US20150107289A1 - High pressure ratio multi-stage centrifugal compressor - Google Patents
High pressure ratio multi-stage centrifugal compressor Download PDFInfo
- Publication number
- US20150107289A1 US20150107289A1 US14/383,750 US201214383750A US2015107289A1 US 20150107289 A1 US20150107289 A1 US 20150107289A1 US 201214383750 A US201214383750 A US 201214383750A US 2015107289 A1 US2015107289 A1 US 2015107289A1
- Authority
- US
- United States
- Prior art keywords
- stage
- compressor
- diffuser
- impellers
- refrigerant
- 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
Images
Classifications
-
- 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
- F25B30/00—Heat pumps
- F25B30/02—Heat pumps of the compression type
-
- 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
- F25B1/00—Compression machines, plants or systems with non-reversible cycle
- F25B1/04—Compression machines, plants or systems with non-reversible cycle with compressor of rotary type
- F25B1/053—Compression machines, plants or systems with non-reversible cycle with compressor of rotary type of turbine type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
- F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/002—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids by varying geometry within the pumps, e.g. by adjusting vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/004—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids by varying driving speed
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/04—Shafts or bearings, or assemblies thereof
- F04D29/046—Bearings
- F04D29/048—Bearings magnetic; electromagnetic
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/46—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/462—Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
-
- 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
- F25B1/00—Compression machines, plants or systems with non-reversible cycle
- F25B1/10—Compression machines, plants or systems with non-reversible cycle with multi-stage compression
-
- 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
- F25B13/00—Compression machines, plants or systems, with reversible cycle
-
- F25B41/046—
-
- 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
- F25B2600/00—Control issues
- F25B2600/02—Compressor control
- F25B2600/025—Compressor control by controlling speed
- F25B2600/0253—Compressor control by controlling speed with variable speed
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B30/00—Energy efficient heating, ventilation or air conditioning [HVAC]
- Y02B30/70—Efficient control or regulation technologies, e.g. for control of refrigerant flow, motor or heating
Definitions
- This disclosure relates to a multi-stage centrifugal compressor for use in a high pressure ratio multi-stage centrifugal compressor having at least one variable geometry diffuser.
- Existing single-stage and two-stage centrifugal refrigeration compressors typically have at least one set of variable inlet guide vanes at a compressor inlet to regulate compressor capacity during various operating conditions.
- Variable-speed centrifugal compressors use speed variation as their primary capacity control mechanisms, but such compressors still need variable inlet guide vanes in order to operate surge-free at low capacity conditions.
- Multi-stage centrifugal compressors have used stages with fixed, typically vaneless, diffusers with inlet guide vanes and variable speed as the capacity control mechanism.
- Single-stage refrigerant compressors have been introduced that employ a variable frequency drive (VFD) for capacity control in addition to a set of rotatable inlet guide vanes upstream of the impeller.
- VFD variable frequency drive
- a variable-geometry diffuser has been used downstream from the impeller to improve the compressor surge characteristics at part-load operating conditions.
- Heat pump systems require compressors having high pressure ratios.
- screw-type or scroll-type compressors are used provide the needed high pressures of heat pump systems.
- a heat pump system includes a refrigerant circuit.
- First and second heat exchangers are arranged in the refrigerant circuit.
- a flow reversing device selectively changes a direction of flow in the refrigerant circuit between the first and second heat exchangers.
- a centrifugal compressor is arranged in the fluid circuit and has first and second impellers arranged in series relative to one another to provide a desired compressor pressure ratio.
- the centrifugal compressor mounts the first and second impellers on opposing ends of a shaft.
- the first and second impellers respectively include first and second stage inlets and outlets.
- One example desired compressor pressure ratio of at least 10:1 corresponds to a second stage outlet pressure to a first stage inlet pressure.
- a first diffuser is arranged at the first stage outlet, and the first diffuser is a variable geometry diffuser.
- FIG. 1 is a highly schematic view of a heat pump system having an example centrifugal compressor with multiple stages.
- FIG. 2 is a cross-sectional view of an example two-stage centrifugal compressor of this disclosure.
- FIG. 3 is a schematic view of an economizer for the disclosed centrifugal compressor.
- FIG. 4 is a schematic view of one example variable geometry diffuser for the disclosed centrifugal compressor.
- a heat pump system 10 includes a centrifugal compressor 12 for circulating a refrigerant in a refrigerant circuit 32 .
- the centrifugal compressor 12 is arranged in the fluid circuit 32 and includes compressor inlet and outlet passages 16 , 18 that are in fluid communication with a flow reversing device 14 .
- the example heat pump system is exemplary of a high pressure ratio system. It should be understood the disclosed centrifugal compressor may be used in other high pressure ratio applications, such as certain air-cooled chiller or refrigeration systems.
- First and second heat exchangers 20 , 22 are fluidly arranged in the refrigerant circuit 32 and respectively arranged at first and second locations 21 , 23 , which may be indoors and outdoors in one example.
- blowers 34 , 36 are respectively associated with each heat exchanger for transferring heat between each heat exchanger and its surrounding environment. It should be understood, however, that although refrigerant-to-air heat exchangers are shown, a heat exchanger may be used that transfers heat between the refrigerant and another fluid, such as water.
- the flow reversing device 14 selectively changes the direction of flow in the refrigerant circuit 32 between the first and second heat exchangers 20 , 22 .
- an “H” depicts a heating direction of refrigerant flow
- a “C” shows a cooling direction of refrigerant flow.
- a first bypass valve 24 and a first thermal expansion valve 26 are associated with the first heat exchanger 20 .
- a second bypass valve 28 and a second thermal expansion valve 30 are associated with the second heat exchanger 22 .
- the bypass valves 24 , 28 act as check valves to permit flow in only one direction.
- the refrigerant flows to the first heat exchanger 20 where heat is rejected to the first location 21 .
- Refrigerant then flow through the bypass valve 24 and is expanded through thermal expansion device 30 .
- the refrigerant is vaporized and then enters the second heat exchanger 22 where the second location 23 rejects heat to the refrigerant before being returned to the centrifugal compressor 12 .
- the flow reversing device 14 actuated to a heating configuration
- the refrigerant flows to the second heat exchanger 22 where heat is rejected to the second location 23 .
- Refrigerant then flow through the bypass valve 28 and is expanded through thermal expansion device 26 .
- the refrigerant is vaporized and then enters the first heat exchanger 20 where the first location 21 rejects heat to the refrigerant before being returned to the centrifugal compressor 12 .
- the heat pump system 10 is intended to be exemplary only.
- the centrifugal compressor 12 includes a housing 39 within which an electric motor 38 is arranged.
- the housing 38 is schematically depicted and may comprise one or more pieces.
- the electric motor 38 rotationally drives first and second impellers 42 , 44 via a rotor shaft 40 about an axis to compress the refrigerant in a two-stage compressor configuration.
- the rotor shaft 40 may comprise one or more pieces.
- two compressor stages are shown, the disclosure may also be used in a compressor having more stages.
- the first and second impellers 42 , 44 are located on opposing ends of the rotor shaft 40 .
- the impellers are centrifugal such that the impeller inlet is arranged axially and the impeller outlet is arranged radially.
- An oil-free bearing arrangement is provided for support of the rotor shaft 40 so that oil-free refrigerant can be used in the centrifugal compressor 12 .
- the rotor shaft 40 is rotationally supported relative to the housing 39 by magnetic bearings 46 , which are illustrated in a schematic fashion.
- the magnetic bearings 46 may include radial and/or axial magnetic bearing elements, for example.
- a bearing controller (not shown) communicates with the magnetic bearing 46 providing a magnetic bearing command to energize the magnetic bearings 46 .
- the magnetic bearings create a magnetic field levitating the rotor shaft 40 and controls its characteristics during operation of the centrifugal compressor 12 . It should be understood that the disclosed diffuser arrangements may also be used with air bearings or other types of bearings.
- One example electric motor 38 includes a rotor supporting multiple magnets about its circumference.
- a stator is arranged about the rotor to impart rotational drive to the rotor shaft 40 when energized.
- a motor controller (not shown) communicates with the stator and provides a variable speed command to rotationally drive the impellers 43 , 44 at a variable speed depending upon compressor operating conditions.
- the motor controller communicates with multiple sensors (not shown) to monitor and maintain the compressor operating conditions.
- the first and second impellers 42 , 44 are arranged in series relative to one another and providing a desired compressor pressure ratio, which in one example is at least 10:1.
- the first impeller 42 includes a first stage inlet 48 and a first stage outlet 52
- the second impeller 44 includes a second stage inlet 54 and a second stage outlet 58 .
- First and second stage volutes 50 , 56 are arranged respective at the first and second stage outlets 52 , 58 .
- the desired compressor pressure ratio corresponds to a second stage outlet pressure to a first stage inlet pressure.
- First and second diffusers 60 , 62 are respectively arranged at the first and second stage outlets 52 , 58 near the first and second stage volutes 50 , 56 .
- the first and second diffusers 60 , 62 are variable geometry diffusers, which may be any suitable type.
- First and second actuators 64 , 66 are configured to respectively move the first and second variable geometry diffusers between first and second positions.
- the second compressor stage is shown as an example.
- a passage 70 is arranged downstream from the second impeller 44 .
- a variable geometry device, such as a movable wall 72 for example is arranged in the passage in the second stage outlet 58 .
- the second actuator 62 moves the wall 72 between a first position F and a second position S to selectively regulate refrigerant flow through the passage 70 .
- variable geometry diffuser includes a plurality of fixed wedge shaped vanes located downstream of the movable diffuser wall element.
- the movable wall element may be serrated with the trailing edge of the serration coinciding with the throat area (which is the smallest cross-sectional flow passage) of the vaned diffuser.
- variable geometry diffuser In another variable geometry diffuser example, a rotatable vane diffuser in the plane normal to the compressor axis. By rotating the vanes, the throat area of the diffuser changes, and, therefore, the capacity of the compressor, is adjusted.
- a split vaned diffuser has an outer diffuser ring and an inner diffuser ring. Throat area adjustment is obtained by rotating one diffuser ring with respect to the other one. Throat area of the fully opened diffuser is reduced as a result of the rotation of the inner diffuser ring relative to the outer diffuser ring.
- An economizer 68 may be mounted to the housing 39 , as shown in FIG. 3 .
- the economizer 68 is a heat exchanger-type economizer.
- the economizer 68 is arranged fluidly between the first stage outlet 52 and the second stage inlet 54 .
- the disclosure may also be used in a compressor having more stages.
- the impellers are arranged on opposing ends of the rotor shaft (the so-called back-to-back configuration) reducing the axial thrust load of the shaft.
- the first compressor stage includes a variable geometry diffuser
- the second and third stages may each include a volute without a diffuser and still achieve the desired compressor pressure ratio.
Abstract
Description
- This disclosure relates to a multi-stage centrifugal compressor for use in a high pressure ratio multi-stage centrifugal compressor having at least one variable geometry diffuser.
- Existing single-stage and two-stage centrifugal refrigeration compressors, with vaneless or vaned diffusers, typically have at least one set of variable inlet guide vanes at a compressor inlet to regulate compressor capacity during various operating conditions.
- Variable-speed centrifugal compressors use speed variation as their primary capacity control mechanisms, but such compressors still need variable inlet guide vanes in order to operate surge-free at low capacity conditions.
- Multi-stage centrifugal compressors have used stages with fixed, typically vaneless, diffusers with inlet guide vanes and variable speed as the capacity control mechanism. Single-stage refrigerant compressors have been introduced that employ a variable frequency drive (VFD) for capacity control in addition to a set of rotatable inlet guide vanes upstream of the impeller. In the case of a variable speed capability, a variable-geometry diffuser has been used downstream from the impeller to improve the compressor surge characteristics at part-load operating conditions.
- Heat pump systems require compressors having high pressure ratios. Typically, screw-type or scroll-type compressors are used provide the needed high pressures of heat pump systems.
- A heat pump system includes a refrigerant circuit. First and second heat exchangers are arranged in the refrigerant circuit. A flow reversing device selectively changes a direction of flow in the refrigerant circuit between the first and second heat exchangers. A centrifugal compressor is arranged in the fluid circuit and has first and second impellers arranged in series relative to one another to provide a desired compressor pressure ratio.
- In one example, the centrifugal compressor mounts the first and second impellers on opposing ends of a shaft. The first and second impellers respectively include first and second stage inlets and outlets. One example desired compressor pressure ratio of at least 10:1 corresponds to a second stage outlet pressure to a first stage inlet pressure. A first diffuser is arranged at the first stage outlet, and the first diffuser is a variable geometry diffuser.
- The disclosure can be further understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
-
FIG. 1 is a highly schematic view of a heat pump system having an example centrifugal compressor with multiple stages. -
FIG. 2 is a cross-sectional view of an example two-stage centrifugal compressor of this disclosure. -
FIG. 3 is a schematic view of an economizer for the disclosed centrifugal compressor. -
FIG. 4 is a schematic view of one example variable geometry diffuser for the disclosed centrifugal compressor. - Referring to
FIG. 1 , aheat pump system 10 includes acentrifugal compressor 12 for circulating a refrigerant in arefrigerant circuit 32. Thecentrifugal compressor 12 is arranged in thefluid circuit 32 and includes compressor inlet andoutlet passages flow reversing device 14. The example heat pump system is exemplary of a high pressure ratio system. It should be understood the disclosed centrifugal compressor may be used in other high pressure ratio applications, such as certain air-cooled chiller or refrigeration systems. - First and
second heat exchangers refrigerant circuit 32 and respectively arranged at first andsecond locations blowers - The
flow reversing device 14 selectively changes the direction of flow in therefrigerant circuit 32 between the first andsecond heat exchangers - A
first bypass valve 24 and a firstthermal expansion valve 26 are associated with thefirst heat exchanger 20. Asecond bypass valve 28 and a secondthermal expansion valve 30 are associated with thesecond heat exchanger 22. Thebypass valves - In operation, with the
flow reversing device 14 actuated to a cooling configuration, the refrigerant flows to thefirst heat exchanger 20 where heat is rejected to thefirst location 21. Refrigerant then flow through thebypass valve 24 and is expanded throughthermal expansion device 30. The refrigerant is vaporized and then enters thesecond heat exchanger 22 where thesecond location 23 rejects heat to the refrigerant before being returned to thecentrifugal compressor 12. With theflow reversing device 14 actuated to a heating configuration, the refrigerant flows to thesecond heat exchanger 22 where heat is rejected to thesecond location 23. Refrigerant then flow through thebypass valve 28 and is expanded throughthermal expansion device 26. The refrigerant is vaporized and then enters thefirst heat exchanger 20 where thefirst location 21 rejects heat to the refrigerant before being returned to thecentrifugal compressor 12. Theheat pump system 10 is intended to be exemplary only. - Referring to
FIG. 2 , thecentrifugal compressor 12 includes ahousing 39 within which anelectric motor 38 is arranged. Thehousing 38 is schematically depicted and may comprise one or more pieces. Theelectric motor 38 rotationally drives first andsecond impellers rotor shaft 40 about an axis to compress the refrigerant in a two-stage compressor configuration. Therotor shaft 40 may comprise one or more pieces. Although two compressor stages are shown, the disclosure may also be used in a compressor having more stages. In the example shown, the first andsecond impellers rotor shaft 40. The impellers are centrifugal such that the impeller inlet is arranged axially and the impeller outlet is arranged radially. - An oil-free bearing arrangement is provided for support of the
rotor shaft 40 so that oil-free refrigerant can be used in thecentrifugal compressor 12. In the example, therotor shaft 40 is rotationally supported relative to thehousing 39 bymagnetic bearings 46, which are illustrated in a schematic fashion. Themagnetic bearings 46 may include radial and/or axial magnetic bearing elements, for example. A bearing controller (not shown) communicates with the magnetic bearing 46 providing a magnetic bearing command to energize themagnetic bearings 46. The magnetic bearings create a magnetic field levitating therotor shaft 40 and controls its characteristics during operation of thecentrifugal compressor 12. It should be understood that the disclosed diffuser arrangements may also be used with air bearings or other types of bearings. - One example
electric motor 38 includes a rotor supporting multiple magnets about its circumference. A stator is arranged about the rotor to impart rotational drive to therotor shaft 40 when energized. In one example, a motor controller (not shown) communicates with the stator and provides a variable speed command to rotationally drive theimpellers 43, 44 at a variable speed depending upon compressor operating conditions. The motor controller communicates with multiple sensors (not shown) to monitor and maintain the compressor operating conditions. - The first and
second impellers first impeller 42 includes afirst stage inlet 48 and afirst stage outlet 52, and thesecond impeller 44 includes asecond stage inlet 54 and asecond stage outlet 58. First andsecond stage volutes second stage outlets - First and
second diffusers second stage outlets second stage volutes second diffusers second actuators FIG. 4 , the second compressor stage is shown as an example. Apassage 70 is arranged downstream from thesecond impeller 44. A variable geometry device, such as amovable wall 72, for example is arranged in the passage in thesecond stage outlet 58. Thesecond actuator 62 moves thewall 72 between a first position F and a second position S to selectively regulate refrigerant flow through thepassage 70. - Any number of variable geometry diffuser arrangements may be used. For example, a movable-wall variable-geometry diffuser includes a plurality of fixed wedge shaped vanes located downstream of the movable diffuser wall element. The movable wall element may be serrated with the trailing edge of the serration coinciding with the throat area (which is the smallest cross-sectional flow passage) of the vaned diffuser.
- In another variable geometry diffuser example, a rotatable vane diffuser in the plane normal to the compressor axis. By rotating the vanes, the throat area of the diffuser changes, and, therefore, the capacity of the compressor, is adjusted.
- In another variable geometry diffuser example, a split vaned diffuser has an outer diffuser ring and an inner diffuser ring. Throat area adjustment is obtained by rotating one diffuser ring with respect to the other one. Throat area of the fully opened diffuser is reduced as a result of the rotation of the inner diffuser ring relative to the outer diffuser ring.
- An
economizer 68 may be mounted to thehousing 39, as shown inFIG. 3 . In one example, theeconomizer 68 is a heat exchanger-type economizer. Theeconomizer 68 is arranged fluidly between thefirst stage outlet 52 and thesecond stage inlet 54. - Although two compressor stages are shown in
FIG. 2 , the disclosure may also be used in a compressor having more stages. For the shown direct-drive gearless multistage compressors the impellers are arranged on opposing ends of the rotor shaft (the so-called back-to-back configuration) reducing the axial thrust load of the shaft. In one example three-stage configuration, only the first compressor stage includes a variable geometry diffuser, and the second and third stages may each include a volute without a diffuser and still achieve the desired compressor pressure ratio. - Although example embodiments have been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of the claims. For that reason, the following claims should be studied to determine their true scope and content.
Claims (15)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US2012/028221 WO2013133832A2 (en) | 2012-03-08 | 2012-03-08 | High pressure ratio multi-stage centrifugal compressor |
Publications (1)
Publication Number | Publication Date |
---|---|
US20150107289A1 true US20150107289A1 (en) | 2015-04-23 |
Family
ID=49117477
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US14/383,750 Abandoned US20150107289A1 (en) | 2012-03-08 | 2012-03-08 | High pressure ratio multi-stage centrifugal compressor |
Country Status (6)
Country | Link |
---|---|
US (1) | US20150107289A1 (en) |
EP (1) | EP2823240B1 (en) |
CN (1) | CN104246394B (en) |
AU (1) | AU2012372806B2 (en) |
IN (1) | IN2014DN07521A (en) |
WO (1) | WO2013133832A2 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20170222592A1 (en) * | 2016-02-01 | 2017-08-03 | Hamilton Sundstrand Corporation | Reducing Fault Energy from an Electric Motor Drive for a Compressor |
US10212861B2 (en) * | 2017-02-24 | 2019-02-19 | Halliburton Energy Services, Inc. | Variable frequency drive cabinet ventilation system, apparatus and method |
US10666113B2 (en) | 2017-03-24 | 2020-05-26 | Johnson Controls Technology Company | Magnetic bearing motor compressor |
US20210324860A1 (en) * | 2020-04-21 | 2021-10-21 | Lg Electronics Inc. | Compressor and chiller system having the same |
US20210324876A1 (en) * | 2020-04-21 | 2021-10-21 | Lg Electronics Inc. | Compressor and chiller including the same |
US11946678B2 (en) | 2022-01-27 | 2024-04-02 | Copeland Lp | System and method for extending the operating range of a dynamic compressor |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR102213355B1 (en) | 2014-02-20 | 2021-02-08 | 댄포스 아/에스 | Control system and method for centrifugal compressor |
CN112696840B (en) * | 2020-12-18 | 2022-04-08 | 无锡同方人工环境有限公司 | All-weather wide-range bidirectional flow regulating device and regulating process thereof |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4033738A (en) * | 1976-03-12 | 1977-07-05 | Westinghouse Electric Corporation | Heat pump system with multi-stage centrifugal compressors |
US4739628A (en) * | 1986-11-28 | 1988-04-26 | Shoemaker James F | Extended range heat pump system and centrifugal compressor for use therewith |
US5857348A (en) * | 1993-06-15 | 1999-01-12 | Multistack International Limited | Compressor |
US6872050B2 (en) * | 2002-12-06 | 2005-03-29 | York International Corporation | Variable geometry diffuser mechanism |
US20100263391A1 (en) * | 2007-12-14 | 2010-10-21 | Carrier Corporation | Control Device for HVAC Systems with Inlet and Outlet Flow Control Devices |
US20110004804A1 (en) * | 2009-07-06 | 2011-01-06 | Changlong Xu | Systems and methods for channel coding of wireless communication |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4232533A (en) * | 1979-06-29 | 1980-11-11 | The Trane Company | Multi-stage economizer |
US6129511A (en) * | 1998-10-27 | 2000-10-10 | Carrier Corporation | Method and apparatus for controlling interaction between variable guide vanes and variable diffuser of a centrifugal compressor |
JP2001200797A (en) * | 2000-01-17 | 2001-07-27 | Hitachi Ltd | Multistage centrifugal compressor |
CN101268281A (en) * | 2005-09-19 | 2008-09-17 | 英格索尔-兰德公司 | Multi-stage compression system including variable speed motors |
US8037713B2 (en) * | 2008-02-20 | 2011-10-18 | Trane International, Inc. | Centrifugal compressor assembly and method |
JP4951583B2 (en) * | 2008-04-28 | 2012-06-13 | 日立アプライアンス株式会社 | Turbo refrigerator |
-
2012
- 2012-03-08 CN CN201280072447.9A patent/CN104246394B/en active Active
- 2012-03-08 US US14/383,750 patent/US20150107289A1/en not_active Abandoned
- 2012-03-08 AU AU2012372806A patent/AU2012372806B2/en not_active Expired - Fee Related
- 2012-03-08 WO PCT/US2012/028221 patent/WO2013133832A2/en active Application Filing
- 2012-03-08 IN IN7521DEN2014 patent/IN2014DN07521A/en unknown
- 2012-03-08 EP EP12870829.4A patent/EP2823240B1/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4033738A (en) * | 1976-03-12 | 1977-07-05 | Westinghouse Electric Corporation | Heat pump system with multi-stage centrifugal compressors |
US4739628A (en) * | 1986-11-28 | 1988-04-26 | Shoemaker James F | Extended range heat pump system and centrifugal compressor for use therewith |
US5857348A (en) * | 1993-06-15 | 1999-01-12 | Multistack International Limited | Compressor |
US6872050B2 (en) * | 2002-12-06 | 2005-03-29 | York International Corporation | Variable geometry diffuser mechanism |
US20100263391A1 (en) * | 2007-12-14 | 2010-10-21 | Carrier Corporation | Control Device for HVAC Systems with Inlet and Outlet Flow Control Devices |
US20110004804A1 (en) * | 2009-07-06 | 2011-01-06 | Changlong Xu | Systems and methods for channel coding of wireless communication |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20170222592A1 (en) * | 2016-02-01 | 2017-08-03 | Hamilton Sundstrand Corporation | Reducing Fault Energy from an Electric Motor Drive for a Compressor |
US10110156B2 (en) * | 2016-02-01 | 2018-10-23 | Hamilton Sunstrand Corporation | Reducing fault energy from an electric motor drive for a compressor |
US10212861B2 (en) * | 2017-02-24 | 2019-02-19 | Halliburton Energy Services, Inc. | Variable frequency drive cabinet ventilation system, apparatus and method |
US10666113B2 (en) | 2017-03-24 | 2020-05-26 | Johnson Controls Technology Company | Magnetic bearing motor compressor |
US11757328B2 (en) | 2017-03-24 | 2023-09-12 | Johnson Controls Tyco IP Holdings LLP | Magnetic bearing motor compressor |
US20210324860A1 (en) * | 2020-04-21 | 2021-10-21 | Lg Electronics Inc. | Compressor and chiller system having the same |
US20210324876A1 (en) * | 2020-04-21 | 2021-10-21 | Lg Electronics Inc. | Compressor and chiller including the same |
US11781561B2 (en) * | 2020-04-21 | 2023-10-10 | Lg Electronics Inc. | Compressor and chiller including the same |
US11946678B2 (en) | 2022-01-27 | 2024-04-02 | Copeland Lp | System and method for extending the operating range of a dynamic compressor |
Also Published As
Publication number | Publication date |
---|---|
IN2014DN07521A (en) | 2015-04-24 |
EP2823240A4 (en) | 2016-03-23 |
EP2823240B1 (en) | 2018-11-14 |
AU2012372806A1 (en) | 2014-10-02 |
WO2013133832A2 (en) | 2013-09-12 |
CN104246394B (en) | 2017-03-08 |
AU2012372806B2 (en) | 2015-12-10 |
CN104246394A (en) | 2014-12-24 |
WO2013133832A3 (en) | 2014-04-03 |
EP2823240A2 (en) | 2015-01-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AU2012372806B2 (en) | High pressure ratio multi-stage centrifugal compressor | |
US10072663B2 (en) | Variable-speed multi-stage refrigerant centrifugal compressor with diffusers | |
US10197064B2 (en) | Centrifugal compressor with fluid injector diffuser | |
US20070065300A1 (en) | Multi-stage compression system including variable speed motors | |
US9212667B2 (en) | Variable-speed oil-free refrigerant centrifugal compressor with variable geometry diffuser | |
US20160327049A1 (en) | Multi-stage compression system and method of operating the same | |
US20170260987A1 (en) | Centrifugal compressor with casing treatment bypass | |
US11808277B2 (en) | Centrifugal compressor with recirculation passage | |
JP2016532053A (en) | Multistage centrifugal compressor and air conditioning unit | |
US11698074B2 (en) | Turbo compressor and turbo chiller including the same | |
CN111373155A (en) | Compact variable geometry diffuser mechanism | |
CN111183294B (en) | Centrifugal compressor with recirculation structure | |
KR102157885B1 (en) | Turbo Compressor | |
KR20220092986A (en) | Active unloading device for mixed flow compressors | |
CN215871123U (en) | MCL compressor system with compressor directly connected with magnetic suspension motor | |
Tamaki et al. | Development of High-Efficiency Centrifugal Compressor for Turbo Chiller | |
CN113629965A (en) | MCL compressor system with compressor directly connected with magnetic suspension motor |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: DANFOSS TURBOCOR COMPRESSORS B.V., NETHERLANDS Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SUN, LIN;BRASZ, JOOST;SIGNING DATES FROM 20120306 TO 20120307;REEL/FRAME:033690/0388 |
|
AS | Assignment |
Owner name: DANFOSS A/S, DENMARK Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:DANFOSS TURBOCOR COMPRESSORS B.V.;REEL/FRAME:035813/0680 Effective date: 20140922 |
|
STPP | Information on status: patent application and granting procedure in general |
Free format text: NON FINAL ACTION MAILED |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |