Patent Grant
11002288
This application is a US 371 Application from PCT/CN2017/103127 filed Sep. 25, 2017, which claims priority to Chinese Application No. 201611102983.5 filed Dec. 5, 2016, the technical disclosures of which are hereby incorporated herein by reference.
The invention relates to the technical field of a centrifugal compressor, and particularly, to an integrated structure of a return device and a pressure diffuser, and a centrifugal compressor.
A centrifugal compressor, also known as a radial flow compressor, is widely used in various processes, mainly for conveying air, various process gases or mixed gases, and increasing their pressure. The multi-stage centrifugal compressor generally includes a main shaft, a first-stage impeller, a first-stage pressure diffuser cover plate, a first-stage pressure diffuser, a return device, a second-stage impeller, a second-stage pressure diffuser cover plate, and a second-stage pressure diffuser. When the compressor is operating, the main shaft drives the first-stage impeller to rotate, and the gas from the gas intake chamber is thrown by the first-stage impeller into the first-stage pressure diffusion flow channel formed by the first-stage pressure diffuser cover plate and the first-stage pressure diffuser; after the gas passes through the first-stage pressure diffusion flow channel, it enters the gas intake flow passage upstream of the second-stage impeller; the second-stage impeller is also driven by the main shaft to rotate, and the gas from the gas intake flow channel is thrown by the second-stage impeller into the second-stage pressure diffusion flow channel formed by the second-stage pressure diffuser cover plate and the second-stage pressure diffuser; in this process, the gas is gradually compressed and thus has a high pressure. In a centrifugal compressor, the function of the return device is to guide a flow and the strong swirling gas flow flowing out of the first-stage pressure diffuser to uniformly enter the next stage impeller in a circumferential direction or in a specific direction.
In the prior art, the return device is usually a separate component, which is connected to the pressure diffuser by screws, pins or welding, so as to be fastened and positioned. This type of structure in the prior art has the following technical defects: (1) the assembly precision is low; the energy loss is large; when the return device, as a separate component, is connected with the diffuser, it needs to be aligned first and then it is connected by screws, pins or welding; in the process, there are not only connection seams generated, but also misalignment easily caused by accumulated errors; when the gas from the pressure diffuser flow channel impacts at the connection seams or the misalignment position, there will be a larger energy loss, such as the kinetic energy loss and the impact loss, etc.; (2) the assembly efficiency is low; since high precision installation is needed, the assembly rate is slow, and the efficiency is low; (3) after the return device is connected with the pressure diffuser, there is a gap between the end of the return device vane and the pressure diffuser, and the gas from the pressure diffusion flow channel is easily leaked from the gap, thus avoiding the flow guiding action of the return device, affecting the gas guided by the return device and impairing the gas flow uniformity; (4) if the return device and the pressure diffuser are connected by screws or pins, threaded holes are needed to be provided in the return device vane, then the screws or pins can go through the pressure diffuser to thread with the threaded holes, so as to realize a fixation; with such a connection manner, the return device vane has to have a certain thickness, which results in that a small number of vanes can be arranged in the return device, and results in that a difference between the vane angle and the gas flow angle of the gas impact is large, and a larger gas impact angle is generated, which is unfavorable for guiding flow and causes energy loss, such as the impact loss.
Therefore, the technical problem to be solved by the present invention is to overcome the technical defects that, the return device in the prior art, as a separate component, is connected with the pressure diffuser by screws, pins or welding, which will result in low assembly efficiency and a large energy loss. The objective of the present invention is to provide an integrated structure of a return device and a compressor diffuser, which has high assembly efficiency and low energy loss.
The present invention further provides a centrifugal compressor including an integrated structure of a return device and a compressor diffuser.
For this purpose, the present invention provides an integrated structure of a return device and a pressure diffuser, including a pressure diffuser portion and a return device portion integrally molded with the pressure diffuser portion; the pressure diffuser portion is configured to form a pressure diffusion flow channel; the return device portion has a return channel; the return channel is in communication with the pressure diffusion flow channel, and is configured to guide gas from the pressure diffusion flow channel.
In an embodiment, the pressure diffuser portion and the return device portion are integrally molded by casting.
In an embodiment, the return channel has an inlet and an outlet, and a width a of the inlet is less than or equal to a width b of the outlet.
In an embodiment, the width b of the outlet is configured to be not greater than four times the width a of the inlet.
In an embodiment, one side of the return channel is vertical, and another side of the return channel is gradually flared outward in a direction from the inlet to the outlet; an angle between said another side and a vertical direction is β, wherein, 0≤β≤45°.
In an embodiment, an inner wall of the return channel is provided with return vanes; and the return vanes are distributed evenly in serial arrays or in a single array.
In an embodiment, an outer edge of the return vane is rigidly connected with an inner wall of the return channel; a vane mounting angle α is formed between a first tangent line of the return vane, which is located at a position where the return vane contacts with the inner wall of the return channel, and a second tangent line of the inner wall of the return channel, which is located at the position; and the vane mounting angle a is ranged from 10° to 80°.
In an embodiment, the integrated structure of the return device and the pressure diffuser further includes pressure diffusion vanes, which are arranged inside the pressure diffusion flow channel.
In an embodiment, a width of the pressure diffusion vane is not greater than a width of an impeller, and the impeller is arranged opposite to the pressure diffusion vane to feed gas into the pressure diffusion flow channel.
The present invention further provides a centrifugal compressor, including a main shaft, an impeller installed on the main shaft, and a pressure diffuser cover plate; the centrifugal compressor further includes any one of the integrated structure of the return device and the pressure diffuser above; and the pressure diffuser cover plate is opposite to the pressure diffuser portion to form the pressure diffusion flow channel.
In an embodiment, the centrifugal compressor has at least two stages; an accommodating space is disposed between the return device portion of a front stage and a second-stage impeller of a subsequent stage; the accommodating space is in communication with a gas supplying passage, and the gas supplying passage is configured to supply gas into the accommodating space.
In an embodiment, the gas supplying passage is in communication with an expansion valve, and configured to feed a part of refrigerant expanded by the expansion valve into the accommodating space to lower temperature and to supply gas.
The technical solutions provided by the present invention have the following advantages:
1. The integrated structure of the return device and the pressure diffuser of the present disclosure includes the pressure diffuser portion and the return device portion, and the pressure diffuser portion and the return device portion are integrated to be one component, which is no longer a prior art structure formed by secondarily connecting and integrating a separate pressure diffuser and a separate return device with screws, pins or welding. With such a configuration, the integrated structure of the present invention not only eliminates a need of independently installing a return device and a pressure diffuser, but also eliminates connection seams caused by assembly and misalignment caused by accumulated errors, etc. Therefore, the gas can smoothly flow from the pressure diffusion flow channel into the return channel, and the energy loss is small; by integrating the return device portion and the pressure diffuser portion, the return vane is separately arranged in the return channel and needs not to be connected to the pressure diffuser any longer, which eliminates the problem in the prior art that air leakage is caused due to a seam between the end of the return vane and the pressure diffuser, and eliminates the phenomenon that part of the gas is leaked from the seam, avoiding the guiding action of the return device and affecting the gas guided by the return device. Therefore, when the integrated structure of the present invention is applied in a centrifugal compressor, it can improve the flow guiding effect and the gas flow uniformity. Preferably, the pressure diffuser portion and the return device portion are integrally molded by casting.
2. In the integrated structure of the present invention, the gas flow flowing from the pressure diffusion flow channel into the return channel is an unstable flow with a larger velocity, and the flow loss is larger, therefore the configuration that the width of the inlet is less than or equal to the width of the outlet enables the return channel to perform a certain function of pressure diffusion, thereby reducing the flow velocity and improving the stability of the gas flow. Considering that the roughness of the inner surface of the return channel is relative large, the width of the outlet is further configured to be not greater than four times the width of the inlet, thereby ensuring the gas to flow through the return channel smoothly; one side of the return channel is vertical, and the other side is gradually flared outward in the direction from the inlet to the outlet. The angle between the other side and the vertical direction is ranged from 0 to 45°, which can guide the gas to flow to a preset side, thereby improving the flow guiding effect.
3. In the integrated structure of the present invention, the inner wall of the return channel is provided with return vanes, which are distributed evenly in serial arrays or in a single array, thereby uniformly guiding the gas from the pressure diffusion flow channel.
4. In the integrated structure of the present invention, the outer edge of the return vane is rigidly connected with the inner wall of the return channel. The vane mounting angle is formed between a first tangent line of the return vane, which is located at a position where the return vane contacts with the inner wall of the return channel, and a second tangent line at a corresponding position of the inner wall of the return channel. The vane mounting angle is ranged from 10° to 80°. Such a structure makes the vane mounting angle of the return vane relatively identical to an actual flow angle of the gas flow, thereby reducing the impact loss.
5. In the integrated structure of the present invention, for certain models with high requirements for gas flow uniformity, such as a heat pump or an ice-storage unit, in order to ensure high performances in the heating conditions or in the ice-storage conditions, pressure diffusion vanes are further arranged inside the pressure diffusion flow channel. The gas flow entering the pressure diffusion flow channel is preliminarily guided by the pressure diffusion vanes, and then is secondarily guided after flowing into the return channel, thereby further improving the gas flow uniformity.
6. In the integrated structure of the present invention, the width of the pressure diffusion vane is not greater than the width of the impeller, which is arranged opposite to the pressure diffusion vane to feed the gas into the pressure diffusion flow channel, thereby preventing gas reflux, and ensuring the convergence of the flow.
7. The present invention also provides a centrifugal compressor, including a main shaft, an impeller, a pressure diffuser cover plate, and any one of the integrated structures described above. The centrifugal compressor of the disclosure employs the integrated structure above, therefore it has all of the advantages brought by the integrated structure above.
8. The centrifugal compressor of the present invention has at least two stages, and an accommodating space is disposed between the return device portion of the front stage and the second-stage impeller of the subsequent stage; the accommodating space is in communication with the gas supplying passage, and the gas supplying passage is configured to supply gas into the accommodating space, thereby improving the compression efficiency; when the centrifugal compressor is applied in a refrigerating apparatus, after the gas is compressed, the gas pressure is increased, and the gas temperature is relatively high; at this time, the gas supplying passage is in communication with an expansion valve, which enables a part of the refrigerant expanded by the expansion valve to flow into the accommodating space, thereby performing the functions of not only supplying gas, but also lowering the temperature.
In order to describe the solutions of the prior art or the solutions of embodiments of the present invention more clearly, the present disclosure will be described briefly with reference to the figures used in describing the embodiments or the prior art. It is obvious that, for those skilled in the art, other figures can be obtained according to the figures provided hereafter without any creative work.
The above figures include the following reference numerals:
1—pressure diffuser portion, 10—pressure diffusion flow channel, 13—pressure diffusion vane, 2—return device portion, 20—return channel, 21—inlet, 22—outlet, 23—return vane, 4—pressure diffuser cover plate, 5—accommodating space, 6—gas supplying passage, 7—second-stage impeller, 8—second-stage pressure diffusion flow channel, 9—second-stage pressure diffuser cover plate.
The technical solutions of the present invention will be described with reference to the accompanying figures. Obviously, what described below are several but not all embodiments of the present invention. For those skilled in the art, other embodiments obtained based on the embodiments of the present invention without creative work are within the scope of the present invention.
It should be specified that, the terms “first” and “second” in the description are just used to describe the object, but should not be understood to indicate or imply the relative importance. What's more, the technical features described below in different embodiments of the present invention may be combined with each other, so long as there are no conflicts.
This embodiment provides an integrated structure of a return device and a pressure diffuser. As shown in
In the integrated structure of the return device and the pressure diffuser of the embodiment, the pressure diffuser portion 1 and the return device portion 2 are integrated to be one component, which is no longer a prior art structure formed by secondarily connecting and integrating a separate pressure diffuser and a separate return device with screws, pins or welding. With such a configuration, the integrated structure of the present invention not only eliminates a need of independently installing a return device and a pressure diffuser, but also eliminates connection seams caused by assembly and misalignment caused by accumulated errors, etc. Therefore, the gas can smoothly flow from the pressure diffusion flow channel 10 into the return channel 20, and the energy loss is small; in the integrated structure of the return device portion 2 and the pressure diffuser portion 1, the return vane 23 is separately arranged in the return channel 20 and is not connected to the pressure diffuser any longer, which eliminates the problem in the prior art that air leakage is caused due to a seam between the end of the return vane 23 and the pressure diffuser, and eliminates the phenomenon that part of the gas is leaked from the seam, avoiding the guiding action of the return device and affecting the gas guided by the return device. Therefore, when the integrated structure of the present invention is applied in a centrifugal compressor, it can improve the flow guiding effect and the gas flow uniformity. In this embodiment, the pressure diffuser portion 1 and the return device portion 2 are integrally molded by casting.
As shown in
One side of the return channel 20 is vertical, and the other side is gradually flared outward in the direction from the inlet 21 to the outlet 22. The angle between the other side and the vertical direction is β, and 0≤β≤45°. Such a structure can guide the gas to flow to a preset side, thereby improving the flow guiding effect.
As shown in
The outer edge of the return vane 23 is rigidly connected with the inner wall of the return channel 20. A vane mounting angle α is formed between a first tangent line of the return vane 23, which is located at a position where the return vane 23 contacts with the inner wall of the return channel 20, and a second tangent line at a corresponding position of the inner wall of the return channel 20. The vane mounting angle α is ranged from 10° to 80°. Such a structure makes the vane mounting angle α of the return vane 23 relatively identical to an actual flow angle of the gas flow, thereby reducing the impact loss.
As shown in
The width of the pressure diffusion vane 13 is not greater than the width of the impeller 3, which is arranged opposite to the pressure diffusion vane to feed the gas into the pressure diffusion flow channel 10. As shown in
The integrated structure of this embodiment can be applied not only in a two-stage centrifugal compressor, but also in a three-stage or multiple-stage centrifugal compressor.
This embodiment provides a centrifugal compressor, including a main shaft, an impeller 3 installed on the main shaft, and a pressure diffuser cover plate 4, and further including the integrated structure described in the first embodiment; the pressure diffuser cover plate 4 is opposite to the pressure diffuser portion 1 to form the pressure diffusion flow channel 10.
The centrifugal compressor of this embodiment employs the integrated structure above, therefore it has all of the advantages brought by the integrated structure above.
The centrifugal compressor has two stages, and an accommodating space 5 is disposed between the return device portion 2 of the front stage and the second-stage impeller 7 of the subsequent stage. The accommodating space 5 is in communication with the gas supplying passage 6, and the gas supplying passage 6 is configured to supply gas into the accommodating space 5, thereby improving the compression efficiency.
The operating process of the two-stage centrifugal compressor is as follows: the main shaft drives the impeller 3 to rotate, throwing the gas into the pressure diffusion flow channel 10, which is formed by the pressure diffuser cover plate 4 and the pressure diffuser portion 1; the gas from the pressure diffusion flow channel 10 flows through the return channel 20, and then enters the accommodating space 5; the second-stage impeller 7 is driven by the main shaft to rotate as well, throwing the gas in the accommodating space 5 into the second-stage pressure diffusion flow channel 8, which is formed by the second-stage pressure diffuser cover plate 9 and the integrated structure, thereby further increasing the gas pressure.
In an embodiment, when the centrifugal compressor of this embodiment is applied in a refrigerating apparatus, the gas supplying passage 6 is in communication with an expansion valve and configured to feed a part of the refrigerant expanded by the expansion valve into the accommodating space 5 to lower the temperature and supply gas, thereby performing the functions of not only supplying gas, but also lowering the temperature.
It is obvious that, what described above are preferred embodiments to provide illustration for the examples clearly, but not intended to limit the present invention. For those skilled in the art, various changes or modifications can be made based on the description above. There is no need for the disclosure to exhaustively describe all possible embodiments. Any obvious changes or modifications derived from the present disclosure are all within the scope of the present invention.
| Number | Date | Country | Kind |
|---|---|---|---|
| 201611102983.5 | Dec 2016 | CN | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/CN2017/103127 | 9/25/2017 | WO | 00 |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2018/103415 | 6/14/2018 | WO | A |
| Number | Name | Date | Kind |
|---|---|---|---|
| 5344285 | O'Sullivan et al. | Sep 1994 | A |
| 8602730 | Richter | Dec 2013 | B2 |
| 10400788 | Nakaniwa | Sep 2019 | B2 |
| 20180172025 | Koga | Jun 2018 | A1 |
| 20200300251 | Yamashita | Sep 2020 | A1 |
| Number | Date | Country |
|---|---|---|
| 102817857 | Dec 2012 | CN |
| 103016409 | Apr 2013 | CN |
| 103062077 | Apr 2013 | CN |
| 203009399 | Jun 2013 | CN |
| 103062077 | May 2014 | CN |
| 204175653 | Feb 2015 | CN |
| 104454652 | Mar 2015 | CN |
| 204828057 | Dec 2015 | CN |
| 106151063 | Nov 2016 | CN |
| 106762841 | May 2017 | CN |
| 106870447 | Jun 2017 | CN |
| 206377069 | Aug 2017 | CN |
| 0703368 | Mar 1996 | EP |
| 0703368 | Apr 1998 | EP |
| 1326166 | May 1963 | FR |
| 2003083281 | Mar 2003 | JP |
| 2010285899 | Dec 2010 | JP |
| 2014088785 | May 2014 | JP |
| 2014240612 | Dec 2014 | JP |
| 2015165109 | Sep 2015 | JP |
| 2016151266 | Aug 2016 | JP |
| WO-2016047256 | Mar 2016 | WO |
| Entry |
|---|
| Extended European Search Report for EP Application No. 17877979.9 dated Oct. 29, 2019 (7 pages). |
| Examination Report for Indian Patent Application No. 201937021837 dated Sep. 22, 2020 (7 pages). |
| Number | Date | Country | |
|---|---|---|---|
| 20200063754 A1 | Feb 2020 | US |
