Multi-stage scroll vacuum pumps and related scroll devices

Abstract
A multi-stage vacuum pump, expander, or compressor, that incorporates one or more stages of a fixed scroll(s) and orbiting scroll(s) that operates simultaneously. The motor drives the orbiting scroll(s) within the structure, and the various fixed and orbiting scrolls are arranged for either parallel generation of a vacuum or high pressure gas, or arranged in series for generating of a significantly high vacuum or gaseous pressure, or a combination of parallel arranged and series arranged fixed and orbiting scrolls may be embodied within the structure, operated by a single motor means, in order to attain the high efficiencies of operation as a vacuum pump, or a gaseous compressor, during its functioning. The various combinations of orbiting and fixed scrolls, when arranged as aforesaid, can be reduced in size, or miniaturized, and used in conjunction with small appliances, or even in hand-held instruments, as for example, for use in conducting mass spectrometry, or for other purposes. The actual structure of the multi-stage devices can include the fixed and orbiting scrolls adjacent the motor, or the singular motor may be located intermediate various stages of the formed vacuum pump/compressor, in its assembly.
Description
FIELD OF THE INVENTION

This invention is related to the field of vacuum pumps, expanders and compressors, and scroll type vacuum pumps, expanders and compressors in particular. The invention describes several inventive configurations for multi-stage scroll type vacuum pumps, expanders and compressors, for the purpose of achieving higher vacuums or pressures, including related scroll devices.


BACKGROUND OF THE INVENTION

Various stage vacuum pumps, and alternatively expanders, generally relate to devices that alter or reduce the pressure of gases within a container, typically to very low vacuums, or alternatively produce power as a gas expands. More specifically, these devices refer to multiple stages of scrolls that greatly increase the vacuums or pressures obtained during usage.


Scroll devices have been used as compressors, expanders and vacuum pumps for many years. In general, they have been limited to a single stage of compression due to the complexity of two or more stages, formed for compression, and for operation. In a single stage, a spiral involute or scroll upon a rotating plate orbits within a fix spiral or scroll upon a stationary plate. A motor shaft turns a shaft that orbits a scroll eccentrically within a fixed scroll and the eccentric orbit forces a gas through and out of the fixed scroll, thus creating a vacuum in a container in communication with the outlet from the fixed scroll. An expander operates under the same principle, only turning the scrolls in reverse, during their operations. When referring to compressors, it is understood that a vacuum pump can be substituted for a compressor, and that the expander can be an alternate usage when the scrolls operate in reverse from an expanding gas.


Often oil is used during manufacture and operations of compressors. Oil free or oil less scroll type compressors and vacuum pumps have difficult and expensive manufacturing, due to the high precision of the scroll in each pump and compressor. For oil lubricated equipment, swing links often minimize the leakage from gaps in the scrolls by allowing the scrolls to contact the plate of the scroll. Such links can not be used in an oil free piece of equipment because of the friction and wear upon the scrolls. If the fixed and orbiting scrolls and oil free equipment lack precision, leakage will occur and the equipment performance will decline as vacuums take longer to induce or do not arise at all.


Prior art designs have previously improved vacuum pumps, particularly in the design of the tips of the scrolls. In the preceding work of this inventor, U.S. Pat. No. 6,511,308, a sealant is applied to the two stage scrolls during manufacturing. The pump with the sealant upon the scrolls is then operated which distributes the sealant between the scrolls. The pump is then disassembled and lets the sealant cure. After curing the sealant, the pump is reassembled for use. During use, this patented pump only achieves a vacuum on the order of 100 mt.


In addition, the current inventor has a variety of patents that relate to two stage scroll devices. For example, Mr. Shaffer's U.S. Pat. No. 6,439,864, is upon a. Two Stage Scroll Vacuum Pump With Improved Pressure Ratio and Performance. The various stages of this pump and spiral involute wraps are of differing sizes in the different stages of the pump construction. This has an effect upon the compression ratio in the operations of the pump, in order to increase its efficiency.


Another patent to Shaffer, U.S. Pat. No. 7,942,655, discloses an advance scroll compressor, vacuum pump, and expander. This device uses bellows that spans between the fixed and orbiting scrolls and hermetically seals the scroll device during its functioning. The bellows also accommodates liquid cooling of the compressor during its operations.


A further patent to Mr. Shaffer, U.S. Pat. No. 8,523,544, shows another three stage scroll vacuum pump. This pump has three stages of fixed scrolls and orbiting scrolls that operate simultaneously. The structure of the scrolls, or the housing for the pump, incorporates fins that have the effect of a heat sink for disseminating the generated heat of the vacuum pump, during its operations.


A further published application of the inventor, U.S. 2011/0176948, discloses a semi-hermetic scroll compressor, vacuum pump, and expander. This invention also incorporated heat sinks upon its structure in order to increase the heat transfer from the compressor during its functioning.


A further published application of the inventor herein is upon a three stage scroll vacuum pump, published under No. U.S. 2011/02560074. This device incorporates magnetic couplings in order to attain the functioning of its orbiting scroll, so that atmosphere does not infiltrate the pump during its usage.


A unique aspect of the present disclosure is the use of a multi-stage scroll vacuum pump and/or compressor; that may be used to attain and is capable of achieving very high vacuums, (low absolute pressures), or high pressures for a multi-stage compressor that are very desirable for a number of applications.


Other U.S. patents have shown related technology, and U.S. Pat. No. 3,802,809, which issued to Vulliez, disclosed a pump having a scroll orbiting within its fixed scroll. Beneath the fixed disc, a bellows guides the gases evacuated from a container. The bellows spans between the involute and the housing, nearly the height of the pump. The pump and many other parts are cooled by ambient air in the vicinity of the pump.


The patent to Mulhouse, et al, U.S. Pat. No. 3,011,694, discloses an encapsulating device for expanders, compressors or the like. Thus, it shows an early multi type of compressor, pump or expander, as noted.


A patent to McCullough, U.S. Pat. No. 3,986,799, shows a fluid-cooled, scroll-type, positive fluid displacement apparatus. It utilizes stationary and orbiting scroll members of a scroll-type apparatus.


A further patent to McCullough, and the inventor herein, early on, U.S. Pat. No. 3,994,636, shows an axial compliance means with radial sealing for scroll-type apparatus.


A further patent to McCullough, et al, U.S. Pat. No. 4,192,152, shows another scroll-type fluid displacement apparatus with peripheral drive.


The patent to Hiraga, et al, U.S. Pat. No. 4,340,339, shows a scroll-type compressor with oil passageways through its housing.


The patent to Buttersworth, U.S. Pat. No. 4,415,317, discloses a wrap element and tip seal for use in fluid apparatus of the scroll-type. The purpose for the seal is to enhance the efficiency of operations of the device for both compression and for pumping purposes.


The patent to Eber, et al, U.S. Pat. No. 4,416,597, shows a further tip seal back-up member for use in fluid apparatus of the scroll-type.


The patent to Teegarden, U.S. Pat. No. 4,462,771, shows another improvement upon a wrap element and tip seal for use in fluid apparatus of the scroll-type and the method for making same.


The patent to Leclaire, et al, U.S. Pat. No. 4,718,836, shows a reciprocating completely sealed fluid-tight vacuum pump.


The patent to Nakamura, et al, U.S. Pat. No. 4,730,375, shows a method for the assembly of a scroll-type apparatus.


The patent to Kotlarek, et al, U.S. Pat. No. 4,867,657, shows a scroll compressor with axial balanced shaft.


Another patent to McCullough, et al, U.S. Pat. No. 4,892,469, shows a compact scroll-type fluid compressor with swing-link driving means.


The scroll-type fluid apparatus having sealing member in the recess forming the suction space, to Okada, et al, is disclosed in U.S. Pat. No. 5,160,253.


It should be noted that most of these prior art patents relate to a single plate pair for use within compressor apparatus.


A further patent to the inventor herein, Mr. Shaffer, U.S. Pat. No. 5,466,134, is upon a scroll compressor having idler cranks and strengthening and heat dissipating ribs. This is also upon a single plate pair for forming the scroll compressor.


Another patent to the inventor herein, Mr. Shaffer, is U.S. Pat. No. 5,632,612, shows a scroll compressor incorporating a tip seal.


The patent to Shin, et al, U.S. Pat. No. 5,632,613, shows a lubricating device for horizontal type hermetic compressor.


Another patent to Shaffer, U.S. Pat. No. 5,752,816, shows a scroll fluid displacement apparatus with improved sealing means.


A further patent to the inventor herein, U.S. Pat. No. 5,759,020, shows a scroll compressor having the tip seals and idler crank assemblies.


The patent to Liepert, U.S. Pat. No. 5,855,473, shows a displacement rate, scroll-type fluid handling apparatus.


The patent to Pottier, et al, U.S. Pat. No. 5,951,268, shows a spherical vacuum pump having a metal bellows for limiting circular translation movement.


A further patent showing various scrolls is disclosed in the patent to Claudet, U.S. Pat. No. 5,987,894, disclosing a temperature lowering apparatus using cryogenic expansion with the aid of spirals.


Another patent to the Inventor herein, U.S. Pat. No. 6,050,792, shows a multi-stage scroll compressor.


Another patent to the inventor herein, Mr. Shaffer, U.S. Pat. No. 6,129,530, discloses a scroll compressor with a two piece idler shaft and two piece scroll plates. This is just a plate pair forming a scroll compressor.


The patent to Fujioka, et al, U.S. Pat. No. 6,190,145, shows a further scroll fluid machine.


A patent to Lizuka, U.S. Pat. No. 6,379,134, discloses a scroll compressor having paired fixed and movable scrolls. This is a multi-scroll compressor that incorporates a pair of fixed scrolls, and orbiting scrolls.


A published application to Ni, U.S. 2007/0172373, shows a scroll-type fluid displacement apparatus with fully compliant floating scrolls.


The published application to Stehouwer, et al, No. U.S. 2009/0246055, shows a discharge chamber for dual drive scroll compressor.


These are examples of the prior art known to the applicant herein.


In some applications scroll-type vacuum pumps have notoriety for achieving high vacuums. A few large scroll vacuums pumps can achieve vacuums as high as 50 mt. However industry, science, and research still demands compact vacuum pumps, including compressors, that can yet achieve higher vacuums and high pressure gas.


The present invention overcomes the limitations of the prior art where the need exist for higher vacuums in equipment of compact form. That is, the art of the present disclosure, a multi-stage scroll vacuum pump, utilizes structure that allows for the generation of very high vacuums, when formed as a pump, or when constructed as a compressor can attain very high pressures, from smaller equipment, for use for operating more compact machinery and equipment, even in hand held devices, in both industrial and cooling and heating equipment, amongst other applications.


SUMMARY OF THE INVENTION

The concept of this invention is to present, in the examples as set forth, three multi-stage and one single stage vacuum pump configurations, each with unique advantages for achieving high vacuum levels in a small package.


Vacuum pumps that are capable of achieving very high vacuums are desirable in a number of applications as previously explained, such as in mass spectrometry. One way to achieve the higher vacuums is to use several stages in series. As previously reviewed in the background, several patents by the inventor herein have issued for a two stage and three stage scroll-type vacuum pump. However, there exist applications where a more compact, or higher vacuum is desirable, such as a hand held mass spectrometer device. Vacuum pumps for hand held mass spectrometers must be extremely compact and light of weight, as can be understood, while delivering very high vacuum levels with lower power consumption.


It needs to be noted herein, that while the examples as described, shown and set forth in this application, for the invention, is described as a vacuum pump, that concepts could just as easily be configured for use as a compressor for generating higher pressures.


The first design of this current invention is either a single stage or a two stage scroll vacuum pump of the spinning scroll or co-rotating scroll-type. The advantage of the spinning scroll is that the motion is pure rotation, so that the scrolls can be perfectly balanced. With the scrolls being balanced, very high rotational speeds are possible, resulting in a very compact vacuum pump, one that is highly efficient and effective of operations, and can be operated for lengthy periods of time. The spinning scroll can be configured as a single stage vacuum pump, when high vacuum is not needed, and as a two stage pump, or more, for higher vacuums.


The second design of the improvements as described herein is a three stage vacuum pump. This design incorporates a first and second stage pumping section operating in parallel, flowing into a third pumping stage arranged in series to the said first and second stages. The design is of the orbiting scroll type, which is the most common type scroll device. The advantages of this design is that large displacements (flow) are possible in a compact package due to the first and second stages being in parallel, while high vacuums are achievable within the third stage during its operations, which is arranged, as aforesaid, in series with the first two stages.


In a third design, this invention incorporates a four stage orbital type scroll vacuum pump. Once again, it could be incorporated and assembled into a four stage orbital compressor. This design has the first and second stages in parallel for high displacement (flow), and a third and fourth stage in series to attain ultra-high vacuums. This results in a relatively compact design for the generation of very high vacuums.


In a fourth design, a two stage in series design with a first stage being arranged closer to the motor so that a part of the motor is within the first stage, and the second stage is outboard of the motor. The flow of the gasses are similar to U.S. Pat. No. 6,439,864. The advantage of this configuration is a more compact design and lighter weight.


Regardless of the number of stages involved, the invention further incorporates a unique tip seal design related to spinning scroll technology that will self actuate into effective sealing due to the spinning motion of the scroll.


This invention also incorporates a method for aligning the scrolls to each other, for proper running clearance, when the Idler shafts are not present. This is particularly so when the pump or compressor is of the co-rotating type.


Once again the descriptions for a vacuum pump, and the designs as described herein could just as easily be made into a compressor, and the term “vacuum pump” and “compressor” will be used to mean either type of design, in the description of the developments herein. Obviously, when the orbiting scroll is moved in one direction, it functions as a pump, but when orbited in an opposite direction, can function as an expander.


It is, therefore, the principal object of this invention to provide a multi-stage scroll vacuum pump or gas compressor, that may provide various scrolls arranged in parallel, and/or in series, in order to attain the generation of very high vacuums, or very high gas pressure, and because of the multi stages of the structures involved, can be miniaturized in their structure and assembly, to minimize the space requirement for the use and application of these devices, even in smaller instrumentation such as for use in mass spectrometry and related applications.


Other objects may become more apparent to those skilled in the art upon review of the summary of the invention as provided herein, and upon undertaking a study of the description of its preferred embodiments, in view of the drawings.





BRIEF DESCRIPTION OF THE DRAWINGS

In referring to the drawings,



FIG. 1 provides a cross sectional view of the single stage spinning or co-rotating scroll vacuum pump/compressor design of this invention;



FIG. 1A provides a right end view of the design of FIG. 1;



FIG. 1B is a left end view of the design of FIG. 1;



FIG. 2 shows a cross sectional view of the two stage spinning scroll vacuum pump or compressor design of this invention;



FIG. 3 shows a cross sectional view of the three stage scroll vacuum pump or compressor design of this invention;



FIG. 4 shows a cross sectional view of the four stage vacuum pump or compressor design of this Invention;



FIGS. 5A through 5C shows a new compact clamping method and apparatus for the bellows of FIG. 1 and FIG. 2, which allows for clamping of the bellows within the same outer diameter of the bellows structure;



FIG. 6 discloses an innovative alignment method for maintaining the phase relationship and running clearances for the scrolls of this invention, when assembled as the spinning scroll type or an orbiting scroll type where idler shafts are not present for alignment, with FIG. 6 being a section taken along the line 6-6 of FIG. 7;



FIG. 7 shows an alignment method for maintaining the phased relationship and running clearances for the scrolls used in this invention, FIG. 7 taken along the line 7-7 of FIG. 1;



FIGS. 8A and 8B show an enlarged view of the tip seals used in the structure of the compressors/pump scrolls of this invention, generally as can be noted as located in FIG. 6 of this disclosure; and



FIG. 9 shows a cross section of a two stage pump or compressor of this invention.





Identification of the various components parts of the pump/compressor designs of this invention are as follows:


Referring to FIG. 1 and FIG. 5, the major component parts are:

    • 1. Driven scroll housing
    • 2. Shaft seal
    • 3. Driven scroll
    • 4. Bellows
    • 5. Drive scroll housing
    • 6. Drive scroll
    • 7. Drive Shaft
    • 8. Motor
    • 9. Back motor bracket
    • 10. Inlet port
    • 11. Port
    • 12. Cross hole
    • 13. Inlet plenum
    • 15. O-rings
    • 16. Port
    • 17. Hole or Passage
    • 18. Clamp
    • 19. Screws


Referring to FIG. 2, the major component parts are:

    • 29. Cross hole
    • 30. Outlet
    • 31. Bellows
    • 32. Second stage inlet plenum


Referring to FIG. 3, the major component parts are:

    • 33. Fixed scroll first stage
    • 34. Orbiting scroll first and second stage
    • 35. Fixed scroll second stage
    • 36. Orbiting scroll third stage
    • 37. Fixed scroll third stage
    • 38. Crankshaft
    • 39. Motor housing
    • 40. Motor
    • 41. Counterweight
    • 42. Idler shafts
    • 43. Inlet port
    • 44. Second stage location port
    • 45. Discharge plenum
    • 46. Port
    • 47. Third stage inlet plenum
    • 48. Annular air movement space
    • 49. Counterweight
    • 50. Eccentric


Referring to FIG. 4, the major components are:

    • 51. Fixed scroll first stage
    • 52. Orbiting scroll first and second stage
    • 53. Fixed scroll second stage
    • 54. Drive housing
    • 55. Motor housing
    • 56. Motor
    • 57. Fixed scroll third stage
    • 58. Orbiting scroll third and fourth stage
    • 59. Fixed scroll fourth stage
    • 60. Crankshaft and counterweight
    • 61. Motor drive shaft
    • 62. Idler shaft first stage
    • 63. Idler shaft third stage
    • 64. Crankshaft and counterweight
    • 65. Inlet port
    • 66. First and second stage inlet plenum
    • 67. Scroll passage
    • 68. Passage
    • 69. Annular air passage area
    • 70. Opening
    • 71. Port
    • 72. Third stage discharge plenum
    • 73. Fourth stage discharge port
    • 74. Cover
    • 75. Cover


Referring to FIGS. 6 and 7, the major components are:

    • 3. Driven scroll
    • 6. Drive scroll
    • 18. Bellows clamp
    • 19. Screws
    • 20. Hole
    • 21. Hole
    • 22. Hole
    • 23. Hole
    • 24. Plugs
    • 25. Plugs
    • 26. Fit


Referring to FIGS. 8A and 8B, the major components are:

    • 101. Involute
    • 100. Tip seal
    • 102. Tip seal
    • 103. Groove for o-ring


DESCRIPTION OF THE PREFERRED EMBODIMENT

In referring to the drawings, FIG. 1 shows a cross-sectional view of the single stage spinning or co-rotating scroll vacuum pump/compressor design of this invention. It includes the various components as previously identified, such as the driven scroll housing 1, provided with a shaft seal 2, and a driven scroll 3. Item 4 provides a bellows that surrounds the driven scroll, that seals the generated pressures, whether it be derived from a vacuum pump, or a compressor that generates high pressure, in its operations: A drive scroll housing 5 surrounds these operative components. The drive scroll 6 has its various scrolls interconnected with the driven scroll 3, as shown. A drive shaft 7, connects with the drive scroll 6, to provide for its rotation relative to the driven scroll, and the drive shaft 7 is rotated by means of the motor 8, as can be noted. There is a back motor bracket 9 that is provided for mounting of the motor, and its pump/compressor, in its configured assembly.


Gas to be evacuated or compressed enters the spinning scroll pump through the inlet port 10, in the driven scroll housing 1, as noted. The gas is sealed from leaking to the atmosphere through the rotary shaft seal 2, as disclosed. In this figure, two lip seals are shown, however, other type seals such as a labyrinth or mechanical seal can also be utilized. The gas enters the driven scroll 3 through the central port 11, as noted. The port 11 intersects a cross path 12, that directs the gas to the inlet plenum 13, on the peripheries of the arranged scrolls. The Inlet plenum 13 is bounded on the outside by the identified flexible bellows 4, which is sealed on its ends by use of the various o-rings 15, as can be noted. The gas then enters the scrolls, and is compressed, through the operations of said scrolls, and then discharged at the center of the drive scroll 6, as at its port 16. The gas then flows through the aperture 17, within the shaft 7, and is discharged to its site of usage. Obviously, the shaft 7 is turned by the motor 8. The bellows 4 performs the function of sealing the inlet chamber 13 from the atmosphere, and also maintains the phase relationship between the drive scroll 6, and the driven scroll 3, in its operations. The driven scroll 3 is driven by the bellows 4. The clamps 18 are designed so that the bellows 4 is retained without increasing the diameter of the assembly, thus keeping the entire pump very compact. As previously summarized, the concept of this invention is to provide for either a parallel arrangement of a series of scroll pump/compressors, or series arranged pump/compressors, or a combination of the two, which can provide for a very high generation of a pressure, or evacuation of a vacuum, within a small scale apparatus, that may even be accommodative of a hand-held type of device, during its usage and application.


The phase relationship between the two scrolls 3 and 6, and their alignment within its assembly is achieved by the alignment pins fixture as shown in FIG. 6, as subsequently described.


As previously described, FIG. 1A provides a left end view of the pump housing, as noted in FIG. 1, while FIG. 1B provides a right end view of the housing, particularly its back motor bracket 9, as previously defined.



FIG. 2 discloses a further modifications to the single stage scroll vacuum pump/compressor design of FIG. 1, but in this particular instance, it includes, in series, a second scroll vacuum pump or compressor design, as noted. In this particular Instance, the back motor bracket is integrally extended rearwardly, and mounts a second scroll vacuum pump or compressor design. As can be seen, the motor or drive shaft 7 further turns a driven scroll 27, which is held into position for eccentrically shifting by means of the clamps 18, that secure the o-rings 15 in position around the perimeter of the scroll plate. The high pressure or vacuum that is transferred through the passage 17, within the drive shaft 7, exits into the cross hole 29, then into the second stage Inlet plenum 32. At this point the gas is subjected to the operations of the movable scroll 27 and the driven scroll 28, and further increases in pressure, or generates further vacuum pressure, which then exits out of the passage 30, for use for purposes of such generated vacuum or compressed gas, as a result of operations of the scroll vacuum pump or compressor design of this invention. Once again, a bellows means 31 is provided between the clamps 18, to assure the hermetic sealing of the scroll compressor, therein, during its functioning. The various screws 19 cooperating with the clamps 18 secure the bellows 31 to the assembly.


This is an example of how a pair of co-rotating scrolls, maintained in series, can provide for a high efficiency in generating a vacuum, or a high pressure gas, in a fairly reduced dimensioned design, as noted and described herein.


The phase relationship between the two scrolls 3 and 6, as previously explained, as positioned within the assembly is achieved through usage of the alignment pin fixture, in the manner as to be subsequently described in FIGS. 6 and 7.


In FIG. 6, in addition to FIG. 7, the apertures 20 and 21 are precision located into the driven scroll 3. Likewise, the apertures 22 and 23 are precision located in the drive scroll 6. There are four such apertures 20-23, that are located such that when a close fitting pin is inserted into the apertures 20, thereby engaging the aperture 22, and another close fitting pin is inserted into the aperture 21, engaging the aperture 23, the alignment between the two scrolls will be precisely as desired so that the fit between the two scrolls will be maintained, and also so that the “phase” relationship between the scrolls is as required and desired for precise operation. In FIG. 7, the scroll and position of the drive scroll 6 relative to the drive scroll 3 must be properly aligned or “phased” for proper operation of the unit.


While the alignment pins are engaged, the bellows clamp 18 is positioned and bolted into place through usage of the screw 19, as previously described, so that the positioning of the scrolls 3 and 6 will be maintained after the alignment pins are removed. The final step is to seal the apertures 20 and 21 with plugs 24 and 25, so there will be no leakage of the vacuum generated gas or compressed gas to the atmosphere.



FIG. 8 shows the enlarged view of the tip seals located at the end of each scroll, generally as shown in the enlarged view identified at 8, in FIG. 6. This shows the enlarged views of two different tip seal designs for use in the spinning type scroll devices, vacuum pumps, compressors, or expanders. In describing the schematics as shown in FIGS. 8A and 8B, the centrifugal forces are shown as “R” and their direction of force as noted in said figure. This will cause the tip seals to jam in a traditional tip seal sense where the angle α is zero. By making the tip seal slides slightly tapered with an angle α greater than zero, the centrifugal forces in the “R” direction will cause a component of force in the axial direction “A”, thus forcing the tip seal to move in the “A” direction and engage the inner surface of the adjacent scroll, thereby effectively enhancing the sealing of any leakage from any pressure differential that exists across the involute, during its functioning.



FIG. 8A shows one embodiment of the invention where the tip seal 100 is trapezoidal of shape, and has the same a angle as the groove in the involute 101. FIG. 8B is the same as FIG. 8A, except the tip seal 102 has a groove 103 for placement of an o-ring cord stock therein, to further enhance the sealing activity of the scrolls, during their functioning.


In referring to FIG. 3, and as previously summarized, this design is shown in a three stage vacuum pump. The design incorporates its first and second stage pumping sections, that operate in parallel, providing for the transfer of its compressed gas for flow into a third pumping stage, arranged in a series, with the first and second stages. The design is of the orbiting scroll type, as known in the art. The advantage of this design is that large displacements, or flow, are possible in a compact package due to the first and second stages being arranged in parallel, while the high vacuums are achievable through the use of the third stage, arranged in series.


During its functioning, the gas to be evacuated or compressed enters the first stage fixed scroll 33, at its inlet port 43. The gas also enters the second stage at the location 44, in the orbiting scroll 34. The gas is then expanded in these first and second stages to the first and second stage discharge plenum 45. The gas then travels through the port 46, in the second stage fixed scroll 35, and into the third stage inlet plenum 47. The gas then enters into the third stage formed by the third stage fixed and orbiting scrolls 36 and 37, respectively. The gas is then compressed in the third stage and is discharged through the annular space 48 between the third stage fixed scroll and the crank shaft 37 and 38. The gas is then discharged through the housing 39, for further usage.


Counterweights are located at 49 and 41, to balance the orbital motion of the orbiting scrolls 34 and 36. The eccentric 50, located on the crank shaft 38, drives the orbiting scroll 36. Three idler shafts 42 are arranged and positioned approximately 120° apart from each other, around the second stage fixed scroll 35, and the third stage orbiting scroll 36, in addition to the orbiting scroll 34, that locate the orbiting scrolls 34 and 36 relative to the fixed scrolls 33, 35, and 37. The idler shafts 42 are supported by their ball bearings, as shown. The idler shafts 42 also serve to maintain the relative “phase” relationship between the fixed and orbiting scrolls, and also serve to drive the second stage orbiting scroll 34.


As noted in FIG. 4, this particular design is of a four stage orbital type Scroll vacuum pump. This design has the first and second stages in parallel, for high displacement, or flow, and then includes a third and fourth stage in series, for generating ultra-high vacuums. This results in a relatively compact unit, for this design, that generates ultra-high vacuums. It may also be structured as a pump or compressor.


In this four stage orbital type scroll vacuum pump or compressor, the gas to be evacuated enters the fixed scroll first stage 51, at the inlet port 65. The gas then travels into the first and second stage inlet plenum 66. The first and second stages are in parallel to increase the displacement of the pump while keeping the unit of compact design. After compression, the gas in the first stage travels through the port 71, and then into the passage 68 into the second stage. From there, the combined flow from the first and second stages travels through the annular area 69, as noted, formed by the crank shaft 60 and the fixed scroll second stage 53. The gas then travels past the motor 56 and into the opening 70. The gas enters the center of the third stage through the annular area formed by the crank shaft 64, and the fixed scroll third stage 57. After expansion, the gas enters the plenum 72, and is then compressed in the fourth stage, and exits the unit through the port 73, in the fixed scroll fourth stage. From there, the gas exits out of the port 73, as can be noted, after passing through the fourth compression stage.


There are three idler shafts 62 and 63 at each scroll pair, that are positioned so that any axial forces can be counteractive and for maintaining the axial positioning of the orbiting scrolls 52 and 58, and for attaining the “phase” relationship between the identified scrolls. The covers 74 and 75 are used to seal the openings in the fixed scrolls 51 and 57. The two orbiting scrolls 52 and 58 are driven by the motor 56, generally in the manner as previously described in earlier designs. The motor rotor turns the shaft 61, which has eccentric crank shafts 60 and 64, with their counterweights for balancing of the unit, during operations. These counterweights are noted at 60 and 64.



FIGS. 5A-5C show the various types of compact clamping means that are used for holding the ends of the bellows sealed in place, as previously shown and described in FIGS. 1 and 2.


In referring to FIG. 9, this shows a two stage orbital style scroll vacuum pump, but it may also be a pump, compressor, or expander. This design has first and second stages in series, but could have said stages in parallel, for generating ultra-high vacuums, pressures, and the like, as can be understood. This structure results in a very compact unit, for this design, and therefore may be made to much lessor dimensions. As noted, the pump 80 includes its structured orbital pump or compressor 81, rendered operative from its motor 82, and its first stage orbital type structures is noted at 83, while the second stage is defined at 04. The gas to be evacuated or pressurized enters the inlet 85 is conveyed past the motor 82 and its crank shaft 86 into the plenum 87 for processing by the first stage or the device. The processed air then passes to the second stage, for further pressuring or evacuation, or expansion, and is discharged through the outlet 88. An alternative inlet 89 may be provided for entering gas directly into the first stage, as can be noted. There are a series of idler shafts 90 that are located within the structure of the device and positioned so that the axial forces can be counteractive and for maintaining the axial positioning of the orbiting scrolls of the stages, for obtaining that phased relationship between the various scrolls. The covers 91 and 92 form the housing and are provided to seal the various scrolls, in their operations, within the said first and second stages, and the orbiting scrolls are rendered operative by the identified motor 82, as stated.


As reviewed throughout this discussion, while the description generally is made for a vacuum pump, formed of the designs of the structure as shown and identified herein, the units can just as easily be made into a compressor; and thus the terms “vacuum pump” and “compressor” are used interchangeably, to mean either type of multi-stage pumps or compressors. Essentially, it is the combination of the various scrolls either in parallel, or in series, or a combination of such, that form the multi-stage scroll devices of this invention.


Variations of modifications to the subject matter of this invention may occur to those skilled in the art upon review of the summary of the invention as provided herein, and upon undertaking a study of the description of its preferred embodiments in view of the drawings. Such variations, if within the spirit of this invention, are intended to be encompassed within the scope of any claims to patent protection issuing hereon. The description of the preferred embodiment, and its depiction in the drawings, are generally set forth for illustrative purposes only.

Claims
  • 1. A three-stage scroll device comprising: a housing;three fixed scrolls fixedly secured to the housing;three orbiting scrolls, each configured to interface with and orbit relative to a separate one of the three fixed scrolls, each pair of one fixed scroll and one orbiting scroll defining a stage;an eccentric drive shaft operably connected to at least one of the three orbiting scrolls, the eccentric drive shaft extending through at least one of the three fixed scrolls; andwherein two of the three stages are configured to receive a gas at a first pressure and discharge the gas at a second pressure higher than the first pressure, and a separate one of the three stages is configured to receive the gas at the second pressure and discharge the gas at a third pressure higher than the second pressure.
  • 2. The three-stage scroll device of claim 1, further comprising a motor in force-transmitting communication with the three orbiting scrolls.
  • 3. The three-stage scroll device of claim 2, wherein the eccentric drive shaft extends from the motor to one of the three orbiting scrolls, and further comprising a counterweight fixedly secured to the drive shaft.
  • 4. The three-stage scroll device of claim 1, wherein two of the orbiting scrolls extend in opposite directions from a single orbiting plate, and the single orbiting plate is connected to another of the orbiting scrolls via a plurality of idler shafts.
  • 5. A multi-stage vacuum pump comprising: a first fixed scroll;a second fixed scroll opposite from, spaced from, and facing the first fixed scroll, the first fixed scroll fixedly secured to the second fixed scroll;an orbiting plate positioned in between the first fixed scroll and the second fixed scroll, the orbiting plate having a first involute extending toward and interfacing with the first fixed scroll to form a first stage, and a second involute extending toward and interfacing with the second fixed scroll to form a second stage;a third fixed scroll fixedly secured to the second fixed scroll; andan orbiting scroll facing the third fixed scroll and having a third involute extending toward and interfacing with the third fixed scroll to form a third stage;wherein a first inlet of the first stage is in fluid communication with a second inlet of the second stage, and a first outlet of the first stage is in fluid communication with a second outlet of the second stage and a third inlet of the third stage via a chamber enclosed by a housing of the pump;wherein the first and second stages are configured to receive a gas at a first pressure and discharge the gas at a second pressure distinct from the first pressure, and the third stage is configured to receive the gas at the second pressure and discharge the gas at a third pressure higher than the second pressure.
  • 6. The multi-stage vacuum pump of claim 5, wherein the orbiting plate and the orbiting scroll are connected via at least one eccentric idler shaft.
  • 7. The multi-stage vacuum pump of claim 6, wherein the orbiting plate and the orbiting scroll are connected via three eccentric idler shafts.
  • 8. The multi-stage vacuum pump of claim 5, wherein the housing contains the first fixed scroll, the second fixed scroll, the orbiting plate, the third fixed scroll, and the orbiting scroll, and the chamber comprises a discharge plenum adjacent to the first outlet and adjacent to the second outlet and further comprises an inlet plenum adjacent to the third inlet.
  • 9. The multi-stage vacuum pump of claim 5, further comprising a motor secured to the third fixed scroll; andan eccentric drive shaft extending from the motor to the orbiting scroll, the eccentric drive shaft configured to cause the orbiting scroll to orbit relative to the third fixed scroll when the motor is in operation.
  • 10. The multi-stage vacuum pump of claim 9, further comprising at least one counterweight affixed to the drive shaft to balance the orbital motion of the orbiting scroll when the motor is in operation.
  • 11. The multi-stage vacuum pump of claim 5, wherein the each of the first fixed scroll, the second fixed scroll, the third fixed scroll, the first involute, the second involute and the orbiting scroll comprises a tip seal.
  • 12. The multi-stage vacuum pump of claim 11, wherein the tip seal has a trapezoidal cross-section.
  • 13. A multi-stage scroll compressor comprising: a first stage compressor comprising:a first fixed scroll,a first orbiting scroll configured to interface with and orbit relative to the first fixed scroll;a first gas inlet; anda first gas outlet;a second stage compressor comprising:a second fixed scroll fixedly secured to the first fixed scroll;a second orbiting scroll configured to interface with and orbit relative to the second fixed scroll;a second gas inlet; anda second gas outlet;a third stage compressor comprising:a third fixed scroll fixed secured to the second fixed scroll;a third orbiting scroll configured to interface with and orbit relative to the fixed scroll;a third gas inlet; anda third gas outlet;wherein the first gas inlet is in fluid communication with the second gas inlet, and the first gas outlet is in fluid communication with the second gas outlet and the third gas inlet, and wherein an eccentric drive shaft extends third orbiting scroll to orbit relative to the third fixed scroll and is configured to cause the third orbiting scroll to orbit relative to the third fixed scroll;wherein the first and second stages are configured to receive a gas at a first pressure and discharge the gas at a second pressure distinct from the first pressure, and the third stage is configured to receive the gas at the second pressure and discharge the gas at a third pressure higher than the second pressure.
  • 14. The multi-stage scroll compressor of claim 13, wherein the first fixed scroll is positioned opposite from and facing the second fixed scroll.
  • 15. The multi-stage scroll compressor of claim 14, wherein the first orbiting scroll and the second orbiting scroll extend from opposites sides of an orbiting plate positioned in between the first fixed scroll and the second fixed scroll.
  • 16. The multi-stage scroll compressor of claim 15, wherein the orbiting plate is connected to the third orbiting scroll by at least one eccentric idler shaft such that orbiting movement of the third orbiting scroll causes orbiting movement of the orbiting plate.
  • 17. The multi-stage scroll compressor of claim 16, further comprising: a motor secured to the third fixed scroll wherein the eccentric drive shall extends from the motor to the third orbiting scroll, and the motor rotates the eccentric drive shaft to cause the third orbiting scroll to orbit relative to the third fixed scroll.
  • 18. The multi-stage scroll compressor of claim 13, further comprising: a housing,wherein the second fixed scroll is fixedly secured to the first fixed scroll via the housing, and the third fixed scroll is fixedly secured to the second fixed scroll via the housing.
  • 19. The multi-stage scroll compressor of claim 13, wherein each of the first, second, and third fixed scrolls and each of the first, second, and third orbiting scrolls comprises a tip seal.
  • 20. The multi-stage scroll compressor of claim 13, wherein the first stage and the second stage are configured to compress a gas by a first amount, and the third stage is configured to further compress the gas by a second amount.
CROSS-REFERENCE TO RELATED APPLICATIONS

This non-provisional patent application claims priority as a divisional patent application to U.S. patent application Ser. No. 14/999,427, filed on May 4, 2016, which claims priority both to U.S. Provisional Patent Application Ser. No. 62/179,437, filed on May 7, 2015; and, as a continuation-in-part, to U.S. patent application Ser. No. 14/544,874, filed on Feb. 27, 2015, now U.S. Pat. No. 9,885,358, issued on Feb. 6, 2018, which is a continuation-in-part of U.S. patent application Ser. No. 13/987,486, filed on Jul. 30, 2013, now U.S. Pat. No. 9,028,230, issued on May 12, 2015, which is a divisional of U.S. patent application Ser. No. 13/066,261, filed on Apr. 11, 2011, now U.S. Pat. No. 8,523,544, issued on Sep. 3, 2013, which claims priority to the provisional patent application having Ser. No. 61/342,690, filed on Apr. 16, 2010.

US Referenced Citations (245)
Number Name Date Kind
801182 Creux Oct 1905 A
2079118 Hingst May 1937 A
2330121 Heintz Sep 1943 A
2968157 Cronan Jan 1961 A
3011694 Mulhouse et al. Dec 1961 A
3262573 Schutte Jul 1966 A
3470704 Kantor Oct 1969 A
3613368 Doerner Oct 1971 A
3802809 Vulliez Apr 1974 A
3842596 Gray Oct 1974 A
3874827 Young Apr 1975 A
3884599 Young et al. May 1975 A
3924977 McCullough Dec 1975 A
3986799 McCullough Oct 1976 A
3986852 Doerner et al. Oct 1976 A
3994633 Shaffer Nov 1976 A
3994635 McCullough Nov 1976 A
3994636 McCullough et al. Nov 1976 A
3999400 Gray Dec 1976 A
4065279 McCullough Dec 1977 A
4069673 Lapeyre Jan 1978 A
4082484 McCullough Apr 1978 A
4121438 McCullough Oct 1978 A
4129405 McCullough Dec 1978 A
4157234 Weaver et al. Jun 1979 A
4160629 Hidden et al. Jul 1979 A
4192152 Armstrong et al. Mar 1980 A
4199308 McCullough Apr 1980 A
4216661 Tojo et al. Aug 1980 A
4259043 Hidden et al. Mar 1981 A
4300875 Fischer et al. Nov 1981 A
4340339 Hiraga et al. Jul 1982 A
4382754 Shaffer et al. May 1983 A
4395205 McCullough Jul 1983 A
4395885 Cozby Aug 1983 A
4403494 McCullough Sep 1983 A
4411605 Sauls Oct 1983 A
4415317 Buttersworth Nov 1983 A
4416597 Eber et al. Nov 1983 A
4424010 McCullough Jan 1984 A
4436495 McCullough Mar 1984 A
4457674 Kawano et al. Jul 1984 A
4462771 Teegarden Jul 1984 A
4463591 McCullough Aug 1984 A
4472120 McCullough Sep 1984 A
4475346 Young et al. Oct 1984 A
4477238 Terauchi Oct 1984 A
4511091 Vasco Apr 1985 A
4512066 McCullough Apr 1985 A
4673339 Hayano et al. Jun 1987 A
4718836 Pottier et al. Jan 1988 A
4722676 Sugimoto Feb 1988 A
4726100 Etemad et al. Feb 1988 A
4730375 Nakamura et al. Mar 1988 A
4732550 Suzuki et al. Mar 1988 A
4802831 Suefuji et al. Feb 1989 A
4867657 Kotlarek et al. Sep 1989 A
4875839 Sakata et al. Oct 1989 A
4892469 McCullough et al. Jan 1990 A
4911621 McCullough et al. Mar 1990 A
4918930 Gaudet et al. Apr 1990 A
4927340 McCullough May 1990 A
5013226 Nishida May 1991 A
5037280 Nishida et al. Aug 1991 A
5040956 Barito et al. Aug 1991 A
5044904 Richardson, Jr. Sep 1991 A
5051075 Young Sep 1991 A
5051079 Richardson, Jr. Sep 1991 A
5082430 Guttinger Jan 1992 A
5099658 Utter et al. Mar 1992 A
5108274 Kakuda et al. Apr 1992 A
5127809 Amata et al. Jul 1992 A
5142885 Utter et al. Sep 1992 A
5149255 Young Sep 1992 A
5157928 Gaudet et al. Oct 1992 A
5160253 Okada et al. Nov 1992 A
5176004 Gaudet Jan 1993 A
5214932 Abdelmalek Jun 1993 A
5222882 McCullough Jun 1993 A
5224849 Forni Jul 1993 A
5228309 McCullough Jul 1993 A
5232355 Fujii et al. Aug 1993 A
5242284 Mitsunaga et al. Sep 1993 A
5247795 McCullough Sep 1993 A
RE34413 McCullough Oct 1993 E
5256042 McCullough et al. Oct 1993 A
5258046 Haga et al. Nov 1993 A
5265431 Gaudet et al. Nov 1993 A
5286179 Forni et al. Feb 1994 A
5314316 Shibamoto et al. May 1994 A
5328341 Forni Jul 1994 A
5338159 Riffe et al. Aug 1994 A
5343708 Gaudet et al. Sep 1994 A
5354184 Forni Oct 1994 A
5417554 Kietzman et al. May 1995 A
5443368 Weeks et al. Aug 1995 A
5449279 Hill et al. Sep 1995 A
5450316 Gaudet et al. Sep 1995 A
5462419 Hill et al. Oct 1995 A
5466134 Shaffer et al. Nov 1995 A
5496161 Machida et al. Mar 1996 A
5609478 Utter et al. Mar 1997 A
5616015 Liepert Apr 1997 A
5616016 Hill et al. Apr 1997 A
5632612 Shaffer May 1997 A
5632613 Shin et al. May 1997 A
5637942 Forni Jun 1997 A
5720602 Hill et al. Feb 1998 A
5746719 Ferra et al. May 1998 A
5752816 Shaffer May 1998 A
5759020 Shaffer Jun 1998 A
5800140 Forni Sep 1998 A
5803723 Suefuji Sep 1998 A
5836752 Calhoun et al. Nov 1998 A
5842843 Haga Dec 1998 A
5855473 Liepert Jan 1999 A
5857844 Lifson et al. Jan 1999 A
5873711 Lifson Feb 1999 A
5938419 Honma et al. Aug 1999 A
5951268 Pottier et al. Sep 1999 A
5961297 Haga et al. Oct 1999 A
5987894 Claudet Nov 1999 A
6008557 Dornhoefer et al. Dec 1999 A
6022195 Gaudet et al. Feb 2000 A
6050792 Shaffer Apr 2000 A
6068459 Clarke et al. May 2000 A
6074185 Protos Jun 2000 A
6098048 Dashefsky et al. Aug 2000 A
6129530 Shaffer Oct 2000 A
6179590 Honma et al. Jan 2001 B1
6186755 Haga Feb 2001 B1
6190145 Fujioka et al. Feb 2001 B1
6193487 Ni Feb 2001 B1
6213970 Nelson et al. Apr 2001 B1
6283737 Kazikis et al. Sep 2001 B1
6318093 Gaudet et al. Nov 2001 B2
6379134 Iizuka Apr 2002 B2
6434943 Garris Aug 2002 B1
6439864 Shaffer Aug 2002 B1
6460351 Gaudet et al. Oct 2002 B2
6461113 Gaudet et al. Oct 2002 B1
6464467 Sullivan et al. Oct 2002 B2
6511308 Shaffer Jan 2003 B2
6623445 Nelson et al. Sep 2003 B1
6644946 Nakane et al. Nov 2003 B2
6663364 Okada et al. Dec 2003 B2
6712589 Mori et al. Mar 2004 B2
6736622 Bush et al. May 2004 B1
6755028 Gaudet et al. Jun 2004 B2
6902378 Gaudet et al. Jun 2005 B2
6905320 Satoh et al. Jun 2005 B2
6922999 Kimura et al. Aug 2005 B2
7111467 Apparao et al. Sep 2006 B2
7124585 Kim et al. Oct 2006 B2
7144383 Arnett et al. Dec 2006 B2
7181928 de Larminat Feb 2007 B2
7234310 Flynn et al. Jun 2007 B2
7249459 Hisanaga et al. Jul 2007 B2
7297133 Nelson et al. Nov 2007 B2
7306439 Unami et al. Dec 2007 B2
7314358 Tsuchiya Jan 2008 B2
7439702 Smith et al. Oct 2008 B2
7458152 Sato Dec 2008 B2
7458414 Simon Dec 2008 B2
7836696 Uno et al. Nov 2010 B2
7861541 Dieckmann et al. Jan 2011 B2
7906016 Weber et al. Mar 2011 B2
7942655 Shaffer May 2011 B2
7980078 McCutchen et al. Jul 2011 B2
8007260 Yanagisawa Aug 2011 B2
8087260 Ogata et al. Jan 2012 B2
8186980 Komai et al. May 2012 B2
8328544 Iwano et al. Dec 2012 B2
8484974 Monson et al. Jul 2013 B1
8523544 Shaffer Sep 2013 B2
8668479 Shaffer Mar 2014 B2
8674525 Van Den Bossche et al. Mar 2014 B2
8858203 Kanizumi et al. Oct 2014 B2
9022758 Roof et al. May 2015 B2
9028230 Shaffer May 2015 B2
9074598 Shaffer et al. Jul 2015 B2
9657733 Chadwick et al. May 2017 B2
9784139 Shaffer et al. Oct 2017 B2
9885358 Shaffer Feb 2018 B2
1022185 Shaffer et al. Mar 2019 A1
10221852 Shaffer Mar 2019 B2
20010001639 Shaffer May 2001 A1
20010012485 Gaudet et al. Aug 2001 A1
20010038800 Kumura et al. Nov 2001 A1
20010043878 Sullivan et al. Nov 2001 A1
20020011332 Oh et al. Jan 2002 A1
20020039534 Moroi et al. Apr 2002 A1
20020071779 Moroi et al. Jun 2002 A1
20020094277 Gaudet et al. Jul 2002 A1
20020104320 Gaudet et al. Aug 2002 A1
20030017070 Moroi et al. Jan 2003 A1
20030051487 Gaudet et al. Mar 2003 A1
20030138339 Scancarello Jul 2003 A1
20030223898 Fujioka et al. Dec 2003 A1
20040020206 Sullivan et al. Feb 2004 A1
20040184940 Nakane et al. Sep 2004 A1
20040194477 Gaudet et al. Oct 2004 A1
20040255591 Hisanga et al. Dec 2004 A1
20050025651 Sowa et al. Feb 2005 A1
20050031469 Yanagisawa et al. Feb 2005 A1
20050081536 Gaudet et al. Apr 2005 A1
20050196284 Gaudet et al. Sep 2005 A1
20050220649 Sato Oct 2005 A1
20060016184 Simon Jan 2006 A1
20060045783 Yanagisawa et al. Mar 2006 A1
20060130495 Dieckmann et al. Jun 2006 A1
20070071626 Tsuchiya et al. Mar 2007 A1
20070104602 Ishikawa et al. May 2007 A1
20070108934 Smith et al. May 2007 A1
20070172373 Ni Jul 2007 A1
20070231174 Ishizuki Oct 2007 A1
20080159888 Nakayama et al. Jul 2008 A1
20080193311 Helies Aug 2008 A1
20080206083 Suefuji et al. Aug 2008 A1
20090148327 Carter et al. Jun 2009 A1
20090246055 Stehouwer et al. Oct 2009 A1
20100044320 Weber et al. Feb 2010 A1
20100111740 Ni May 2010 A1
20100254835 Kane et al. Oct 2010 A1
20100287954 Harman et al. Nov 2010 A1
20110129362 Kameya et al. Jun 2011 A1
20110256007 Shaffer Oct 2011 A1
20120134862 Hockliffe et al. May 2012 A1
20130149179 Sato et al. Jun 2013 A1
20130207396 Tsuboi Aug 2013 A1
20130232975 Shaffer et al. Sep 2013 A1
20140023540 Heidecker et al. Jan 2014 A1
20140260364 Litch Sep 2014 A1
20170045046 Afshari Feb 2017 A1
20170051741 Shaffer et al. Feb 2017 A1
20170074265 Asami et al. Mar 2017 A1
20170268514 Shaffer Sep 2017 A1
20170284284 Takamiya Oct 2017 A1
20170306956 Monet Oct 2017 A1
20170321699 Kawano et al. Nov 2017 A1
20170362962 Shaffer et al. Dec 2017 A1
20180163725 Valdez et al. Jun 2018 A1
20180163726 Shaffer et al. Jun 2018 A1
20180216498 Shaffer et al. Aug 2018 A1
20200040892 Dieckmann et al. Feb 2020 A1
Foreign Referenced Citations (24)
Number Date Country
104235018 Dec 2014 CN
104632636 May 2015 CN
105402134 Mar 2016 CN
460936 Jun 1928 DE
19957425 Aug 2000 DE
0513824 Nov 1992 EP
0780576 Jun 1997 EP
1464838 Oct 2004 EP
3239526 Nov 2017 EP
0513827 Oct 1939 GB
2002455 Feb 1979 GB
1575684 Sep 1980 GB
S56-019369 Feb 1981 JP
S57-171002 Oct 1982 JP
H05-157076 Jun 1993 JP
H07-109981 Apr 1995 JP
H07-324688 Dec 1995 JP
H08-261182 Oct 1996 JP
2000213475 Aug 2000 JP
2011-012629 Jan 2011 JP
WO 2004008829 Jan 2004 WO
WO 2009050126 Apr 2009 WO
WO 2015164453 Oct 2015 WO
WO 2017089745 Jun 2017 WO
Non-Patent Literature Citations (68)
Entry
English translation of JP-2000213475 by J Piat Pat Jul. 31, 2020.
“Operating Manual: OM WGZC-2 Water-Cooled Scroll Compressor Chillers,” McQuay International, 2010, 102 pages.
“R410A // Hermetic Scroll Compressors,” Bitzer, 2016, 12 pages.
“Refrigeration Technologies: scroll-compressor chillers,” Misto, last modified Jan. 2013, 7 pages.
Notice of Allowance for U.S. Appl. No. 15/330,223, dated Jan. 23, 2020 10 pages.
Official Action for U.S. Appl. No. 15/932,150, dated Nov. 25, 2019 26 pages.
Official Action for U.S. Appl. No. 15/932,150, dated Mar. 5, 2020 19 pages.
Official Action for U.S. Appl. No. 15/732,593, dated Nov. 14, 2019 7 pages Restriction Requirement.
Official Action for U.S. Appl. No. 15/732,593, dated Feb. 19, 2020 13 pages.
“Digital Scroll Compressor Technology,” Wikipedia, 2010, 3 pages [retrieved online from: en.wikipedia.org/wiki/Digital_Scroll_Compressor_Technology].
Official Action for U.S. Appl. No. 15/731,929, dated Jun. 4, 2019 10 pages.
Notice of Allowance for U.S. Appl. No. 15/731,929, dated Aug. 14, 2019 9 pages.
Notice of Allowance for U.S. Appl. No. 15/731,324, dated Aug. 2, 2019 11 pages.
Notice of Allowance for U.S. Appl. No. 15/373,979, dated Apr. 26, 2019 9 pages.
Official Action for U.S. Appl. No. 16/275,943, dated Oct. 9, 2020 15 pages.
Official Action for U.S. Appl. No. 16/213,111, dated Sep. 30, 2020 22 pages.
Notice of Allowance for U.S. Appl. No. 15/732,593, dated Aug. 13, 2020 9 pages.
“Heat Pump and Refrigeration Cycle,” Wikipedia, last updated May 10, 2013, 4 pages [retrieved online from: en.wikipedia.org/wiki/Heat_pump_and_refrigeration_cycle].
“Involute,” Wikipedia, last modified Jun. 2, 2012, 5 pages [retrieved online from: en.wikipedia.org/wiki/Involute].
“Oldham Coupler,” Wikipedia, last modified, Feb. 9, 2010, 2 pages [retrieved online from: en.wikipedia.org/wiki/Oldham_coupler].
“Organic Rankine Cycle,” Wikipedia, last modified May 19, 2013, 4 pages [retrieved online from: en.wikipedia.org/wiki/Organic_Rankine_Cycle].
“Rankine Cycle,” Wikipedia, last modified Apr. 29, 2013, 4 pages [retrieved online from: en.wikipedia.org/wiki/Rankine_cycle].
“Scroll Compressor,” Wikipedia, last modified Apr. 24, 2013, 3 pages [retrieved online from: en.wikipedia.org/wiki/Scroll_compressor].
“Thrust Bearing,” Wikipedia, last modified Dec. 19, 2012, 2 pages [retrieved online from: en.wikipedia.org/wiki/Thrust_bearing].
International Search Report and Written Opinion for Interiantional (PCT) Patent Application No. PCT/US2018/064427, dated Feb. 5, 2019 14 pages.
International Search Report for International (PCT) Patent Application No. PCT/US01/43523, dated Jun. 5, 2002 1 page.
International Search Report for International (PCT) Patent Application No. PCT/US01/50377, dated May 13, 2002 1 page.
Partial Search Report for European Patent Application No. 13003663.5, dated May 28, 2014 5 pages.
Extended Search Report for European Patent Application No. 13003663.5, dated Sep. 3, 2014 11 pages.
International Search Report and Written Opinion for International (PCT) Patent Application No. PCT/US14/00076, dated Dec. 17, 2014 6 pages.
International Search Report and Written Opinion for International (PCT) Patent Application No. PCT/US18/00118, dated Sep. 24, 2018 19 pages.
Official Action for U.S. Appl. No. 11/703,585, dated Dec. 18, 2009 7 pages.
Official Action for U.S. Appl. No. 11/703,585, dated Jul. 20, 2010 7 pages.
Notice of Allowance for U.S. Appl. No. 11/703,585, dated Feb. 4, 2011 4 pages.
Official Action for U.S. Appl. No. 12/930,140, dated Jan. 14, 2013 22 pages.
Official Action for U.S. Appl. No. 12/930,140, dated Jun. 13, 2013 21 pages.
Notice of Allowance for U.S. Appl. No. 12/930,140, dated Oct. 24, 2013 12 pages.
Official Action for U.S. Appl. No. 13/066,261, dated Feb. 11, 2013 5 pages Restriction Requirement.
Notice of Allowance for U.S. Appl. No. 13/066,261, dated Apr. 4, 2013 13 pages.
Official Action for U.S. Appl. No. 13/987,486, dated Dec. 16, 2013 5 pages Restriction Requirement.
Official Action for U.S. Appl. No. 13/987,486, dated Apr. 23, 2014 13 pages.
Official Action for U.S. Appl. No. 13/987,486, dated Oct. 20, 2014 11 pages.
Notice of Allowance for U.S. Appl. No. 13/987,486, dated Jan. 5, 2015 5 pages.
Corrected Notice of Allowance for U.S. Appl. No. 13/987,486, dated Feb. 20, 2015 8 pages.
Official Action for U.S. Appl. No. 14/544,874, dated Dec. 23, 2016 5 pages Restriction Requirement.
Official Action for U.S. Appl. No. 14/544,874, dated Jan. 26, 2017 9 pages.
Official Action for U.S. Appl. No. 14/544,874, dated Jul. 21, 2017 6 pages.
Notice of Allowance for U.S. Appl. No. 14/544,874, dated Sep. 28, 2017 5 pages.
Official Action for U.S. Appl. No. 15/330,223, dated Nov. 15, 2017 6 pages Restriction Requirement.
Official Action for U.S. Appl. No. 15/330,223, dated Feb. 7, 2018 10 pages.
Official Action for U.S. Appl. No. 15/330,223, dated Aug. 7, 2018 10 pages.
Official Action for U.S. Appl. No. 15/330,223, dated Jan. 11, 2019 14 pages.
Official Action for U.S. Appl. No. 14/507,779, dated Apr. 8, 2014 17 pages.
Official Action for U.S. Appl. No. 13/507,779, dated Dec. 1, 2014 17 pages.
Notice of Allowance for U.S. Appl. No. 14/507,779, dated Mar. 6, 2015 8 pages.
Official Action for U.S. Appl. No. 13/986,349, dated Jan. 21, 2015 25 pages.
Official Action for U.S. Appl. No. 13/986,349, dated Aug. 12, 2015 20 pages.
Official Action for U.S. Appl. No. 14/756,594, dated Mar. 29, 2017 13 pages.
Notice of Allowance for U.S. Appl. No. 14/756,594, dated Jun. 5, 2017 8 pages.
Official Action for U.S. Appl. No. 15/731,929, dated Jan. 31, 2019 11 pages.
Official Action for U.S. Appl. No. 14/999,427, dated Oct. 5, 2017 6 pages Restriction Requirement.
Official Action for U.S. Appl. No. 14/999,427, dated Feb. 9, 2018 9 pages.
Notice of Allowance for U.S. Appl. No. 14/999,427, dated Sep. 21, 2018 18 pages.
Official Action for U.S. Appl. No. 15/731,324, dated Feb. 7, 2019 15 pages.
Official Action for U.S. Appl. No. 15/373,979, dated Jan. 29, 2019 12 pages.
International Preliminary Report on Patentability for International (PCT) Patent Application No. PCT/US18/00118, dated Jun. 11, 2020 13 pages.
Notice of Allowance for U.S. Appl. No. 15/932,150, dated May 14, 2020 9 pages.
International Preliminary Report on Patentability for International (PCT) Patent Application No. PCT/US2018/064427, dated Nov. 19, 2020 8 pages.
Related Publications (1)
Number Date Country
20190211824 A1 Jul 2019 US
Provisional Applications (2)
Number Date Country
62179437 May 2015 US
61342690 Apr 2010 US
Divisions (2)
Number Date Country
Parent 14999427 May 2016 US
Child 16291984 US
Parent 13066261 Apr 2011 US
Child 13987486 US
Continuations (1)
Number Date Country
Parent 13987486 Jul 2013 US
Child 14544874 US
Continuation in Parts (1)
Number Date Country
Parent 14544874 Feb 2015 US
Child 14999427 US