This disclosure relates to cooling of a motor for a centrifugal compressor of a refrigeration system. Centrifugal refrigerant compressors are known, and include one or more impellers driven by a motor. The motor in some examples is an electric motor including a rotor and a stator. In one known example the motor is cooled by circulating refrigerant about the stator, to cool the stator, and then directing that refrigerant between the rotor and the stator to cool the rotor. After cooling the rotor, the refrigerant is returned to a refrigeration loop.
One exemplary embodiment of this disclosure includes a centrifugal compressor for a refrigeration system having an electric motor, which includes a rotor and a stator. The compressor further includes a housing enclosing the electric motor, a stator cooling passageway provided within the housing, and a rotor cooling passageway provided within the housing. The rotor cooling passageway is independent of the stator cooling passageway.
Another exemplary embodiment of this disclosure includes a centrifugal compressor for a refrigeration system including an impeller, and an electric motor including a rotor and a stator. The electric motor is configured to rotationally drive the impeller via a shaft, and the impeller is separated from the electric motor by a seal. The compressor further includes a housing enclosing the electric motor. A rotor cooling passageway is provided within the housing, and is configured to provide a flow of fluid to cool the rotor. The rotor cooling passageway is provided with a flow of fluid leaked over the seal.
A further exemplary embodiment of this disclosure includes a refrigeration system having a refrigerant loop including a condenser, an evaporator, and an expansion device. The refrigeration system further includes a compressor in fluid communication with the refrigerant loop. The compressor has an electric motor including a rotor and a stator, a housing enclosing the electric motor, a stator cooling passageway provided within the housing, and a rotor cooling passageway provided within the housing. The rotor cooling passageway is independent of the stator cooling passageway.
These and other features of the present disclosure can be best understood from the following drawings and detailed description.
The drawings can be briefly described as follows:
In this example, the compressor 12 is in fluid communication with a refrigeration loop L. While not illustrated, refrigeration loops, such as the refrigeration loop L, are known to include a condenser, an evaporator, and an expansion device. In some known examples, the refrigeration loop L circulates refrigerant to a load, such as a chiller.
In this example, as refrigerant enters an inlet end 241 of the impeller 24 and is expelled radially outward from an outlet end 240 thereof, a flow F1 is leaked over the labyrinth seal 30 (e.g., in particular, the flow F1 leaks axially between the radial clearance between the rotor shaft 22 and the labyrinth seal 30), and is directed downstream toward the first bearing assembly 26. The flow F1 is then directed out an outlet 32 of the housing 14 at a point upstream of the motor 16. The outlet 32 of the housing 14 is directed to the evaporator of the refrigerant loop L.
With further reference to
Downstream of the stator 18, the cooling flow F2 is directed toward the second bearing assembly 28, and passes axially between the rotor 20 and the stator 18 to cool the rotor. Then, the cooling flow F2 intermixes with the flow F1 at a point adjacent the first bearing assembly 26, flows to the outlet 32, and ultimately is directed to the evaporator of the refrigerant loop L.
Again, in this example, the cooling flow F2 is provided into the housing 14 initially as a liquid-vapor mixture. However, the cooling flow F2 is required to be in a gaseous state when passing between the rotor 20 and the stator 18. Thus, in the example of
In this example, a rotor cooling passageway is provided from a flow F1 leaked over the labyrinth seal 130. As used herein, the term rotor cooling passageway refers to the passageway providing fluid to cool the rotor 120. As one skilled in this art would appreciate, the rotor cooling passageway also provides cooling to the radially inner surface of the stator 118, however. As refrigerant is expelled radially outwardly from the impeller 124, a flow F1 is leaked over the labyrinth seal 130 between a radial clearance between the rotor shaft 122 and the labyrinth seal 130. The flow F1 then passes downstream to the first bearing assembly 126, and then between a radially inner surface of the stator 118 and a radially outer surface of the rotor 120. Next, the flow F1 passes downstream to the second bearing assembly 128, and then to a rotor cooling outlet 140 of the housing 114 provided downstream of the motor 116. The flow F1 is ultimately directed to the evaporator of the refrigerant loop L, in one example.
Regarding the stator cooling passageway, a flow of fluid F2 is tapped from the refrigerant loop L, and may optionally be expanded by an expansion device 142 before entering a stator cooling inlet 144 of the housing 114. Downstream of the stator cooling inlet 144, the fluid F2 circulates radially around the stator 118 by way of a circumferential passageway 136. After circulating about the stator 118, the fluid F2 is directed to a stator cooling outlet 148, and ultimately back to the refrigerant loop L, in this example to the evaporator. Accordingly, the rotor and stator cooling passageways are independent of one another, as the fluid cooling the stator 118 is not also used to cool the rotor 120. In other words, the stator 118 and the rotor 120 are cooled in parallel, and not in series like in the prior art system of
The impeller 124 compresses refrigerant in a gaseous state. The flow F1 is thus initially in a gaseous state, and remains in a gaseous state as it flows within the rotor cooling passageway to cool the rotor 120. Accordingly, there is no need to continually monitor the fluid cooling the rotor for a phase change, and thus the superheat controller of
In
Although the different examples have the specific components shown in the illustrations, embodiments of this disclosure are not limited to those particular combinations. It is possible to use some of the components or features from one of the examples in combination with features or components from another one of the examples.
One of ordinary skill in this art would understand that the above-described embodiments are exemplary and non-limiting. That is, modifications of this disclosure would come within the scope of the claims. Accordingly, the following claims should be studied to determine their true scope and content.
Filing Document | Filing Date | Country | Kind |
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PCT/US2013/045391 | 6/12/2013 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2014/200476 | 12/18/2014 | WO | A |
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Entry |
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International Preliminary Report for International Application No. PCT/US2013/045391 dated Dec. 23, 2015. |
Number | Date | Country | |
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20160138841 A1 | May 2016 | US |