Patent Publication Number: US-11047381-B2

Title: Method and apparatus for orientation independent compression

Description:
CROSS-REFERENCE TO RELATED APPLICATION 
     The present application claims the benefit of U.S. Provisional Application Ser. No. 61/115,429, filed Nov. 17, 2008, which is hereby incorporated by reference herein in its entirety, including any figures, tables, or drawings. 
    
    
     BACKGROUND OF INVENTION 
     With respect to conventional compressors, the lubrication of the moving compressor parts is achieved by separated oil drawn from the oil-vapor mixture that exits the compressor. The oil can be separated from the oil vapor mixture by an oil separator and collected into an oil sump that supplies the compressor with oil for proper operation. On the compressor exhaust, after compression, the exhausted fluid consists of an oil-vapor mixture. Prior to sending the oil-vapor mixture to further components in the vapor compression system, the oil drops out of the flow inside the oil separator and is separated from the vapor and can be fed to an oil sump through gravity acting on the oil. The vapor only is then exited to the further components in the system. The separated oil is then directed back to the compressor inlet without traveling through the remainder of the vapor compression system. In addition to oil separators with gravity oil-fed oil sumps to separate the oil from the vapor, other components such as accumulators and some evaporator types with oil bleed ports can be used to separate the oil from the vapor. Thus, with conventional compressors, the vast majority of the oil contained in the vapor compression system is kept inside the compressor and oil separation mechanism alone (stored in the oil sump or other device such as an accumulator), as it is in continuous recirculation between the compressor and oil separation mechanism. 
     Therefore, conventional compressors, requiring some form of an oil separation mechanism either through the use of oil separators or other means such as through the use of oil bleed lines from some evaporator types or accumulators, are commonly orientation dependent, meaning dependent on the orientation of the compressor and oil separation mechanism with respect to the surrounding gravitational field, due to the gravity dependence of the oil-sump requirement and the gravity dependent location of any oil bleed lines drawn from other devices such as accumulators. The movement of oil from the exhaust of the compressor to the oil separation mechanism and back to the compressor is gravity dependent. Accordingly, with conventional compressors, there exists certain compressor orientations that restrict or completely cut off the gravity driven flow of oil to the compressor due to improper oil levels or no oil at all being located in the designated areas of the supplied oil sump or other oil storage device. With inadequate or no oil lubrication, the compressor performance can be significantly reduced. Short term operation effects without adequate oil lubrication can include an increase in the compressor power required due to increase frictional effects from the sliding components, a reduction in the flow output per compressor stroke due to a reduction in gas sealing, and an increase in frictional heat resulting in an increase of the compressor temperature. Both higher compressor power and reduced flow output can adversely affect vapor compression cycle system performance. Long term compressor operation without adequate oil lubrication can damage vital compressor components thus causing the compressor to fail. 
     Therefore, there is a need in the art for an orientation independent compressor and an orientation independent vapor compression cycle system. 
     BRIEF SUMMARY 
     Embodiments of the subject invention pertain to a method and apparatus for an orientation independent compressor. Embodiments of the subject invention also relate to a method and apparatus for an orientation independent vapor compression cycle system. The subject compressor can be part of a vapor compression cycle system. Embodiments of the subject compressor can use one or more of a variety of working fluids, including, but not limited to, one or more gases, such as nitrogen, oxygen, hydrogen, and air, gas mixtures, and/or refrigerants such as r-134a, r-22, CO 2 , and NH 3 . Embodiments of the compressor can utilize positive displacement means to compress the vapor. In a specific embodiment, the compressor can incorporate an oil-lubricated rotary lobed type positive displacement compressor. In alternate embodiments, the compressor can operate on a different principle, such as a rotary compressor, a piston compressor, a screw compressor, a scroll compressor, or a centrifugal compressor. In a specific embodiment, the working fluid can be a refrigerant incorporating entrained oil. In a further specific embodiment, the working fluid can be a hydrogen fluorocarbon (HFC) refrigerant, such as r-134a, incorporating entrained oil, such as miscible lubricating oils. Examples of such miscible lubricating oils that can be used are mineral oils, Polyalkylene Glycol (PAG) oil, Alkylbenzene oil, and Polyol Ester (POE) oil. 
     In accordance with embodiments of the subject invention, proper compressor lubrication and operation is achieved by the oil-entrained working fluid vapor entering the compressor. Preferred embodiments can achieve proper compression lubrication without an oil separation mechanism and without the need for an oil sump to collect the separated oil. In accordance with embodiments of the subject invention, the oil-vapor mixture remains as a mixture upon entering and exiting the compressor within a flow path that does not allow significant amounts of, if any, oil to collect, so as to reduce the mass flow rate of oil entrained in the oil-entrained working fluid entering the compressor in a way so as to not adequately lubricate the compressor independent of the orientation of the compressor, with respect to the surrounding gravitational field. 
     The oil-vapor flow path can be achieved by actively minimizing the internal volumes of the compressor that can potentially fill with separated oil. When oil fills into such internal volumes, the oil loses contact with the working fluid due to the localized reduction in vapor velocity through the internal volume of flow path such that the oil in such internal volumes does not remain entrained with the working fluid vapor. By reducing the amount of internal volume that oil can reside so as to avoid the forces of the moving working fluid vapor, enough of the oil by volume is circulated in the working fluid though the vapor compression cycle and entrained in the flow path for the working fluid vapor and oil mixture at the compressor inlet and outlet, such that proper compressor lubrication can be achieved. In specific embodiments, more than 70%, more than 80%, and more than 90%, respectively, of the oil by volume is circulated in the working fluid through the vapor compression cycle and entrained in the flow path for the working fluid vapor, independent of the orientation of the compressor with respect to the surrounding gravitational field. In further embodiments, the amount of the lubricating oil entrained in the working fluid vapor, or oil mass flow rate, at any orientation of the compressor with respect to the surrounding gravitational field is at least 80%, at least 90%, and at least 95%, respectively, of the maximum amount of the lubricating oil entrained in the working fluid vapor, or maximum oil mass flow rate, where the maximum amount of the lubricating oil entrained in the working fluid, or maximum oil mass flow rate vapor is achieved at one or more orientations of the compressor, or vapor compression cycle system, that results in a maximum mass flow rate of lubricating oil being entrained in the working fluid vapor. In this way, the mass flow rate of oil entrained remains within a certain range of a maximum mass flow rate of oil, based on the mass flow rate of oil in the compressor, or vapor compression cycle system, and the design of the compressor, or vapor compression cycle system, respectively. 
     Achieving sufficient velocity for the working fluid vapor can ensure the movement of the working fluid vapor keeps the oil entrained in the working fluid vapor through the compressor from the compressor inlet (or suction side) to the compressor outlet (or discharge side). Sufficient fluid velocities also ensure proper oil propagation in the flow path connecting the compressor to the components incorporated in the vapor compression cycle. The relationship of the pressure differential between the input to the compressor and the output of the compressor, the volume of the flow path from the input of the compressor to the output of the compressor, the length of the flow path from the input of the compressor to the output of the compressor and the cross-sectional area of the flow path can assure the adequacy of the velocity of the working fluid vapor through the flow path through the compressor. In a specific embodiment using r-134a as a working fluid, the compressor and compressor flow path is designed to achieve a working fluid vapor velocity of 0.1 m/sec to 5 m/sec, so as to entrain the lubricating oil in the flowing working fluid vapor. In specific embodiments, using r-134a as a working fluid, an oil-entrained working fluid vapor velocity of at least 2 m/sec; of at least 3 m/sec; and in a range of 5-7 m/sec, is achieved. In addition, the structure of the vapor fluid flow path can be designed to maintain the velocity of the oil-entrained working fluid vapor above the minimum vapor velocity to maintain oil entrainment in the oil-vapor mixture. Straight sections of the internal flow path are preferred and smooth surfaces are preferred. The typical operating surface Roughness Average (Ra) range varies from 16 micro-inch Ra (ground) to 250 micro-inch Ra (milled), with a typical value of 63 micro-inch Ra (milled). If a bend in the vapor flow path cannot be avoided, slower curving angles, such as less than 60 degrees, are preferred to sharper angles, which include those angles greater than 60 degrees from the fluid direction. In specific embodiments, the operating flow path angles remain in the range 20-45 degrees. Fluid vapor flow path angles can incorporate radii of curvature that keep the working fluid flowing smoothly. In specific embodiments, the radii of curvature is greater than 0.025″, and greater than 0.050″. 
     In order to maintain an adequate oil-vapor mixture velocity, compressor internal volumes, often unavoidable during manufacture and compressor assembly, can be partially, or completely, filled. Internal volumes that can cause oil to be removed from the flow can be minimized, when possible, prior to manufacture. Empty volumes inside the compressor can be avoided during construction of the compressor and flow path, or can be filled with various filler materials, such as metals, epoxies, plastics, and rubbers once construction is complete. With few, if any, empty volumes or pockets for the oil to collect, the oil remains mixed with the refrigerant vapor as it travels to and from the compressor, and results in an oil mass flow balance across the compressor and the entire vapor compression cycle. The mass flow rate of oil that enters the compressor is equivalent to the mass flow rate of oil that exits the compressor and requires no oil separation mechanism. 
     In further embodiments, the flow path of the working fluid and oil outputted from the compressor into a vapor compression cycle system can be designed using the same techniques previously mentioned to reduce or eliminate empty spaces that can gather oil in a way that would impact the oil entrained in the working fluid entering the compressor. Preferably, the mass flow rate of oil that exits the compressor flows through the flow path and enters the compressor independent of the orientation to the surrounding gravitational field. In a specific embodiment, the mass flow rate of oil that enters the rest of the vapor compression system from the output port of the compressor is equal to the mass flow rate of oil that enters the input port of the compressor from the vapor compression system and the vapor compression system does not include any means of active oil separation, thus enabling gravitational independence. In this way, oil does not build up in internal volumes connected to the flow path when the vapor compression cycle system is in a first orientation, so as to be removed from the flow through the flow path, and then release back into the flow path when the orientation of the vapor compression cycle system is changed to a second orientation. After compression, the oil-vapor mixture is then directed to the next component in the vapor compression cycle. Components of a vapor compression cycle system can include, for example, a condenser, an expansion device, an evaporator, one or more filters, one or more receivers, one or more accumulators, one or more by-pass valves, and one or more interconnection tubes or other interconnection apparatus. In a specific embodiment, the working fluid and oil are outputted by the compressor, pass through a condenser, then pass through an expansion device, and finally pass through an evaporator before being inputted back into the compressor. 
     Embodiments of the subject invention can enable proper compressor operation largely, or completely, independent of compressor orientation with respect to the gravitation field. Orientation independence is accomplished by maintaining adequate oil lubrication in many, if not all, possible geometric orientations by removing the oil separation mechanisms, oil sumps, oil bypass and bleed lines, and other means of oil separation incorporated in conventional compressors. With embodiments of the subject invention, the oil and vapor remain mixed through the implementation of a clearly defined oil-vapor flow path by filling in, reducing, and/or eliminating, empty volumes for oil collection to occur. Removing the oil separation mechanisms that are gravity dependent allows proper compressor operation independent of the compressors orientation, whether vertical, horizontal, or in any other orientation angle. 
    
    
     
       BRIEF DESCRIPTION OF DRAWINGS 
         FIG. 1  shows an embodiment of the subject invention, showing a cross-sectional view of a compressor attached to an electric motor with the clearly defined, non-separated, oil-vapor mixture flow path illustrated. 
         FIG. 2  shows a perspective, exploded view of an embodiment of a compressor in accordance with an embodiment of the subject invention. 
         FIG. 3  shows another perspective, exploded view of the embodiment of  FIG. 2 . 
         FIG. 4  shows a side view, with cut away, of the embodiment of  FIG. 2 . 
         FIG. 5  shows an embodiment of the subject invention, showing a cross-sectional view of a compressor using a shaft seal with the clearly defined, non-separated, oil-vapor flow path illustrated. 
         FIG. 6  shows a perspective, exploded view of an embodiment of the compressor in accordance with an embodiment of the subject invention. 
         FIG. 7  shows another perspective, exploded view of the embodiment of  FIG. 6 . 
         FIG. 8  shows a side view, with cut away, of the embodiment of  FIG. 6 . 
         FIG. 9  shows an embodiment of an evaporator in accordance with the subject invention. 
         FIG. 10  shows an exploded view of a specific embodiment of a compressor in accordance with the subject invention. 
         FIGS. 11A and 11B  show two views of a specific embodiment of an evaporator in accordance with the subject invention. 
         FIG. 12A  shows an inner wall piece with a spiral spacer and an outer wall piece with pin fins of a specific embodiment of a condenser in accordance with the subject invention. 
         FIG. 12B  shows the condenser shown in  FIG. 12A  with the inner wall piece into the outer wall piece to form a refrigerant annulus. 
         FIG. 13A  shows a schematic of a cooling system in accordance with the subject invention, incorporating a condenser, an expansion valve, an evaporator, and a compressor. 
         FIG. 13B  shows a basic vapor compression cycle temperature/entropy diagram. 
     
    
    
     DETAILED DISCLOSURE 
     Embodiments of the subject invention pertains to a method and apparatus for an orientation independent compressor. Embodiments of the subject invention also relate to a method and apparatus for an orientation independent vapor compression cycle system. The subject compressor can be part of a basic vapor compression cycle system using one or more of a variety of working fluids including, but not limited to, one or more gases, such as nitrogen, oxygen, hydrogen, and air, gas mixtures, and/or refrigerants such as hydrogen fluorocarbon (HFC) refrigerant, r-134a, r-22, CO 2 , or NH 3 . The compressor can utilize positive displacement means to compress the vapor. In a specific embodiment, the compressor can incorporate an oil-lubricated rotary lobed type positive displacement compression. In a specific embodiment, the working fluid can be a refrigerant incorporating entrained oil. In a further specific embodiment, the working fluid can be a refrigerant, specifically r-134a, containing entrained oil, such as miscible lubricating oils. Examples of such miscible lubricating oils that can be used are mineral oils, Polyalkylene Glycol (PAG) oil, Alkylbenzene oil, and Polyol Ester (POE) oil. The compressor requires oil for adequate lubrication so as to properly perform. A properly performing compressor is one in which required power and oil-vapor flow output are within acceptable levels needed for overall vapor compression cycle system operation. Inadequate lubrication can lead to higher required power, in addition to reduced flow output, both of which are unacceptable to proper performance. If a compressor is continued to operate with inadequate oil lubrication, compressor component accelerated wear and ultimately component failure can occur. 
     With respect to specific embodiments of the subject invention, proper compressor lubrication and operation is achieved without any oil separation mechanism and without an oil sump to collect the separated oil. This is in contrast to conventional compressors in which oil is contained and re-circulated between the compressor  50  and the oil separation mechanism after being separated and collected into an orientation dependent, gravity-fed oil sump or other gravity dependent oil storage vapor compression cycle component or device. By removing the oil separation mechanism needed to lubricate the compressor, orientation independence is achieved. While maintaining the oil-vapor mixture in the compressor as a mixture without any active oil separation mechanism either in the flow path first segment  30  leading to the inlet or the flow path second segment  35  leading to the outlet of the compressor in a clearly defined flow path, embodiments of the subject compressor is able to properly perform in any position, such as vertical, horizontal, or any other angled orientation. Specific embodiments can allow proper performance independent of angular rotation of the subject compressor as well as independent of the angle the compressor makes to the gravitational field. 
     In an embodiment, the oil-vapor mixture is kept as a mixture and is constrained within a clearly defined flow path by filling in empty volumes in the flow path after construction and actively minimizing the internal volumes in the design of the flow path prior to construction of the compressor, which can potentially fill with separated oil, such as when the localized vapor velocity falls below the minimum requirement to maintain oil entrainment. In an embodiment, this minimum is 2-3 m/s. In an embodiment, after filling in and minimizing empty internal volumes within the flow path, the sum of all the empty volumes in the flow path where the velocity is not enough to entrain the oil is less than 20 percent of the total value of the volume of the oil charge. 
     Empty volumes inside the compressor can be filled with various filler materials, such as metals, epoxies, plastics, rubbers, or any other filler material that is compatible with the mixture that is used in the particular vapor compression system  80 . During the design phase, the internal structure of the flow path is preferably designed to avoid vapor velocities below the acceptable minimum, by, for example, including but not limited to, minimizing the number of sharp directional changes, such as directional changes greater than 70 degrees; incorporating radii of curvature for any flow path angles i with a radii of 0.050 in. or greater; and yielding operating surfaces  19  having finishes on internal parts, with an operating surface  19  having a finish value or Roughness Average (Ra) in the range of 16 (ground) to 250 micro-inch Ra (milled). With few, or no, empty volumes or pockets for the oil to collect by actively and properly designing the internal flow path and filling in any empty volumes remaining after construction, the oil remains mixed with the refrigerant vapor as it travels to and from the compressor  50  and results in an oil mass flow balance across the compressor, preferably without an oil separation mechanism. The mass flow rate of oil that enters the compressor is equivalent to the mass flow rate of oil that exits the compressor, which is equivalent to the mass flow rate of oil that enters the rest of the vapor compression system  80  from the oil-flow balanced compressor and the mass flow rate of oil that returns to the compressor from the vapor compression system. 
     After compression, the oil-vapor mixture can then be directed to the next component in the vapor compression system. In specific embodiments, the same techniques of filling in and minimizing the internal volumes in the compressor flow path are applied to the components of the vapor compression system as well, such that the vapor compression system becomes gravity and orientation independent in the same manner as the orientation independent compressor. Further, in addition to being orientation independent with respect to the surrounding gravitational field, embodiments of the subject compressor and/or vapor compression cycle system can be orientation independent with respect to acceleration of the compressor and/or vapor compression cycle system. Specific embodiments can be orientation independent with respect to accelerations up to 2 times gravity, 3 times gravity, and 5 times gravity, respectively. 
     By minimizing empty volumes for oil to accumulate, the oil charge becomes critical as there is no oil separation mechanism and no sump or other extra spaces to collect any excess oil added to the vapor compression system. In a specific embodiment, the oil mass flow rate can range from 0.1-10% of the vapor mass flow rate, with the range for a further specific embodiment of approximately 1-2% of the vapor mass flow rate. An adequate oil quantity present in the oil-vapor mixture allows proper compressor performance, and can ensure proper operation of other components in the vapor compression system. A shortage of oil can result in improper compressor performance due to inadequate lubrication. However, excess oil, as a percentage of the vapor mass flow rate, can lead to performance degradation on other components in the vapor compression cycle system, such as a heat transfer reduction in the evaporator and/or condenser. 
     The oil-entrained working fluid vapor is input into a compressor head input port  12 , is compressed within the compressor head, and is output from the compressor head output port. In this way, in specific embodiments, the oil-entrained working fluid vapor can have an input pressure in the range of 20 to 100 psi upon entry of the compressor head and in the range of 150 to 350 psi upon exiting the compressor head. Other ranges can also be achieved for the input and output pressures. In specific embodiments, the output pressure to input pressure ratio can vary from 1.5 to 17.5. In specific embodiments, the differential between output pressure and input pressure can vary from 50 psi to 330 psi. 
     An embodiment of a compressor  50  in accordance with the subject invention is shown in  FIG. 1 .  FIG. 1  shows a cross-sectional view of a positive displacement compressor directly attached to an electric motor driving the compressor shaft. The oil-vapor mixture can enter from the bottom of the compressor at the compressor intake  1 , or input port. The oil-vapor mixture can then be directed up through the inside of the electric motor, through a first segment  30  of the flow path indicated by the flow arrows  2 . The oil-vapor mixture flow can be directed between the electric motor stator windings  3  and the electric motor rotor  4  that drives the compressor shaft  5 . The filler material  6  can fill in some, or all, of the empty spaces to clearly define the first segment of the oil-vapor flow path. The filler material can include metals, epoxies, plastics, rubbers, or any other material that is compatible with the oil-vapor mixture. In the specific embodiment, the filler material  6  is an epoxy to completely fill in the voids found in the electric motor stator windings  3  and a combination of aluminum and epoxy define the flow path through the inlet manifold  7 . In addition, epoxy can be used to fill in the gap between the top of the electric motor stator windings  3  and the bottom of the inlet manifold  7 . 
     After the oil-vapor mixture travels through the inlet manifold  7 , the oil-vapor mixture can enter into the compression housing  8 , through a compressor head input port  12 , and can be subsequently compressed by the compressor rotary lobe  9 . The compressed oil-vapor mixture can then be outputted out of the compressor head output port  18  and passed through the outlet manifold  10 . In the specific embodiment, the oil-vapor mixture is guided through a flow path in the outlet manifold  10  by filling in any extra volume with aluminum. The compressed oil-vapor mixture can then be exited through the outlet  11 , or output port, of the compressor and can be directed to further vapor compression system  80  components without any oil separation or accumulation having taken place within the compressor. The mass flow rate of oil that was entrained in the vapor at the inlet of the compressor  1  is equivalent to the mass flow rate of oil that is entrained in the vapor at the outlet  11  of the compressor  50 . This oil mass balance then enables orientation independent operation, as many, if not all, empty spaces in  3 ,  7 , and  10  were actively filled in with material to clearly define the non-separated, oil-vapor mixture flow path. 
       FIGS. 2 and 3  show perspective, exploded views from different angles of a specific embodiment of a compressor that is similar to the compressor shown in  FIG. 1 .  FIG. 4  shows a side view, with cut away, of the embodiment of  FIGS. 2 and 3 . The reference numbers on  FIGS. 2, 3, and 4  correspond to similar structures as referenced by the same reference numbers in  FIG. 1 , where reference number  6  tries to show some of the locations that can have filled spaces that were once empty spaces that could trap the lubricating oil. Advantageously, as compressors in accordance with the subject invention do not need oil sumps, the compressors shown in  FIGS. 1-4  can be operated, with appropriate modifications of the compressor head as needed, with the working fluid going in the opposite direction as shown in  FIGS. 1-4 . 
     In the embodiment shown in  FIG. 5 , a cross-sectional view of a positive displacement compressor is shown with a shaft seal  22  preventing the oil-vapor mixture from leaking down the compressor shaft  21 . The oil-vapor mixture can enter the compressor from a side inlet  23 , or compressor input port. After entering the compressor, the oil-vapor mixture is guided through a flow path through the inlet manifold  24 . Filler materials can be used in inlet manifold  24  to form the oil-vapor mixture flow path to reduce, or prevent any oil separation and accumulation. In the specific embodiment, the filler material used in  24  is a combination of epoxy and aluminum. Once passed through the inlet manifold  24 , the oil-vapor mixture can enter into the compression housing  25 , e.g., through a compressor head input port  12 , and can be subsequently compressed by the compressor rotary lobe  26 . The compressed oil-vapor mixture can then be outputted out of a compressor head output port  18  and passed through the outlet manifold  27  in a clearly defined path. In the specific embodiment, the oil-vapor mixture the flow path in the outlet manifold  27  is formed by filling in any extra volume with aluminum. The compressed oil-vapor mixture can then be exited through the outlet  28  of the compressor, e.g., compressor output port, and can be directed to further vapor compression system  80  components without any oil separation or accumulation having taken place within the compressor. The mass flow rate of oil that was entrained in the vapor at the inlet of the compressor  23  is equivalent to the mass flow rate of oil that is entrained in the vapor at the outlet of the compressor  50 . This oil mass balance then enables orientation independent operation, as many, if not all, empty spaces in  24  and  27  were actively filled in with filler material to clearly define the non-separated, oil-vapor mixture flow path. 
       FIGS. 6 and 7  show perspective, exploded views from different angles of a specific embodiment of a compressor that is similar to the compressor shown in  FIG. 5 .  FIG. 8  shows a side view, with cut away, of the embodiment of  FIGS. 6 and 7 . The reference numbers on  FIGS. 6, 7, and 8  correspond to similar structures as referenced by the same reference numbers in  FIG. 5 . Advantageously, as compressors in accordance with the subject invention do not need oil sumps, the compressors shown in  FIGS. 5-8  can be operated, with appropriate modifications of the compressor head as needed, with the working fluid going in the opposite direction as shown in  FIGS. 5-8 . 
     Empty volumes for oil to gather can also be reduced or eliminated in other components of the vapor compression cycle system, such as a condenser, an expansion device, an evaporator, and/or interconnecting tubes or other interconnection apparatus, such that these additional components and the flow path, having at least a first segment  30  and a second segment  35 , connecting the components to the compressor head do not gather oil in a way that makes the vapor compression cycle system&#39;s performance dependent on the orientation of the system with respect to the surrounding gravitational field. 
     Various embodiments of the subject invention can incorporate one or more of the following taught by U.S. Pat. No. 7,010,936: an evaporator, a compressor, a condenser, and a vapor compression cycle system, where the one or more components allow orientation independent operation of the vapor compression cycle system in accordance with the subject invention. In a particular embodiment, any of the compressors of  FIGS. 1-8  can be utilized with the vapor compression cycle system taught in U.S. Pat. No. 7,010,936, wherein the components of the system allow orientation independent operation of the system with respect to the orientation of compressor and/or system with respect to the surrounding gravitational field.  FIG. 9  shows an embodiment of an evaporator, as described in U.S. Pat. No. 7,010,936, that can be utilized in accordance with a vapor compression cycle system of the subject invention.  FIG. 10  shows an exploded view of a rotary lobe compressor, as described in U.S. Pat. No. 7,010,936, in accordance with an embodiment of the subject invention.  FIGS. 11A and 11B  show two views of an evaporator that can be used with an embodiment of the subject invention.  FIGS. 12A and 12  B show an embodiment of a condenser, as described in U.S. Pat. No. 7,010,936, that can be incorporated with an embodiment of the subject invention.  FIGS. 13A and 13B  show a schematic of a vapor compression cycle system utilized in a cooling system and a basic vapor compression cycle temperature/entropy diagram, respectively, as described in U.S. Pat. No. 7,010,936, which can be implemented in accordance with the subject invention. Each of these components, and the system, can be implemented to reduce, or eliminate, empty spaces that may cause lubricating oil to become unentrained, so as to reduce or eliminate unentrained oil in the vapor compression cycle system. In specific embodiments, the various embodiments of the compressor and/or vapor compression cycle system described in the subject application can be incorporated into a cooling system as described in U.S. Pat. No. 7,010,936, which is hereby incorporated by reference in its entirety, and in particular for its teaching of various components, including but not limited to, condenser, evaporator, compressor, and expansion device. 
     Evaporator  700 , shown in  FIG. 9 , can receive the cooled, compressed liquid refrigerant, which can travel through a connector tube and enter evaporator  700  via, for example, throttle device  760 . Expanding liquid cools and enters refrigerant evaporation path  780 . The refrigerant can exit the evaporator via port  750  and enter a connection tube that terminates at the compressor. The coolant that is to be cooled can enter the evaporator via a coolant connection tube and travel to coolant port  711 . A pump  512  can pump the coolant through the cooling path  770 . In a specific embodiment, pump  512  is built into the evaporator. Alternatively, a pump external to the evaporator can be utilized. The chilled coolant can exit the evaporator via fluid exit port  790  and flow out of a connection tube. 
     In an embodiment, referring to  FIG. 10 , the flow through the compressor can be controlled by inlet port  517  and valved exhaust ports  629 . In a specific embodiment, a triangular inlet port  517  design based on the rotational path of the rotor can be used on the bottom face of the compressor. Although a triangular shaped port is shown here, other shapes such as oval, round, and square can also be used. This design can allow the cool refrigerant vapor into the compressor. Rotor  624  can then travel over the top of the intake port so as to close the intake port as rotor  624  begins to compress the refrigerant vapor. This design feature can eliminate the need for an intake check valve, typically used by positive displacement compressors. Exhaust valve  618  and valve stop  616  can be placed on the top face of the compressor and positioned on top of the exhaust port  629  to allow for the maximum compression to occur. The exhaust valve is a check valve that can prevent hot high pressure refrigerant vapor from flowing backwards into the compressor. In a specific embodiment, cantilevered flapper valves can be used to reduce the amount of space required for the outlet port  629 . 
     To reduce the vibrations caused by the mass of the rotor spinning eccentrically in the compressor, a counter balance  635  can be placed on the main shaft. A second rotor can be used to balance the compressor. In embodiment the second rotor can be positioned 180° out of phase with the first rotor so as to counter balance the rotating force. The addition of the second rotor adds complexity to the compressor, but can double the mass flow rate for a given RPM speed. 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  614  and  628  while internal sealing of the compression chambers can be accomplished using, for example, a sealing gasket  622  or o-ring. 
     In an embodiment, referring to  FIGS. 12A and 12B , the fluid that the heat is rejected to can flow through the condenser due to the forces generated by, for example, wind, natural convection, fans, blowers, or compressors. In a specific embodiment, air can be blown into the condenser via, for example, a fan, such that air is blown into the condenser and removes heat from the extended surface features  860 . 
     The condenser can be, for example, a general purpose heat exchanger. On a first side of the heat exchanger the compressed hot refrigerant gas can flow and on a second side of the heat exchanger an external fluid can flow. Typically, ambient air or water can be used on the second side of the heat exchanger. The heat is transferred between the two fluids via dividing wall  870  such that an external fluid flowing on the outer surface, or heat transfer surface  880 , of dividing wall  870  will remove heat from dividing wall which has absorbed from the refrigerant flowing through the condenser. The design of the subject condenser can involve optimizing the heat transfer between the two fluids flowing on either side of dividing wall  870 . 
     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.