CN214007588U - Flow passage sealing structure of compressor and refrigeration equipment - Google Patents
Flow passage sealing structure of compressor and refrigeration equipment Download PDFInfo
- Publication number
- CN214007588U CN214007588U CN202022796762.0U CN202022796762U CN214007588U CN 214007588 U CN214007588 U CN 214007588U CN 202022796762 U CN202022796762 U CN 202022796762U CN 214007588 U CN214007588 U CN 214007588U
- Authority
- CN
- China
- Prior art keywords
- sealing structure
- sealing
- impeller
- protrusion
- compressor
- 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
- 238000005057 refrigeration Methods 0.000 title claims abstract description 10
- 238000007789 sealing Methods 0.000 title claims description 123
- 244000126211 Hericium coralloides Species 0.000 claims description 53
- 239000000945 filler Substances 0.000 claims description 23
- 230000000903 blocking effect Effects 0.000 claims description 21
- 239000000463 material Substances 0.000 claims description 4
- -1 polytetrafluoroethylene Polymers 0.000 claims description 4
- 229920001343 polytetrafluoroethylene Polymers 0.000 claims description 4
- 239000004810 polytetrafluoroethylene Substances 0.000 claims description 4
- 239000012530 fluid Substances 0.000 description 8
- 230000000694 effects Effects 0.000 description 7
- 238000010992 reflux Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The utility model provides a runner seal structure and refrigeration plant of compressor, wherein runner seal structure includes impeller subassembly, spiral case, is equipped with seal structure between impeller and the spiral case relative motion's the surface, and seal structure includes radial seal structure and axial seal structure. The utility model provides a runner seal structure and refrigeration plant constantly increases radial broach seal structure and axial seal structure between the pneumatic runner of compressor, impeller and spiral case relative motion's surface to reach sealed purpose, the broach through whole pneumatic runner is constantly sealed, can reduce effectively to leak the efficiency that improves the compressor.
Description
Technical Field
The utility model relates to a refrigeration technology field, more specifically say, relate to a runner seal structure and refrigeration plant of compressor.
Background
With the continuous development of science and technology, the centrifugal compressor is also continuously innovated. A centrifugal compressor, which is a speed type compressor, increases pressure by compressing the inside thereof, and the higher the operating speed, the higher the pressure reached.
The energy efficiency of a centrifugal compressor is an important index for measuring the quality of one compressor, and in order to achieve higher energy efficiency, the leakage loss in the compressor needs to be reduced. Because the centrifugal compressor is a speed type compressor, comb teeth are arranged between a rotating part and a fixed part of the centrifugal compressor, and fluid passes through a channel formed by a plurality of throttling gaps and an expansion cavity and is subjected to multiple throttling to generate great energy loss, so that the pressure of the fluid is greatly reduced, the fluid is difficult to leak, and the aim of sealing is fulfilled.
However, the comb teeth as the static part and the rotating part have gaps, so that the comb teeth part still has partial leakage, and the internal integral comb tooth structure needs to be optimized for achieving higher energy efficiency.
Therefore, the comb tooth part of the existing centrifugal compressor still has certain leakage, so that the energy efficiency cannot be further improved, which is a technical problem to be solved in the field.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a solve current centrifugal compressor's broach part still to have certain leakage and lead to the technical problem that the efficiency can't further improve, provide a runner seal structure, compressor and the refrigeration plant of compressor.
For solving the above problem, the utility model discloses a technical scheme be: the flow passage sealing structure of the compressor comprises an impeller assembly and a volute, wherein a sealing structure is arranged between surfaces of the impeller and the volute which move relatively, and the sealing structure comprises a radial sealing structure and an axial sealing structure.
Further, the compressor is a centrifugal compressor, the impeller assembly comprises a two-stage impeller, a first sealing element, a first diffuser, a first backflow device, a second sealing element, a second backflow device, a volute air outlet, a third diffuser and an oil blocking sealing element are sequentially arranged on the outer side of the volute from an air inlet to an air outlet of the flow channel, and a second diffuser is arranged on the inner side of the volute.
Further, the primary impeller of the impeller assembly comprises: the first-stage wheel cover is matched with the first sealing element and the first diffuser through a first sealing structure, and the first-stage wheel hub is matched with the second diffuser through a second sealing structure and is connected with the first-stage wheel cover through a plurality of blades.
Further, the secondary impeller of the impeller assembly comprises: the second-stage wheel cover is matched with the second sealing element and the second backflow device through a third sealing structure, and the second-stage wheel hub is matched with the third diffuser and the oil blocking sealing element through a fourth sealing structure and is connected with the second-stage wheel cover through a plurality of blades.
Further, the impeller assembly further comprises an oil blocking sleeve which is connected with the secondary hub and matched with the oil blocking sealing piece through a fifth sealing structure.
Further, the impeller assembly further comprises a supporting sleeve which is correspondingly connected with the first-stage hub and the second-stage hub and is matched with the second diffuser through a sixth sealing structure.
Preferably, the sealing structure is a comb sealing structure.
Preferably, the first sealing structure comprises protruding structures arranged on the first-level wheel cover at intervals and comb tooth structures arranged on the first sealing element and corresponding to the protruding structures in a staggered mode, and the outer diameter of each protruding structure is smaller than the inner diameter of each comb tooth structure.
Preferably, the clearance between the convex structures and the comb tooth structures is 0.15-0.30 mm.
Preferably, the comb structure further comprises flexible filling strips which are arranged between the protruding parts of the comb tooth structures and correspond to the intervals of the protruding parts of the protruding structures, and the intervals of the protruding parts of the comb tooth structures are smaller than the width of the flexible filling strips.
Preferably, the inner diameter of the flexible filler strip is smaller than the inner diameter of the comb tooth structure and larger than the inner diameter of the protruding structure, and the inner diameter of the flexible filler strip is smaller than the outer diameter of the protruding structure.
Preferably, the protruding structure includes first protruding structure and the second protruding structure that is the echelonment and distributes, and the internal diameter and the external diameter of the protruding structure of second correspond and are greater than the internal diameter and the external diameter of first protruding structure, and the protruding structure of broach structure correspondence includes first broach structure and second broach structure.
Preferably, the flexible filler strip is made of a polytetrafluoroethylene material.
The utility model also provides a refrigeration plant, including the compressor, the compressor includes foretell runner seal structure.
Compared with the prior art, the utility model provides a main control board box structure and refrigerator have following beneficial effect:
the utility model provides a flow passage sealing structure, which continuously increases comb teeth in a pneumatic flow passage of a compressor to achieve the purpose of sealing; the air inlet of the impeller is provided with a comb seal which is adjusted to be step-shaped to form a secondary seal; the comb teeth are added on the diffuser, the part between the impeller diffuser and the impeller belongs to a high-pressure part, after the comb teeth are added, pressure drop can be formed inside by utilizing high-speed rotation of the impeller, when fluid leaks to the comb teeth of the next-stage impeller, the pressure is very small, and the sealing purpose can be effectively achieved through secondary sealing of the comb teeth; comb teeth are arranged at the supporting sleeve to achieve the purpose of sealing; when the gas reaches the secondary impeller, the comb teeth are added at the sealing element and the reflux device, the pressure is reduced by utilizing the rotation pressure drop of the comb teeth, and the sealing effect is achieved by the comb teeth sealing of the secondary impeller; comb teeth are added on the other side of the secondary impeller and the oil-resistant sealing element; the comb teeth are additionally arranged at the positions of the oil blocking sealing piece and the oil blocking sleeve, leakage is reduced, the comb teeth passing through the whole pneumatic flow channel are continuously sealed, leakage can be effectively reduced, and the energy efficiency of the compressor is improved.
Drawings
Fig. 1 is a cross-sectional view of a first embodiment of a flow passage sealing structure of a compressor according to the present invention;
fig. 2 is a cross-sectional view of a first sealing member and an impeller of a first embodiment of a flow passage sealing structure of a compressor according to the present invention;
FIG. 3 is an enlarged view of a portion of region D of FIG. 1;
fig. 4 is a cross-sectional view of an oil blocking sealing member and an oil blocking sleeve according to a first embodiment of a flow passage sealing structure of a compressor provided by the present invention;
fig. 5 is a cross-sectional view of a second embodiment of a flow passage sealing structure of a compressor according to the present invention;
fig. 6 is a cross-sectional view of a first sealing member and an impeller of a second embodiment of a flow passage sealing structure of a compressor according to the present invention;
FIG. 7 is an enlarged view of a portion of area E in FIG. 5;
fig. 8 is a schematic structural view of a flexible filler strip of a second embodiment of a flow passage sealing structure of a compressor according to the present invention.
Wherein, in the drawings, the reference numerals are mainly as follows:
1-a first seal; 2-a first diffuser; 3-a second diffuser; 4-a first reflux unit; 5-a second seal; 6-volute air outlet; 7-a third diffuser; 8-oil resistant seals; 9-oil blocking sleeve; 10-a secondary hub; 11-a support sleeve; 12-a primary hub; 13-a second reflux vessel; 14-primary wheel cover; 15-secondary wheel cover; 16-a first sealing structure; 161-a first raised structure; 162-a first comb tooth structure; 163-flexible filler strip; 164-a second raised structure; 165-a second comb tooth structure; 166-a third raised structure; 17-a second sealing structure; 18-a third seal configuration; 19-a fourth seal configuration; 20-a fifth seal configuration; 21-a sixth sealing structure; 22-a blade; 23-a main shaft; 24-a flow channel; 25-a first-stage impeller air inlet; 26-the outlet of the first-stage impeller; 27-a secondary impeller air inlet; 28-the outlet of the secondary impeller;
wherein, other reference numbers:
l1-spacing of the projections of the first comb tooth structure; l2-width of flexible filler strip; d1 — outer diameter of second projection arrangement; d2-outer diameter of the secondary impeller air outlet; d3-inner diameter of second comb tooth structure; d4 — outer diameter of first projection arrangement; d5-inner diameter of first comb tooth structure; d6 — inner diameter of first projection structure; d7-outer diameter of first comb tooth structure; d8-outer diameter of flexible filler strip; d9-inner diameter of Flexible Filler Bar.
Detailed Description
In order to make the technical problems, technical solutions and advantageous effects to be solved by the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings 1 to 8 and the embodiments.
The utility model provides a runner seal structure of compressor, including main shaft 23, as the rotor along with main shaft 23 pivoted impeller subassembly, as the spiral case of stator, the compressor is preferred centrifugal compressor, and the impeller subassembly includes the two-stage impeller, is equipped with seal structure between the surface of relative motion between impeller and the spiral case, and seal structure includes radial seal structure and axial seal structure, preferably is broach seal structure.
A flow passage 24 is formed between the volute and the impeller assembly, a first sealing element 1, a first diffuser 2, a first flow return device 4, a second sealing element 5, a second flow return device 13, a volute air outlet 6, a third diffuser 7 and an oil blocking sealing element 8 are sequentially arranged on the outer side of the volute along the air inlet to the air outlet of the flow passage 24, and a second diffuser 3 is arranged on the inner side of the volute.
The first stage impeller of the impeller assembly comprises: the first-stage wheel cover 14 is matched with the first sealing element 1 and the first diffuser 2 at the air inlet of the flow passage 24, namely the outer side of the first-stage impeller air inlet 25 through a first sealing structure 16, and the first-stage wheel hub 12 is matched with the second diffuser 3 at the inner side of the first-stage impeller air outlet 26 in the flow passage 24 through a second sealing structure 17 and is connected with the first-stage wheel cover 14 through a plurality of blades 22.
As the utility model provides a pair of embodiment one:
the first sealing structure 16 comprises protruding structures arranged on the first-level wheel cover 14 at intervals and comb tooth structures arranged on the first sealing element 1 and corresponding to the protruding structures in a staggered mode, the outer diameter of each protruding structure is smaller than the inner diameter of each comb tooth structure, and the gap between each protruding structure and each comb tooth structure is 0.15-0.30 mm.
In a preferred embodiment, the protruding structures include a first protruding structure 161 and a second protruding structure 164 distributed in a step shape, an inner diameter of the second protruding structure 164 and an outer diameter D1 of the second protruding structure 164 are respectively greater than an inner diameter D6 of the first protruding structure 161 and an outer diameter D4 of the first protruding structure 161, and the comb-tooth-structure-corresponding protruding structure includes a first comb-tooth structure 162 and a second comb-tooth structure 165. Wherein: the outer diameter D4 of the first projection structure 161 is smaller than the inner diameter D5 of the first comb tooth structure 162; the outer diameter D1 of the second projection structure 164 is less than the inner diameter D3 of the second comb tooth structure 165; gaps between the first convex structures 161 and the first comb tooth structures 162 and between the second convex structures 164 and the second comb tooth structures 165 are kept at 0.15-0.30mm, namely D3-D1 are larger than or equal to 0.15mm and smaller than or equal to 0.30mm, D5-D4 are larger than or equal to 0.15mm and smaller than or equal to 0.30mm, normal assembly is guaranteed, leakage is reduced, and sealing performance is improved; the air inlet of the impeller is provided with a comb seal, and the comb seal structure is adjusted to be a step type to form a secondary seal.
The first seal member 1 and the first diffuser 2 are connected as a whole, and the first seal structure 16 further includes: a third comb tooth structure (not shown) provided on the first diffuser 2 outside the first-stage impeller air outlet 26 in the flow passage 24 and a third protrusion structure 166 provided on the first seal member 1 in staggered correspondence with the third comb tooth structure. The sealing structure formed by the third comb tooth structure and the third protrusion structure 166 is connected with the sealing structure formed by the first protrusion structure 161, the first comb tooth structure 162, the second protrusion structure 164 and the second comb tooth structure 165 into a whole to form the first sealing structure 16, including radial and axial seal configurations, since the third comb tooth structure and the third projection structure 166 are located at the first-stage impeller gas outlet 26 in the flow passage 24, which is the high-pressure side in the flow passage 24, and tend to leak toward the low-pressure side, when the gas outside the first-stage impeller gas outlet 26 leaks to the low-pressure side, the gas passes through the third comb tooth structure, the third protrusion structure 166, the first protrusion structure 161, the first comb tooth structure 162, the second protrusion structure 164, and the gap between the protrusions of the first sealing structure 16 and the comb teeth of the second comb tooth structure 165, and then the rotary pressure drop is generated, so that the pressure is gradually reduced; after pressure drop, the fluid passes through the comb tooth sealing structure, passes through a plurality of axially or radially staggered throttling gaps, forms an expansion cavity between the gaps, passes through a channel formed by the throttling gaps and the expansion cavity, is throttled for a plurality of times and generates great energy loss, so that the pressure of the fluid is greatly reduced, the fluid is difficult to leak, and finally the sealing purpose is achieved. Similarly, the second sealing structure 17 between the back of the first-stage hub 12 inside the first-stage impeller gas outlet 26 in the flow passage 24 and the second diffuser 3 also achieves the effect of reducing the gas inside the first-stage impeller gas outlet 26 from the other direction so as to achieve sealing; increase the broach on the diffuser, the part between diffuser and the impeller belongs to the high pressure part, increases the broach back, utilizes the high-speed rotation of impeller, can form the pressure drop in inside, leaks to next-stage broach department when the fluid, and pressure is very little, and the secondary seal through the broach can effectually reach sealed purpose.
The secondary impeller of the impeller assembly comprises: the secondary impeller hub 10 is provided with a secondary shroud 15 fitted with the second seal 5 and the second return device 13 through the third seal structure 18 on the outer side of the secondary impeller air inlet 27 in the flow passage 24, and a secondary hub 10 fitted with the third diffuser 7 and the oil-blocking seal 8 through the fourth seal structure 19 on the inner side of the secondary impeller air outlet 28 in the flow passage 24 and connected with the secondary shroud 15 by a plurality of blades 22. The third diffuser 7 and the oil-blocking sealing member 8 are connected into a whole; the specific structures of the third sealing structure 18 and the fourth sealing structure 19 are similar to those of the first sealing structure 16 and the second sealing structure 17, and accordingly the effect of reducing leakage of gas outside the secondary impeller gas outlet 28 and in the inner layer so as to realize sealing is achieved.
The impeller assembly further comprises an oil blocking sleeve 9 connected with the secondary hub 10 and matched with the oil blocking sealing member 8 through a fifth sealing structure 20. The concrete structure of the fifth sealing structure 20 is similar to that of the first sealing structure 16, so that the air outlet 28 of the secondary impeller is connected with the fifth sealing structure 20 through the fourth sealing structure 19; because the oil blocking sleeve 9 and the oil blocking sealing element 8 are arranged behind the motor box body and belong to the low-pressure side, the leakage direction starts to leak from the back of the secondary hub 10, under the condition that the pressure of a flow channel 24 where the secondary impeller is located is larger than that of a flow channel 24 where the primary impeller is located and the compressor needs to be sealed more strongly, the gas at the gas outlet 28 of the secondary impeller and between the oil blocking sealing element 8 and the oil blocking sleeve 9 is reduced and leaked through the comb tooth structure of the fourth sealing structure 19 between the secondary hub 10 and the oil blocking sealing element 8 and the double sealing structure of the comb tooth structure of the fifth sealing structure 20 between the oil blocking sleeve 9 and the oil blocking sealing element 8, so that the sealing effect is realized.
The impeller assembly further comprises a support sleeve 11 which is correspondingly connected with the first-stage hub 12 and the second-stage hub 10 and is matched with the second diffuser 3 through a sixth sealing structure 21. The sixth sealing structure 21 is preferably an axial sealing structure, and the second-stage impeller air inlet 27 with relatively high pressure and the first-stage impeller air outlet 26 with relatively low pressure are communicated with the sixth sealing structure 21 through the second sealing structure 17, the cavity between the first-stage hub 12 and the second diffuser 3, so that the gas leakage at the first-stage impeller air outlet 26 is reduced to realize the sealing effect.
As a preferred embodiment of the present invention:
the first sealing structure 16 further comprises flexible filler strips 163 disposed between the protrusions of the comb tooth structure corresponding to the intervals of the protrusions of the protrusion structure, the flexible filler strips 163 preferably being made of polytetrafluoroethylene material; during assembly, the flexible filling strips 163 are assembled with the comb tooth structure, in order to ensure that the filling strips are tightly matched with the comb tooth structure, the interval of the protruding parts of the comb tooth structure is smaller than the width L2 of the flexible filling strips 163, and the outer diameter D8 of the flexible filling strips 163 is equal to the outer diameter of the comb tooth structure; the two are assembled with the primary wheel cover 14, and because the polytetrafluoroethylene material is soft, the inner diameter D9 of the flexible filler strip 163 is smaller than the inner diameter of the comb structure and larger than the inner diameter of the protruding structure, and meanwhile, the inner diameter D9 of the flexible filler strip 163 is smaller than the outer diameter of the protruding structure.
As a preferred embodiment, the convex structure comprises a first convex structure 161 and a second convex structure 164 distributed in a step shape, the comb-tooth-structure-corresponding convex structure comprises a first comb-tooth structure 162 and a second comb-tooth structure 165, and the radial dimensions of the first convex structure 161, the second convex structure 164, the first comb-tooth structure 162 and the second comb-tooth structure 165 are preferably the same as those in the first embodiment; the spacing L1 of the projections of the first comb tooth structure 162 is less than the width L2 of the flexible filler strip 163, and the outer diameter D8 of the flexible filler strip 163 is equal to the outer diameter D7 of the first comb tooth structure 162; the inner diameter D9 of the flexible filler strip 163 is smaller than the inner diameter D5 of the first comb tooth structure 162 and larger than the inner diameter D6 of the first protrusion structure 161, while the inner diameter D9 of the flexible filler strip 163 is smaller than the outer diameter D4 of the first protrusion structure 161. The radial dimensional relationship of the second comb structures 165, the second protrusion structures 164 and the flexible filler strips 163 is similar to the radial dimensional relationship of the first comb structures 162, the first protrusion structures 161 and the flexible filler strips 163.
In a preferred embodiment, when the outer diameter D1 of the second protrusion 164 and the outer diameter D2 of the secondary impeller air outlet 28 satisfy: when D2/D1 is more than or equal to 1.1 and less than or equal to 1.6, the sealing effect is better.
The utility model also provides a refrigeration plant, including the compressor, the compressor includes foretell runner 24 seal structure. The compressor is preferably a centrifugal compressor.
The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.
Claims (14)
1. The flow passage sealing structure of the compressor comprises an impeller assembly and a volute, and is characterized in that a sealing structure is arranged between the surfaces of the impeller and the volute which move relatively, and the sealing structure comprises a radial sealing structure and an axial sealing structure.
2. The flow path sealing structure according to claim 1, wherein the compressor is a centrifugal compressor, the impeller assembly includes a two-stage impeller, a first sealing member, a first diffuser, a first flow return device, a second sealing member, a second flow return device, an air outlet, a third diffuser, and an oil blocking sealing member are sequentially disposed on an outer side of the scroll casing along an air inlet to an air outlet of the flow path, and a second diffuser is disposed on an inner side of the scroll casing.
3. The flow path sealing structure of claim 2, wherein the primary impeller of the impeller assembly comprises: the first-stage wheel cover is matched with the first sealing element and the first diffuser through a first sealing structure, and the first-stage wheel hub is matched with the second diffuser through a second sealing structure and is connected with the first-stage wheel cover through a plurality of blades.
4. The flow path sealing structure of claim 3, wherein the secondary impeller of the impeller assembly comprises: the second-stage wheel cover is matched with the second sealing element and the second backflow device through a third sealing structure, and the second-stage wheel hub is matched with the third diffuser and the oil blocking sealing element through a fourth sealing structure and is connected with the second-stage wheel cover through a plurality of blades.
5. The flow path seal arrangement of claim 4, wherein said impeller assembly further comprises an oil dam sleeve connected to said secondary hub and cooperating with said oil dam seal via a fifth seal arrangement.
6. The flow path sealing structure of claim 4, wherein the impeller assembly further comprises a support sleeve coupled to the first stage hub and the second stage hub and coupled to the second diffuser via a sixth sealing structure.
7. A flow path sealing structure according to any one of claims 3 to 6, characterized in that said sealing structure is a comb sealing structure.
8. The flow channel sealing structure of claim 7, wherein said first sealing structure comprises a protrusion structure spaced apart from said primary shroud and a comb structure disposed on said first sealing member in staggered correspondence with said protrusion structure, said protrusion structure having an outer diameter smaller than an inner diameter of said comb structure.
9. The flow channel sealing structure of claim 8, wherein a gap between the protrusion structure and the comb tooth structure is 0.15-0.30 mm.
10. The flow channel sealing structure of claim 8, further comprising flexible filler strips disposed between the protrusions of the comb tooth structures corresponding to the spacing of the protrusions of the protrusion structures, the spacing of the protrusions of the comb tooth structures being less than the width of the flexible filler strips.
11. The flow path sealing structure of claim 10, wherein the inner diameter of the flexible filler strip is smaller than the inner diameter of the comb structure and larger than the inner diameter of the protrusion structure, and the inner diameter of the flexible filler strip is smaller than the outer diameter of the protrusion structure.
12. The flow channel sealing structure of claim 10, wherein the protrusion structures comprise a first protrusion structure and a second protrusion structure distributed in a step shape, the inner diameter and the outer diameter of the second protrusion structure are correspondingly larger than the inner diameter and the outer diameter of the first protrusion structure, and the comb tooth structure comprises a first comb tooth structure and a second comb tooth structure corresponding to the protrusion structures.
13. The runner seal structure of claim 10, wherein said flexible filler strip is made of a polytetrafluoroethylene material.
14. A refrigeration device comprising a compressor, wherein said compressor comprises a flow path sealing structure according to any one of claims 1-13.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022796762.0U CN214007588U (en) | 2020-11-27 | 2020-11-27 | Flow passage sealing structure of compressor and refrigeration equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022796762.0U CN214007588U (en) | 2020-11-27 | 2020-11-27 | Flow passage sealing structure of compressor and refrigeration equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214007588U true CN214007588U (en) | 2021-08-20 |
Family
ID=77307642
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022796762.0U Active CN214007588U (en) | 2020-11-27 | 2020-11-27 | Flow passage sealing structure of compressor and refrigeration equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214007588U (en) |
-
2020
- 2020-11-27 CN CN202022796762.0U patent/CN214007588U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8066475B2 (en) | Labyrinth compression seal and turbine incorporating the same | |
| US9260979B2 (en) | Outer rim seal assembly in a turbine engine | |
| CN111720175B (en) | Impeller machinery movable vane top seal structure | |
| JP2000054996A (en) | Radial compressor, and its operation method | |
| CN112392760A (en) | Flow passage sealing structure of compressor and refrigeration equipment | |
| CN106151063B (en) | CO circulating gas compressor | |
| US6264425B1 (en) | Fluid-flow machine for compressing or expanding a compressible medium | |
| CN214007588U (en) | Flow passage sealing structure of compressor and refrigeration equipment | |
| JPH11350917A (en) | Structure for reducing leakage in steam turbine | |
| CN212671868U (en) | Impeller machinery movable vane top seal structure | |
| CN104632645A (en) | Double inlet multistage centrifugal compressor | |
| CN108278221B (en) | Air inlet sealing structure and fan | |
| RU2263809C2 (en) | Multistage gas turbine | |
| US3252421A (en) | Pumps | |
| WO2020031625A1 (en) | Rotary machine and seal member | |
| CN114876865A (en) | Supercritical carbon dioxide compressor impeller sealing structure and compressor | |
| CN115726841A (en) | Novel seal gas circuit structure and turbine disc | |
| CN110645355B (en) | Flow guide type combined labyrinth sealing device | |
| CN115013104A (en) | Fuel cell energy recovery system | |
| CN213235233U (en) | Gas turbine, low-pressure compressor and mechanical impeller sealing assembly of low-pressure compressor | |
| RU2369749C1 (en) | Two-stage turbine of has turbine engine | |
| CN215633947U (en) | Gas sealing device for air compressor and air compressor | |
| CN216922228U (en) | Rotor and stator step type labyrinth sealing structure with axial side teeth | |
| CN220286035U (en) | Improved semi-open centrifugal impeller and automobile air conditioner fan using same | |
| JP3362643B2 (en) | Shaft end refrigerant flow type gas turbine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |