US20070186581A1 - Compressor cooling system - Google Patents
Compressor cooling system Download PDFInfo
- Publication number
- US20070186581A1 US20070186581A1 US11/353,413 US35341306A US2007186581A1 US 20070186581 A1 US20070186581 A1 US 20070186581A1 US 35341306 A US35341306 A US 35341306A US 2007186581 A1 US2007186581 A1 US 2007186581A1
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- US
- United States
- Prior art keywords
- compressor
- flow
- refrigerant
- cool
- cooling passage
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000001816 cooling Methods 0.000 title claims abstract description 50
- 239000003507 refrigerant Substances 0.000 claims abstract description 67
- 239000012530 fluid Substances 0.000 claims abstract description 61
- 238000005057 refrigeration Methods 0.000 claims abstract description 32
- 238000011144 upstream manufacturing Methods 0.000 claims abstract description 3
- 238000007906 compression Methods 0.000 claims description 13
- 230000006835 compression Effects 0.000 claims description 12
- 238000000034 method Methods 0.000 claims description 11
- 230000008878 coupling Effects 0.000 claims description 4
- 238000010168 coupling process Methods 0.000 claims description 4
- 238000005859 coupling reaction Methods 0.000 claims description 4
- 239000003921 oil Substances 0.000 description 27
- 238000010276 construction Methods 0.000 description 24
- 230000000712 assembly Effects 0.000 description 7
- 238000000429 assembly Methods 0.000 description 7
- 238000004891 communication Methods 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000002274 desiccant Substances 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000010729 system oil Substances 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B31/00—Compressor arrangements
- F25B31/006—Cooling of compressor or motor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/06—Cooling; Heating; Prevention of freezing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0007—Injection of a fluid in the working chamber for sealing, cooling and lubricating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C18/12—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
- F04C18/14—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
- F04C18/16—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B2400/00—General features or devices for refrigeration machines, plants or systems, combined heating and refrigeration systems or heat-pump systems, i.e. not limited to a particular subgroup of F25B
- F25B2400/07—Details of compressors or related parts
- F25B2400/075—Details of compressors or related parts with parallel compressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B49/00—Arrangement or mounting of control or safety devices
- F25B49/02—Arrangement or mounting of control or safety devices for compression type machines, plants or systems
- F25B49/025—Motor control arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B5/00—Compression machines, plants or systems, with several evaporator circuits, e.g. for varying refrigerating capacity
Definitions
- the present invention relates to a cooling system for use in a compressor system. More particularly, the present invention relates to a refrigeration system configured to cool components of a compressor system.
- Compressor assemblies typically include a compressor that is driven by a drive member to create a flow of compressed fluid.
- the process of creating the flow of compressed fluid can produce a considerable amount of heat.
- the flow of compressed fluid exits the compressor at a high temperature. Therefore, the flow of compressed fluid is cooled before it is utilized.
- the heat generated by the compression process also raises the temperature of a fluid, such as oil, utilized by the compressor for lubricating, sealing and cooling.
- other components of the compressor system such as, the drive member, a variable frequency drive, and a control system can in some circumstances create undesirable amounts of heat that can damage these components or shorten their operating lives.
- the invention provides a compressor system that includes a compressor that is operable to produce a flow of compressed fluid and a refrigeration system that includes an evaporator.
- the evaporator passes a flow of refrigerant therethrough and is operable to cool the flow of compressed fluid.
- the compressor system also includes a drive member that is coupled to the compressor and is operable to drive the compressor.
- a cooling passage extends from a point downstream of the evaporator to a point upstream of the compressor and at least a portion of the cooling passage is in thermal exchange relationship with the drive member.
- the invention provides a method of operating a fluid compression system that includes coupling a compressor to a drive member and operating the drive member to produce a corresponding operation of the compressor to produce a flow of compressed fluid.
- the method also includes passing a flow of refrigerant through an evaporator to cool the flow of compressed fluid and passing the flow of refrigerant from the evaporator into a return line. A portion of the flow of refrigerant is diverted from the return line to the drive member to cool the drive member.
- the invention provides a fluid compression system that includes a plurality of compressors operable to provide a flow of compressed fluid and a plurality of drive members. Each drive member is associated with one of the compressors and is operable to drive the compressor.
- the system also includes a refrigeration system that includes a refrigeration compressor, operable to compress and discharge a flow of refrigerant. The flow of refrigerant is in thermal exchange relationship with the flow of compressed fluid such that the flow of refrigerant cools the flow of compressed fluid.
- a cooling passage is positioned to receive a portion of the flow of refrigerant. At least a portion of the cooling passage is positioned in thermal exchange relationship with one of the plurality of drive members to cool one of the plurality of drive members.
- FIG. 1 is a schematic view of a compressor system embodying the present invention
- FIG. 2 is a schematic view of a portion of the compressor system of FIG. 1 ;
- FIG. 3 is a schematic view of another compressor system embodying the invention.
- FIG. 1 schematically illustrates a compressor system 10 that includes a compressor assembly 12 and a refrigeration system 14 .
- the illustrated compressor assembly 12 includes a compressor 16 , a drive member 18 , a variable frequency drive (VFD) 20 and a control system 22 .
- VFD variable frequency drive
- the compressor 16 can be any suitable compressor design, such as a rotary screw compressor, a centrifugal compressor, or a reciprocating compressor.
- the illustrated compressor 16 includes a compressor outlet 24 and an after-cooler 26 .
- the compressor outlet 24 is in fluid communication with the compressor 16 and the after-cooler 26 .
- the compressor 16 also includes an oil cooler 28 and an oil passage 30 .
- the oil passage 30 is in fluid communication with the compressor 16 and the oil cooler 28 . While the illustrated compressor 16 includes the oil cooler 28 and the after-cooler 26 , in other constructions the compressor 16 may omit one or both of the oil cooler 28 and the after-cooler 26 .
- the compressor 16 is a single stage compressor, in other constructions, the compressor 16 can be a multi-stage compressor and can include an inter-cooler located between each stage.
- the inter-cooler is configured to cool the air or working fluid compressed by the compressor 16 .
- the output of the first compressor stage is directed to the inlet of the second compressor stage. This arrangement allows for a greater pressure increase, which may be necessary in some application.
- bypassage and line should be interpreted broadly. Specifically, the terms “passage” and “line” should be interpreted to include but not limited to, conduits, channels, tubes, pipes, valves, flanges, hoses, and the like. Thus, a “passage” or “line” is essentially any structural element that is able to direct fluid between first and second points.
- the drive member 18 is coupled to the compressor 16 , and in one construction, includes a motor, such as a variable speed motor.
- the drive member 18 can include other suitable drive members, such as a turbine, an internal combustion engine, a diesel engine and the like.
- the refrigeration system 14 includes a refrigerant compressor 32 , a condenser 34 , an expansion device 36 , an evaporator 38 and a return line 40 .
- the refrigerant compressor 32 is fluidly coupled to the condenser 34 .
- the condenser 34 is fluidly coupled to the expansion device 36 and the expansion device 36 is fluidly coupled to the evaporator 38 .
- the evaporator 38 is in thermal exchange relationship with the compressor outlet 24 downstream of the after-cooler 26 to cool the air or working fluid compressed by the compressor 16 .
- the evaporator 38 includes an evaporator outlet 42 that is fluidly coupled to the return line 40 .
- the return line 40 fluidly couples the evaporator outlet 42 to the refrigerant compressor 32 to return refrigerant to the refrigerant compressor 32 and complete the cycle.
- the illustrated refrigeration system 18 includes a single refrigerant compressor 32 , condenser 34 , expansion device 36 , evaporator 38 , and return line 40
- the refrigeration system 18 can include multiple refrigerant compressors 32 , condensers 34 , expansion devices 36 , evaporators 38 , and return lines 40 , as may be desired.
- refrigeration systems may include other components not illustrated in FIG. 1 . These additional components include tanks, valves, sensors, separators, and the like. As such, the refrigeration system should not be limited to the components illustrated in FIG. 1 .
- the refrigeration system 14 defines a portion of an air dryer system 44 .
- the air dryer system 44 includes the refrigerant compressor 32 , the condenser 34 , the expansion device 36 and the evaporator 38 .
- the air dryer system may not include the refrigeration system 14 and may include another suitable air dryer design, such as a desiccant type air dryer. In such a construction, the refrigeration system 14 would be a separate system, independent of the air dryer 44 .
- the air dryer system 44 can employ a refrigeration system separate and distinct from the refrigeration system 14 .
- a cooling passage 46 is in fluid communication with the return line 40 to draw a portion of the refrigerant from the refrigeration system 14 after the refrigerant has passed through the evaporator 38 . It should be understood that the cooling passage 46 can connect to the return line 40 at any point between the evaporator 38 and the refrigerant compressor 32 . In other constructions, the cooling passage 46 connects directly to the evaporator 38 or to another point within the refrigeration system 14 . In preferred constructions, the cooling passage 46 may include a pipe, a tube, or other conduit.
- the cooling passage 46 may include a plurality of portions 48 that are in thermal exchange relationship with one or more of the after-cooler 26 , the oil cooler 28 , the drive member 18 , the VFD 20 , the control system 22 , or other components within the compressor system (e.g., gearbox).
- Each of the plurality of portions 48 includes a flow path that directs a portion of refrigerant to a component to be cooled.
- each of the plurality of portions 48 includes a heat exchanger that allows the flow of refrigerant to cool the component to be cooled with greater efficiency.
- one of the plurality of cooling passage portions 48 includes a heat exchanger 50 configured to allow the flow of refrigerant to cool the drive member 18 .
- a fan 51 is driven by the drive member 18 or a separate fan drive member, to move air across the heat exchanger 50 .
- the air that passes across the heat exchanger 50 is cooled and then passes across the drive member 18 to cool the drive member 18 .
- the separate fan drive member can be an electric motor, and in such a construction, the motor can be selectively turned off and on to control the amount of air that moves across the heat exchanger 50 and the drive member 18 .
- a temperature switch can be used to start and stop the fan drive member when the drive member 18 has reached predetermined temperatures.
- the temperature switch can be configured to turn on the fan drive member when the temperature of the drive member 18 exceeds a predetermined temperature, and the temperature switch can be configured to turn off the fan drive member when the temperature of the drive member 18 falls below a predetermined temperature.
- the heat exchanger 50 and the fan 51 illustrate just one possible arrangement of a thermal exchange relationship between one of the cooling passage portions 48 and the drive member 18 . It should be understood that any suitable thermal exchange relationship between the plurality of cooling passage portions 48 and the after-cooler 26 , the oil cooler 28 , the drive member 18 , the VFD 20 , or the control system 22 can be utilized.
- a valve or other suitable control device, can be disposed in the cooling passage 46 or in the return line 40 to provide selective fluid communication between the evaporator outlet 42 and the cooling passage 46 .
- a valve may be disposed in any one of, or each of the plurality of cooling passage portions 48 to provide selective fluid communication between the evaporator outlet 42 and the cooling passage portion 48 .
- FIG. 3 illustrates an alternative construction in which a compressor system 10 ′ includes a plurality of compressor assemblies 12 ′ and a refrigeration system 14 ′. Although three compressor assemblies 12 ′ are illustrated, it should be understood two compressor assemblies or four or more compressor assemblies can be utilized as desired.
- each of the compressor assemblies 12 ′ includes a compressor 16 ′.
- the compressors 16 ′ can be any suitable compressor design, such as rotary screw compressors, centrifugal compressors, reciprocating compressors, or any combination thereof.
- the illustrated compressors 16 ′ each include a compressor outlet 24 ′ that is fluidly coupled to an outlet header 54 .
- the compressor outlets 24 ′ may not be fluidly coupled to the common outlet header 54 , and the outlets 24 ′ can remain independent to their respective compressor 16 ′.
- a drive member 18 ′, an after-cooler 26 ′, an oil cooler 28 ′, a VFD 20 ′ and a control system 22 ′ may be associated with each one of, or all of the plurality of compressors 16 ′.
- each of the compressor assemblies 12 ′ may omit one or more of the after-cooler 26 ′, the oil cooler 28 ′, the VFD 20 ′ and/or the control system 22 ′.
- one control system, a single oil cooler, or a single after-cooler may function to control the entire compressor system 10 ′, cool all of the system oil, or cool all of the compressed air (or other fluid) discharged by the compressors 16 ′.
- the drive member 18 drives the compressor 16 to produce a flow of compressed fluid, typically air.
- the flow of compressed fluid exits the compressor 16 and passes to the compressor outlet 24 .
- the compressor outlet 24 directs the flow of compressed fluid to the after-cooler 26 that is configured to cool the flow of compressed fluid.
- the flow of compressed fluid exits the after-cooler 26 and flows to the evaporator 38 that defines a portion of the air dryer system 44 .
- the evaporator 38 is configured to further cool the flow of compressed fluid to allow the air dryer 44 to reduce the amount of moisture contained within the flow of compressed fluid.
- the flow of compressed fluid exits the evaporator 38 and flows through the remainder of the air dryer 44 before being passed to equipment that utilizes the flow of compressed fluid.
- the VFD 20 operates to vary the rotational speed (i.e. revolutions per minute) of the associated drive member 18 in response to one or more control signals. Changing the rotational speed of the drive member 18 results in a corresponding change in the rotational speed of the compressor 16 . By varying the rotational speed of the compressor 16 , the volume of compressed fluid discharged by the compressor 16 can be varied.
- the control system 22 controls the operation of the compressor assembly 12 .
- the control system 22 may control the loading and unloading of the compressor 16 or may cycle the compressor 16 on and off.
- the control system 22 may also monitor various operating parameters of the compressor assembly 12 , such as an outlet fluid pressure, an oil temperature, an outlet fluid temperature, etc.
- the control system 22 controls the VFD 20 to control the rotational speed of the compressor 16 and the volume of compressed fluid discharged by the compressor 16 .
- a flow of oil is utilized by the compressor 16 to lubricate and cool components of the compressor 16 , such as screw rotors and bearings.
- the temperature of the flow of oil can increase and it may be desirable to cool the flow of oil.
- the flow of oil exits the compressor 16 through the oil passage 30 and is passed to the oil cooler 28 .
- the oil cooler 28 cools the flow of oil and then the oil passage 30 directs the flow of oil back to the compressor 16 to be re-used to cool and lubricate the compressor components.
- the refrigeration system 14 is operable to produce a cool flow of refrigerant.
- the flow of refrigerant may include any suitable refrigerant, such as argon or FREON.
- the refrigeration compressor 32 is configured to create a compressed flow of refrigerant that exits the refrigeration compressor 32 and passes to the condenser 34 .
- the condenser 34 removes heat from the flow of refrigerant, thereby at least partially condensing the flow of refrigerant.
- the flow of refrigerant enters the expansion device 36 where it is expanded, thereby causing a reduction in the pressure and temperature of the flow.
- the expanded flow of refrigerant exits the expansion device 36 and passes to the evaporator 38 where the flow of refrigerant is in thermal exchange relationship with the flow of compressed fluid, such that the flow of refrigerant cools the flow of compressed fluid.
- the flow of refrigerant exits the evaporator 38 through the evaporator outlet 42 and flows to the return line 40 .
- a portion of the flow of refrigerant may be diverted from the return line 40 to the cooling passage 46 .
- the portion of the flow of refrigerant can be further diverted into portions that are passed to the plurality of cooling passage portions 48 .
- One of the plurality of cooling passage portions 48 may be in thermal exchange relationship with the drive member 18 and the flow of refrigerant within the cooling passage portion 48 is operable to cool the drive member 18 .
- Another one of the cooling passage portions 48 may be in thermal exchange relationship with the after-cooler 26 , such that the flow of refrigerant is operable with the after-cooler 26 to cool the flow of the compressed fluid. Yet another cooling passage portion 48 may be in thermal exchange relationship with the oil-cooler 28 , such that the flow of refrigerant is operable with the oil-cooler 28 to cool the flow of oil. The cooling passage portions 48 may also be in thermal exchange relationship with the VFD 20 and the control system 22 , such that the flows of refrigerant within the cooling passage portions 48 are operable to cool the VFD 20 and the control system 22 . In other constructions, one of the cooling passage portions 48 can be in thermal exchange relationship with the inter-cooler or inter-coolers that are configured to cool the flow of compressed fluid between each stage of compression.
- the illustrated compressor assembly 12 includes the after-cooler 26 , the oil-cooler 28 , the drive member 18 , the VFD 20 and the control system 22 all in thermal exchange relationship with portions 48 of the cooling passage 46 , it is not necessary for all of these components to be in thermal exchange relationship with the cooling passage 46 .
- the oil-cooler 28 can be air cooled and therefore, the oil cooler 28 may not be in thermal exchange relationship with the cooling passage 46 .
- the after-cooler 26 , the oil-cooler 28 , the VFD 20 and the control system 22 are all air cooled and only the drive member 18 is in thermal exchange relationship with the cooling passage 46 .
- any one or combination of the components can be cooled using the refrigeration system 14 described herein.
- the portions of the flow of refrigerant are passed into the return line 40 .
- the return line 40 collects the portions of the flow of refrigerant, along with the portion of the flow of the refrigerant that was not passed through the cooling passage 46 , and returns the flow of refrigerant back to the refrigerant compressor 32 .
- the flow of refrigerant returned to the refrigerant compressor 32 repeats the refrigeration process described above to create the cool flow of refrigerant.
- the invention provides, among other things, a compressor system 10 that includes a compressor 16 , a drive member 18 and a refrigeration system 14 .
- the refrigeration system 14 may operate as part of an air dryer 44 to dry the compressed fluid exiting the compressor 16 and is also operable to cool other components such as the drive member 18 , a variable frequency drive 20 , a control system 22 , an after-cooler 26 , and/or an oil cooler 28 .
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Compressor (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
A compressor system that includes a compressor, a refrigeration system, a drive member and a cooling passage. The compressor is operable to produce a flow of compressed fluid. The refrigeration system includes an evaporator, and a flow of refrigerant passes through the evaporator and is operable to cool the flow of compressed fluid. The drive member is coupled to the compressor and is operable to drive the compressor. The cooling passage extends from a point downstream of the evaporator to a point upstream of the compressor. At least a portion of the cooling passage is in thermal exchange relationship with the drive member.
Description
- The present invention relates to a cooling system for use in a compressor system. More particularly, the present invention relates to a refrigeration system configured to cool components of a compressor system.
- Compressor assemblies typically include a compressor that is driven by a drive member to create a flow of compressed fluid. The process of creating the flow of compressed fluid can produce a considerable amount of heat. Typically, the flow of compressed fluid exits the compressor at a high temperature. Therefore, the flow of compressed fluid is cooled before it is utilized. Furthermore, the heat generated by the compression process also raises the temperature of a fluid, such as oil, utilized by the compressor for lubricating, sealing and cooling. In addition, other components of the compressor system such as, the drive member, a variable frequency drive, and a control system can in some circumstances create undesirable amounts of heat that can damage these components or shorten their operating lives.
- In one embodiment, the invention provides a compressor system that includes a compressor that is operable to produce a flow of compressed fluid and a refrigeration system that includes an evaporator. The evaporator passes a flow of refrigerant therethrough and is operable to cool the flow of compressed fluid. The compressor system also includes a drive member that is coupled to the compressor and is operable to drive the compressor. A cooling passage extends from a point downstream of the evaporator to a point upstream of the compressor and at least a portion of the cooling passage is in thermal exchange relationship with the drive member.
- In another embodiment the invention provides a method of operating a fluid compression system that includes coupling a compressor to a drive member and operating the drive member to produce a corresponding operation of the compressor to produce a flow of compressed fluid. The method also includes passing a flow of refrigerant through an evaporator to cool the flow of compressed fluid and passing the flow of refrigerant from the evaporator into a return line. A portion of the flow of refrigerant is diverted from the return line to the drive member to cool the drive member.
- In yet another embodiment, the invention provides a fluid compression system that includes a plurality of compressors operable to provide a flow of compressed fluid and a plurality of drive members. Each drive member is associated with one of the compressors and is operable to drive the compressor. The system also includes a refrigeration system that includes a refrigeration compressor, operable to compress and discharge a flow of refrigerant. The flow of refrigerant is in thermal exchange relationship with the flow of compressed fluid such that the flow of refrigerant cools the flow of compressed fluid. A cooling passage is positioned to receive a portion of the flow of refrigerant. At least a portion of the cooling passage is positioned in thermal exchange relationship with one of the plurality of drive members to cool one of the plurality of drive members.
- Other aspects of the invention will become apparent by consideration of the detailed description and accompanying drawings.
-
FIG. 1 is a schematic view of a compressor system embodying the present invention; -
FIG. 2 is a schematic view of a portion of the compressor system ofFIG. 1 ; and -
FIG. 3 is a schematic view of another compressor system embodying the invention. - Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use of “including,” “comprising,” or “having” and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. Unless specified or limited otherwise, the terms “mounted,” “connected,”
- “supported,” and “coupled” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, “connected” and “coupled” are not restricted to physical or mechanical connections or couplings.
-
FIG. 1 schematically illustrates acompressor system 10 that includes acompressor assembly 12 and arefrigeration system 14. The illustratedcompressor assembly 12 includes acompressor 16, adrive member 18, a variable frequency drive (VFD) 20 and acontrol system 22. - The
compressor 16 can be any suitable compressor design, such as a rotary screw compressor, a centrifugal compressor, or a reciprocating compressor. The illustratedcompressor 16 includes acompressor outlet 24 and an after-cooler 26. Thecompressor outlet 24 is in fluid communication with thecompressor 16 and the after-cooler 26. Thecompressor 16 also includes anoil cooler 28 and anoil passage 30. Theoil passage 30 is in fluid communication with thecompressor 16 and theoil cooler 28. While the illustratedcompressor 16 includes theoil cooler 28 and the after-cooler 26, in other constructions thecompressor 16 may omit one or both of theoil cooler 28 and the after-cooler 26. - Furthermore, while the illustrated
compressor 16 is a single stage compressor, in other constructions, thecompressor 16 can be a multi-stage compressor and can include an inter-cooler located between each stage. The inter-cooler is configured to cool the air or working fluid compressed by thecompressor 16. In this arrangement, the output of the first compressor stage is directed to the inlet of the second compressor stage. This arrangement allows for a greater pressure increase, which may be necessary in some application. - Before proceeding, it should be noted that the term “passage” and “line” as used herein should be interpreted broadly. Specifically, the terms “passage” and “line” should be interpreted to include but not limited to, conduits, channels, tubes, pipes, valves, flanges, hoses, and the like. Thus, a “passage” or “line” is essentially any structural element that is able to direct fluid between first and second points.
- Referring to
FIG. 1 , thedrive member 18 is coupled to thecompressor 16, and in one construction, includes a motor, such as a variable speed motor. In other constructions, thedrive member 18 can include other suitable drive members, such as a turbine, an internal combustion engine, a diesel engine and the like. - The
refrigeration system 14 includes arefrigerant compressor 32, acondenser 34, anexpansion device 36, anevaporator 38 and areturn line 40. As schematically illustrated inFIG. 1 , therefrigerant compressor 32 is fluidly coupled to thecondenser 34. Thecondenser 34 is fluidly coupled to theexpansion device 36 and theexpansion device 36 is fluidly coupled to theevaporator 38. Theevaporator 38 is in thermal exchange relationship with thecompressor outlet 24 downstream of the after-cooler 26 to cool the air or working fluid compressed by thecompressor 16. Theevaporator 38 includes anevaporator outlet 42 that is fluidly coupled to thereturn line 40. Thereturn line 40 fluidly couples theevaporator outlet 42 to therefrigerant compressor 32 to return refrigerant to therefrigerant compressor 32 and complete the cycle. While the illustratedrefrigeration system 18 includes asingle refrigerant compressor 32,condenser 34,expansion device 36,evaporator 38, andreturn line 40, in other constructions, therefrigeration system 18 can includemultiple refrigerant compressors 32,condensers 34,expansion devices 36,evaporators 38, andreturn lines 40, as may be desired. In addition, as one of ordinary skill in the art will realize, refrigeration systems may include other components not illustrated inFIG. 1 . These additional components include tanks, valves, sensors, separators, and the like. As such, the refrigeration system should not be limited to the components illustrated inFIG. 1 . - As illustrated in
FIG. 1 , therefrigeration system 14 defines a portion of anair dryer system 44. Theair dryer system 44 includes therefrigerant compressor 32, thecondenser 34, theexpansion device 36 and theevaporator 38. It should be understood that in other constructions, the air dryer system may not include therefrigeration system 14 and may include another suitable air dryer design, such as a desiccant type air dryer. In such a construction, therefrigeration system 14 would be a separate system, independent of theair dryer 44. In yet another construction, theair dryer system 44 can employ a refrigeration system separate and distinct from therefrigeration system 14. - With continued reference to
FIG. 1 , acooling passage 46 is in fluid communication with thereturn line 40 to draw a portion of the refrigerant from therefrigeration system 14 after the refrigerant has passed through theevaporator 38. It should be understood that thecooling passage 46 can connect to thereturn line 40 at any point between the evaporator 38 and therefrigerant compressor 32. In other constructions, thecooling passage 46 connects directly to theevaporator 38 or to another point within therefrigeration system 14. In preferred constructions, thecooling passage 46 may include a pipe, a tube, or other conduit. - The
cooling passage 46 may include a plurality ofportions 48 that are in thermal exchange relationship with one or more of the after-cooler 26, theoil cooler 28, thedrive member 18, theVFD 20, thecontrol system 22, or other components within the compressor system (e.g., gearbox). Each of the plurality ofportions 48 includes a flow path that directs a portion of refrigerant to a component to be cooled. In preferred arrangements, each of the plurality ofportions 48 includes a heat exchanger that allows the flow of refrigerant to cool the component to be cooled with greater efficiency. - As schematically illustrated in
FIG. 2 , in one construction, one of the plurality of coolingpassage portions 48 includes aheat exchanger 50 configured to allow the flow of refrigerant to cool thedrive member 18. In such a construction, afan 51 is driven by thedrive member 18 or a separate fan drive member, to move air across theheat exchanger 50. The air that passes across theheat exchanger 50 is cooled and then passes across thedrive member 18 to cool thedrive member 18. In one construction the separate fan drive member can be an electric motor, and in such a construction, the motor can be selectively turned off and on to control the amount of air that moves across theheat exchanger 50 and thedrive member 18. A temperature switch, or other suitable device, can be used to start and stop the fan drive member when thedrive member 18 has reached predetermined temperatures. For example, the temperature switch can be configured to turn on the fan drive member when the temperature of thedrive member 18 exceeds a predetermined temperature, and the temperature switch can be configured to turn off the fan drive member when the temperature of thedrive member 18 falls below a predetermined temperature. - The
heat exchanger 50 and thefan 51 illustrate just one possible arrangement of a thermal exchange relationship between one of thecooling passage portions 48 and thedrive member 18. It should be understood that any suitable thermal exchange relationship between the plurality of coolingpassage portions 48 and the after-cooler 26, theoil cooler 28, thedrive member 18, theVFD 20, or thecontrol system 22 can be utilized. - A valve, or other suitable control device, can be disposed in the
cooling passage 46 or in thereturn line 40 to provide selective fluid communication between theevaporator outlet 42 and thecooling passage 46. In other constructions, a valve may be disposed in any one of, or each of the plurality of coolingpassage portions 48 to provide selective fluid communication between theevaporator outlet 42 and thecooling passage portion 48. -
FIG. 3 illustrates an alternative construction in which acompressor system 10′ includes a plurality ofcompressor assemblies 12′ and arefrigeration system 14′. Although threecompressor assemblies 12′ are illustrated, it should be understood two compressor assemblies or four or more compressor assemblies can be utilized as desired. - As schematically illustrated in
FIG. 3 , each of thecompressor assemblies 12′ includes acompressor 16′. Thecompressors 16′ can be any suitable compressor design, such as rotary screw compressors, centrifugal compressors, reciprocating compressors, or any combination thereof. The illustratedcompressors 16′ each include acompressor outlet 24′ that is fluidly coupled to anoutlet header 54. In other constructions, thecompressor outlets 24′ may not be fluidly coupled to thecommon outlet header 54, and theoutlets 24′ can remain independent to theirrespective compressor 16′. - A
drive member 18′, an after-cooler 26′, an oil cooler 28′, aVFD 20′ and acontrol system 22′ may be associated with each one of, or all of the plurality ofcompressors 16′. In another construction, each of thecompressor assemblies 12′ may omit one or more of the after-cooler 26′, the oil cooler 28′, theVFD 20′ and/or thecontrol system 22′. In these constructions one control system, a single oil cooler, or a single after-cooler may function to control theentire compressor system 10′, cool all of the system oil, or cool all of the compressed air (or other fluid) discharged by thecompressors 16′. - It should be understood that the remainder of the
compressor system 10′ illustrated inFIG. 3 , including therefrigeration system 14′, is substantially the same as thecompressor system 10′ illustrated inFIG. 1 . Therefore, similar items have been given similar reference numbers. - The operation of the
10, 10′ ofcompressor systems FIGS. 1 and 3 are similar in many ways. Therefore, only the operation of thecompressor system 10 ofFIG. 1 will be discussed in detail. In operation, thedrive member 18 drives thecompressor 16 to produce a flow of compressed fluid, typically air. The flow of compressed fluid exits thecompressor 16 and passes to thecompressor outlet 24. - The
compressor outlet 24 directs the flow of compressed fluid to the after-cooler 26 that is configured to cool the flow of compressed fluid. The flow of compressed fluid exits the after-cooler 26 and flows to theevaporator 38 that defines a portion of theair dryer system 44. Theevaporator 38 is configured to further cool the flow of compressed fluid to allow theair dryer 44 to reduce the amount of moisture contained within the flow of compressed fluid. The flow of compressed fluid exits theevaporator 38 and flows through the remainder of theair dryer 44 before being passed to equipment that utilizes the flow of compressed fluid. - The
VFD 20 operates to vary the rotational speed (i.e. revolutions per minute) of the associateddrive member 18 in response to one or more control signals. Changing the rotational speed of thedrive member 18 results in a corresponding change in the rotational speed of thecompressor 16. By varying the rotational speed of thecompressor 16, the volume of compressed fluid discharged by thecompressor 16 can be varied. - The
control system 22 controls the operation of thecompressor assembly 12. For example, thecontrol system 22 may control the loading and unloading of thecompressor 16 or may cycle thecompressor 16 on and off. Thecontrol system 22 may also monitor various operating parameters of thecompressor assembly 12, such as an outlet fluid pressure, an oil temperature, an outlet fluid temperature, etc. In addition, thecontrol system 22 controls theVFD 20 to control the rotational speed of thecompressor 16 and the volume of compressed fluid discharged by thecompressor 16. - A flow of oil is utilized by the
compressor 16 to lubricate and cool components of thecompressor 16, such as screw rotors and bearings. During operation of thecompressor 16, the temperature of the flow of oil can increase and it may be desirable to cool the flow of oil. In one construction, the flow of oil exits thecompressor 16 through theoil passage 30 and is passed to theoil cooler 28. Theoil cooler 28 cools the flow of oil and then theoil passage 30 directs the flow of oil back to thecompressor 16 to be re-used to cool and lubricate the compressor components. - The
refrigeration system 14 is operable to produce a cool flow of refrigerant. The flow of refrigerant may include any suitable refrigerant, such as argon or FREON. Therefrigeration compressor 32 is configured to create a compressed flow of refrigerant that exits therefrigeration compressor 32 and passes to thecondenser 34. Thecondenser 34 removes heat from the flow of refrigerant, thereby at least partially condensing the flow of refrigerant. Next, the flow of refrigerant enters theexpansion device 36 where it is expanded, thereby causing a reduction in the pressure and temperature of the flow. The expanded flow of refrigerant exits theexpansion device 36 and passes to theevaporator 38 where the flow of refrigerant is in thermal exchange relationship with the flow of compressed fluid, such that the flow of refrigerant cools the flow of compressed fluid. - The flow of refrigerant exits the
evaporator 38 through theevaporator outlet 42 and flows to thereturn line 40. A portion of the flow of refrigerant may be diverted from thereturn line 40 to thecooling passage 46. In thecooling passage 46, the portion of the flow of refrigerant can be further diverted into portions that are passed to the plurality of coolingpassage portions 48. One of the plurality of coolingpassage portions 48 may be in thermal exchange relationship with thedrive member 18 and the flow of refrigerant within thecooling passage portion 48 is operable to cool thedrive member 18. Another one of thecooling passage portions 48 may be in thermal exchange relationship with the after-cooler 26, such that the flow of refrigerant is operable with the after-cooler 26 to cool the flow of the compressed fluid. Yet anothercooling passage portion 48 may be in thermal exchange relationship with the oil-cooler 28, such that the flow of refrigerant is operable with the oil-cooler 28 to cool the flow of oil. Thecooling passage portions 48 may also be in thermal exchange relationship with theVFD 20 and thecontrol system 22, such that the flows of refrigerant within thecooling passage portions 48 are operable to cool theVFD 20 and thecontrol system 22. In other constructions, one of thecooling passage portions 48 can be in thermal exchange relationship with the inter-cooler or inter-coolers that are configured to cool the flow of compressed fluid between each stage of compression. - It should be understood that although the illustrated
compressor assembly 12 includes the after-cooler 26, the oil-cooler 28, thedrive member 18, theVFD 20 and thecontrol system 22 all in thermal exchange relationship withportions 48 of thecooling passage 46, it is not necessary for all of these components to be in thermal exchange relationship with thecooling passage 46. For example, in one construction the oil-cooler 28 can be air cooled and therefore, theoil cooler 28 may not be in thermal exchange relationship with thecooling passage 46. In yet another construction, the after-cooler 26, the oil-cooler 28, theVFD 20 and thecontrol system 22 are all air cooled and only thedrive member 18 is in thermal exchange relationship with thecooling passage 46. Thus, as one of ordinary skill will realize, any one or combination of the components can be cooled using therefrigeration system 14 described herein. - After the portions of the flow of refrigerant complete the thermal exchange relationship with the after-
cooler 26, theoil cooler 28, thedrive member 18, theVFD 20 and/or thecontrol system 22, the portions of the flow of refrigerant are passed into thereturn line 40. Thereturn line 40 collects the portions of the flow of refrigerant, along with the portion of the flow of the refrigerant that was not passed through thecooling passage 46, and returns the flow of refrigerant back to therefrigerant compressor 32. The flow of refrigerant returned to therefrigerant compressor 32 repeats the refrigeration process described above to create the cool flow of refrigerant. - Thus, the invention provides, among other things, a
compressor system 10 that includes acompressor 16, adrive member 18 and arefrigeration system 14. Therefrigeration system 14 may operate as part of anair dryer 44 to dry the compressed fluid exiting thecompressor 16 and is also operable to cool other components such as thedrive member 18, avariable frequency drive 20, acontrol system 22, an after-cooler 26, and/or anoil cooler 28.
Claims (20)
1. A compressor system comprising:
a compressor operable to produce a flow of compressed fluid;
a refrigeration system including an evaporator, the evaporator passing a flow of refrigerant therethrough and operable to cool the flow of compressed fluid;
a drive member coupled to the compressor and operable to drive the compressor; and
a cooling passage extending from a point downstream of the evaporator to a point upstream of the compressor, at least a portion of the cooling passing in thermal exchange relationship with the drive member.
2. The compressor system of claim 1 , wherein the drive member includes a motor.
3. The compressor system of claim 2 , wherein the drive member includes a variable frequency drive, and wherein at least a portion of the flow of refrigerant within the cooling passage is operable to cool at least one of the motor and the variable frequency drive.
4. The compressor system of claim 1 , wherein the compressor includes an oil cooler, and wherein at least a portion of the flow of refrigerant within the cooling passage passes through the oil cooler to cool a flow of oil.
5. The compressor system of claim 1 , wherein the compressor includes a control system, and wherein at least a portion of the flow of refrigerant within the cooling passage is operable to cool the control system.
6. The compressor system of claim 1 , further comprising a heat exchanger positioned within the cooling passage, at least a portion of the flow of refrigerant within the cooling passage passing through the heat exchanger to cool the drive member.
7. A method of operating a fluid compression system, the method comprising:
coupling a compressor to a drive member;
operating the drive member to produce a corresponding operation of the compressor to produce a flow of compressed fluid;
passing a flow of refrigerant through an evaporator to cool the flow of compressed fluid;
passing the flow of refrigerant from the evaporator to a return line;
diverting a portion of the flow of refrigerant from the return line to the drive member to cool the drive member.
8. The method of claim 7 , wherein the drive member includes a motor.
9. The method of claim 7 , further comprising directing a portion of the refrigerant from the return line to an oil cooler to cool a flow of oil.
10. The method of claim 7 , further comprising directing a portion of the refrigerant from the return line to a variable frequency drive to cool the variable frequency drive.
11. The method of claim 7 , further comprising directing a portion of the refrigerant from the return line to a control system to cool the control system.
12. The method of claim 7 , further comprising directing a portion of the compressed fluid from the compressor through the refrigeration system to cool the flow of compressed fluid.
13. A fluid compression system comprising:
a plurality of compressors operable to provide a flow of compressed fluid;
a plurality of drive members, each drive member associated with one of the compressors to drive the compressor;
a refrigeration system including a refrigerant compressor operable to compress and discharge a flow of refrigerant, the flow of refrigerant in thermal exchange relationship with the flow of compressed fluid such that the flow of refrigerant cools the flow of compressed fluid; and
a cooling passage positioned to receive a portion of the flow of refrigerant, at least a portion of the cooling passage positioned in thermal exchange relationship with at least one of the plurality of drive members to cool the at least one of the plurality of drive members.
14. The fluid compression system of claim 13 , wherein at least one of the plurality of drive members includes a motor.
15. The fluid compression system of claim 14 , wherein at least one of the plurality of drive members includes a variable frequency drive.
16. The fluid compression system of claim 13 , further comprising a control system operable to control the plurality of compressors and in thermal exchange relationship with at least a portion of the cooling passage to cool the control system.
17. The fluid compression system of claim 13 , wherein at least one of the plurality of compressors includes an oil cooler in thermal exchange relationship with at least a portion of the cooling passage to cool a flow of oil.
18. The fluid compression system of claim 13 , further comprising a heat exchanger positioned within the cooling passage to cool at least one of the drive members.
19. The fluid compression system of claim 13 , wherein the refrigeration system includes an evaporator having an outlet.
20. The fluid compression system of claim 19 , further comprising a return passage extending from the outlet to the refrigerant compressor, the cooling passage connected to the return passage to receive the portion of the flow of refrigerant.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/353,413 US20070186581A1 (en) | 2006-02-14 | 2006-02-14 | Compressor cooling system |
| EP07250507.6A EP1818629B1 (en) | 2006-02-14 | 2007-02-08 | Compressor cooling system |
| CN200710005348XA CN101025310B (en) | 2006-02-14 | 2007-02-14 | Compressor cooling system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/353,413 US20070186581A1 (en) | 2006-02-14 | 2006-02-14 | Compressor cooling system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20070186581A1 true US20070186581A1 (en) | 2007-08-16 |
Family
ID=38162157
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/353,413 Abandoned US20070186581A1 (en) | 2006-02-14 | 2006-02-14 | Compressor cooling system |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20070186581A1 (en) |
| EP (1) | EP1818629B1 (en) |
| CN (1) | CN101025310B (en) |
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| US20120272673A1 (en) * | 2009-11-25 | 2012-11-01 | Kazuma Yokohara | Container refrigeration apparatus |
| US20150047381A1 (en) * | 2011-12-09 | 2015-02-19 | Daikin Industries, Ltd. | Container refrigeration device |
| US20150114031A1 (en) * | 2013-10-31 | 2015-04-30 | Emerson Climate Technologies, Inc. | Heat pump system |
| EP2884204A3 (en) * | 2013-12-10 | 2015-06-24 | Robert Bosch Gmbh | Heat pump with an inverter cooled by coolant |
| US20180160570A1 (en) * | 2016-12-02 | 2018-06-07 | Dell Products L.P. | Dynamic cooling system |
| US10260783B2 (en) | 2014-09-09 | 2019-04-16 | Carrier Corporation | Chiller compressor oil conditioning |
| US10962009B2 (en) | 2007-10-08 | 2021-03-30 | Emerson Climate Technologies, Inc. | Variable speed compressor protection system and method |
| US11206743B2 (en) | 2019-07-25 | 2021-12-21 | Emerson Climate Technolgies, Inc. | Electronics enclosure with heat-transfer element |
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| CN103047167A (en) * | 2011-10-17 | 2013-04-17 | 复盛易利达(上海)压缩机有限公司 | Exhausting device of final stage exhaust pipe of centrifugal compressor |
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| US20150114031A1 (en) * | 2013-10-31 | 2015-04-30 | Emerson Climate Technologies, Inc. | Heat pump system |
| US10156384B2 (en) * | 2013-10-31 | 2018-12-18 | Emerson Climate Technologies, Inc. | Heat pump system |
| EP2884204A3 (en) * | 2013-12-10 | 2015-06-24 | Robert Bosch Gmbh | Heat pump with an inverter cooled by coolant |
| US10260783B2 (en) | 2014-09-09 | 2019-04-16 | Carrier Corporation | Chiller compressor oil conditioning |
| US20180160570A1 (en) * | 2016-12-02 | 2018-06-07 | Dell Products L.P. | Dynamic cooling system |
| US10856449B2 (en) * | 2016-12-02 | 2020-12-01 | Dell Products L.P. | Dynamic cooling system |
| US11206743B2 (en) | 2019-07-25 | 2021-12-21 | Emerson Climate Technolgies, Inc. | Electronics enclosure with heat-transfer element |
| US11706899B2 (en) | 2019-07-25 | 2023-07-18 | Emerson Climate Technologies, Inc. | Electronics enclosure with heat-transfer element |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1818629A2 (en) | 2007-08-15 |
| EP1818629B1 (en) | 2016-12-21 |
| CN101025310B (en) | 2010-10-20 |
| CN101025310A (en) | 2007-08-29 |
| EP1818629A3 (en) | 2009-04-22 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: INGERSOLL-RAND COMPANY, NEW JERSEY Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MISTRY, VIPUL R.;COLLINS, JAMES C.;HASELEY, ROBERT K.;REEL/FRAME:017241/0428 Effective date: 20060118 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- AFTER EXAMINER'S ANSWER OR BOARD OF APPEALS DECISION |