LOW PRESSURE RATIO PISTON COMPRESSOR

Abstract: A reciprocating compressor capable of producing a steady-state, continuous, non-pulsing outflow at volumes less than 25 gallons per hour. The compressor utilizes at least two pistons driven in a near axial manner with any lateral forces imparted to the compressor subsequently removed. The compressor is useful in a vapor compression distillate system but could also be adapted to pump liquids. A rotating cam is provided which through cam followers drives the pistons such that the compression stroke of one compensates for the vibrational force introduced into the apparatus by another piston caused by change in that piston's direction.

Description: LOW PRESSURE RATIO COMPRESSOR BACKGROUND OF THE INVENTION This invention relates generally to the technology of energy and liquid recycling and more particularly to an improved compressor apparatus for use in such technology. Such an improved compressor has great potential for use in vapor compression distillation and other applications in which low levels of vibration and steady output are desirable. Vapor compression distillation is well known and understood in the broader field of distillation of liquids. In a vapor compression system, a liquid supply is at least partially evaporated. The vapor extracted is then adiabatically compressed thus elevating the temperature at which the vapor will recondense to some value higher than its original evaporative temperature. When the vapor recondenses it returns all of the latent heat that originally went into evaporating it back to the system. The only energy placed into the system which is not recovered is the energy required to compress the vapor. Vapor compression distillers generally make use of centrifugal compression due to this process being simple, cost-effective, and fairly efficient. However, as the distiller is scaled downward, centrifugal compression becomes more problematic. Efficiency falls off rapidly below 25 gallons of distillate per hour. As the output of the distiller decreases so too does the efficiency of the centrifugal compressor. Compressors operating on the principle of reciprocation are more efficient in smaller sizes but generally are not suitable for vapor compression systems. Some of the problems associated with reciprocation are: 1) a piston-based compressor is more mechanically complicated and generally requires lubrication of the piston rings within the cylinder; 2) a piston-based compressor exhibits more severe wear characteristics; and 3) a piston-base compressor introduces pressure pulses due to the action of the piston. There is no theoretical lower output limit to a vapor compression distillation unit. However, the practical problems associated with low output vapor compression which limit its feasibility are due to: 1) inefficiencies in heat transfer between the vapor and the incoming liquid; and 2) the compressor design. Low output vapor compression distillation is desirable for small incoming liquid streams such as commonly occur in residential waste collection systems. By distilling the water from a household waste stream and recycling it for use in watering the lawn, the garden or even as potable water great savings in waste management will be gained. Other uses certainly abound for systems operating at volumes less than 25 gallons per hour. Many techniques exist with respect to improving heat transfer, but improvements to compressor design are not progressing forward at the same pace. What is needed is a compressor suitable to operate a small vapor compression distiller, one that will enable proper operation of a distiller even at levels as low as those producing a fraction of a gallon of distillate per hour. SUMMARY OF THE INVENTION The invention in its broad form resides in a compressor apparatus comprising a housing capable of being pressurized said housing having a plurality of chambers; a plurality of pistons, one slidably contained within each of said chambers for reciprocation; driving means for reciprocating said pistons within each chamber in a substantially axial direction without introducing lateral forces; means for introducing a vapor into a first of said chambers to be partially compressed by a first of said pistons; means for continuously pumping said compressed vapor from said first chamber successively through remaining of said plurality of chambers; means for removing said compressed vapor in a constant flow from a last of said chambers; and means for maintaining an interior of said housing at a pressure higher than ambient. A preferred embodiment of the present invention provides a positive displacement compressor suitable for use in a vapor compression distiller characterized by an output volume of less than 25 gallons per hour. Embodiments described hereinafter provide: (i) a compressor which produces a substantially steady output, (ii) a compressor that has the added ability to run with little or no lubrication in the piston cylinder, (iii) a compressor exhibiting minimal vibrational tendencies, (iv) a compressor suitable for use in a liquid waste disposal system, all of which may be adaptable to pump liquids. As described hereinafter, there is provided a positive displacement compressor in which two pistons are arranged co-axially within co-axially aligned piston cylinders. The pistons are driven by a cam and the piston strokes are timed to produce an even output flow. Lateral forces imposed by the cam on cam followers are absorbed by links which impart purely axial loads on the pistons. Substantial elimination of the lateral forces eliminate side loads, resultant wear, and the necessity of piston rings and added lubrication. By timing the pistons to move in opposite directions, the accelerations associated with reversing each piston's vector of travel counteracts one another so as to minimize vibration. BRIEF DESCRIPTION OF THE DRAWINGS The novel features considered characteristic of the invention are set forth in the appended claims. The invention itself, however, both as to its construction and its method of operation, together with additional objects and advantages thereof, will best be understood from the following description of the specific embodiments when read and understood in connection with the accompanying drawings. FIG. 1 is a cross-sectional elevation depicting one preferred embodiment of a compressor in accordance with a preferred embodiment of the invention; FIG. 2 is a view similar to FIG. 1 rotated ninety degrees; FIG. 3 is a top cross-sectional view of the FIG. 1 compressor; FIG. 4 is a cutaway detail view of a cam follower portion of the FIG. 1 embodiment; FIG. 5 is a diagrammatic cutaway view of a second preferred embodiment of a compressor in accordance with a preferred embodiment of the invention; FIG. 6 is a sectional view of FIG. 5 rotated ninety degrees; FIG. 7 is a diagrammatic view of a piston for use in a preferred embodiment of the invention; FIG. 8 is a diagrammatic view of a cam follower portion of the FIG. 5 embodiment; FIG. 9 is a cross-sectional elevation depicting a third preferred embodiment of axial driving means for use in a compressor in accordance with a preferred embodiment of the invention; FIG. 10 is a diagrammatic view of a drive cam used in each embodiment of the compressor; FIG. 11 is a depiction of the profile of the FIG. 8 drive cam over a single 360 degree revolution of the cam; FIG. 12 is a cross-sectional elevation of the compressor embodied within a vapor compression distillation unit; FIG. 13 is a cross-sectional elevation of the second embodiment of the compressor portion used in the FIG. 10 vapor compression distillation unit; and FIG. 14 depicts in cross-section the check valves associated with each piston. THE DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Overview of the Preferred Embodiments In FIG. 1, a compressor 1 comprises; a cylinder 3 divided into a first chamber 7 and a second chamber 9 by a dividing wall or partition 5, pistons 11 and 21 which are made to reciprocate respectively within the chambers 7 and 9, and means for driving the pistons in a substantially axial manner. It should be understood that though the compressor 1 has been described and will hereafter be described as having two pistons, the number of pistons utilized does not define the invention. The importance placed upon the number of pistons is based solely upon the ability of one piston's motion to be timed such that it counteracts another piston's motion thereby evening out flow and minimizing vibration. The steady state output and vibrationless operation of the compressor are the critical features of the described embodiment, not the number of pistons required to realize this. Though the use of a single piston would not seem to accommodate this requirement, other means for dampening vibration could be utilized in conjunction with means to create even flow. More appropriately, some number of pistons in excess of two would perform the function in a more direct fashion however the advantages gained by using a quantity of pistons in excess of two is not considered to be worth the added complexity. As such, two pistons are considered to be the most appropriate compromise between the desired function and complexity. Another critical aspect of this compressor is that it requires a means for driving each piston in a substantially axial direction. The term "substantially axial" refers to the requirement to provide a purely axial force to the piston perpendicular to the piston's face such that any non-axial forces are negligible. By eliminating side or lateral forces, the piston can be made to fit closely within the cylinder without resorting to the use of split piston rings. Some of the advantages gained by this form of drive means are: 1) little or no piston/cylinder lubrication is required; 2) the reduction in friction substantially reduces the need to compensate for the energy consumed as friction heat losses; and 3) the compressor can operate on less power since it does not need to compensate as much for friction losses. There are a number of possible ways to achieve this, some of which will be discussed as preferred embodiments, and all of which are considered to form a part of this invention. A 1st Preferred Means for Driving Pistons in a Substantially Axial Manner One preferred means for driving the pistons in a substantially axial manner comprises a rotating cam 17 driving a cam follower 13 via a roller 19, which in turn drives the piston 21 via a connecting rod 15. Similarly by looking at FIG. 2, it can be seen that the piston 11 is made to reciprocate in the chamber 7 by being driven by a cam follower 23 via rods 25, the cam follower 23 in turn is driven by the cam 17 via another roller 27. The pistons are driven in this manner to eliminate the introduction of side forces thus minimizing friction and wear, eliminating the need for split piston rings, and also reducing the clearance between the piston and cylinder side wall. The rods 15 and 25 are preferably rigidly affixed to their respective pistons. The rod 15 rides within a receiving pocket 41 within the cam follower 13 and each of the rods 25 in turn ride within similar receiving pockets 43 of the cam follower 23. The centers of rotation in each of the pockets 41 and 43 are made to oscillate about the axial centerline of the rod 15 and rods 25. Each cam follower is made to pivot about the cylinder side wall. For instance, looking to FIGs. 1 and 3, the cam follower 13 is depicted. A first end of the cam follower 13, that end opposite pocket 41 is arced. This arced surface 45 enables the cam follower to pivot against a suitable surface at the side wall of the cylinder. In FIG. 4, one manner of accomplishing this is depicted. A biasing means such as a spring 47 maintains contact between the arced surface 45 and the surface at the side wall of the cylinder. As such, the spring and the cam follower are coupled together by a coupling means such as a pin 49. The pin 49 passes through the cam follower 13 and rides in slots 51 and 53. The cam follower 23 is held in place in a similar fashion. A 2nd Preferred Means for Driving Pistons in a Substantially Axial Manner Another preferred means for driving the pistons in a substantially axial manner is depicted in FIGs. 5 and 6. To ease explanation, those items which remain substantially identical between each embodiment are identified with the same numbers. The items which are not identical but perform the same function are labeled with the same number followed by a prime ( ' ). Items which substantially differ between embodiments are given entirely different numbers. That being said, as in the first preferred embodiment, a rotating cam 17 drives a cam follower 13' which is maintained in continuous contact with the cam 17. In order to decrease friction between the two components yet provide for continuous but moving contact, a preferred means is to utilize a semi-spherical contact surface 20. This contact surface is formed as a profile within the cam follower 13' or alternatively comprises a sphere affixed within said cam follower or alternatively embedded within said cam follower but allowed to rotate therein. The desirable feature being that the friction between the two components should be minimized to reduce any power losses. Again, a cam follower 23' is also provided which operates the second piston in a similar manner. Rods 15 and 25 are provided to drive the pistons 11 and 21. The rods 25 perform the same function as the rods of the first embodiment, however, their relative placement as measured from the axial centerline of the rod 15 differs. Fundamentally, placement of the rods is not important so long as the piston is made to reciprocate within its cylinder and placement of the rods introduces negligible side loading. The rods 15 and 25 are also provided with a semi-spherical contact surface 40 similar to the surface 20. Means for receiving and slidably engaging the surface 40 are provided for in each of the cam followers 13' and 23'. A preferred configuration for said means would be a receiving socket 42. Interaction between the surfaces 40 and said surface's respective socket 42 would be in the manner of a ball and socket joint similar to that found in the human shoulder or hip. Each cam follower further comprises at one end an arced surface 45', the arced surface is toothed with a plurality of gear teeth 46. These gear teeth are made to ride in a mating set of rack teeth 48 disposed in or against the cylinder side wall. The arced surface 45' is curved such that it forms a sector of the pitch circle of the gear teeth 46. To further minimize friction between moving parts no requirements pertaining to gear face width are necessary. In other words, the gear teeth do not need to extend over the entire length of the arced surface 45' along the axial plane and can also contain non- toothed clearance regions. A 3rd Preferred Means for Driving Pistons in a Substantially Axial Manner A third means for driving the pistons in a substantially axial manner is depicted in FIG 7. This means requires the application of a magnetic field and the use of spring biasing means to oppose the magnetic force thus causing the pistons to reciprocate. The piston 11 is moved to a first position by a magnet 111 via a magnetic core 117 and the rod 15. When the magnetic core 117 is demagnetized, the piston is released. The piston is then pushed against the pressure head by a spring biasing means 115, thereby creating a compression stroke. Similarly, the piston 21 is operated by a magnet 109 via a magnetic core 121 and a sleeve 123 within which rod 15 reciprocates. When the piston 21 is released, it too is pushed against the pressure head by a biasing spring 113. The magnets 109 and 111 can be energized 180 degrees out of synchronization so that the pistons are moving in opposite directions. In the preferred embodiment of this compressor, the downward stroke of each piston takes more time than the upward stroke. Thus, there is no gap in the downward working strokes. The force on the pistons is constant over the stroke length so that a continuous flow of vapor is produced at constant pressure. At the present time, the second preferred means comprises the best mode of practicing the invention. It should be iterated that in reciting the various embodiments, concepts from each are cross-adaptable. Furthermore, other similar methods of driving the pistons in a substantially axial manner can be adapted for use in this invention. As such all alternative embodiments within the spirit of the invention are considered to form a part of the invention. Operation of the Compressor In any of the embodiments of the present invention which utilize two pistons, i.e., pistons 11 and 21, each piston is timed to perform its respective compression stroke in opposition to the other as explained more fully below. Timing of the pistons in this manner forms an important aspect of this invention. It tends to smooth out the functioning of the apparatus. If more than two pistons are utilized, the compression stroke of each additional piston will have to be adjusted appropriately to minimize vibration throughout the system. This is a straight forward concept utilized in many fields, including the field of internal combustion engines. Nevertheless, resorting to the preferred embodiment comprising two pistons, the cam 17 is depicted in FIG. 8 and its profile is depicted in FIG. 9. Looking at these FIGs. in conjunction with FIG. 1 , it can be seen that compression occurs as the pistons are moved away from the cam. The cam 17 drives the pistons against the biasing springs 29 and 31. Pressure is at its highest when the springs 29 and 31 are fully compressed. The pressure decreases as the springs relax. The spring 29 returns the piston 11 to its original position while the spring 31 returns the piston 21 to its original position. The profile of the cam 17 in conjunction with the spring constant of each of the springs 29 and 31 enable the speed of the compression stroke of each piston to remain constant and eliminate any significant period where neither piston is moving downward. By looking at FIG. 9 with respect to any one piston, for instance piston 11 , a pattern will emerge. The pattern is identical for each piston, it is only delayed by some factor for any subsequent number of pistons. Using as a reference base, the revolution of the cam 17, and starting at zero degrees of revolution, the following will occur. From zero degrees to 180 degrees, the piston is driven downward by the cam to form a compression stroke identified as 33 on the cam profile. The slope of the compression stroke as stated above is linear. The reversing and return portion 35 of the cam profile encompass the remaining 180 degrees of cam rotation. More specifically, at the end of the compression stroke or at the 180 degree mark, the direction of piston travel is reversed during a brief interval of overtravel labeled section 37. This reversal is accomplished in as short an interval as practical, so that by 270 degrees of cam rotation the piston is returned to its midpoint for its entire stroke length. Subsequently, the piston's direction of travel is reversed again when it reaches section 39 which also is accomplished in as short an interval as practical. The acceleration forces occurring at each piston travel reversal, i.e., sections 37 and 39 are made to be substantially equal in scale. The forces are induced at a point as close to 180 degrees apart as possible so that very little vibration occurs. By introducing the reversal forces in the latter 180 degrees of rotation of one piston, that piston is prevented from reversing before the other piston completes its compression stroke. The vibrational forces introduced by piston reversal are not compounded by having more than one piston incur them at any one time. By sequencing the compression strokes 33 and the reversing and return portion 35 of the stroke in this manner, vibration of the apparatus is greatly reduced. Though making the compression stroke last 180 degrees of revolution forms the preferred embodiment, a level of precompression can be introduced into the system by allowing the compression stroke of the piston 11 to extend more than 180 degrees. Since fluid enters the first chamber of the compressor and subsequently moves through the second chamber of the compressor, by forcing the piston 11 to continue with its compression stroke beyond 180 degrees of the cam revolution, the fluid will be compressed to a higher threshold prior to entering the second chamber. The fluid path through the apparatus begins when vapor flows into the compressor via a suitable path. The vapor enters the first chamber 7 through a flow control means such as a check valve 55 in the piston 11. At some point at or near the end of the compression stroke of the piston 11, the vapor enters the second chamber 9 through a check valve 57 of the piston 21. The now compressed fluid is pushed out of the chamber 9 by the piston 21 in a continuous fashion so that the outlet flow is substantially constant. Each of the check valves 55 and 57 would preferably comprise thin flexible washers that float within a defined cavity. Piston cylinder rings 59 and 61 are provided and held captive within the pistons 21 and 11 respectively. The check valves 55 and 57 seal against the piston rings. This construction eliminates a leak path between the piston and its respective piston ring which is usually found in conventional designs. To eliminate the need for lubrication other than that provided by the fluid, the piston rings should be made of a low friction polymer, such as polytetraflouroethylene (Teflon®), polyetheretherketone (PEEK®), or another polymer having similar characteristics. In fact, PEEK with Teflon impregnated therein provides the most suitable combination currently anticipated. Whereas the mechanical operation of the invention has been described above, in its preferred embodiment it can be utilized as a fluid compressor, a pump, or as a perfect example, a compressor within a vapor compression distillation system. Of course the apparatus can be adapted to provide higher compression ratios and thus its potential uses would increase. Turning now to FIG. 10, the apparatus is depicted as part of a simplified vapor compression distiller 63. The compressor 1 is installed in the cavity of a heat exchanger 65, which in one variation can be made in the form of a corrugated cylinder 66 comprising an outer evaporator surface 67 and an inner condensing surface 69. The entire cylinder 3 sits within an evaporator chamber 71 which is in turn sealed from a condenser chamber 73 by the corrugated cylinder 66. Vapor is drawn into the first chamber 7, passes through the check valve 55 into the first chamber 7, is compressed by the first piston 11, passes through the check valve 57 into the second chamber 9 where it is further compressed by the second piston 21. Upon being subjected to the second compression stage, the now compressed vapor exits the cylinder 3 through a suitable opening 75 into the condenser chamber 73 where it is condensed and removed via a drain port 77. The advantage to the drain port is that it eliminates manifolding and allows the use of larger check valves thereby minimizing pressure losses through the compressor. In fact, losses of efficiency in a compressor designed in this fashion are related to flow not friction. If the check valves 55 and 57 are made as large as practical, even approaching the size of the entire piston face, losses in efficiency are reduced. In order to operate more effectively as an evaporator, it is envisioned that the corrugated cylinder 66 be made to rotate while a thin film of liquid is applied to the evaporator surface 67. To rotate the device, a motor 79 is utilized which can also be adapted to provide a means for transmitting power to drive the cam 17 which as detailed above in turn drives the pistons within the compressor 1. One possible manner as illustrated in FIG. 10 depicts a plurality of gears 81 adapted to drive a shaft 83 which in turn drives a rotating tray 85 via an attached pinion 87. Affixed to the shaft 83 is a pinion 91, which engages a ring gear 89. The rotating tray 85 drives a plurality of applicator mechanisms that apply liquid to the evaporator surface 67 while the ring gear 89 drives a set of wiper mechanisms that remove condensate from the condensing surface 69. The shaft 83 can also be adapted to drive a gear pump 93 which pumps a liquid from a sump 95 via a port 97 to be delivered to a tray 85 from where it is distributed to the applicator mechanisms for subsequent evaporation. As such the method of making and using the device described above constitutes the preferred embodiment and alternative embodiments of the invention. The inventor is aware that numerous configurations of the device as a whole or some of its constituent parts are available which would provide the desired results. While the invention has been described and illustrated with reference to specific embodiments, it is understood that these other embodiments may be resorted to without departing from the invention. Therefore the form of the invention set out above should be considered illustrative and not as limiting the scope of the following claims.

Claims: CLAIMS 1. A compressor apparatus comprising: a housing capable of being pressurized said housing having a plurality of chambers; a plurality of pistons, one slidably contained within each of said chambers for reciprocation; driving means for reciprocating said pistons within each chamber in a substantially axial direction without introducing lateral forces; means for introducing a vapor into a first of said chambers to be compressed by a first of said pistons; means for continuously pumping said compressed vapor from said first chamber successively through remaining of said plurality of chambers; means for removing said compressed vapor in a constant flow from a last of said chambers; and means for maintaining an interior of said housing at a pressure higher than ambient. 2. Apparatus as in claim 1 wherein said driving means comprise a plurality of piston rods affixed to said pistons at a first end, in operational engagement with a transmission means for transmitting power from a power source at a second end. 3. Apparatus as in claim 2 wherein said transmission means comprise: a plurality of magnetic poles defining a magnetic field space therebetween, within which said second ends of said piston rods are placed and caused to axially reciprocate from a first position to a second position by energizing said magnetic poles; and a plurality of biasing springs engaging said pistons to move said pistons from said second position to said first position upon de-energizing said magnetic poles. 4. Apparatus as in claim 2 wherein said transmission means comprise: at least one rotating cam driven by said power source; and a plurality of cam followers each in continuous sliding contact with at least one of said cams, each of said cam followers further in continuous sliding contact with one of said piston rod second ends; wherein rotation of the cam is translated to reciprocating motion by the cam followers imparting said reciprocating motion in turn to said pistons; and wherein non-axially directed forces are dissipated by the sliding interactions between said cam, said cam followers, and said piston rod second ends. 5. A compressor apparatus comprising: a housing capable of being pressurized having a first chamber and a second chamber; a first piston contained within said first chamber and a second piston contained within said second chamber; a plurality of piston rods each having a first and a second end, at least one piston rod rigidly affixed to each piston at said first end; a rotating cam affixed to and driven by a power source; a first and a second cam follower each in continuous sliding contact with said cam at a cam contacting surface and each further in continuous sliding contact with at least one of said piston rod second ends at a piston rod contacting surface, wherein said cam followers translate the cam's rotational motion to a reciprocating motion which in turn is imparted to said pistons through contact with said piston rods, and wherein forces in non-axial alignment with said piston rods are dissipated by the sliding interactions between said cam, said cam followers, and said piston rod second ends; means for introducing a fluid into said first chamber to be compressed by a compression stroke of said first piston; means for transferring said compressed fluid from said first chamber to said second chamber; means for removing said compressed fluid in a constant flow from said second chamber; and means for maintaining the interior of said housing at a pressure higher than ambient. 6. An apparatus as recited in claim 5 further comprising: a first working volume defined by an area bounded by said first chamber and said first piston; a second working volume defined by an area bounded by said second chamber and said second piston; wherein means for removing fluid from said second chamber is an unobstructed passage through said housing; and wherein motion of each of said pistons is timed to enable transfer of fluid from said first chamber to said second chamber such that fluid volumetric flow at said unobstructed passage through said housing is steady-state and continuous. 7. Apparatus as recited in claim 6 wherein said pistons are of identical mass; and said cam is profiled to time the compression stroke of each piston to cancel out forces induced into the apparatus by changes in direction of the opposite piston between the end of the compression stroke and the beginning of the next compression stroke of the opposite piston. 8. Apparatus as recited in claim 5 wherein motion of each of said pistons is timed to enable transfer of fluid from said first chamber to said second chamber such that fluid volumetric flow exiting said second chamber is constant. 9. An apparatus as recited in claim 5 wherein said pistons are of identical mass; and said cam is profiled to time the compression stroke of each piston to cancel out forces induced into the apparatus by changes in direction of the opposite piston between the end of the compression stroke and the beginning of the next compression stroke of the opposite piston. 10. Apparatus as recited in claim 9 for use in a vapor compression distillation system wherein; said fluid originates in an evaporative stage of said vapor compression distillation system and is at atmospheric pressure upon entry into said first chamber; said fluid exits said second chamber at a pressure greater than atmospheric pressure and enters a condensing stage of said vapor compression distillation system. 11. Apparatus as recited in claim 5 wherein means for removing fluid from said second chamber is an unobstructed passage through said housing. 12. Apparatus as recited in claim 5 wherein said means for introducing a fluid into said first chamber and said means for transferring said partially compressed fluid from said first chamber to said second chamber comprise pressure activated check valves. 13. Apparatus as recited in claim 12 wherein said check valves are within said pistons. 14. Apparatus as recited in claim 5 wherein said moveable contact between components is accomplished by the use of a lubricated sphere rotatingly embedded in one of said components and interacting with the other of said components. 15. Apparatus as recited in claim 5 further comprising a spring biasing means operationally engaged with said pistons wherein said pistons are driven by said cam and this driving motion is opposed by said spring biasing means. 16. Apparatus as recited in claim 5 further comprising a spring biasing means operationally engaged with said pistons wherein said pistons are driven by said spring biasing means and this driving motion is opposed by said cam. 17. Apparatus as recited in claim 5 wherein said power source comprises a motor with a drive shaft, and said drive shaft is axially aligned with the direction of piston reciprocation. 18. An apparatus as recited in claim 5 for use in a vapor compression distillation system wherein; said fluid originates in an evaporative stage of said vapor compression distillation system and is at atmospheric pressure upon entry into said first chamber; said fluid exits said second chamber at a pressure greater than atmospheric pressure and enters a condensing stage of said vapor compression distillation system. 19. An apparatus as recited in claim 8 for use in a vapor compression distillation system wherein; said fluid originates in an evaporative stage of said vapor compression distillation system and is at atmospheric pressure upon entry into said first chamber; said fluid exits said second chamber at a pressure greater than atmospheric pressure and enters a condensing stage of said vapor compression distillation system. 20. A compressor apparatus contained within a vapor compression distillation apparatus having an evaporative stage and a condensing stage separated by a thin heat conducting material comprising: a housing containing a plurality of chambers therein; means for introducing a vapor into said housing; means for pressurizing said vapor within said housing; means for transferring said pressurized vapor from one chamber to another chamber; and means for removing vapor from said housing. 21. A compressor apparatus for compressing a fluid comprising: a single working volume; a plurality of moveable boundary means therein; and means for intake of a quantity of said fluid at continuous intervals into said single working volume to be first compressed by a first of said moveable boundaries and transparently passed at the higher pressure to each subsequent moveable boundary until said quantity of fluid reaches a last of said moveable boundaries; wherein said last moveable boundary receiving said quantities of said fluid at continuous intervals expels each quantity from said single working volume to an external environment; and wherein movement of said moveable boundaries permits each of said quantities of compressed fluid to flow through said subsequent moveable boundaries continuously such that movement of said last moveable boundary creates a pumping effect characterized by constant flow of said fluid to said external environment.

Inventors: ZEBUHR WILLIAM H, ZEBUHR, WILLIAM, H.
Applicants: OVATION PRODUCTS CORP, OVATION PRODUCTS CORPORATION
Application year: 1999
Main classification: F04B35
IPC codes: F01B3, F04B1, F04B3, F04B9, F04B23, F04B25, F04B35, F04B37, F04B41