heat transfer medium of Claim 1, wherein the second layer comprises cobaltous oxide, manganese sesquioxide, beryUium oxide, strontium chromate, strontium carbonate, cupric oxide, titanium, potassium dichromate, boron oxide, calcium dichromate, and a metal dichromate. 6. The superconducting heat transfer medium of Claim 5, wherein the metal dichromate is selected from the group consisting of alurninum dichromate and manganese dichromate; and the titanium is β-titanium. 7. The superconducting heat transfer medium of Claim 1, wherein the second layer comprises cobaltous oxide, beryUium oxide, strontium chromate, strontium carbonate, cupric oxide, titanium, potassium dichromate, boron oxide, calcium dichromate, a metal dichromate, and one or more oxides selected from the group consisting of rhodium oxide and radium oxide. 8. The superconducting heat transfer medium of Claim 7, wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate; and the titanium is β-titanium. 9. The superconducting heat transfer medium of Claim 8, wherein the second layer further comprises manganese sesquioxide. 10. The superconducting heat transfer medium of Claim 1, wherein the third layer is a powder comprising one or more denatured oxides selected from the group consisting of denatured rhodium oxide, denatured radium oxide, and combinations thereof; one or more Group LA dichromates selected from the group consisting of sodium dichromate, potassium dichromate, and combinations thereof; sUver dichromate; monocrystaUine siUcon; beryUium oxide; strontium chromate; boron oxide; sodium peroxide; titanium; and a metal dichromate. 11. The superconducting heat transfer medium of Claim 10, wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate; and the titanium is β-titanium. 12. The superconducting heat transfer medium of Claim 10, wherein the monocrystaUine siUcon is pretreated by magnetic penetration. 13. The superconducting heat transfer medium of Claim 2, wherein the first layer has a thickness of between about 0.008 mm and about 0.012 mm. 14. The superconducting heat transfer medium of Claim 5, wherein the second layer is appUed on top of the first layer. 15. The superconducting heat transfer medium of Claim 14, wherein the second layer forms a film on top of the first layer. 16. The superconducting heat transfer medium of Claim 5, wherein the second layer has a thickness of between about 0.008 mm and about 0.012 mm. 17. The superconducting heat transfer medium of Claim 1, wherein the third layer is a powder. 18. The superconducting heat transfer medium of Claim 10, wherein the third layer is appUed on top of the second layer. 19. The superconducting heat transfer medium of Claim 18, wherein the third layer is evenly distributed across the second layer. 20. A superconducting heat transfer device comprising first, second, and third layers disposed on a substrate, wherein: the first layer has a thickness of between about 0.008 mm and about 0.012 mm and comprises at least one compound selected from the group consisting of sodium peroxide, sodium oxide, beryUium oxide, manganese sesquioxide, aluminum dichromate, calcium dichromate, boron oxide, dichromate radical, and combinations thereof; the second layer has a thickness of between about 0.008 mm and about 0.012 mm and comprises at least one compound selected from the group consisting cobaltous oxide, manganese sesquioxide, beryUium oxide, strontium chromate, strontium carbonate, rhodium oxide, cupric oxide, β-titanium, potassium dichromate, boron oxide, calcium dichromate, manganese dichromate, aluminum dichromate, dichromate radical, and combinations thereof; and the third layer comprises at least one compound selected from the group consisting of denatured rhodium oxide, potassium dichromate, denatured radium oxide, sodium dichromate, sUver dichromate, monocrystaUine siUcon, beryUium oxide, strontium chromate, boron oxide, sodium peroxide β-titanium, a metal dichromate, and combinations thereof. 21. The superconducting heat transfer device of Claim 20, wherein the first layer comprises beryUium oxide, a metal dichromate, calcium dichromate, and boron oxide. 22. The superconducting heat transfer device of Claim 21, wherein the first layer further comprises one or more sodium compounds selected from the group consisting of sodium peroxide and sodium oxide; wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate; and the titanium is β-titanium. 23. The superconducting heat transfer device of Claim 20, wherein the second layer comprises cobaltous oxide, manganese sesquioxide, beryUium oxide, strontium chromate, strontium carbonate, cupric oxide, β-titanium, potassium dichromate, boron oxide, calcium dichromate, and a metal dichromate. 24. The superconducting heat transfer device of Claim 23, wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate. 25. The superconducting heat transfer device of Claim 20, wherein the second layer comprises cobaltous oxide, beryUium oxide, strontium chromate, strontium carbonate, cupric oxide, titanium, potassium dichromate, boron oxide, calcium dichromate, a metal dichromate, and one or more oxides selected from the group consisting of rhodium oxide and radium oxide. 26. The superconducting heat transfer device of Claim 25, wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate; and the titanium is β-titanium. 27. The superconducting heat transfer device of Claim 26, wherein the second layer further comprises manganese sesquioxide. 28. The superconducting heat transfer device of Claim 21, wherein the third layer is a powder comprising: one or more denatured oxides selected from the group consisting of denatured rhodium oxide, denatured radium oxide, and combinations thereof; one or more Group LA dichromates selected from the group consisting of sodium dichromate, potassium dichromate, and combinations thereof; sUver dichromate; monocrystaUine siUcon; beryUium oxide; strontium chromate; boron oxide; sodium peroxide; titanium; and a metal dichromate. 29. The superconducting heat transfer device of Claim 28, wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate; the titanium is β-titanium; and the monocrystaUine siUcon is pretreated by magnetic penetration. 30. The superconducting heat transfer device of Claim 28, wherein the third layer is appUed on top of the second layer. 31. The superconducting heat transfer device of Claim 30, wherein the third layer is evenly distributed across the second layer. 32. The superconducting heat transfer device of Claim 20, wherein the substrate comprises at least one surface; and the first layer penetrates into the at least one surface of the substrate. 33. The superconducting heat transfer device of Claim 32, wherein the substrate is a sealed conduit comprising an inner surface and an outer surface; and the first, second, and third layers are appUed to the inner surface. 34. The superconducting heat transfer device of Claim 33, wherein the conduit is heat polarized. 35. The superconducting heat transfer device of Claim 20, wherein the substrate is a pair of plates each having a proximal surface and a distal surface with the proximal surfaces facing each other and the distal surfaces facing away from each other, and the plates being spaced apart so as to form a cavity between the plates. 36. The superconducting heat transfer device of Claim 35, wherein the first, second, and third layers are appUed to the proximal surface of each plate. 37. The superconducting heat transfer device of Claim 36, wherein the cavity volume is smaU relative to the surface area of the plates. 38. A method for preparing a superconducting heat transfer medium comprising three layers, comprising the steps of: (a) preparing a first layer solution; (b) applying the first layer solution to a surface of a substrate so as to form a first layer; (c) preparing a second layer solution; (d) applying the second layer solution to the first layer so as to form a second layer on top of the first layer; (e) preparing a third layer powder; and (f) exposing the second layer to the third layer powder so as to form a third layer on top of the second layer, thus forming the three layer superconducting heat transfer medium. 39. The method for producing the superconducting heat transfer medium of Claim 38, wherein the first layer solution comprises water, beryUium oxide, a metal dichromate, calcium dichromate, and boron oxide. 40. The method for producing the superconducting heat transfer medium of Claim 39, wherein the first layer solution further comprises one or more sodium compounds selected from the group consisting of sodium peroxide and sodium oxide. 41. The method for producing the superconducting heat transfer medium of Claim 40, wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate; and the titanium is β-titanium. 42. The method for producing the superconducting heat transfer medium of Claim 41, wherein the second layer is prepared from an ionic solution comprising water, cobaltous oxide, manganese sesquioxide, beryUium oxide, strontium chromate, strontium carbonate, cupric oxide, titanium, potassium dichromate, boron oxide, calcium dichromate, and a metal dichromate. 43. The method for producing the superconducting heat transfer medium of Claim 42, wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate; and the titanium is β-titanium. 44. The method for producing the superconducting heat transfer medium of Claim 38, wherein the second layer is prepared from a second layer solution comprising water, cobaltous oxide, beryUium oxide, strontium chromate, strontium carbonate, cupric oxide, titanium, potassium dichromate, boron oxide, calcium dichromate, a metal dichromate, and one or more oxides selected from the group consisting of rhodium oxide and radium oxide. 45. The method for producing the superconducting heat transfer medium of Claim 44, wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate; and the titanium is β-titanium. 46. The method for producing the superconducting heat transfer medium of Claim 45, wherein the second layer solution further comprises manganese sesquioxide. 47. The method for producing the superconducting heat transfer medium of Claim 38, wherein the third layer is a powder prepared from a blend comprising: one or more denatured oxides selected from the group consisting of denatured rhodium oxide, denatured radium oxide, and combinations thereof; one or more Group LA dichromates selected from the group consisting of sodium dichromate, potassium dichromate, and combinations thereof; stiver dichromate; monocrystaUine siUcon; berylUum oxide; strontium chromate; boron oxide; sodium peroxide; titanium; and a metal dichromate. 48. The method for producing the superconducting heat transfer medium of Claim 47, wherein the metal dichromate is selected from the group consisting of aluminum dichromate and manganese dichromate; and the titanium is β-titanium. 49. The method for producing the superconducting heat transfer medium of Claim 38, wherein the first layer solution, the second layer solution and the third layer powder are prepared at a temperature of between about 0 °C and about 30 °C; and at a relative humidity of no greater than 40%. 50. The method for producing the superconducting heat transfer medium of Claim 48, wherein the first layer solution is prepared at a temperature of between about 5 °C and about 8 °C. 51. The method for producing the superconducting heat transfer medium of Claim 49, wherein the third layer powder is prepared at a relative humidity of between about 30% and 35%. 52. The method for producing the superconducting heat transfer medium of Claim 38, wherein the first layer solution is manufactured by a process comprising the steps of: (a) placing 100 parts, by weight, of distiUed water into an inert container; (b) dissolving and mixing between 2.0 and 5.0 parts, by weight, of sodium peroxide into the water; (c) dissolving and mixing between 0.0 and 0.5 parts, by weight, of sodium oxide into the solution of step (b); (d) dissolving and mixing between 0.0 and 0.5 parts, by weight, of beryUium oxide into the solution of step (c); (e) dissolving and mixing between 0.3 and 2.0 parts, by weight, of a metal dichromate selected from the group consisting of aluminum dichromate and magnesium dichromate into the solution of step (d); (f) dissolving and mixing between 0.0 and 3.5 parts, by weight, of calcium dichromate into the solution of step (e); and (g) dissolving and mixing between 1.0 and 3.0 parts, by weight, of boron oxide into the solution of step (f). 53. The method for producing the superconducting heat transfer medium of Claim 52, wherein the step of preparing a second layer solution comprises the steps of: (a) placing 100 parts, by weight, of twice-distiUed water into an inert container; (b) dissolving and mixing between 0.2 and 0.5 parts, by weight, of cobaltous oxide into the twice-distiUed water; (c) dissolving and mixing between 0.0 and 0.5 parts, by weight, of manganese sesquioxide into the solution of step (b); (d) dissolving and mixing between 0.0 and 0.01 parts, by weight, of beryUium oxide into the solution of step (c); (e) dissolving and mixing between 0.0 and 0.5 parts, by weight, of strontium chromate into the solution of step (d); (f) dissolving and mixing between 0.0 and 0.5 parts, by weight, of strontium carbonate into the solution of step (e); (g) dissolving and mixing between 0.0 and 0.2 parts, by weight, of rhodium oxide into the solution of step (f); (h) dissolving and mixing between 0.0 and 0.8 parts, by weight, of cupric oxide into the solution of step (g); (i) dissolving and mixing between 0.0 and 0.6 parts, by weight, of β-titanium into the solution of step (h); (j) dissolving and mixing between 1.0 and 1.2 parts, by weight, of potassium dichromate into the solution of step (i); (k) dissolving and mixing between 0.0 and 1.0 parts, by weight, of boron oxide into the solution of step (j); (1) dissolving and mixing between 0.0 and 1.0 parts, by weight, of calcium dichromate into the solution of step (k); and (m) dissolving and mixing between 0.0 and 2.0 parts, by weight, of aluminum dichromate or magnesium dichromate, into the solution of step (1). 54. The method for producing the superconducting heat transfer medium of Claim 53, wherein the step of preparing the third layer powder comprises the steps of: (a) placing between 0.0 and 1.75 parts, by weight, of denatured rhodium oxide into an inert container; (b) blending between 0.3 and 2.6 parts, by weight, of sodium dichromate with the rhodium oxide; (c) blending between 0.0 and 0.8 parts, by weight, of potassium dichromate with the mixture of step (b); (d) blending between 0.0 and 3.1 parts, by weight, of denatured radium oxide with the mixture of step (c); (e) blending between 0.1 and 0.4 parts, by weight, of sUver dichromate with the mixture of step (d); (f) blending between 0.2 and 0.9 parts, by weight, of the monocrystaUine siUcon powder treated by magnetic penetration with the rnixture of step (e); (g) blending between 0.0 and 0.01 parts, by weight, of beryUium oxide with the mixture of step (f); (h) blending between 0.0 and 0.1 parts, by weight, of strontium chromate with the mixture of step (g); (i) blending between 0.0 and 0.1 parts, by weight, of boron oxide with the mixture of step (h); (j) blending between 0.0 and 0.1 parts, by weight, of sodium peroxide with the mixture of step (i); (k) blending between 0.0 and 1.25 parts, by weight, of β-titanium with the rnixture of step (j); and (1) blending between 0.0 and 0.2 parts, by weight, of aluminum dichromate or magnesium dichromate, into the mixture of step (k). 55. The method for producing the superconducting heat transfer medium of Claim 54, wherein: said step of applying the first layer solution comprises the steps of: (1) submerging at least a portion of the substrate within the first layer solution such that the first layer solution contacts at least a selected portion of the substrate; and (2) drying the substrate naturaUy at ambient conditions to form first layer on the selected portion of the substrate; said step of applying the second layer solution comprises the steps of: (1) submerging at least a portion of the substrate with the first layer thereon within the second layer solution such that the second layer solution contacts at least a selected portion of the first layer; and (2) drying the substrate naturaUy at ambient conditions to form a film of second layer on the selected portion of the first layer; and said step of applying the third layer solution comprises the step of exposing at least a selected portion of the second layer to the third layer powder. 56. The method for producing the superconducting heat transfer medium of Claim 55, wherein said step of applying the first layer solution is carried out at a temperature of between about 0 °C and about 30 °C for at least 8 hours. 57. The method for producing the superconducting heat transfer medium of Claim 55, wherein said step of applying the third layer is carried out at a temperature of between about 55 °C and about 65 °C for at least 4 hours. 58. A method for producing a superconducting heat transfer device comprising the superconducting heat transfer medium of Claim 55, wherein: said step of applying said first layer comprises the steps of: (1) submerging a substrate having a cavity and first and second ends within the first layer solution such that the first layer solution fitts the cavity; (2) drying the substrate naturaUy at ambient conditions to form the first layer within the cavity; said step of applying said second layer comprises the steps of: (1) submerging the substrate within the second layer solution such that the second layer solution fills the cavity; (2) drying the substrate naturaUy at ambient conditions to form a film of the second layer within the cavity; (3) attaching an end cap on the second end of the substrate; (4) attaching an injection cap having a bore therethrough on the first end of the substrate; and (5) heating the first end of the substrate to a temperature not to exceed 120 °C; and said step of applying said third layer comprises the steps of: (1) injecting the third layer powder through the bore in an amount of at least 1 cubic meter per 400,000 cubic meters of the cavity volume; (2) inserting a plug into the bore; (3) heating the first end of the substrate to a temperature between 80 °C and 125 °C; (4) removing the plug from the bore; and (5) reinserting the plug into the bore. 59. The method for producing a superconducting heat transfer device of Claim 58, wherein the substrate is placed within the first layer solution in a non-horizontal anangement at a temperature of between about 0 °C and about 30 °C for at least 8 hours; and the first layer solution penetrates the surface of the carrier to a depth of between 0.008 mm and 0.012 mm. 60. The method for producing a superconducting heat transfer device of Claim 58, wherein the first end of the substrate is oriented in a downward direction within the second layer solution, at a temperature of between about 55 °C and about 65 °C for at least 4 hours; forming a second layer having a thickness of between about 0.008 mm and about 0.012 mm. 61. The method for producing a superconducting heat transfer device of Claim 58, wherein the temperature of the heating step when applying the second layer is approximately 40 °C; and wherein the plug is removed from the bore for no more that approximately 2 seconds.

Inventors: QU YUZHI, QU, YUZHI
Applicants: QU YUZHI, QU, YUZHI
Application year: 1997
Main classification: B32B15
IPC codes: B32B9, B32B15, B32B33, C09K5, F24J1, F28D15, F28F3, F28F13, F28F21, H01L23