The present disclosure relates generally to compressor centrifugal compressors, and more specifically to a centrifugal compressor including a discharge pressure equalization feature.
This application claims priority to U.S. Provisional Application No. 62/847,360 filed on May 15, 2019.
Rotary machines, such as centrifugal compressors, are commonly utilized in refrigeration and turbine applications. Centrifugal compressors include an impeller that drives and compresses a fluid and provides the compressed fluid to a discharge plenum. The discharge plenum distributes the compressed fluid to a system configured to utilize the compressed fluid. Non-Uniform provision of pressure to the diffuser impacts the upstream space between the impeller and the diffuser inlets and can have a negative impact on compressor operations.
Centrifugal compressors have a range of viable operations, with the range being controlled by a choke dictated by the diffuser configuration and a surge dictated by the impeller and diffuser configuration and flow interaction. In some compressor configurations an outlet of the impeller is connected to the diffuser via multiple distinct passages. Such a configuration can have a reduced range resulting at least in part from local non-uniformity of flow through each of the distinct passages as described above.
In one exemplary embodiment a centrifugal compressor includes an impeller configured to drive fluid along a fluid flowpath via a plurality of discrete passages, each of the discrete passages including a discrete passage exit, a diffuser portion disposed circumferentially about the impeller, the diffuser portion including a plenum connected to each exit of the discrete passages via a plurality of diffuser inlets, and an equalization plenum defined adjacent to the impeller, the equalization plenum being fluidly connected to each discrete passage exit via a corresponding slot.
In another example of the above described centrifugal compressor each corresponding slot is an intrusion defined in a diffuser portion body.
In another example of any of the above described centrifugal compressors each corresponding slot is a hole in a radially outward flowpath wall near the exit of the impeller.
The centrifugal compressor of claim 1, wherein the equalization plenum is sealed such that the corresponding slots are the only inlet and outlet to the equalization plenum.
In another example of any of the above described centrifugal compressors the equalization plenum is disposed on a hub side of the impeller.
In another example of any of the above described centrifugal compressors the equalization plenum is disposed on a shroud side of the impeller.
In another example of any of the above described centrifugal compressors the equalization plenum includes a hub side portion and a shroud side portion.
In another example of any of the above described centrifugal compressors the diffuser portion is connected to a compressor outlet via a volute.
In another example of any of the above described centrifugal compressors the slots are defined at least partially in a diffuser portion body.
In another example of any of the above described centrifugal compressors the slots are defined at least partially in an impeller body.
In one exemplary embodiment a centrifugal compressor includes an impeller including a plurality of discrete passages, each of the discrete passages including a discrete passage exit, and an equalization plenum fluidly connected to each discrete passage exit.
In another example of the above described centrifugal compressor the equalization plenum is fluidly connected to each discrete passage exit via a plurality of equalization slots.
In another example of any of the above described centrifugal compressors each equalization slot in the plurality of equalization slots connects an exit of one of the discrete passages in the plurality of discrete passages to the equalization plenum.
In another example of any of the above described centrifugal compressors the equalization plenum is sealed such that the plurality of equalization slots is the only inlet and outlet to the equalization plenum.
In another example of any of the above described centrifugal compressors the equalization plenum is disposed on a shroud side of the impeller.
In another example of any of the above described centrifugal compressors the equalization plenum is disposed on a hub side of the impeller.
In another example of any of the above described centrifugal compressors the equalization plenum includes a first portion and a second portion distinct from the first portion.
In another example of any of the above described centrifugal compressors the first portion is disposed on a hub side of the impeller and the second portion is disposed on a shroud side of the impeller.
In another example of any of the above described centrifugal compressors the centrifugal compressor is a mixed-flow centrifugal compressor.
An exemplary method for equalizing pressure at a centrifugal compressor diffuser inlet, the method includes fluidly connecting an outlet of a plurality of discrete impeller passages with an equalization plenum.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
The impeller 16 defines multiple distinct passages 22 each of which turns the incoming fluid from an axial flow direction to a radial flow direction. The passages 22 expel the fluid from the impeller 16 into a diffuser section 30 through multiple diffuser section inlets 32. The diffuser section 30 is generally circumferentially disposed about the impeller 16 and directs the compressed fluid toward a compressor outlet. In one example, the fluid is directed into a volute which directs the fluid toward the compressor outlet see
Due to the distinct passages 22, the fluid pressure at an exit 24 of each passage 22 can be different from the fluid pressure at the exit of one or more other of the passages 22. This variance is referred to as a local non-uniformity and can increase the occurrence of surge within the compressor 10. An increase in surge can cause a decrease in the total range of the compressor, which in turn decreases the overall performance of the system. In addition to the discrete passages, manufacturing variations in a body 31 defining the diffuser section 30 can create a non-uniformity at the throat of the diffuser portion which will likewise increase the surge behavior, and decrease the range of operations of the compressor 10.
Also included in the compressor 10 is a plenum 11 disposed on a shroud side 2 of the impeller 16. Each of the passages 22 is fluidly connected to the plenum 11 via a slot 40. The fluid connection with the plenum 11, by extension, connects an exit 24 of each of the passages 22 to the exit 24 of each other passage 22 through the plenum 11 and the slots 40. By connecting the passages 22 via the plenum 11, the centrifugal compressor 10 is able to provide a more uniform pressure field across the fluid exits 24 of the impeller 16 as the fluid is provided to the diffuser section 30, thereby reducing non-uniformity of flow into the diffuser section 30.
In some examples, the plenum 11 is a sealed plenum, with the only inlets and outlets being the slots 40. As a result, when the local pressure at one of the exits 24 exceeds the pressure within the plenum 11, the corresponding slot 40 allows for compressed fluid to pass into the plenum 11 and the local pressure at the exit 24 is decreased. Conversely, when the fluid pressure at an exit 24 is lower than the pressure within the plenum 11 fluid from the plenum 11 is provided to the exit 24 and the local pressure at the exit 24 is increased. As both of these features occur simultaneously, and throughout operation of the centrifugal compressor 10, the localized pressure at any given exit 24 is equalized, and the local non-uniformity of fluid pressure being provided into the diffuser section 30 is substantially reduced.
With continued reference to
The impeller 116 defines multiple distinct passages 122 each of which turns the incoming fluid from an axial flow direction to a radial flow direct. The passages 122 expel the fluid from the impeller 116 into a diffuser section 130 through multiple diffuser section inlets 132. The diffuser section 130 is generally circumferentially disposed about the impeller 116 and directs the compressed fluid toward a compressor outlet.
Unlike the example of
Slots 140 are defined in the impeller 116 body and the diffuser portion body 131. The slots 140 fluidly connect each of the exits 124 to the hub side equalization plenum 150. The hub side equalization plenum 150 operates to equalize the local pressure at the exits 124 in the same manner as the shroud side equalization plenum 11 of
With continued reference to
The impeller 216 defines multiple distinct passages 222 each of which turns the incoming fluid from an axial flow direction to a radial flow direct. The passages 222 expel the fluid from the impeller 216 into a diffuser section 230 through multiple diffuser section inlets 232. The diffuser section 230 is generally circumferentially disposed about the impeller 216 and directs the compressed fluid toward a compressor outlet 236 through a volute 234.
In the example of
With reference to all of
While described and illustrated herein with reference to a mixed flow centrifugal compressor, it is appreciated that the local non-uniformity mitigating feature provided by the equalization plenums can be applied to any alternative centrifugal flow compressor and are not limited to the specific example described and illustrated herein.
It is further understood that any of the above described concepts can be used alone or in combination with any or all of the other above described concepts. Although an embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.
Filing Document | Filing Date | Country | Kind |
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PCT/US2020/032069 | 5/8/2020 | WO |
Publishing Document | Publishing Date | Country | Kind |
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WO2020/231798 | 11/19/2020 | WO | A |
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International search Report and Written Opinion for International Application No. PCT/US2020/032069 dated Jul. 31, 2020. |
International Preliminary Report on Patentability for International Patent Application No. PCT/US2020/032069 completed on Nov. 16, 2021. |
Number | Date | Country | |
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20210270289 A1 | Sep 2021 | US |
Number | Date | Country | |
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62847360 | May 2019 | US |