The subject invention relates to microclimate heating or cooling, and a miniature heating or cooling system, that can be used for any purpose that requires a compact heating or cooling system. Such applications include, but are not limited to, personal and portable heating or cooling systems.
Deep submersion operations performed by free-swimming divers, such as Navy divers, often expose them to extremely cold conditions. Currently, there is no effective and/or efficient method of heating divers during exposure to such conditions. This deficiency can induce cold stress, which in turn impairs diver performance, shortens dive duration, and creates an unnecessary health risk to divers. The issue usually arises during cold water dives, and the affects of the cold typically manifest first in the diver's extremities, such as hands and feet.
Currently available solutions, such as electrical resistor type systems, which at maximum can only supply as much heat as the electrical power expended for unit operation, are inefficient and require large amounts of portable power supplies. Other alternative solutions, such as umbilical chord attachments to the diver that can supply warm water and electrical power, are also too bulky and significantly restrict the user's freedom of movement.
Accordingly, there is need for a heating system having a high coefficient of performance and a light compact design. The solution should heat effectively to maintain core body temperatures. The solution should preferably be low profile, small volume, power efficient, resistant to corrosive saltwater, and operate for the duration of a typical dive.
Embodiments of the subject invention pertain to a method and apparatus for heating or cooling. Embodiments relate to a method and apparatus utilizing a vapor compression cycle to accomplish active heating or cooling. In a specific embodiment, the subject invention relates to a lightweight, compact, reliable, and efficient heating or cooling system for underwater applications. The subject system can provide heating or cooling stress relief to individuals operating under, for example, hazardous conditions, or in low temperature underwater environments where passive protective clothing provides insufficient mitigation of cooling stress. Further embodiments can be utilized to provide heat stress relief to users who are working in thermally encapsulated ensembles that hinder the body's natural ability to expel heat. The subject system can be utilized in other applications that can benefit from this type of heating or cooling system. The performance of this system cannot be matched simply by using smaller versions of currently available designs or technologies.
Embodiments of the subject invention relate to an underwater diver heating system that utilizes two-phase heat pump cycle technology. This vapor compression heat pump process can be efficient, such that for a given amount of electrical power supplied to the system at least 2 times that amount of heat, removed from the sea water, is delivered to the diver's body.
In a specific embodiment, the subject invention pertains to a heating system having a total weight of less than about 4.0 pounds, a coefficient of performance of at least 2.4, and a volume of less than about 1200 cc with a heating capacity between about 100 and about 500 watts. In a further embodiment, the subject invention pertains to a heating system having a total weight of less than about 6.0 pounds, a coefficient of performance of at least 1.5, and a volume of less than about 2000 cc with a heating capacity between about 100 and about 500 watts. The subject heating system can provide between 22 and 40 watts of heating per pound and occupy between 2.4 and 12 cc of volume per watt of cooling. In comparison, conventional technology units for heating in this range would between two and three times the amount of battery volume and weight in order to provide the same heating level for a given operation time. Resistive heating devices can only provide a maximum of 1 watt of cooling for every watt of provided electrical energy, thus requiring significantly larger amounts of batteries to provide heat rates similar to the subject invention. Similarly, heating technologies that rely on chemical processes would require a significant amount of large and bulky support equipment
The subject system can be scaled to larger or smaller sizes for different applications. The subject system can incorporate a compressor and heat exchanger design so as to achieve a high coefficient of performance and a light and compact design. Incorporation of a compressor can enhance the overall performance of the vapor compression system, and incorporation of the heat exchanger can reduce the overall weight and size of the subject apparatus. Embodiments of the subject cooling system can utilize a miniaturized, high efficiency motor, along with the integration of compact heat exchangers for refrigerant evaporation and liquid pumps.
Specific embodiments of the subject cooling system can involve the use of one or more of the following: micro-fabrication techniques, an innovative rotary lobed compressor, a miniature high efficiency permanent magnet motor, compact heat exchanger for refrigerant evaporation and condensation, and liquid pumps. In a specific embodiment, the subject system can provide approximately 300 watts of heating or 200 watts of cooling for microclimate and other temperature control environments.
Embodiments of the subject invention pertain to a method and apparatus for heating or cooling. Embodiments relate to a method and apparatus utilizing a vapor compression cycle to accomplish active heating or cooling. In a specific embodiment, the subject invention relates to a lightweight, compact, reliable, and efficient heating or cooling system for underwater applications. The subject system can provide supplemental heating or cooling to individuals operating in, for example, underwater environments where the loss of control of body temperature or personal comfort can not be mitigated through passive devices such as wetsuits or dry-suits. The subject system can be utilized in other applications that can benefit from this type of heating or cooling system. The performance of this system cannot be matched simply by using smaller versions of currently available designs or technologies.
In a specific embodiment, the subject microclimate system can provide at least about 300 watts of heat while consuming less than about 125 watts of power, and weigh less than about 4.5 pounds (not including the water jacket or the power source) while having less than about a 1200 cubic centimeter volume. In a specific embodiment, the subject system can run for at least about 1.5 hours or more with the use of batteries. In a specific embodiment, a heating power to weight ratio of more than 66 W/lb and/or a volume to heating power ratio of less than 4 cc/W can be achieved utilizing a vapor compression cycle with heating capacities of approximately 300 W.
The same subject microclimate system can provide at least about 200 watts of cooling while consuming less than about 90 watts of power. In a specific embodiment, the subject system can run for at least about 2.0 hours or more with the use of batteries. In a specific embodiment, a cooling power to weight ratio of more than 44 W/lb and/or a volume to heating power ratio of less than 6 cc/W can be achieved utilizing a vapor compression cycle with cooling capacities lower than 200 W.
A heat pump cycle for an embodiment of a microclimate heating and cooling system in accordance with the subject invention can incorporate a vapor compression cycle intended for use with compressible refrigerants. There are four basic features to such a vapor compression cycle, including vapor compression, condensation within a heat exchanger, sub-cooled liquid expansion, and vaporization within an evaporative heat exchanger. The cycle begins with a compressor that compresses refrigerant vapor to a pressure at which the corresponding vapor temperature is above the desired operating fluid temperature of the condenser. This heated fluid can in turn be utilized to provide warmth to the user via, for example, a tube suit or water jacket. The compressed hot refrigerant vapor flows to a condensing heat exchanger, which is typically a gas to vapor or liquid to vapor heat exchanger, where the vapor is hotter than the gas or liquid. Heat is removed from the compressed refrigerant vapor by the entering fluid on the other side of the heat exchanger. This causes the temperature of the compressed, vaporized refrigerant to decrease below the saturation temperature of the refrigerant and the vapor condenses to liquid. The high pressure liquid can then be expanded through an expansion device, such as a throttling valve, capillary tube or pin-hole orifice, which can cause a rapid decrease in refrigerant pressure after the valve. The lower pressure can cause the temperature of the liquid coolant to drop to, for example, the corresponding lower saturation temperature.
In a specific embodiment the expanded, cool liquid refrigerant can then flow through an evaporator that allows the liquid refrigerant to absorb the heat from a fluid that is desired to be cooled. The evaporator can act as another heat exchanger with cool refrigerant on one side and the fluid, either liquid or gas, that is desired to be cooled on the other side of the heat exchanger. The absorption of heat in the evaporator from the entering coolant liquid causes the liquid refrigerant to boil. The vaporized refrigerant then flows back into the compressor to begin the cycle again. The exiting coolant can then be either ejected to the ambient or re-circulated to cool an individual wearing a cooling jacket or to cool surfaces. In the heating mode of operation the evaporator transfers heat from the ambient water to the refrigerant and the condenser transfers heat from the refrigerant to the liquid used to deliver heat. This liquid can deliver heat via, for example, a warming garment. In the cooling mode of operation the condenser transfers heat from the refrigerant to the ambient water and the evaporator transfers heat from the liquid in used to remove heat to the refrigerant.
In a specific embodiment, the subject invention can allow the use of the standard vapor compression cycle in a compact and lightweight design by utilizing specialized components that have been developed specifically for the subject system.
In an alternative operation mode, where the user desires to circulate cooled liquid in a warm ambient, the re-circulation tubes of a cooling garment or similar device can be attached to the evaporative heat exchange portion of the subject invention. In this mode of operation the compressor, evaporator, condenser, and expansion device may operate in a similar manner while removing heat from the tube suit loop and ejecting heat at an elevated ambient on the condensation side. The liquid side of the condenser can incorporate a liquid pump flowing ambient water through the condensing heat exchanger, which warms the fluid and in turn condenses the refrigerant vapor in point 2 to point 3 of
In a specific embodiment, one of the two heat exchangers in the system can be located to form at least a portion of an outer shell of the system. A specific embodiment is shown in
In a specific embodiment, the subject invention can incorporate compressor 3 shown in
Referring to
The shape of an epiterchoid chamber is determined by the following equations:
where MA is the major axis.
In a specific embodiment, a length of 49 mm can be utilized for the major axis of the epitrochoid with a height of 6 mm. The values of the major axis and height can be modified based on the cooling capacity requirements of the vapor compression cycle and the desired angular velocity of the compressor. Once these two constraints are set, the basic designs of the main components of the compressor can be determined as a function of the geometry. The major axis determines the size of the rotor and the shape of the epitrochoid, as well as the gears that are used in the compressor.
Using the equations relating to the shape of the epitrochoid chamber provided above, the rotor size and shape can also be chosen. Finally, the geometric height of the epitrochoid and rotor can be determined by the amount of fluid that is desired to be displaced on each revolution. After having calculated these dimensions, the compressor's speed can be chosen to determine the displacement per unit time or volumetric flow rate. In a specific embodiment, incorporating an epitrochoidal chamber with a major axis of 49 mm and a height of 6 mm, a speed of 2000 rpm is chosen to provide a mass flow rate of approximately 1.5 g/s of vapor refrigerant 134a at an inlet pressure of 50 psi.
The flow through the compressor can be controlled by inlet port 10 (shown in
Shaft seals and bearings can be used along the shaft to assist in sealing and to absorb the loads caused by the rotating parts. External sealing can be achieved by the shaft seals and gaskets or by encapsulating the entire compressor and driving motor unit in a hermetic casing, while internal sealing of the compression chambers can be accomplished using, for example, a sealing gasket 14 or o-ring.
To increase the efficiency and life of the compressor, referring to
Additional methods of sealing may be considered for the compressor as well. Rather than face sealing with gaskets and spring loaded plastics, sufficient sealing can be created by machining the parts with very high precision. In a specific embodiment, the gaps between the rotor and the upper or lower walls are machined to fit to within a range of between 0.0001 and 0.002 inches so that the fluid being pressurized has significant difficulty in leaking past the two surfaces.
The subject compressor can incorporate low friction, low corrosion materials. In addition, wear parts other than the seals can be coated with low friction, high hardness coating, such as diamond like carbon, TiN, and MoSi2. In a specific embodiment, the subject compressor can operate without coolant oil. Compressor oil can reduce the heat transfer performance of the condenser and evaporators, requiring a larger heat exchanger to properly transfer heat. Accordingly, the use of a specific embodiment of the subject compressor that can operate without oil can allow the use of a smaller heat exchanger.
The motor 16 as shown in
The subject cooling system can be powered by, for example, by batteries, AC power, or DC power. An embodiment powered by batteries can connect to external battery packs or can utilize a central power unit.
The compressed vapor refrigerant exiting outlets 18 of the compressor can flow into a condenser inlet port 19, shown in
A specific embodiment of a condenser 4 in accordance with the subject invention is shown in
The liquid that is to be heated can enter the condenser via liquid connection tube 24 and travel to liquid port 25. A pump 1 can pump the heated liquid through the heating path 26. In a specific embodiment, pump 1 is built into the condenser. Alternatively, a pump external to the condenser or external to the entire heat pump system can be utilized. The heated liquid can exit the condenser via fluid exit port 27 and flow out of connection tube 28. The heated liquid type can vary depending on the application and can be, for example, a liquid, gas, or two-phase mixture. The geometry of the heat exchanging condenser can vary depending on the type of fluid and required performance. In a specific embodiment, the liquid is water. Although the embodiment shown in
The subject condenser can exchange heat between a liquid and the refrigerant. While the refrigerant passes through the condensing heat exchanger, it can experience a phase change from vapor to liquid as it loses heat to the heated liquid on the opposing side. With respect to this atypical heat exchanger, non-traditional methods can be utilized for predicting the performance of and designing of the heat exchanger. The liquid side can adhere to well established heat transfer correlations, which suggest that the total heat transfer between two substances at different temperatures is equal to a heat transfer coefficient constant times the total area that it is acting on and the temperature gradient.
Heat transfer characterization and prediction on the refrigerant side, however, is more complicated due to the phase change process that occurs while the refrigerant is passing through the heat exchanger. Approximate correlations, which include experimental correction factors, have been recently determined and are discussed in detail in Carey, Van P., Liquid-Vapor Phase Change Phenomena, Taylor and Francis, New York (1992), which is hereby incorporated by reference. A specific embodiment of the subject invention can utilize a heat exchanger geometry that is based on correlation approximations from Carey (1992) that maximize the amount of heat transfer on the refrigerant side from the heated liquid on the other side.
Similar to the heated liquid side, however, the two phase heat transfer phenomenon is highly dependent upon the amount of area available for heat transfer to take place. In a specific embodiment, the design of the subject condensing heat exchanger can, in general, maximize heat transfer area, while minimizing overall weight and dimensions and minimizing the liquid pressure drop through the heat exchanger. Preferably, the two fluids pass as close to each other as possible in order to minimize conduction heat transfer resistance through the separating medium. In a specific embodiment, a parallel channel construction configuration can be utilized. In a further specific embodiment, the parallel channel configuration can have a separation wall of 0.5 mm and can follow the path of an Archemedian spiral. An archemidian spiral is defined in a parametric coordinate system as:
x(t)=A·t·cos(B·t)
y(t)=A·t·sin(B·t)
where the constants A and B govern the number of spiral revolutions and the overall diameter of the geometry. One example yields a spiral path as is seen in
In a specific embodiment, the path for both fluids can begin on the outer edge of the cylinder and terminate in the center, where both fluids can exit perpendicular to the plane that they are flowing parallel on. Such a design can eliminate abrupt fluid turning points, thus minimizing pressure drop. Thin separation walls can be used to provide a sufficient length of, for example, approximately 26 inches within the limited area of the condenser having a diameter of 2.2 inches. The channel depth can be chosen, using two-phase heat transfer correlations as a guide, to maximize the heat transfer area available for both fluids and meet the heat exchange rate requirements of the condenser.
Condensed high pressure liquid refrigerant can flow from the condenser 4 via exit port 23 (shown in
A specific embodiment of the subject compact vapor compression cooling system, shown in
All patents, patent applications, provisional applications, and publications referred to or cited herein are incorporated by reference in their entirety, including all figures and tables, to the extent they are not inconsistent with the explicit teachings of this specification.
It should be understood that the examples and embodiments described herein are for illustrative purposes only and that various modifications or changes in light thereof will be suggested to persons skilled in the art and are to be included within the spirit and purview of this application.
The present application claims the benefit of U.S. Provisional Application Ser. No. 61/056,357, filed May 27, 2008, which is hereby incorporated by reference herein in its entirety, including any figures, tables, or drawings.
Number | Date | Country | |
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61056357 | May 2008 | US |