TURBO CHILLER

Abstract

A turbo chiller that has an oil-free configuration, which reduces the frequency of maintenance and maintenance-induced release of refrigerant, and can achieve a reduced environmental impact by utilizing the characteristics of the low-pressure refrigerant R1233zd(E) that reaches negative pressure at a saturation temperature of 18° C. or lower. The turbo chiller comprises a refrigeration cycle that includes a turbo compressor, a condenser, a decompression device, and an evaporator connected in sequence via piping and is filled with a refrigerant; wherein the refrigerant is a low-pressure refrigerant R1233zd(E) refrigerant with low global warming potential and low ozone depletion potential; the turbo compressor has a direct drive configuration in which a rotating shaft of impellers is directly joined to a motor; and the rotating shaft is supported by magnetic bearings.

Claims

1. A turbo chiller comprising: a closed refrigeration cycle that includes a turbo compressor, a condenser, a decompression device, and an evaporator connected in sequence via piping and is filled with a refrigerant; wherein the refrigerant is a low-pressure refrigerant R1233zd(E) refrigerant with low global warming potential and low ozone depletion potential; the turbo compressor has a direct drive configuration in which a rotating shaft of an impeller is directly joined to a motor; the motor is disposed inside a motor housing; the motor housing includes an extension portion that extends an internal space of the motor housing in a direction intersecting with the rotating shaft; the extension portion is provided only at a position that does not overlap with a center portion of the motor as seen from a direction perpendicular to the rotating shaft; and the rotating shaft is supported by a magnetic bearing.

2. A turbo chiller comprising: a closed refrigeration cycle that includes a turbo compressor, a condenser, a decompression device, and an evaporator connected in sequence via piping and is filled with a refrigerant; wherein the refrigerant is a low-pressure refrigerant R1233zd(E) refrigerant with low global warming potential and low ozone depletion potential; the turbo compressor has a direct drive configuration in which a rotating shaft of an impeller is directly joined to a motor; the motor is disposed inside a motor housing; the motor housing includes an extension portion that extends an internal space of the motor housing in a direction intersecting with the rotating shaft, and the motor housing has a stepped surface formed between the extension portion and another portion of the motor housing; the stepped surface is provided only at a position that avoids a center portion of the motor as seen from a direction perpendicular to the rotating shaft; the extension portion is configured to store liquid, and the rotating shaft is supported by a magnetic bearing.

3. The turbo chiller according to claim 1, wherein the extension portion is a refrigerant sump in which the refrigerant is collected.

4. The turbo chiller according to claim 1, wherein the extension portion extends the internal space of the motor housing in a gravity direction.

5. The turbo chiller according to claim 1, wherein the extension portion is disposed between the motor and the impeller as seen from the direction perpendicular to the rotating shaft.

6. The turbo chiller according to claim 1, wherein the extension portion is connected with a refrigerant discharge pipe.

7. The turbo chiller according to claim 2, wherein the stepped portion is disposed between the motor and the impeller as seen from the direction perpendicular to the rotating shaft.

8. The turbo chiller according to claim 2, wherein the extension portion is a refrigerant sump in which the refrigerant is collected.

9. The turbo chiller according to claim 2, wherein the extension portion extends the internal space of the motor housing in a gravity direction.

10. The turbo chiller according to claim 2, wherein the extension portion is connected with a refrigerant discharge pipe.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0023] FIG. 1 is a configuration diagram illustrating a turbo chiller according to a first embodiment of the present invention.

[0024] FIG. 2 is a schematic configuration diagram illustrating a turbo compressor applied to the turbo chiller.

[0025] FIG. 3 is a schematic configuration diagram illustrating a turbo compressor according to a second embodiment of the present embodiment.

[0026] FIG. 4 is an enlarged view of a portion of a drive motor for the turbo compressor illustrated in FIG. 3.

DESCRIPTION OF THE EMBODIMENTS

[0027] Embodiments of the present invention will be described below with reference to the attached drawings.

First Embodiment

[0028] A first embodiment of the present invention will be described below, using FIGS. 1 and 2.

[0029] FIG. 1 illustrates a configuration diagram of a turbo chiller according to the first embodiment. FIG. 2 illustrates a schematic configuration diagram of a turbo compressor applied to the turbo chiller.

[0030] The turbo chiller 1, as illustrated in FIG. 1, is provided with a closed refrigeration cycle 9 in which a turbo compressor 2, a condenser 3, a first decompression device 4, a gas-liquid separator 5 that functions as an economizer, a second decompression device 6, and an evaporator 7 are connected in sequence via a refrigerant pipe (piping) 8.

[0031] The refrigeration cycle 9 of the present embodiment is further provided with a known economizer circuit 10 configured to inject the gas refrigerant separated at the gas-liquid separator 5 into the intermediate pressure refrigerant compressed at a lower stage compression portion 14 of the turbo compressor 2 via an intermediate port. The economizer circuit 10 here is of a gas-liquid separation type provided with the gas-liquid separator 5. However, the economizer circuit 10 may be of an intercooler type with an intercooler for providing heat exchange between a liquid refrigerant and a portion of the refrigerant condensed and liquefied at the condenser 3 which is branched off and decompressed. Note that the economizer circuit 10 is not required in the present invention.

[0032] The refrigeration cycle 9 described above is filled with R1233zd(E) refrigerant at the necessary amount. The R1233zd(E) refrigerant has a low global warming potential (GWP) of 5 or less and a low ozone depletion potential (ODP) of 0.00031, and reaches negative pressure at a saturation temperature of 18° C. or lower. The R1233zd(E) refrigerant is a hydrochlorofluoroolefin (HCFO) refrigerant with a low GWP. The R1233zd(E) refrigerant is a low-pressure refrigerant with low density, having approximately ⅕ of the density of R134a, a hydrofluorocarbon (HFC) refrigerant used in conventional turbo chillers.

[0033] In the present embodiment, the turbo compressor 2 installed in the turbo chiller 1 filled with the R1233zd(E) refrigerant has the following configuration.

[0034] FIG. 2 is a schematic configuration diagram of the turbo compressor 2.

[0035] The turbo compressor 2 may be a known centrifugal compressor that compresses low-pressure gas refrigerant into high-pressure gas refrigerant via a rotating impeller and circulates the high-pressure gas through the refrigeration cycle 9.

[0036] The turbo compressor 2 of the present embodiment has a direct drive configuration in which a rotating shaft 18 is directly joined to a rotor 19A of a motor 19. A lower stage and upper stage impeller 15, 17 rotate about the rotating shaft 18 driven by the motor 19. The rotating shaft 18 is supported in a manner allowing for free rotation by a pair of radial magnetic bearings 20, 21 disposed at the front and rear with respect to a housing 11 and by a pair of thrust magnetic bearings 23, 24 disposed in opposition.

[0037] In other words, the turbo compressor 2 has the following configuration. The turbo compressor 2 is provided with the housing 11, which includes a compressor housing 11A and a motor housing 11B integrated with the compressor housing 11A. The low-pressure gas refrigerant evaporated at the evaporator 7 is taken in from a refrigerant suction port 12 and passes through an inlet vane 13. Thereafter, the low-pressure gas refrigerant is compressed in two stages, at the lower stage compression portion 14 with the lower stage impeller 15 and an upper stage compression portion 16 with the upper stage impeller 17, and becomes a high-temperature high-pressure gas refrigerant. The high-temperature high-pressure gas refrigerant is discharged from a discharge port of the scroll casing to the condenser 3 outside. The intermediate pressure refrigerant gas is injected from the economizer circuit 10 between the lower stage compression portion 14 and the upper stage compression portion 16 via the intermediate port.

[0038] The lower stage impeller 15 and the upper stage impeller 17 are integrally joined to the rotating shaft 18 on the end to one side of the rotating shaft 18, separated by a predetermined interval. The rotating shaft 18 is joined to a rotor 19B of the motor 19, and thus the rotating shaft 18 of the impellers 15, 17 is directly joined to the motor 19. Additionally, the motor 19 is provided with the rotor 19A and a stator 19B, is substantially centrally disposed inside the motor housing 11B, and is configured to variably control RPM via an inverter, which is not illustrated. An air gap 19D is provided.

[0039] The rotating shaft 18 described above is supported in a manner allowing for free rotation by the pair of radial magnetic bearings 20, 21 disposed at the front and rear of the motor 19. At the rear portion, a thrust disk 22 is disposed in a fixed manner. The pair of thrust magnetic bearings 23, 24 are disposed on opposite sides of the thrust disk 22 in opposition and also support the rotating shaft 18. Note that the pair of thrust magnetic bearings 23, 24 are imparted with magnetic attraction force when current is supplied through the coil, and by centrally disposing the thrust disk 22, the thrust load received by the rotating shaft 18 is supported.

[0040] According to the configuration described above, the present embodiment has the following actions and effects.

[0041] In the turbo chiller 1 described above, by driving the turbo compressor 2, the low-pressure gas refrigerant evaporated at the evaporator 7 is taken in from the suction port 12 and passes through the inlet vane 13. The low-pressure refrigerant is centrifugally compressed in two stages at the lower stage compression portion 14 and the upper stage compression portion 16, first from low pressure to intermediate pressure, then from intermediate pressure to high pressure via the lower stage impeller 15 and the upper stage impeller 17 that are rotating at high speed. After being discharged to the scroll casing, the refrigerant is fed to the condenser 3 outside.

[0042] The refrigerant exchanges heat with a cooling medium at the condenser 3 and is condensed and liquefied. The condensed and liquefied refrigerant passes through the first decompression device 4, the gas-liquid separator 5 that functions as an economizer, and the second decompression device 6 and is subcooled and reduced to a low pressure, before being guided to the evaporator 7. The low-pressure liquid refrigerant guided to the evaporator 7 exchanges heat with a medium to be cooled, absorbs heat from the medium to be cooled thus cooling the medium to be cooled, and itself becoming vaporized. The vaporized refrigerant is then taken into the turbo compressor 2 and compressed once again, and the operation repeats.

[0043] Additionally, the economizer function of improving the cooling performance may be achieved by the liquid refrigerant that was separated at the gas-liquid separator 5, evaporated, and has subcooled the liquid refrigerant being injected into the intermediate pressure gas refrigerant compressed at the lower stage compression portion 14 from the intermediate port of the turbo compressor 2 via the economizer circuit 10.

[0044] The refrigeration cycle 9 of the turbo chiller 1 is filled with the R1233zd(E) refrigerant. The R1233zd(E) refrigerant is a low-pressure refrigerant with low density, and has low global warming potential (GWP) and low ozone depletion potential (ODP). This refrigerant has been considered to have difficulties involved in ensuring suitable performance. However, in the present embodiment, a turbo compressor 2 suitable for high flow rate refrigerant compression has a configuration in which the rotating shaft 18 of the impellers 15, 17 is directly joined to the motor 19, and the rotating shaft 18 is supported by the radial magnetic bearings 20, 21 and the thrust magnetic bearings 23, 24.

[0045] Accordingly, power loss at the speed-increasing gear unit and bearing losses of rolling bearings are reduced, allowing the turbo compressor 2 to have higher rotation suitable for high flow rate refrigerant compression, thus compensating for inherent problems with using the R1233zd(E) refrigerant, which has been considered to have difficulties involved in ensuring suitable performance due to the low density of the low-pressure refrigerant and its high sonic velocity compared to HFC refrigerants. Additionally, by having an oil-free configuration without a speed-increasing gear unit or rolling bearings that require oil lubrication, the maintenance of lubrication systems such as the changing of lubricant oil and oil filters can be omitted.

[0046] Thus, a turbo chiller 1 can be provided in which necessary performance can be ensured with the application of the R1233zd(E) refrigerant, which is a low-pressure refrigerant with low density. Additionally, the turbo chiller 1 has a reduced environmental impact due to the frequency of maintenance and maintenance-induced release of refrigerant being reduced and the characteristics of a refrigerant that reaches negative pressure at a saturation temperature of 18° C. or lower being utilized so that the refrigerant is prevented from being released into the atmosphere. Furthermore, a highly reliable turbo chiller 1 can be provided at low cost due to the simplified configuration in which a lubrication system is omitted.

[0047] Note that in the embodiment described above, an example of a turbo compressor 2 with two stage compression has been described. However, in the present invention, the turbo compressor 2 is not limited to have two stage compression and may have single stage, or three or more stage compression. In other words, it is only required that the turbo compressor 2 have a direct drive configuration in which the rotating shaft 18 of an impeller(s) is directly joined to the motor 19 and the rotating shaft 18 is supported by magnetic bearings.

Second Embodiment

[0048] Next, a second embodiment of the present invention will be described using FIGS. 3 and 4.

[0049] The present embodiment is different from the first embodiment in that the rotating shaft 18 is supported in a manner allowing free rotation by oil-free ceramic bearings 25, 26. Other points are similar to the first embodiment, so their descriptions are omitted here.

[0050] In the present embodiment, the rotating shaft 18 is supported in a manner allowing for free rotation by the oil-free ceramic slide bearings or rolling bearings 25, 26 (hereinafter, in the present invention, referred to as ceramic bearings) as illustrated in FIG. 3, instead of the radial magnetic bearings 20, 21 and the thrust magnetic bearings 23, 24.

[0051] The ceramic bearings 25, 26 are made from silicon nitride, have high durability, and a long lifetime despite being oil-free. In the present embodiment, the ceramic bearings 25, 26 can be cooled and lubricated by liquid refrigerant extracted from the refrigeration cycle 9. In other words, a portion of high-pressure liquid refrigerant condensed and liquefied at the condenser 3 from the refrigeration cycle 9 or a portion of low-pressure liquid refrigerant from the piping or a device between the condenser 3 and the evaporator 7 is extracted via a refrigerant extraction pipe 27. The flow rate of the extracted liquid refrigerant is adjusted at a flow rate control valve 28 and supplied to bearing housings 25A, 26A of the ceramic bearings 25, 26. As a result, the ceramic bearings 25, 26 can be cooled and lubricated by the liquid refrigerant.

[0052] In the present embodiment, in addition to the ceramic bearings 25, 26, the motor 19 can also be cooled by the liquid refrigerant described above. In such a configuration, a portion of the liquid refrigerant introduced through the refrigerant extraction pipe 27 and the flow rate control valve 28 is introduced into an air gap 19D of the motor 19 through a refrigerant introduction hole 19C provided in the stator 19B of the motor 19, enabling the rotor 19A and the stator 19B to be cooled. After cooling the ceramic bearings 25, 26 and the motor 19, the refrigerant is collected in a refrigerant sump 29 of the motor housing 11B before being returned to the low-pressure region of the refrigeration cycle 9, i.e. the evaporator 7 and the like, via a refrigerant discharge pipe 30.

[0053] Additionally, to reduce windage loss at the motor 19 by the swift discharge of the liquid refrigerant introduced into the air gap 19D, as illustrated in FIG. 4, helical grooves 32A, 32B, 32C, which allow the liquid refrigerant supplied into the air gap 19D to flow axially outward, are provided on at least one of the outer peripheral surface of the rotor 19A of the motor 19, the inner peripheral surface of the stator 19B, and the outer peripheral surface of a balance ring 31 provided on an end surface of the rotor 19A. Note that of the helical grooves 32A, 32B, 32C, from a machining standpoint, the helical groove 32C is most preferably provided on the outer peripheral surface of the balance ring 31.

[0054] According to this embodiment in which the rotating shaft 18 is supported by the oil-free ceramic bearings 25, 26, in a similar manner to that of the first embodiment, power loss at the speed-increasing gear unit and bearing losses of rolling bearings are reduced, allowing for the turbo compressor 2 to have higher rotation suitable for high flow rate refrigerant compression, thus compensating for inherent problems with using the R1233zd(E) refrigerant, which has been considered to have difficulties involved in ensuring suitable performance due to the low density of the low-pressure refrigerant and its high sonic velocity compared to conventional HFC refrigerants. Additionally, by having an oil-free configuration without a speed-increasing gear unit or rolling bearings that require oil lubrication, the maintenance of lubrication systems such as the changing of lubricant oil and oil filters can be omitted.

[0055] Thus, a turbo chiller 1 can be provided in which necessary performance can be ensured with the application of the R1233zd(E) refrigerant, which is a low-pressure refrigerant with low density. Additionally, the turbo chiller 1 has a reduced environmental impact due to the frequency of maintenance and maintenance-induced release of refrigerant being reduced and the characteristics of a refrigerant that reaches negative pressure at a saturation temperature of 18° C. or lower being utilized so that the refrigerant is prevented from being released into the atmosphere. Furthermore, a highly reliable turbo chiller 1 can be provided at low cost due to the simplified configuration in which a lubrication system is omitted.

[0056] Additionally, the liquid refrigerant which acts as a cooling and lubricating medium for the bearing housings 25A, 26A of the ceramic bearings 25, 26 and the air gap 19D of the motor 19 can be circulated through the refrigerant extraction pipe 27, the flow rate control valve 28, and the refrigerant discharge pipe 30 from the refrigeration cycle 9. By the ceramic bearings 25, 26 being cooled and lubricated by the liquid refrigerant, the durability of the ceramic bearings 25, 26 can be improved, and heat loss and failsafe operations can be reduced by ensuring the cooling performance of the liquid refrigerant cooling the high rotation motor 19. This configuration successfully cools and lubricates the oil-free ceramic bearings 25, 26 and the motor 19, with their improved durability and performance, which imparts high performance and reliability to the turbo chiller 1.

[0057] Furthermore, in the embodiment described above, the helical grooves 32A, 32B, 32C, which allow the liquid refrigerant supplied into the air gap 19D of the motor 19 to flow axially outward, are provided on at least one of the inner peripheral surface of the stator 19B of the motor 19, the outer peripheral surface of the rotor 19A, and the outer peripheral surface of the balance ring 31 provided on the end surface of the rotor 19A. Accordingly, the liquid refrigerant supplied into the air gap 19D can be swiftly discharged axially outward via the helical grooves 32A, 32B, 32C. Thus, the cooling effect of the liquid refrigerant on the motor 19 can be further improved, and the motor efficiency can be further increased by the reduction in windage loss of the motor 19 due to the agitated liquid refrigerant.

[0058] Additionally, in the embodiment described above, the motor 19 is cooled by introducing high-pressure liquid refrigerant or low-pressure liquid refrigerant from the refrigerant introduction hole 19C. However, instead of liquid refrigerant, low-pressure gas refrigerant formed by evaporation at the evaporator 7 may be introduced to cool the motor 19. In a configuration in which low-pressure gas refrigerant is introduced as the cooling medium for the motor 19, the agitation loss due to the motor 19 can be reduced more than in configurations in which liquid refrigerant is introduced. As a result, the motor 19 can be sufficiently cooled, thus allowing heat loss and the like to be reduced; and agitation loss can be further reduced, giving the motor 19 high efficiency, and enabling higher rotations.

[0059] Note that the present invention is not limited to the invention according to the above-described embodiments and can be modified as required without departing from the spirit of the present invention. For example, in the embodiments described above, an example of an application of the refrigeration cycle 9 provided with the economizer circuit 10 has been described. However, a heat pump cycle of a turbo heat pump can be similarly applied. Additionally, the first embodiment may have a configuration similar to that of the second embodiment in which the magnetic bearings 20, 21, 23, 24 and the motor 19 are able to be cooled by the refrigerant.

REFERENCE SIGNS LIST

[0060] 1 Turbo chiller [0061] 2 Turbo compressor [0062] 3 Condenser [0063] 4 First decompression device [0064] 5 Gas-liquid separator [0065] 6 Second decompression device [0066] 7 Evaporator [0067] 8 Refrigerant pipe (piping) [0068] 9 Refrigeration cycle [0069] 10 Economizer circuit [0070] 11 Housing [0071] 11A Compressor housing [0072] 11B Motor housing [0073] 12 Refrigerant suction port [0074] 12 Inlet vane [0075] 14 Lower stage compression portion [0076] 15 Lower stage impeller [0077] 16 Upper stage compression portion [0078] 17 Upper stage impeller [0079] 18 Rotating shaft [0080] 19 Motor [0081] 19A Rotor [0082] 19B Stator [0083] 19C Refrigerant introduction hole [0084] 19D Air gap [0085] 20, 21 Radial magnetic bearing [0086] 22 Thrust disk [0087] 23, 24 Thrust magnetic bearing [0088] 25, 26 Ceramic bearing [0089] 25A, 26A Bearing housing [0090] 27 Refrigerant extraction pipe [0091] 28 Flow rate control valve [0092] 29 Refrigerant sump [0093] 30 Refrigerant discharge pipe [0094] 31 Balance ring [0095] 32A, 32B, 32C Helical groove