CN214577903U - Closed impeller, compressor and gas turbine - Google Patents
Closed impeller, compressor and gas turbine Download PDFInfo
- Publication number
- CN214577903U CN214577903U CN202022667337.1U CN202022667337U CN214577903U CN 214577903 U CN214577903 U CN 214577903U CN 202022667337 U CN202022667337 U CN 202022667337U CN 214577903 U CN214577903 U CN 214577903U
- Authority
- CN
- China
- Prior art keywords
- blade
- blades
- front cover
- impeller
- rear cover
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The utility model discloses a closed impeller, which comprises a rear cover, blades, a sleeve body and a front cover, wherein the front cover is arranged on the blades, the front cover is in the shape of a circular truncated cone, an air inlet surface is a curved surface which is in smooth transition along the profile of a ridge line of the blades, a back air surface is provided with grooves matched with the end parts of the blades, and the end parts of the blades 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. The utility model also discloses a compressor, the gas turbine that contain this closed impeller structure. The utility model discloses a closed impeller sets up the protecgulum, and the during operation gas is revealed fewly, and frictional loss is little, and flow resistance is little, and is efficient. The front cover is made of carbon fiber composite materials, and the impeller is light in overall weight and high in strength. 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 efficiency of the whole compressor can be improved.
Description
Technical Field
The utility model relates to a closed impeller, compressor and gas turbine 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 used by the air compressor is divided into an open type impeller, a semi-open type impeller and a closed type impeller, and the three impellers have the following characteristics:
open impeller: the friction loss and the flow resistance are large, the impeller efficiency is the lowest, the vibration is easy to generate, and the impeller is not suitable for working at high rotating speed.
Semi-open impeller: the friction loss and flow resistance are less than open, the efficiency is higher, and certain rigidity and strength are provided, so that the device can work at higher peripheral speed.
Closed impeller: the friction loss and the flow resistance are both minimum, the efficiency is highest, but the structure is complex and heavy, and the wheel cover can generate huge stress on the blades when rotating, so the strength is poor, and the wheel cover is not suitable for being used under the working condition of high rotating speed.
Most of the impellers adopted by the existing gas compressor are semi-open impellers. The problems to be overcome in developing the compressor are as follows: how to achieve less friction loss and flow resistance, higher efficiency, lightness and high strength.
In addition, the existing gas compressor generally adopts a bearing group consisting of a plurality of radial bearings and thrust bearings, and usually needs a rotating shaft with enough length for installation, so that the problem is that the axial size of the gas compressor is increased, if the gas compressor is used in equipment such as a micro gas turbine generator set, the occupied space of the equipment is increased, the whole weight is increased, and the integrated design is not facilitated; 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.
Disclosure of Invention
To the above-mentioned prior art, the utility model provides a closed impeller, its frictional loss is little, and flow resistance is little, and is efficient, light and handy and have high strength. The utility model discloses compressor, gas turbine who contains this closed impeller structure are still provided.
The utility model discloses a realize through following technical scheme:
a closed impeller 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 the rear cover and the center of the sleeve body are provided with an integrated through hole for sleeving and fixing 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 covered on the blade and 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, 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.
The compressor comprises a rotating shaft, wherein an impeller and a motor are sleeved on the rotating shaft, and the impeller is structurally as described above.
Furthermore, the stator is arranged outside the closed impeller cover, one circle or more circles of air holes are uniformly formed in the part, opposite to 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 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.
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 closed impeller, the compressor and the gas turbine of the utility model are provided with the detachable front cover which is in the shape of a circular truncated cone, the air inlet surface 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 the groove which is matched with the end part of the blade, so that 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 of the utility model is made of carbon fiber composite material, and through the addition of the steel base body, the carbon fiber and the adhesive, the formed composite material breaks through the modulus upper limit of the conventional steel base body materials, the rigidity is greatly increased, simultaneously, the tensile strength and the breaking force of the steel are enhanced, the shearing strength is also greatly improved, and the performances of the front cover are far higher than those 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 diagram of closed impeller.
FIG. 2: the structure of the rear cover, the blades and the sleeve body is schematically shown.
FIG. 3: the front view of fig. 2.
FIG. 4: fig. 2 is a side view.
FIG. 5: the cross-sectional view at the position a-a in fig. 4.
FIG. 6: the utility model discloses an assembly relation schematic diagram of closed impeller and stator.
FIG. 7: a manufacturing flow chart of the front cover.
FIG. 8: the stator is also used as the oblique thrust structure schematic diagram of the air bearing.
FIG. 9: the two sides of the motor are provided with a schematic structural diagram of a radial bearing sleeved on the rotating shaft.
FIG. 10: one side of the motor is provided with a structural schematic diagram of a radial bearing sleeved on the rotating shaft.
FIG. 11: the two sides of the motor are not provided with radial bearings.
The motor 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 and a motor 4.
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.
Example 1
A closed impeller comprises a rear cover 201, blades 202, a sleeve body 203 and a front cover 204, as shown in figures 1-5, wherein the rear cover 201 is arranged at the tail end of the sleeve body 203, and the center of the rear cover 201 and the center of the sleeve body 203 are provided with an integrated through hole for being sleeved and fixed on a rotating 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 is covered on the blade 202, and the front cover 204 is in a circular truncated cone shape; 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. 2 to 5.
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, and the specific preparation method comprises the following steps (the flow chart is shown in fig. 7):
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.
An air compressor comprises a rotating shaft 1, as shown in figure 6, an impeller 2 and a motor 4 are sleeved on the rotating shaft 1, a stator 3 is arranged outside the impeller 2, and the structure of the impeller is as described above.
A gas turbine adopts the compressor.
The closed impeller, the compressor and the gas turbine are provided with the detachable front cover, 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, and the air outlet surface is provided with the groove matched with the end part of the blade, so that the closed impeller, the compressor and the gas turbine are small in friction loss during working, small in flow resistance and high in efficiency; 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.
Example 2
A compressor comprises a rotating shaft 1, wherein an impeller 2 and a motor 4 are sleeved on the rotating shaft 1; wherein, the structure of the impeller 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. 1-5, 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 is covered on the blade 202, and the front cover 204 is in a circular truncated cone shape; 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; the outer edges of the blades 202 protrude out of the end face of the rear cover 201 in the axial direction; 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 front cover 204 is made of a carbon fiber composite material.
The stator 3 is covered outside the closed impeller, as shown in fig. 8, a circle or a plurality of circles of air holes 301 are uniformly formed in the part, facing the front cover 204, of the stator 3, air can be decomposed into axial and radial air flows after entering the air, the impeller is suspended in the stator 3 to stably rotate through the radial air flows, the impeller is pushed backwards through the axial air flows, 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 (figure 9) sleeved on the rotating shaft, or one side of the motor is provided with a radial bearing (figure 10) sleeved on the rotating shaft, or the radial bearing (figure 11) 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 included, the length of the rotating shaft is shortened (in the figures 9-11, the shaft length is sequentially 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 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.
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 (10)
1. A shrouded impeller characterized by: 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 covered on the blade and 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, 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.
2. The shrouded impeller according to claim 1 wherein: the rear cover, the blades and the sleeve body are integrally formed.
3. The shrouded impeller according to claim 1 wherein: the outer edge of the vane protrudes out of the end face of the rear cover in the axial direction.
4. The shrouded impeller according to claim 1 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 shrouded impeller according to claim 1 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 shrouded impeller according to claim 1 wherein: the front cover is made of carbon fiber composite material.
7. The utility model provides a compressor, includes the pivot, overlaps in the pivot and establishes impeller and motor, its characterized in that: the impeller is the closed impeller of any one of claims 1 to 6.
8. An air compressor according to claim 7, characterized in that: the closed impeller is covered by a stator, and one or more circles of air holes are uniformly formed in the part, which is opposite to the front cover, of the stator.
9. An air compressor according to claim 7 or 8, characterized in that: 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;
or/and: the rotating shaft may or may not be provided with a thrust bearing.
10. A gas turbine using the compressor as claimed in any one of claims 7 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022667337.1U CN214577903U (en) | 2020-11-18 | 2020-11-18 | Closed impeller, compressor and gas turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022667337.1U CN214577903U (en) | 2020-11-18 | 2020-11-18 | Closed impeller, compressor and gas turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214577903U true CN214577903U (en) | 2021-11-02 |
Family
ID=78324556
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022667337.1U Active CN214577903U (en) | 2020-11-18 | 2020-11-18 | Closed impeller, compressor and gas turbine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214577903U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112503002A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Gas compressor with oblique thrust structure and rotor system |
| CN112503004A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Back-to-back type compressor |
| CN112503022A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Closed impeller and compressor |
-
2020
- 2020-11-18 CN CN202022667337.1U patent/CN214577903U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112503002A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Gas compressor with oblique thrust structure and rotor system |
| CN112503004A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Back-to-back type compressor |
| CN112503022A (en) * | 2020-11-18 | 2021-03-16 | 靳普 | Closed impeller and compressor |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN214577903U (en) | Closed impeller, compressor and gas turbine | |
| CN112503004A (en) | Back-to-back type compressor | |
| CN112503022A (en) | Closed impeller and compressor | |
| CN214577780U (en) | Two-stage bilateral compressor | |
| CN112503002A (en) | Gas compressor with oblique thrust structure and rotor system | |
| CN112503003A (en) | Two-stage bilateral compressor | |
| JP4841222B2 (en) | Reverse rotating turbine engine and method of assembling it | |
| CN1654804B (en) | Three-axis bypass turbojet engine having bypass ratio | |
| CN112628161A (en) | Air-cooled compressor | |
| CN215058258U (en) | Gas compressor with oblique thrust structure and rotor system | |
| CN106948968B (en) | Gas-turbine unit and its actuating device | |
| CN214577781U (en) | Back-to-back type compressor | |
| CN112502833A (en) | Double-shaft power generation gas turbine | |
| US20080014095A1 (en) | Turbofan engine and method of operating the same | |
| CN115306561A (en) | Gas turbine engine | |
| CN102834622A (en) | Method for adapting the air flow of a turbine engine having a centrifugal compressor and diffuser for implementing same | |
| CN214577793U (en) | Air-cooled compressor | |
| CN214577383U (en) | Slant thrust bearing type miniature gas turbine | |
| US6709243B1 (en) | Rotary machine with reduced axial thrust loads | |
| CN210623090U (en) | Compact axial flow pipeline pump | |
| CN112943679A (en) | Rotating shaft transmission structure, air compression device, fan, cutting machine and airplane blade | |
| CN211343737U (en) | Axial thrust structure of rotating shaft | |
| CN112096509A (en) | Streamline tunnel type turbocharger adopting outline type air bearing | |
| CN107524627B (en) | Static pressure radial impeller and its design method | |
| CN201810353U (en) | Sweepforward type shaft seal structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230620 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 |