The present invention relates to plural compressors disposed within a single shell. More particularly, the present invention relates to plural compressors disposed within a single shell where two compressors, located at opposite ends of a motor, are both driven by the motor.
Due to energy costs and conservation, there is a demand for refrigerant motor-compressor systems which have an output which can be varied in accordance with demand. To satisfy this demand, a large number of systems have been developed. One such system involves the unloading of one or more cylinders in a multi-cylinder compressor or the varying of re-expansion volume for the purpose of varying the output of the compressor system. These variable capacity systems tend to be relatively complex and the efficiency of the compressor in an unloaded stated is not optimum. Variable speed compressors have also been used, but these variable speed compressors require expensive controls. The efficiency of the speed control, as well as the efficiency of the motor-compressor, present problems at least when the system is operating in a reduced capacity condition.
Compressor systems have also been developed which, in place of a single compressor large enough to carry the maximum load demand, include a plurality of smaller motor compressors having a combined output equal to the required maximum load demand. These multi-compressor systems include means for controlling the total system in such a manner as to selectively activate and deactivate each of the plurality of motor compressors independently when the load demand varies so that the compressor system output meets the required load demand. These multi-compressor systems have good efficiency but they require complex piping and plumbing systems, including means for dealing with lubricating oil management in order to ensure that all of the lubricating oil remains equally distributed between each of the individual compressors.
Additional designs for the multi-compressor systems have included the incorporation of a plurality of standard motor compressor units in a common single compressor shell. The common shell maximizes the compactness of the system and it provides a common oil sump for equal oil distribution, a common suction gas inlet and a common discharge gas outlet. These single shell multi-compressor systems have proved to be acceptable in the market place, but they tend to be relatively large and the means for controlling the total system is still somewhat complex.
The continued development of multi-compressor systems has been directed towards reducing the overall costs and the overall size of the system as well as simplifying the control systems which determine the compressor system's output in relation to the system demand.
The present invention provides the art with a multi-compressor compression system where a single compressor is located at opposing sides of a single drive shaft. A single motor rotor is press fit to the central portion of the drive shaft and the single motor rotor is disposed within a single motor stator. Thus, both compressors are powered by the same rotor and stator of a single motor. The control of the output of the multi-compressor system is accomplished by a variable speed motor or by a pulsed width modulation (PWM) capacity control system incorporated into one or both of the opposing compressors. When incorporating a variable speed motor for capacity control, the capacity can be varied from 0% to 100%. When incorporating the PWM capacity control system into one of the compressors, the capacity can be varied from 50% and 100%. When incorporating the PWM capacity control system into both compressors, the capacity can be varied from 0% to 100%. The capacity of one or both of the compressors can be increased to approximately 120% of capacity using a vapor injection system to further increase the range of the dual compressor system if desired. More than one of these dual-compressor/single motor systems can be incorporated into a single shell if desired.
Further areas of applicability of the present invention will become apparent from the detailed description provided hereinafter. It should be understood that the detailed description and specific examples, while indicating the preferred embodiment of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
The present invention will become more fully understood from the detailed description and the accompanying drawings, wherein:
The following description of the preferred embodiment(s) is merely exemplary in nature and is in no way intended to limit the invention, its application, or uses.
There is shown in
Shell assembly 12 comprises a central shell 18 and a pair of intermediate shells 20, with each intermediate shell 20 being located at opposite ends of central shell 18. Each intermediate shell 20 is bolted to central shell 18 as shown in
Each partition plate assembly 14 comprises an outer plate 28 and a transversely extending separation plate 30. Each outer plate 28 is bolted between a respective intermediate shell 20 of shell assembly 12 and a respective end cap 16. Each separation plate 30 sealingly engages a respective outer plate 28 to define a discharge pressure chamber 32 located at opposite ends of compression system 10 and a single suction pressure chamber 34 located between the two partition plate assemblies 14. Discharge pressure chamber 32 is in communication with discharge fitting 26 through a conduit 36 which is spaced from the main body of central shell 18 as illustrated in
A compressor mounting frame 40 is formed by end caps 16, partition plate assemblies 14 and shell assembly 12.
Major elements of compression system 10 that are affixed to shell assembly 12 include a pair of two-piece main bearing assemblies 42 and a motor stator 44. A single drive shaft or crank shaft 50 having a pair of eccentric crank pins 52 at opposite ends thereof is rotatably journaled in a pair of bearings 54, each secured within a respective main bearing assembly 42. Each crank pin 52 has a driving flat 56 on one surface. Driving flats 56 are out of rotational phase with one another by 180°, as illustrated in
An oil pump 58 is secured to one of the main bearing assemblies 42, and the impeller of oil pump 58 is driven by crank shaft 50 using a drive pin hole 60. Crank shaft 50 has an axially extending bore 62 extending from one end and an axially extending bore 64 extending from the opposite end. Axial bore 62 is in communication with a radial bore 66 to receive lubricating oil from oil pump 58 and provide the lubricating oil to one side of compression system 10. Axial bore 64 is in communication with a radial bore 68 to receive lubricating oil from oil pump 58 and provide the lubricating oil to the opposite side of compression system 10. A radial vent hole 70 is in communication with axial bore 64. In addition, a pair of radial bores 72, one extending from axial bore 62 and one extending from axial bore 64, provide lubricating oil to main bearing assemblies 42. A second set of radial bores 74 extending from axial bore 64 provide lubricating oil to windings 76 passing through motor stator 44 for cooling purposes. The lower portion of shell assembly 12 defines an oil sump 78 which is filled with lubricating oil to a level slightly below the lower end of motor stator 44. Oil pump 58 draws oil from oil sump 78 and pumps the lubricating oil through the various bores and holes in crank shaft 50 to the components of compression system 10.
Crank shaft 50 is rotatably driven by an electric motor which includes motor stator 44, windings 76 passing through motor stator 44, and a rotor 80 press fit to crank shaft 50. A pair of counterweights 82 are secured to opposite ends of crank shaft 50 adjacent a respective crank pin 52.
The upper surface of each two-piece main bearing assembly 42 is provided with a flat thrust bearing surface 84 on which is disposed a respective orbiting scroll member 86 having the usual spiral vane or wrap 88 extending outwardly from an end plate 90. Projecting outwardly from the lower surface of each end plate 90 of each orbiting scroll member 86 is a cylindrical hub 92 having a journal bearing therein and in which is rotatably disposed a drive bushing 96 having an inner bore in which a respective crank pin 52 is drivingly disposed. Each crank pin 52 has driving flat 56 on one surface which drivingly engages a flat surface formed in a portion of the inner bore of each drive bushing 96 to provide a radially compliant driving arrangement, such as shown in Assignee's U.S. Pat. No. 4,877,382, the disclosure of which is hereby incorporated herein by reference. As detailed earlier, flats 56 are 180° out of phase with one another. A pair of Oldham couplings 98 are also provided, with one being provided between each orbiting scroll member 86 and each two-piece main bearing assembly 42. Each Oldham coupling 98 is keyed to a respective orbiting scroll member 86 and to a respective non-orbiting scroll member 100 to prevent rotation of orbiting scroll members 86. Each Oldham coupling 98 can be keyed to a respective orbiting scroll member 86 and to a respective main bearing assembly 42, if desired.
Each non-orbiting scroll member 100 is also provided with a wrap 102 extending outwardly from an end plate 104 which is positioned in meshing engagement with a respective wrap 88 of a respective orbiting scroll member 86. Each non-orbiting scroll member 100 has a centrally disposed discharge passage 106 which communicates with a centrally located open recess 108 which is, in turn, in fluid communication with a respective discharge pressure chamber 32. An annular recess 112 is also formed in each non-orbiting scroll member 100 within which is disposed a respective floating seal assembly
Recesses 108 and 112 and floating seal assemblies 114 cooperate to define axial pressure biasing chambers which receive pressurized fluid being compressed by respective wraps 88 and 102 so as to exert an axial biasing force on a respective non-orbiting scroll member 100 to thereby urge the tips of respective wraps 88 and 102 into sealing engagement with the opposed end plate surfaces of end plates 104 and 90, respectively. Floating seal assemblies 114 are preferably of the type described in greater detail in Assignee's U.S. Pat. No. 5,156,539, the disclosure of which is hereby incorporated herein by reference. Non-orbiting scroll members 100 are designed to be mounted for limited axial movement with respect to two-piece main bearing assembly 42 in a suitable manner, such as disclosed in the aforementioned U.S. Pat. No. 4,877,382 or Assignee's U.S. Pat. No. 5,102,316, the disclosure of which is hereby incorporated herein by reference.
Shell assembly 12 defines suction pressure chamber 34 which receives a gas for compression from suction inlet fitting 24 through conduit 38. The gas within suction pressure chamber 34 is taken in at the radially outer portion of both sets of intermeshed scrolls 86 and 100, is compressed by both sets of wraps 88 and 102, and then discharged into discharge pressure chambers 32 through discharge passage 106 and recesses 108. The compressed gas exits each discharge pressure chamber 32 through conduit 36 and discharge fitting 26.
When it is desired to incorporate a capacity control system into compression system 10, the electric motor can be designed as a variable speed motor. The design for the variable speed motor, which includes motor stator 44, windings 76 and rotor 80, are well known in the art and will not be discussed in detail. By providing variable speed capacity to the electric motor, the capacity of compression system 10 can be varied between 0% and 100%.
Referring now to
Capacity control system 212 includes a discharge fitting 216, a piston 218, a shell fitting 220, a solenoid valve 222, a control module 224, and a sensor array 226 having one or more appropriate sensors. Discharge fitting 216 is threadingly received or otherwise secured within open recess 108, and discharge fitting 216 defines an internal cavity 228 and a plurality of discharge passages 230. A discharge valve 232 is disposed below discharge fitting 216. Thus, pressurized gas overcomes the biasing load of discharge valve 232 to open discharge valve 232 and allow the pressurized gas to flow into cavity 228 through discharge passages 230 and into discharge pressure chamber 32.
Referring now to
In order to bias non-orbiting scroll member 100 into sealing engagement with orbiting scroll member 86 for normal full load operation, solenoid valve 222 is deactivated (or it is activated) by control module 224 in response to sensor array 226 to block fluid flow between tubes 250 and tube 252. In this position, pressure chamber 246 is in communication with discharge pressure chamber 32 through passageway 242 and orifice 244. The pressurized fluid at discharge pressure within pressure chambers 32 and 246 will act against opposite sides of piston 218 thus allowing for the normal biasing of non-orbiting scroll member 100 towards orbiting scroll member 86 to sealingly engage the axial ends of each scroll member with the respective end plate of the opposite scroll member. The axial sealing of the two scroll members 86 and 100 causes compression system 210 to operate at 100% capacity.
In order to unload compression system 210, solenoid valve 222 will be activated (or it will be deactivated) by control module 224 in response to sensor array 226. When solenoid valve 222 is actuated (or unactuated), suction pressure chamber 34 is in direct communication with pressure chamber 246 through tube 252, solenoid valve 222 and tube 250. With the discharge pressure pressurized fluid released to suction from pressure chamber 246, the pressure difference on opposite sides of piston 218 will move non-orbiting scroll member 100 to the right as shown in
Control module 224 is in communication with sensor array 226 to provide the required information for control module 224 to determine the degree of unloading required for the particular conditions of the refrigeration system including compression system 210 existing at that time. Based upon this information, control module 224 will operate solenoid valve 222 in a pulsed width modulation mode to alternately place chamber 246 in communication with discharge pressure chamber 32 and suction pressure chamber 34. The frequency with which solenoid valve 222 is operated in the pulsed width modulated mode will determine the percent capacity of operation of one set of scrolls 86 and 100 of compression system 210. As the sensed conditions change, control module 224 will vary the frequency of operation for solenoid valve 222 and thus the relative time periods at which one set of scrolls 86 and 100 of compression system 210 is operated in a loaded and unloaded condition. The varying of the frequency of operation of solenoid valve 222 can cause the operation of one set of scrolls 86 and 100 between fully loaded or 100% capacity and completely unloaded or 0% capacity or at any of an infinite number of settings in between in response to system demands. This has the effect of varying the capacity of compression system 210 between 50% and 100%.
Referring now to
Referring now to
The incorporation of flash tank 298 and the remainder of vapor injection system 214, allows the capacity of one set of scrolls 86 and 100 of compression system 210 to increase above the fixed capacity of one set of scrolls 86 and 100 of compression system 210. Typically, at standard air conditioning conditions, the capacity of one of the compressors can be increased by approximately 20% to provide one set of the scrolls with 120% of its capacity which is 110% of the capacity of compression system 210. In order to be able to control the capacity of one set of scrolls 86 and 100 of compression system 210, a solenoid valve 308 is positioned within piping 306. The amount of percent increase in the capacity of one set of scrolls 86 and 100 of compression system 210 can be controlled by operating solenoid valve 308 in a pulse width modulation mode. Solenoid valve 308 when operated in a pulse width modulation mode in combination with capacity control system 212 of compression system 210 allows the capacity of compression system 210 to be positioned anywhere between 50% and 110%.
Referring now to
Referring now to
Central shell 318 defines discharge fitting 26 and conduit 36 which is separated from the main body of central shell 318. In addition, central shell 318 defines an electrical connection access 326 for providing both power and diagnostics to the motor positioned within central shell 318. One end cap 316 defines suction inlet fitting 24, thus eliminating the need for conduit 38.
The motor and compressors that are positioned within shell assembly 12 illustrated in
End cap 316 can be adapted to include capacity control system 212 in a manner similar to that illustrated in
In addition, central shell 318 can be adapted to incorporate vapor injection system 214 detailed above. Thus, the description of capacity control system 212 and vapor injection system 214 detailed above for
The description of the invention is merely exemplary in nature and, thus, variations that do not depart from the gist of the invention are intended to be within the scope of the invention. Such variations are not to be regarded as a departure from the spirit and scope of the invention.
Number | Name | Date | Kind |
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5123818 | Gormley et al. | Jun 1992 | A |
5211031 | Murayama et al. | May 1993 | A |
6672846 | Rajendran et al. | Jan 2004 | B2 |
6988876 | Ke et al. | Jan 2006 | B2 |
Number | Date | Country | |
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20040258542 A1 | Dec 2004 | US |