CN214577780U - Two-stage bilateral compressor - Google Patents
Two-stage bilateral compressor Download PDFInfo
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- CN214577780U CN214577780U CN202022667215.2U CN202022667215U CN214577780U CN 214577780 U CN214577780 U CN 214577780U CN 202022667215 U CN202022667215 U CN 202022667215U CN 214577780 U CN214577780 U CN 214577780U
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Abstract
The utility model discloses a two-stage bilateral compressor, which comprises a rotating shaft, wherein a motor is sleeved in the middle of the rotating shaft, impellers are sleeved on two sides of the rotating shaft, the impellers are respectively a first impeller and a second impeller, a stator is arranged on an impeller outer cover, a first gas outlet is arranged on the stator covered outside the first impeller, a second gas outlet is arranged on the stator covered outside the second impeller, and the first gas outlet is communicated with an inlet of the second impeller through an air passage; and the air inlet ends of the impellers face one side of the end part of the rotating shaft. Further, the impeller is provided with a front cover which is in a circular truncated cone shape; the air inlet surface of the front cover is a curved surface which is in smooth transition along the profile of the ridge line of the blade, and the air outlet surface is provided with a groove which is matched with the end part of the blade. Furthermore, one or more circles of air holes are uniformly formed in the part, opposite to the impeller or the front cover, of the stator. The utility model discloses a two side compressors of two-stage adopts two sides to admit air, and the flow is big, and the direction of admitting air is opposite, can balanced partial axial force.
Description
Technical Field
The utility model relates to a two-stage bilateral compressor belongs to compressor technical field.
Background
The industrial gas turbine mainly comprises three parts of a compressor, a combustion chamber and a turbine. The compressor is a component which utilizes blades rotating at high speed to do work on gas (mostly air) so as to improve the gas pressure, the air is compressed into high-temperature and high-pressure air, then the high-temperature and high-pressure air is supplied to a combustion chamber for fuel combustion, and the generated high-temperature and high-pressure gas expands in a turbine to do work.
The impeller of the compressor in the prior art is usually one-stage, and if the flow is increased, a multi-stage impeller needs to be added, but due to the addition of the impellers, a sufficiently long rotating shaft is needed for installation, so that the problems that the axial size of the compressor is increased and the compressor is not easy to balance are caused. In addition, the existing compressor generally adopts a bearing group consisting of a plurality of radial bearings and thrust bearings, and also needs a rotating shaft with enough length for installation, so that the problem of increase of the axial size of the compressor is brought; and the processing and assembling errors caused by the arrangement of a plurality of bearings are increased, and the processing and assembling difficulty is high. Furthermore, most of the impellers adopted by the existing compressor are semi-open impellers, and there is still room for improvement on how to obtain smaller friction loss and flow resistance, higher efficiency, lightness, high strength and the like.
Disclosure of Invention
To the above-mentioned prior art, the utility model provides a two side compressors of two-stage adopts two sides to admit air, and flow is big, and the direction of admitting air is opposite, can balanced partial axial force, practices thrift pivot axial space, makes the unit operation more steady.
The utility model discloses a realize through following technical scheme:
a two-stage bilateral compressor comprises a rotating shaft, wherein a motor is sleeved in the middle of the rotating shaft, impellers are sleeved on two sides of the rotating shaft, and respectively comprise a first impeller and a second impeller, a stator is arranged outside an impeller housing, a first gas outlet is formed in the stator which is covered outside the first impeller, a second gas outlet is formed in the stator which is covered outside the second impeller, and the first gas outlet is communicated with an inlet of the second impeller through an air passage; the inlet end of impeller all faces to one side of the end part of the rotating shaft, namely: the air inlet directions of the first impeller and the second impeller are opposite, so that partial axial force can be balanced. When the compressor works, gas enters from the first impeller, flows to the inlet of the second impeller from the first outlet through the gas channel after being compressed, and is output from the second outlet after being compressed.
Further, the impeller is a closed impeller, and the specific structure is as follows: the blade-free telescopic sleeve comprises a rear cover, blades, a sleeve body and a front cover, wherein the rear cover is arranged at the tail end of the sleeve body, and a through hole which is integrated with the center of the sleeve body is arranged in the rear cover for being sleeved and fixed on a rotating shaft; the blades are arranged around the sleeve body and rotate towards the same direction, one end of each blade is connected with the outer wall of the sleeve body, and the other end of each blade is connected with the end face of the rear cover; the front cover is arranged on the blade, and the stator covers the front cover; the front cover is circular truncated cone-shaped; the air inlet surface of the front cover is a curved surface which is in smooth transition along the profile of the ridge line of the blade, the air outlet surface is provided with grooves which are matched with the end parts of the blade, and the end parts of the blade corresponding to the grooves are embedded into the grooves and are in tight fit connection; a flow passage is formed among the blade, the rear cover and the front cover; the air outlet is separated by the blades between the tail part of the front cover and the rear cover, and the air flows out of the air outlet from the front part of the blades through the flow channel.
Furthermore, the rear cover, the blades and the sleeve body are integrally formed.
Further, the outer edge of the blade protrudes out of the end face of the rear cover in the axial direction.
Further, the blade includes longer main leaf and shorter splitter blade, and main leaf and splitter blade set up at interval in proper order. The front cover groove is divided into a main blade groove and a splitter blade groove which are respectively arranged corresponding to the end parts of the main blade and the splitter blade.
Furthermore, the front edge of the front cover protrudes out of the front edge of the blade, or is flat with the front edge of the blade, or is shorter than the front edge of the blade.
Further, the front cover is made of carbon fiber composite material. The preparation method comprises the following steps:
step A, putting carbon fibers with a set volume into an oil bed, and infiltrating the carbon fibers by using a liquid adhesive in the oil bed;
b, extracting the fully soaked carbon fibers, and extruding to remove redundant adhesive in the carbon fibers;
c, winding the carbon fiber after the excess adhesive is extruded to form spongy carbon fiber which is fully soaked with the adhesive and has a three-dimensional structure;
d, carrying out vacuum-pumping treatment on the spongy carbon fiber which is fully soaked with the adhesive and has the three-dimensional structure, so that gas in the three-dimensional structure of the carbon fiber is pumped out;
step E, injecting a liquid steel-based material into the carbon fiber three-dimensional structure through a micro-injector, and performing micro-vibration on the carbon fiber three-dimensional structure in the injection process to obtain a composite material of the steel-based material and the carbon fiber which is stained with the adhesive;
and F, putting the steel-based material and the composite material which is full of the adhesive carbon fibers into a mould, pressurizing, cooling and forming to obtain the formed steel-based carbon fiber composite front cover connected through chemical bonds.
Furthermore, one or more circles of air holes are uniformly formed in the part, opposite to the impeller blades or the front cover, of the stator, the part can be decomposed into axial and radial air flows after air is fed, the impeller is suspended in the stator to stably rotate through the radial air flows, the impeller is pushed backwards through the axial air flows, and the stator serves as an air bearing and plays a role of a radial bearing and a thrust bearing at the same time.
Furthermore, one side or/and two sides of the motor are/is provided with a radial bearing sleeved on the rotating shaft, or the radial bearing is not arranged. When being equipped with two radial bearing, be equivalent to totally three radial bearing supports, whole vibration is little, and the operation is stable. When the radial bearing is not arranged or only one of the radial bearing is included, the length of the rotating shaft is shortened (the length of the air compressor is shortened, when the air compressor is used in equipment such as a micro gas turbine and the like, the whole length of the equipment is shortened, the integration is higher), the coaxiality of parts on the shaft is easily ensured, the processing is easier, the integration level is high, and the reliability of the whole machine is high.
Further, the radial bearing is an air bearing.
Further, the rotating shaft may or may not be provided with a thrust bearing, and it is determined according to the calculation result of the axial force, and if the axial force is too large and is difficult to offset, the thrust bearing needs to be provided.
The utility model discloses a two side compressors of two-stage adopts two sides to admit air, and the flow is big, and the direction of admitting air is opposite, can balance partial axial force, practices thrift pivot axial space, makes the unit operation more steady.
The impeller of the compressor is a closed impeller, the detachable front cover is arranged, the front cover is in a circular truncated cone shape, the air inlet surface is a curved surface which is in smooth transition along the outline of the ridge line of the blade, the air outlet surface is provided with a groove matched with the end part of the blade, the friction loss is small during the work, the flow resistance is small, and the efficiency is high; during operation, the front cover is tightly occluded with the blades, gas flows out from the air outlet through the flow channel from the front parts of the blades, and gas leakage is little. The protecgulum is made by carbon-fibre composite, and the whole quality of impeller is light and have high strength, and blade (metal material) can expand during the rotation, and the protecgulum does not expand, consequently along with the increase of pivoted speed up, time increase, interlock between the recess of blade and protecgulum can be more and more tight (be provided with the stator when as air bearing, its admission also can be applyed on the protecgulum, further prevents the recess separation of blade and protecgulum), is fit for high-speed rotatory operating mode. The splitter blade is arranged, so that the blockage of inlet airflow can be reduced, the sliding coefficient of the outlet of the impeller can be improved, the efficiency of the impeller is improved, and the overall efficiency of the gas compressor can be improved due to the improvement of the flow field of the outlet of the impeller. The front cover is made of a carbon fiber composite material, and the formed composite material far breaks through the modulus upper limit of each conventional steel base material by adding the steel base, the carbon fiber and the adhesive, so that the rigidity is greatly increased, meanwhile, the tensile strength and the breaking force of the steel are enhanced, the shearing strength is also greatly improved, and each performance of the composite material is far higher than that of the common steel; meanwhile, the production cost, the process threshold, the batch flow, the universality and the like are all controlled in a metal material system, so that the industry with high-performance material requirements generally benefits.
The utility model discloses a compressor is equipped with slant thrust structure, and the stator has played journal bearing and thrust bearing's effect simultaneously as air bearing (let in gas in the clearance between stator and the impeller from the gas pocket, make and form even stable air film in the clearance, make the impeller steady rotation in the stator to play air bearing's effect), can reduce or even replace original journal bearing and thrust bearing. When the stator is simultaneously used as a thrust bearing, if other radial bearings are arranged on the rotating shaft, a plurality of radial bearings are equivalently supported, the whole vibration is small, and the operation is stable. If no other radial bearing or only a small number of radial bearings are arranged on the rotating shaft, the length of the rotating shaft is shortened, the coaxiality of parts on the shaft is easily ensured, the processing is easier, the integration level is high, and the reliability of the whole machine is high.
The various terms and phrases used herein have the ordinary meaning as is well known to those skilled in the art. To the extent that the terms and phrases are not inconsistent with a known meaning, the meaning of the present invention is expressed, the specification is set forth.
Drawings
FIG. 1: the utility model discloses a structural schematic of two side compressors of two-stage.
FIG. 2: the utility model discloses a structural schematic diagram of closed impeller.
FIG. 3: the structure of the rear cover, the blades and the sleeve body is schematically shown.
FIG. 4: the front view of fig. 3.
FIG. 5: fig. 3 is a side view.
FIG. 6: fig. 5 is a cross-sectional view taken at the position a-a.
FIG. 7: a manufacturing flow chart of the front cover.
FIG. 8: schematic structural diagram of the two-stage double-sided compressor of example 2.
The air-conditioner comprises a rotating shaft 1, an impeller 2, a rear cover 201, a blade 202, a sleeve 203, a front cover 204, a flow channel 205, an air outlet 206, a stator 3, an air hole 301, a motor 4 and an air channel 5.
Detailed Description
The present invention will be further described with reference to the following examples. However, the scope of the present invention is not limited to the following examples. Those skilled in the art will appreciate that various changes and modifications may be made to the invention without departing from the spirit and scope of the invention.
The present invention describes the materials used in the test and the test methods generally and/or specifically. Although many materials and methods of operation are known in the art for carrying out the objects of the invention, the invention is nevertheless described in detail herein.
The instruments, reagents, materials and the like used in the following examples are conventional instruments, reagents, materials and the like in the prior art and are commercially available in a normal manner unless otherwise specified. Unless otherwise specified, the experimental methods, detection methods, and the like described in the following examples are conventional experimental methods, detection methods, and the like in the prior art.
Example 1
A two-stage bilateral compressor comprises a rotating shaft 1, wherein a motor 4 is sleeved in the middle of the rotating shaft 1, impellers 2 are sleeved on two sides of the rotating shaft and respectively comprise a first impeller and a second impeller, as shown in figure 1, a stator 3 is arranged outside the impeller 2, a first gas outlet (not shown in the figure) is arranged on the stator covered outside the first impeller, a second gas outlet (not shown in the figure) is arranged on the stator covered outside the second impeller, and the first gas outlet is communicated with an inlet of the second impeller through an air passage; the inlet end of impeller all faces to one side of the end part of the rotating shaft, namely: the air inlet directions of the first impeller and the second impeller are opposite, so that partial axial force can be balanced. When the compressor works, gas enters from the first impeller, flows to the inlet of the second impeller from the first gas outlet through the gas channel 5 after being compressed, and is output from the second gas outlet after being compressed.
The impeller is a closed impeller, and the specific structure is as follows: the blade-free rotary shaft comprises a rear cover 201, blades 202, a sleeve body 203 and a front cover 204, as shown in fig. 2-6, wherein the rear cover 201 is arranged at the tail end of the sleeve body 203, and the rear cover 201 and the sleeve body 203 are provided with an integrated through hole at the center for being sleeved and fixed on the rotary shaft 1; the blades 202 are arranged around the sleeve body 203 and rotate towards the same direction, one end of each blade 202 is connected with the outer wall of the sleeve body 203, and the other end of each blade 202 is connected with the end face of the rear cover 201; the front cover 204 covers the blades 202, and the stator 3 covers the front cover 204; the front cover 204 is circular truncated cone-shaped; the air inlet surface of the front cover 204 is a curved surface which is in smooth transition along the ridge line profile of the blade 202, the air outlet surface is provided with grooves which are matched with the end parts of the blade 202, and the end parts of the blade 202 corresponding to the grooves are embedded into the grooves and are in tight fit connection; a flow passage 205 is formed among the blade 202, the rear cover 201 and the front cover 204; an air outlet 206 is formed between the rear part of the front cover 204 and the rear cover 201 and is partitioned by the blades 202, and air flows out of the air outlet 206 from the front part of the blades 202 through a flow passage 205.
The rear cover 201, the blade 202 and the sleeve 203 are integrally formed as shown in fig. 3 to 6.
The outer edge of the vane 202 protrudes from the end face of the rear cover 201 in the axial direction.
The blades 202 include a longer main blade and a shorter splitter blade, and the main blade and the splitter blade are sequentially arranged at intervals. The groove of the front cover 204 is divided into a main blade groove and a splitter blade groove, which are respectively arranged corresponding to the ends of the main blade and the splitter blade.
The front edge of the front cover 204 protrudes from the front edge of the blade 202, or is parallel to the front edge of the blade 202, or is shorter than the front edge of the blade 202.
The front cover 204 is made of a carbon fiber composite material. The specific preparation method (the flow is shown in figure 7) is as follows:
step A, putting carbon fibers with a set volume into an oil bed, and infiltrating the carbon fibers by using a liquid adhesive in the oil bed;
b, extracting the fully soaked carbon fibers, and extruding to remove redundant adhesive in the carbon fibers;
c, winding the carbon fiber after the excess adhesive is extruded to form spongy carbon fiber which is fully soaked with the adhesive and has a three-dimensional structure;
d, carrying out vacuum-pumping treatment on the spongy carbon fiber which is fully soaked with the adhesive and has the three-dimensional structure, so that gas in the three-dimensional structure of the carbon fiber is pumped out;
step E, injecting a liquid steel-based material into the carbon fiber three-dimensional structure through a micro-injector, and performing micro-vibration on the carbon fiber three-dimensional structure in the injection process to obtain a composite material of the steel-based material and the carbon fiber which is stained with the adhesive;
and F, putting the steel-based material and the composite material which is full of the adhesive carbon fibers into a mould, pressurizing, cooling and forming to obtain the formed steel-based carbon fiber composite front cover connected through chemical bonds.
One or more circles of air holes 301 are uniformly formed in the part, opposite to the front cover 204, of the stator 3, air can be decomposed into axial air flow and radial air flow after entering the air, the impeller is suspended in the stator 3 to stably rotate through the radial air flow, the impeller is pushed backwards through the axial air flow, and the stator 3 serves as an air bearing and plays a role of a radial bearing and a thrust bearing at the same time.
The two sides of the motor are provided with radial bearings sleeved on the rotating shaft, or one side of the motor is provided with a radial bearing sleeved on the rotating shaft, or the radial bearing is not arranged. When being equipped with two radial bearing, be equivalent to totally three radial bearing supports, whole vibration is little, and the operation is stable. When the radial bearing is not arranged or only one of the radial bearings is contained, the length of the rotating shaft is shortened, the coaxiality of parts on the shaft is easily guaranteed, the processing is easier, the integration level is high, and the reliability of the whole machine is high.
The radial bearing is an air bearing.
The rotating shaft can be provided with or without a thrust bearing, and is determined according to the calculation result of the axial force, and if the axial force is too large and is difficult to offset, the thrust bearing needs to be arranged.
The two-stage bilateral compressor adopts bilateral air intake, has large flow and opposite air intake direction, and can balance partial axial force.
The impeller is a closed impeller, the detachable front cover is arranged, the front cover is in a circular truncated cone shape, the air inlet surface is a curved surface which is in smooth transition along the ridge line profile of the blade, the air outlet surface is provided with a groove which is matched with the end part of the blade, and the impeller has small friction loss, small flow resistance and high efficiency in work; during operation, the front cover is tightly occluded with the blades, gas flows out from the air outlet through the flow channel from the front parts of the blades, and gas leakage is little. The protecgulum is made by carbon-fibre composite, and the whole quality of impeller is light and have high strength, and blade (metal material) can expand during the rotation, and the protecgulum does not expand, consequently along with the increase of pivoted speed up, time, interlock between the recess of blade and protecgulum can be more and more tight, is fit for high-speed rotatory operating mode. The splitter blade is arranged, so that the blockage of inlet airflow can be reduced, the sliding coefficient of the outlet of the impeller can be improved, the efficiency of the impeller is improved, and the overall efficiency of the gas compressor can be improved due to the improvement of the flow field of the outlet of the impeller. The front cover is made of a carbon fiber composite material, and the formed composite material far breaks through the modulus upper limit of each conventional steel base material by adding the steel base, the carbon fiber and the adhesive, so that the rigidity is greatly increased, meanwhile, the tensile strength and the breaking force of the steel are enhanced, the shearing strength is also greatly improved, and each performance of the composite material is far higher than that of the common steel; meanwhile, the production cost, the process threshold, the batch flow, the universality and the like are all controlled in a metal material system, so that the industry with high-performance material requirements generally benefits.
The compressor is provided with the oblique thrust structure, the stator serves as an air bearing and simultaneously plays the roles of a radial bearing and a thrust bearing (gas is introduced into a gap between the stator and the impeller from the air hole, so that a uniform and stable air film is formed in the gap, the impeller rotates stably in the stator, and the effect of the air bearing is achieved), and the original radial bearing and the original thrust bearing can be reduced or even replaced. When the stator is simultaneously used as a thrust bearing, if other radial bearings are arranged on the rotating shaft, a plurality of radial bearings are equivalently supported, the whole vibration is small, and the operation is stable. If no other radial bearing or only a small number of radial bearings are arranged on the rotating shaft, the length of the rotating shaft is shortened, the coaxiality of parts on the shaft is easily ensured, the processing is easier, the integration level is high, and the reliability of the whole machine is high. In addition, the air inlet of the air hole is applied to the front cover, so that the separation of the blade and the groove of the front cover can be better prevented, and the air hole is more suitable for the working condition of high-speed rotation.
Example 2
A two-stage bilateral compressor, a two-stage bilateral compressor, including the spindle 1, the middle part of the spindle 1 is fitted with the electrical machinery 4, both sides are fitted with the impeller 2, it is the first impeller, the second impeller separately, as shown in figure 8, the outer cover of the impeller 2 sets up the stator 3, the stator covering and setting up outside the first impeller has the first gas outlet (not shown in the figure), the stator covering and setting up outside the second impeller has the second gas outlet (not shown in the figure), the first gas outlet communicates with inlet of the second impeller through the air drain; the inlet end of impeller all faces to one side of the end part of the rotating shaft, namely: the air inlet directions of the first impeller and the second impeller are opposite, so that partial axial force can be balanced. When the compressor works, gas enters from the first impeller, flows to the inlet of the second impeller from the first gas outlet through the gas channel 5 after being compressed, and is output from the second gas outlet after being compressed.
The impeller is a closed impeller, and the specific structure is as follows: the blade-free rotary shaft comprises a rear cover 201, blades 202, a sleeve body 203 and a front cover 204, as shown in fig. 2-6, wherein the rear cover 201 is arranged at the tail end of the sleeve body 203, and the rear cover 201 and the sleeve body 203 are provided with an integrated through hole at the center for being sleeved and fixed on the rotary shaft 1; the blades 202 are arranged around the sleeve body 203 and rotate towards the same direction, one end of each blade 202 is connected with the outer wall of the sleeve body 203, and the other end of each blade 202 is connected with the end face of the rear cover 201; the front cover 204 covers the blades 202, and the stator 3 covers the front cover 204; the front cover 204 is circular truncated cone-shaped; the air inlet surface of the front cover 204 is a curved surface which is in smooth transition along the ridge line profile of the blade 202, the air outlet surface is provided with grooves which are matched with the end parts of the blade 202, and the end parts of the blade 202 corresponding to the grooves are embedded into the grooves and are in tight fit connection; a flow passage 205 is formed among the blade 202, the rear cover 201 and the front cover 204; an air outlet 206 is formed between the rear part of the front cover 204 and the rear cover 201 and is partitioned by the blades 202, and air flows out of the air outlet 206 from the front part of the blades 202 through a flow passage 205.
The rear cover 201, the blade 202 and the sleeve 203 are integrally formed as shown in fig. 3 to 6.
The outer edge of the vane 202 protrudes from the end face of the rear cover 201 in the axial direction.
The blades 202 include a longer main blade and a shorter splitter blade, and the main blade and the splitter blade are sequentially arranged at intervals. The groove of the front cover 204 is divided into a main blade groove and a splitter blade groove, which are respectively arranged corresponding to the ends of the main blade and the splitter blade.
The front edge of the front cover 204 protrudes from the front edge of the blade 202, or is parallel to the front edge of the blade 202, or is shorter than the front edge of the blade 202.
The front cover 204 is made of a carbon fiber composite material. The specific preparation method is the same as that of example 1.
The two-stage bilateral compressor adopts bilateral air intake, has large flow and opposite air intake direction, and can balance partial axial force. The impeller is a closed impeller, the detachable front cover is arranged, the front cover is in a circular truncated cone shape, the air inlet surface is a curved surface which is in smooth transition along the ridge line profile of the blade, the air outlet surface is provided with a groove which is matched with the end part of the blade, and the impeller has small friction loss, small flow resistance and high efficiency in work; during operation, the front cover is tightly occluded with the blades, gas flows out from the air outlet through the flow channel from the front parts of the blades, and gas leakage is little. The protecgulum is made by carbon-fibre composite, and the whole quality of impeller is light and have high strength, and blade (metal material) can expand during the rotation, and the protecgulum does not expand, consequently along with the increase of pivoted speed up, time, interlock between the recess of blade and protecgulum can be more and more tight, is fit for high-speed rotatory operating mode. The splitter blade is arranged, so that the blockage of inlet airflow can be reduced, the sliding coefficient of the outlet of the impeller can be improved, the efficiency of the impeller is improved, and the overall efficiency of the gas compressor can be improved due to the improvement of the flow field of the outlet of the impeller. The front cover is made of a carbon fiber composite material, and the formed composite material far breaks through the modulus upper limit of each conventional steel base material by adding the steel base, the carbon fiber and the adhesive, so that the rigidity is greatly increased, meanwhile, the tensile strength and the breaking force of the steel are enhanced, the shearing strength is also greatly improved, and each performance of the composite material is far higher than that of the common steel; meanwhile, the production cost, the process threshold, the batch flow, the universality and the like are all controlled in a metal material system, so that the industry with high-performance material requirements generally benefits.
The above examples are provided to those of ordinary skill in the art to fully disclose and describe how to make and use the claimed embodiments, and are not intended to limit the scope of the disclosure herein. Modifications apparent to those skilled in the art are intended to be within the scope of the appended claims.
Claims (12)
1. A two-stage double-sided compressor characterized by: the air purifier comprises a rotating shaft, wherein a motor is sleeved in the middle of the rotating shaft, impellers are sleeved on two sides of the rotating shaft, the impellers are respectively a first impeller and a second impeller, a stator is arranged outside an impeller housing, a first gas outlet is formed in the stator which is covered outside the first impeller, a second gas outlet is formed in the stator which is covered outside the second impeller, and the first gas outlet is communicated with an inlet of the second impeller through an air passage; and the air inlet ends of the impellers face one side of the end part of the rotating shaft.
2. The two-stage double-sided compressor as recited in claim 1, wherein: the impeller is a closed impeller, and the specific structure is as follows: the blade-free telescopic sleeve comprises a rear cover, blades, a sleeve body and a front cover, wherein the rear cover is arranged at the tail end of the sleeve body, and a through hole which is integrated with the center of the sleeve body is arranged in the rear cover for being sleeved and fixed on a rotating shaft; the blades are arranged around the sleeve body and rotate towards the same direction, one end of each blade is connected with the outer wall of the sleeve body, and the other end of each blade is connected with the end face of the rear cover; the front cover is arranged on the blade, and the stator covers the front cover; the front cover is circular truncated cone-shaped; the air inlet surface of the front cover is a curved surface which is in smooth transition along the profile of the ridge line of the blade, the air outlet surface is provided with grooves which are matched with the end parts of the blade, and the end parts of the blade corresponding to the grooves are embedded into the grooves and are in tight fit connection; a flow passage is formed among the blade, the rear cover and the front cover; the air outlet is separated by the blades between the tail part of the front cover and the rear cover, and the air flows out of the air outlet from the front part of the blades through the flow channel.
3. The two-stage double-sided compressor as recited in claim 2, wherein: the rear cover, the blades and the sleeve body are integrally formed; or/and: the outer edge of the vane protrudes out of the end face of the rear cover in the axial direction.
4. The two-stage double-sided compressor as recited in claim 2, wherein: the blades comprise longer main blades and shorter splitter blades, and the main blades and the splitter blades are sequentially arranged at intervals; the front cover groove is divided into a main blade groove and a splitter blade groove which are respectively arranged corresponding to the end parts of the main blade and the splitter blade.
5. The two-stage double-sided compressor as recited in claim 2, wherein: the front edge of the front cover protrudes out of the front edge of the blade, or is parallel to the front edge of the blade, or is shorter than the front edge of the blade.
6. The two-stage double-sided compressor as recited in claim 2, wherein: the front cover is made of carbon fiber composite material.
7. The two-stage double-sided compressor according to claim 1 or 2, characterized in that: one or more circles of air holes are uniformly formed in the part, opposite to the impeller blades or the front cover, of the stator.
8. The two-stage double-sided compressor as recited in claim 1, wherein: and one side or/and two sides of the motor are/is/are provided with radial bearings sleeved on the rotating shaft or are not provided with the radial bearings.
9. The two-stage double-sided compressor as recited in claim 7, wherein: and one side or/and two sides of the motor are/is/are provided with radial bearings sleeved on the rotating shaft or are not provided with the radial bearings.
10. The two-stage double-sided compressor as recited in claim 8, wherein: the radial bearing is an air bearing.
11. The two-stage double-sided compressor as recited in claim 1, wherein: the rotating shaft may or may not be provided with a thrust bearing.
12. The two-stage double-sided compressor as recited in claim 7, wherein: the rotating shaft may or may not be provided with a thrust bearing.
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| CN202022667215.2U CN214577780U (en) | 2020-11-18 | 2020-11-18 | Two-stage bilateral compressor |
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| CN202022667215.2U CN214577780U (en) | 2020-11-18 | 2020-11-18 | Two-stage bilateral compressor |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112503004A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Back-to-back type compressor |
| CN112503002A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Gas compressor with oblique thrust structure and rotor system |
| CN112503003A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Two-stage bilateral compressor |
| CN114109861A (en) * | 2021-11-25 | 2022-03-01 | 海德韦尔(太仓)能源科技有限公司 | Thrust bearing arrangement structure of air compressor |
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2020
- 2020-11-18 CN CN202022667215.2U patent/CN214577780U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112503004A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Back-to-back type compressor |
| CN112503002A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Gas compressor with oblique thrust structure and rotor system |
| CN112503003A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Two-stage bilateral compressor |
| CN114109861A (en) * | 2021-11-25 | 2022-03-01 | 海德韦尔(太仓)能源科技有限公司 | Thrust bearing arrangement structure of air compressor |
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Effective date of registration: 20230407 Address after: 518063 10 Nanshan District Road, Gaoxin south, Nanshan District, Shenzhen, Guangdong. Patentee after: Liu Muhua Address before: 100176 room 1202a, block B, Chaolin Plaza, No.19, Ronghua Middle Road, economic and Technological Development Zone, Daxing District, Beijing Patentee before: Jin Pu |