CN111241642A - Design method of axial air inlet and axial air outlet centrifugal compressor - Google Patents

Design method of axial air inlet and axial air outlet centrifugal compressor Download PDF

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Publication number
CN111241642A
CN111241642A CN202010054229.9A CN202010054229A CN111241642A CN 111241642 A CN111241642 A CN 111241642A CN 202010054229 A CN202010054229 A CN 202010054229A CN 111241642 A CN111241642 A CN 111241642A
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exhaust
air inlet
air
channel
axial
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CN202010054229.9A
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孙钧
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Sichuan Deyang Yulong Power Equipment Co Ltd
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Sichuan Deyang Yulong Power Equipment Co Ltd
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Priority to CN202010054229.9A priority Critical patent/CN111241642A/en
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    • 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
    • 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
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for 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
    • 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
    • F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • 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
    • F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention discloses a design method of an axial air inlet and axial air outlet centrifugal compressor, which comprises the following steps: selecting an impeller, a reflux device and an air cylinder with preset parameters and an air inlet and exhaust sleeve connected with the air cylinder and the reflux device; the pipe wall of the air inlet and exhaust sleeve is divided into two layers, namely an outer wall layer and an inner wall layer from outside to inside, an exhaust flow channel is formed between the outer wall layer and the inner wall layer, the exhaust flow channel is a guide layer, and guide blades are arranged in the guide layer and positioned in the exhaust flow channel; an air inlet flow channel is arranged in the air inlet and outlet sleeve; setting a U-shaped flow channel formed between the air cylinder and the reflux device, wherein the U-shaped flow channel is divided into a diffusion section and a reflux section along the advancing direction of airflow; setting a diffusion section to be connected with the air inlet flow passage, and setting a backflow section to be communicated with the exhaust flow passage; modeling, drawing and structural design are completed.

Description

Design method of axial air inlet and axial air outlet centrifugal compressor
Technical Field
The invention relates to the field of centrifugal compressors, in particular to a design method of an axial air inlet and axial air outlet centrifugal compressor.
Background
The steam compressor can be used for low-temperature waste heat, the grade of the working medium is improved by compressing steam, and the effective utilization of the low-temperature waste heat is realized. At present, the saturated temperature rise of a steam compressor unit on the market is low, condensation is easy to occur due to the fact that an inlet is a saturated parameter, and the density of a working medium is greatly changed after condensation, so that the steam compressor unit cannot stably operate or the stable operation range is narrow.
Disclosure of Invention
Based on the above, the invention provides a design method of an axial air inlet and axial air outlet centrifugal compressor, and the designed axial air inlet and axial air outlet centrifugal compressor can effectively improve the dryness of inlet working media for the working media with saturated parameters at the inlet and avoid the condensation of the inlet working media; meanwhile, the size of the high-temperature pipeline is shortened, and the size of a peripheral pipeline of the equipment is reduced; the loss of the exhaust volute can be effectively reduced, and the unit efficiency is improved.
The technical scheme of the invention is as follows:
a design method of an axial air inlet and axial air outlet centrifugal compressor comprises the following steps:
selecting an impeller, a reflux device and an air cylinder with preset parameters and an air inlet and exhaust sleeve connected with the air cylinder and the reflux device;
setting the pipe wall of the air inlet and exhaust casing to be divided into two layers, namely an outer wall layer and an inner wall layer from outside to inside, forming an exhaust channel between the outer wall layer and the inner wall layer, wherein the exhaust channel is a guide layer, and guide blades are arranged in the guide layer and are positioned in the exhaust channel;
setting an air inlet channel in the air inlet and outlet sleeve, wherein the air inlet channel extends to a position between the impeller and the reflux device;
setting a U-shaped flow channel formed between the air cylinder and the reflux device, wherein the U-shaped flow channel is divided into a diffusion section and a reflux section along the advancing direction of the airflow;
step five, setting a diffusion section to be connected with the gas inlet channel, setting a backflow section to be communicated with the exhaust channel, and setting a straight line where the gas flow direction of the gas inlet channel is parallel to a straight line where the gas flow direction of the exhaust channel is;
and step six, modeling, drawing and structural design are completed.
In a preferred embodiment, the guide vanes are uniformly distributed in the guide layer, and the cross section of each guide vane is streamline, one end of each guide vane is connected with the outer wall layer, and the other end of each guide vane is connected with the inner wall layer.
In a preferred embodiment, a trumpet-shaped air inlet flow channel is formed between the impeller and the reflux device, and the caliber of the flow channel is gradually reduced along the air inlet direction.
In a preferred embodiment, the aperture of the return section is set to increase gradually in the intake direction.
In a preferred embodiment, the working medium inlet and outlet channels are all in the form of sleeves.
In a preferred embodiment, both the intake and exhaust are provided as annular flow passages.
The centrifugal compressor with axial air inlet and axial air exhaust designed by the design method comprises an impeller, a reflux device, an air cylinder and an air inlet and exhaust sleeve connected with the air cylinder and the reflux device, wherein the pipe wall of the air inlet and exhaust sleeve is divided into two layers which are an outer wall layer and an inner wall layer from outside to inside in sequence, an exhaust channel is formed between the outer wall layer and the inner wall layer and is a guide layer, and guide blades are arranged in the guide layer and positioned in the exhaust channel; the air inlet and exhaust sleeve is internally provided with an air inlet flow channel, the air inlet flow channel extends to a position between the impeller and the reflux device, a U-shaped flow channel is formed between the cylinder and the reflux device, the U-shaped flow channel is divided into a diffusion section and a reflux section along the advancing direction of air flow, the diffusion section is connected with the air inlet flow channel, the reflux section is communicated with the exhaust flow channel, and the straight line of the air flow direction of the air inlet flow channel is parallel to the straight line of the air flow direction of the exhaust flow channel.
The working principle of the structural design is as follows:
the unit is axially air-intake and axially air-exhaust, and the air intake and the air exhaust are positioned at the same side of the unit. The working medium enters the unit from the air inlet channel on the inner side of the air inlet and outlet sleeve along the axial direction; the impeller is rotated by external input power to pressurize the working medium; the pressurized working medium enters a diffusion section of a flow passage consisting of the cylinder and the reflux device, and the pressure is further increased; the working medium is turned to enter a backflow section of a flow passage formed by the cylinder and the backflow device, and the working medium is turned to be discharged out of the unit through an exhaust flow passage formed by the inner wall and the outer wall of the air inlet and exhaust sleeve in the axial direction.
In a preferred embodiment, the guide vanes are uniformly distributed in the guide layer, and the cross section of each guide vane is streamline, one end of each guide vane is connected with the outer wall layer, and the other end of each guide vane is connected with the inner wall layer. Because the temperature of the working medium is further increased after being compressed, when the high-temperature exhaust working medium flows through the exhaust runner, partial heat is conducted to the inner side surface of the air inlet and exhaust sleeve, so that the outer side of the air inlet runner of the unit is heated, a boundary layer of the air inlet runner absorbs heat, and the dryness of the working medium is improved. The working medium condensation caused by the influence of the boundary layer is avoided.
In a preferred embodiment, a trumpet-shaped air inlet flow channel is formed between the impeller and the reflux device, and the caliber of the flow channel is gradually reduced along the air inlet direction. The purpose is to make the effect of the supercharging better.
In a preferred embodiment, the aperture of the return section increases gradually in the intake direction. The purpose is to allow the displacement to be increased, further relieving the gas pressure.
The method for axial air intake and axial air exhaust of the centrifugal compressor comprises the following steps:
a. setting the unit to axially intake and axially exhaust, wherein the intake and exhaust are positioned at the same side of the unit;
b. the working medium axially enters the air inlet channel from the inner side of the air inlet and outlet sleeve and enters the unit;
c. external input power drives the impeller to rotate, and the working medium is pressurized;
d. the pressurized working medium enters a diffusion section of a flow passage formed by the cylinder and the reflux device, so that the pressure is further increased;
e. the working medium turns and then enters a backflow section of a flow channel consisting of the cylinder and the backflow device;
f. the working medium is converted into an exhaust flow channel which is axially formed by the inner wall and the outer wall of the air inlet and exhaust sleeve and is exhausted out of the unit.
In a preferred embodiment, the method further comprises the following steps:
the temperature of the compressed working medium is further increased, and when the high-temperature exhaust working medium channel exhausts the channel, part of heat is conducted to the inner side surface of the air inlet and exhaust sleeve, so that the outer side of the air inlet channel of the unit is heated, the boundary layer of the air inlet channel absorbs heat, and the dryness of the working medium is improved. The working medium condensation caused by the influence of the boundary layer is avoided.
In a preferred embodiment, the working fluid inlet and outlet channels are in the form of sleeves. For high-temperature exhaust, the length of a high-temperature pipeline can be effectively shortened, so that the unit cost is reduced.
In a preferred embodiment, the intake and exhaust are both annular flow passages. Because the air inlet and the air outlet are all annular flow passages, the loss caused by the air outlet of the volute of the conventional unit is reduced, and the efficiency of the unit is further improved.
The invention has the beneficial effects that:
1. the humidity of a working medium inlet and the steam dryness can be effectively increased, so that the unit can run more stably;
2. the size of a high-temperature pipeline is shortened, and the size of a peripheral pipeline of equipment is reduced;
3. the unit exhausts uniformly, so that the loss of the volute is effectively reduced, and the efficiency of the unit can be effectively improved;
4. the whole circumference of the unit exhausts, and the flow field is more uniform;
5. because the temperature of the working medium is further increased after being compressed, when the high-temperature exhaust working medium flows through the exhaust runner, partial heat is conducted to the inner side surface of the air inlet and exhaust sleeve, so that the outer side of the air inlet runner of the unit is heated, a boundary layer of the air inlet runner absorbs heat, and the dryness of the working medium is improved. Working medium condensation caused by the influence of a boundary layer is avoided;
6. the working medium air inlet and outlet flow channel adopts a sleeve form, and the length of a high-temperature pipeline can be effectively shortened for high-temperature exhaust, so that the unit cost is reduced;
7. because the air inlet and the air outlet are all annular flow passages, the loss caused by the air outlet of the volute of the conventional unit is reduced, and the efficiency of the unit is further improved.
Drawings
FIG. 1 is a schematic structural view of an axial intake and axial discharge centrifugal compressor according to an embodiment of the present invention;
FIG. 2 is a perspective view of the air inlet and outlet sleeve of FIG. 1;
description of reference numerals:
1-air inlet and outlet sleeve, 101-inner wall layer, 102-guide blade, 103-outer wall layer, 2-impeller, 3-reflux device, 4-cylinder, a-air inlet channel, b-diffusion section, c-reflux section and d-exhaust channel.
Detailed Description
Embodiments of the present invention will be described in detail below with reference to the accompanying drawings.
A design method of an axial air inlet and axial air outlet centrifugal compressor comprises the following steps:
selecting an impeller, a reflux device and an air cylinder with preset parameters and an air inlet and exhaust sleeve connected with the air cylinder and the reflux device;
setting the pipe wall of the air inlet and exhaust casing to be divided into two layers, namely an outer wall layer and an inner wall layer from outside to inside, forming an exhaust channel between the outer wall layer and the inner wall layer, wherein the exhaust channel is a guide layer, and guide blades are arranged in the guide layer and are positioned in the exhaust channel;
setting an air inlet channel in the air inlet and outlet sleeve, wherein the air inlet channel extends to a position between the impeller and the reflux device;
setting a U-shaped flow channel formed between the air cylinder and the reflux device, wherein the U-shaped flow channel is divided into a diffusion section and a reflux section along the advancing direction of the airflow;
step five, setting a diffusion section to be connected with the gas inlet channel, setting a backflow section to be communicated with the exhaust channel, and setting a straight line where the gas flow direction of the gas inlet channel is parallel to a straight line where the gas flow direction of the exhaust channel is;
and step six, modeling, drawing and structural design are completed.
In a preferred structural design embodiment, the guide vanes are uniformly distributed in the guide layer, the cross section of each guide vane is streamline, one end of each guide vane is connected with the outer wall layer, and the other end of each guide vane is connected with the inner wall layer.
In a preferred structural design embodiment, a trumpet-shaped air inlet flow channel is formed between the impeller and the reflux device, and the caliber of the flow channel is gradually reduced along the air inlet direction.
In a preferred embodiment, the diameter of the return section is set to increase gradually in the intake direction.
In a preferred structural design embodiment, the working medium inlet and outlet flow passages are all set to be in the form of sleeves.
In a preferred embodiment, both the intake and exhaust are provided as annular flow passages.
Example 1:
the present embodiment 1 is a centrifugal compressor designed by the above design method and capable of axially intake and axially exhaust, and as shown in fig. 1 and 2, the centrifugal compressor includes an impeller 2, a reflux device 3, a cylinder 4, and an intake and exhaust casing 1 connected to the cylinder 4 and the reflux device 3, a pipe wall of the intake and exhaust casing 1 is divided into two layers, which are an outer wall layer 103 and an inner wall layer 101 in sequence from outside to inside, an exhaust flow channel d is formed between the outer wall layer 103 and the inner wall layer 101, a guide vane 102 is provided in the guide flow channel d, and the guide vane 102 is located in the exhaust flow channel d; the air inlet and outlet sleeve 1 is internally provided with an air inlet flow passage a, the air inlet flow passage a extends to a position between the impeller 2 and the reflux device 3, a U-shaped flow passage is formed between the cylinder 4 and the reflux device 3 and is divided into a diffusion section b and a reflux section c along the advancing direction of air flow, the diffusion section b is connected with the air inlet flow passage a, the reflux section c is communicated with the air outlet flow passage d, and the straight line of the air inlet flow passage a where the air flows is parallel to the straight line of the air outlet flow passage d where the air flows.
The working principle of the structure is as follows:
the unit is axially air-intake and axially air-exhaust, and the air intake and the air exhaust are positioned at the same side of the unit. Working medium enters the unit from an air inlet flow passage a on the inner side of the air inlet and outlet sleeve 1 along the axial direction; the impeller 2 rotates by external input power to pressurize the working medium; the pressurized working medium enters a diffusion section b of a flow channel consisting of the cylinder 4 and the reflux device 3, and the pressure is further increased; the working medium turns and then enters a backflow section c of a flow passage formed by the cylinder 4 and the backflow device 3, and the working medium turns to an exhaust flow passage d formed by the inner wall and the outer wall of the air inlet and exhaust sleeve 1 in the axial direction and is exhausted out of the unit.
Example 2:
compared with the embodiment 1, the following scheme is also included:
as shown in fig. 1 and 2, the guide blades 102 are uniformly distributed in the guide layer, and the cross section of the guide blade 102 is streamline, one end of which is connected to the outer wall layer 103, and the other end of which is connected to the inner wall layer 101. Because the temperature of the working medium is further increased after being compressed, when the high-temperature exhaust working medium flows through the exhaust flow channel d, part of heat is conducted to the inner side surface of the air inlet and exhaust sleeve 1, so that the outer side of the air inlet flow channel a of the unit is heated, a boundary layer of the air inlet flow channel a absorbs heat, and the dryness of the working medium is improved. The working medium condensation caused by the influence of the boundary layer is avoided.
Example 3:
compared with the embodiment 1, the following scheme is also included:
as shown in fig. 1 and 2, a trumpet-shaped intake flow channel a is formed between the impeller 2 and the return device 3, and the aperture of the flow channel gradually decreases along the intake direction. The purpose is to make the effect of the supercharging better.
Example 4:
compared with the embodiment 1, the following scheme is also included:
as shown in fig. 1 and 2, the caliber of the backflow segment c gradually increases along the air intake direction. The purpose is to allow the displacement to be increased, further relieving the gas pressure.
Example 5:
with reference to the axial air intake and axial air exhaust structure of the centrifugal compressor in embodiment 1, a method for axial air intake and axial air exhaust of the centrifugal compressor may further be provided, including the following steps:
a. setting the unit to axially intake and axially exhaust, wherein the intake and exhaust are positioned at the same side of the unit;
b. the working medium axially enters the air inlet flow passage a from the inner side of the air inlet and outlet sleeve 1 and enters the unit;
c. external input power drives the impeller 2 to rotate, and the working medium is pressurized;
d. the pressurized working medium enters a diffusion section b of a flow passage formed by the cylinder 4 and the reflux device 3, so that the pressure is further increased;
e. the working medium turns and then enters a backflow section c of a flow channel formed by the cylinder 4 and the backflow device 3;
f. the working medium is converted into an exhaust flow channel d which is axially formed by the inner wall and the outer wall of the air inlet and exhaust sleeve 1 and is exhausted out of the unit.
In the above embodiment 5, the method may further include:
the temperature of the compressed working medium is further increased, and when the high-temperature exhaust working medium channel is in the exhaust channel d, part of heat is conducted to the inner side surface of the air inlet and exhaust sleeve 1, so that the outer side of the air inlet channel a of the unit is heated, a boundary layer of the air inlet channel a absorbs heat, and the dryness of the working medium is improved. The working medium condensation caused by the influence of the boundary layer is avoided.
In the above embodiment 5, the working medium inlet and outlet flow passages d may all be in the form of sleeves. For high-temperature exhaust, the length of a high-temperature pipeline can be effectively shortened, so that the unit cost is reduced.
In embodiment 5 described above, both intake and exhaust may be annular flow passages. Because the air inlet and the air outlet are all annular flow passages, the loss caused by the air outlet of the volute of the conventional unit is reduced, and the efficiency of the unit is further improved.
The axial air inlet and axial air exhaust structure and the method of the centrifugal compressor can effectively increase the humidity of the working medium inlet and the steam dryness, so that the unit can run more stably; the size of a high-temperature pipeline is shortened, and the size of a peripheral pipeline of equipment is reduced; the unit exhausts uniformly, so that the loss of the volute is effectively reduced, and the efficiency of the unit can be effectively improved; the whole circumference of the unit exhausts, and the flow field is more uniform; because the temperature of the working medium is further increased after being compressed, when the high-temperature exhaust working medium flows through the exhaust flow channel d, part of heat is conducted to the inner side surface of the air inlet and exhaust sleeve 1, so that the outer side of the air inlet flow channel a of the unit is heated, a boundary layer of the air inlet flow channel a absorbs heat, and the dryness of the working medium is improved. Working medium condensation caused by the influence of a boundary layer is avoided; the working medium air inlet and outlet flow channel d adopts a sleeve form, and the length of a high-temperature pipeline can be effectively shortened for high-temperature exhaust, so that the unit cost is reduced; because the air inlet and the air outlet are all annular flow passages, the loss caused by the air outlet of the volute of the conventional unit is reduced, and the efficiency of the unit is further improved.
Working medium axially enters from an air inlet flow passage a on the inner wall of the air inlet and outlet sleeve 1; the impeller 2 drives the impeller 2 to rotate by external input shaft power, and the working medium is pressurized; after pressurization, the working medium enters a diffusion section b, and the pressure is further increased; the working medium enters a backflow section c consisting of the outer wall of the backflow device 3 and the inner wall of the air cylinder 4, the steering is realized, the direction of the working medium is changed to be the same as the air inlet direction, and the flow direction is opposite; the working medium axially enters an exhaust runner d formed by the inner wall and the outer wall of the air inlet and exhaust sleeve 1 and is axially discharged out of the unit.
Because the exhaust is full-circle exhaust, the unevenness of the exhaust flow channel d is reduced, so that the efficiency of the unit exhaust volute is improved, the unit exhaust loss is reduced, and the unit efficiency is improved.
Because the exhaust is axially positioned outside the air inlet pipe, compared with the traditional side exhaust, the unit exhaust size is further shortened. And the unit exhaust temperature is higher than the inlet air temperature, and especially for a high-pressure ratio unit, the exhaust temperature is higher. After the high-temperature exhaust pipe is shortened, the high-temperature pipeline cost is reduced.
Because the inlet of the unit is saturated steam, when the unit enters air, working media contacted with the air inlet pipe are liquefied due to friction and boundary layer influence on the steam with smaller dryness, and therefore the efficiency and stable operation of the unit are influenced. The invention adopts a sleeve form that the unit exhaust is arranged at the periphery of the inlet air, the exhaust conducts heat through the inner wall of the inlet and outlet sleeve 1, so that the temperature of the inner wall surface is higher than the inlet temperature of the working medium, thereby exchanging heat with the working medium of the boundary layer, improving the temperature of the working medium of the boundary layer, and ensuring that the temperature of the working medium of the boundary layer is higher than the saturation temperature or the dryness of the working medium, thereby avoiding liquefaction.
Guide vanes 102 are provided between the outer and inner walls of the inlet and outlet casing 1 for support and location of the inner wall. So that the air inlet and outlet sleeve 1 is integrally mounted at the end of the unit through the end flange of the outer wall. To reduce the flow path loss, the guide vane 102 may have an airfoil cross section.
The above-mentioned embodiments only express the specific embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the present invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention.

Claims (6)

1. A design method of an axial air inlet and axial air outlet centrifugal compressor is characterized by comprising the following steps:
selecting an impeller, a reflux device and an air cylinder with preset parameters and an air inlet and exhaust sleeve connected with the air cylinder and the reflux device;
setting the pipe wall of the air inlet and exhaust casing to be divided into two layers, namely an outer wall layer and an inner wall layer from outside to inside, forming an exhaust channel between the outer wall layer and the inner wall layer, wherein the exhaust channel is a guide layer, and guide blades are arranged in the guide layer and are positioned in the exhaust channel;
setting an air inlet channel in the air inlet and outlet sleeve, wherein the air inlet channel extends to a position between the impeller and the reflux device;
setting a U-shaped flow channel formed between the air cylinder and the reflux device, wherein the U-shaped flow channel is divided into a diffusion section and a reflux section along the advancing direction of the airflow;
step five, setting a diffusion section to be connected with the gas inlet channel, setting a backflow section to be communicated with the exhaust channel, and setting a straight line where the gas flow direction of the gas inlet channel is parallel to a straight line where the gas flow direction of the exhaust channel is;
and step six, modeling, drawing and structural design are completed.
2. The method of claim 1, wherein the guide vanes are uniformly distributed in the guide layer, and the cross section of the guide vanes is streamlined, and one end of the guide vanes is connected to the outer wall layer and the other end of the guide vanes is connected to the inner wall layer.
3. The design method of axial-intake axial-exhaust centrifugal compressor as claimed in claim 1, wherein a trumpet-shaped intake flow passage is formed between the impeller and the return device, and the diameter of the flow passage is gradually reduced along the intake direction.
4. The design method of axial air inlet and axial air outlet centrifugal compressor as claimed in claim 1, wherein the caliber of the return section is set to increase gradually along the air inlet direction.
5. The design method of axial air intake and axial air exhaust centrifugal compressor as claimed in claim 1, wherein the working medium air intake and exhaust flow passages are all in the form of sleeves.
6. The method of claim 1, wherein the air intake and exhaust are both annular flow passages.
CN202010054229.9A 2020-01-17 2020-01-17 Design method of axial air inlet and axial air outlet centrifugal compressor Pending CN111241642A (en)

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Application publication date: 20200605