CN116591988A - Compressor impeller - Google Patents
Compressor impeller Download PDFInfo
- Publication number
- CN116591988A CN116591988A CN202310682231.4A CN202310682231A CN116591988A CN 116591988 A CN116591988 A CN 116591988A CN 202310682231 A CN202310682231 A CN 202310682231A CN 116591988 A CN116591988 A CN 116591988A
- Authority
- CN
- China
- Prior art keywords
- blade
- edge
- splitter
- hub
- air inlet
- 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.)
- Pending
Links
- 238000003801 milling Methods 0.000 claims description 25
- 238000000034 method Methods 0.000 claims description 3
- 230000035939 shock Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 239000000306 component Substances 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/30—Vanes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention discloses an impeller of a compressor, which comprises a hub, wherein a plurality of long blades and splitter blades are arranged on the hub, the long blades and the splitter blades are distributed on the hub at intervals, dense tooth comb-shaped flow passages are distributed on the hub between the long blades and the splitter blades, each splitter blade comprises an air inlet edge, and a plurality of arc-shaped flow passages are densely distributed on the edge of the air inlet edge; the special splitter blade is in a curved-swept front edge blade shape, so that the strength of the front edge shock wave of the blade can be effectively reduced, the flow in the impeller is improved, the occurrence of secondary flow is restrained, the air flow uniformity in a low-speed area is improved through the special dense-tooth comb-shaped flow passage and the arc-shaped flow passage on the impeller, the surge margin of the air compressor can be remarkably improved, the stability of the air compressor is improved, and the efficiency of the turbocharger is greatly improved.
Description
Technical Field
The invention relates to the technical field of turbochargers, in particular to a compressor impeller.
Background
The turbocharger is a mechanical device which can increase the output power of the engine under the condition of unchanged working efficiency, and simultaneously, the fuel consumption rate of the engine is effectively reduced. In recent years, an engine supercharging technology is rapidly developed, and the supercharging technology plays an important role in reducing emission, improving power, recovering plateau performance and the like.
For turbochargers, the compressor wheel is the core component of the turbocharger, and high pressure ratio, high efficiency compressor design has been the goal of compressor wheel pursuit.
However, the structural design of the traditional impeller is unreasonable, the blade profile of the traditional impeller has no variability feature, the further improvement of the impeller performance is limited, the efficiency of the compressor is limited, and the efficiency of the whole turbocharger is further influenced.
Disclosure of Invention
The present invention is directed to a compressor impeller, which solves the above-mentioned problems.
In order to achieve the above purpose, the present invention provides the following technical solutions: the utility model provides a compressor impeller, includes the wheel is equipped with a plurality of long blades and splitter blade on the wheel is kept off, a plurality of long blades and splitter blade interval distribution are kept off on the wheel, lie in on the wheel between long blades and the splitter blade distribute have close tooth comb runner, every splitter blade includes the limit of admitting air, the limit of admitting air is gone up densely to have a plurality of arc runners.
Preferably, the long blade is in a ternary curved surface shape, the top of the long blade adopts a front edge curve structure, and the long blade is arranged in a radial curve by taking the hub as the center.
Preferably, the shape of the splitter blade is a curved-swept leading edge blade profile, and the splitter blades are also arranged in a radial curve.
Preferably, the milling mode of the dense tooth comb-shaped runner and the arc runner is as follows:
the step of milling the dense-tooth comb-shaped runner comprises the following steps: firstly, milling a plurality of grooves with the width of 0.4mm along the periphery of a splitter blade by using a milling cutter, ensuring that the left side of each groove body has a margin of 0.2mm, and then performing side milling on the margin of the left side by using the milling cutter to form grooves with the width of 0.6mm and a certain radian;
the arc runner milling step comprises the following steps: the cutter head of the ball end milling cutter is aligned with the top of the air inlet edge of the splitter blade, cutting is started along the streamline direction of the blade, in the feeding process, the cutter head moves from one side to the other side along the edge radian of the air inlet edge, and then the cutter is retracted to repeat operation until the whole edge of the air inlet edge is completely machined.
Compared with the prior art, the invention has the beneficial effects that: the special splitter blade is in a curved-swept front edge blade shape, so that the strength of the front edge shock wave of the blade can be effectively reduced, the flow in the impeller is improved, the occurrence of secondary flow is restrained, the air flow uniformity in a low-speed area is improved through the special dense-tooth comb-shaped flow passage and the arc-shaped flow passage on the impeller, the surge margin of the air compressor can be remarkably improved, the stability of the air compressor is improved, and the efficiency of the turbocharger is greatly improved.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present invention;
FIG. 2 is a schematic diagram of the trend of a cutter head for milling a comb-shaped runner with dense teeth;
fig. 3 is a schematic diagram of the trend of a cutter head for milling an arc-shaped runner according to the present invention.
Description of the embodiments
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
In the description of the present invention, it should be noted that the directions or positional relationships indicated by the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of description and simplification of description, and do not indicate or imply that the apparatus or element to be referred to must have a specific direction, be configured and operated in the specific direction, and thus should not be construed as limiting the invention. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "provided," "connected," and the like are to be construed broadly, and may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the terms in the invention will be understood by those of ordinary skill in the art in a specific context.
The uniformity of the impeller outlet flow field mainly refers to the angular distribution and absolute Mach number distribution of the airflow from the flow channel hub to the hroud side. The uniformity of the two parameters directly influences the design of the rear stator component, the overall stage efficiency and the variable working condition operation range, and is a very important assessment index when the compressor impeller is designed.
Referring to fig. 1, the present invention provides a technical solution: the compressor impeller comprises a hub 1, wherein a plurality of long blades 2 and splitter blades 3 are arranged on the hub 1, the long blades 2 and the splitter blades 3 are distributed on the hub 1 at intervals, dense-tooth comb-shaped flow channels 11 are distributed on the hub 1 between the long blades 2 and the splitter blades 3, each splitter blade 3 comprises an air inlet edge 31, and a plurality of arc-shaped flow channels 32 are densely distributed on the edge of the air inlet edge 31;
the air flow in the centrifugal compressor can generate a low-speed area in the side corner area of the impeller outlet casing under the comprehensive influence of centrifugal force and turning Golgi force, and the special dense-tooth comb-shaped flow channel 11 and the arc-shaped flow channel 32 improve the air flow angle in the middle main flow area, thereby ensuring the uniformity of the passing air flow, stabilizing the air flow difference to be about plus or minus 5%, and avoiding the generation of the low-speed area.
In this embodiment, the long blade 2 is in a ternary curved surface shape, the top of the long blade 2 adopts a front edge curve structure, and the long blade 2 is arranged in a radial curve with the hub 1 as the center.
In this embodiment, the shape of the splitter blade 3 is a curved leading edge blade profile, and by adopting the curved leading edge blade profile design, the outlet flow field of the splitter blade 3 can be ensured to be more uniform, so that the airflow is more stable, and the splitter blade 3 is also arranged in a radial curve.
In this embodiment, the milling method of the close-toothed comb-shaped runner 11 and the arc-shaped runner 32 is as follows:
as shown in conjunction with the tool bit trend of fig. 2, the milling step of the dense tooth comb-shaped runner 11 includes: firstly, milling a plurality of grooves with the width of 0.4mm along the periphery of the splitter blade 3 by using a milling cutter, ensuring that the left side of each groove body has a margin of 0.2mm, and then performing side milling on the margin of the left side by using the milling cutter to form grooves with the width of 0.6mm and a certain radian;
as shown in connection with the tool bit orientation of fig. 3, the arcuate flow passage 32 milling step includes: the head of the ball end milling cutter is aligned with the top of the air inlet edge 31 of the splitter blade 3, cutting is started along the streamline direction of the blade, in the feeding process, the head moves from one side to the other side along the edge radian of the air inlet edge, and then the tool is retracted to repeat the operation until the whole edge of the air inlet edge is completely machined.
In summary, the special splitter blade has the shape of a curved and swept front edge blade profile, so that the strength of the front edge shock wave of the blade can be effectively reduced, the flow in the impeller is improved, the occurrence of secondary flow is restrained, the air flow uniformity in a low-speed area is improved through the special close-tooth comb-shaped flow passage and the arc-shaped flow passage on the impeller, the surge margin of the compressor can be remarkably improved, the stability of the compressor is improved, and the efficiency of the turbocharger is greatly improved.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (4)
1. The utility model provides a compressor impeller, includes that the wheel is spared (1), be equipped with a plurality of long blades (2) and splitter blade (3) on the wheel is spared (1), a plurality of long blades (2) and splitter blade (3) interval distribution are spared (1), its characterized in that: the hub is characterized in that dense-tooth comb-shaped runners (11) are distributed on the hub (1) between the long blades (2) and the split blades (3), each split blade (3) comprises an air inlet edge (31), and a plurality of arc-shaped runners (32) are densely distributed on the edge of the air inlet edge (31).
2. A compressor wheel according to claim 1, wherein: the long blade (2) is in a ternary curved surface shape, the top of the long blade (2) adopts a front edge curve structure, and the long blade (2) is arranged in a radial curve by taking the hub (1) as the center.
3. A compressor wheel according to claim 1, wherein: the shape of the splitter blade (3) is a curved front edge blade shape, and the splitter blade (3) is also arranged in a radial curve.
4. A compressor wheel according to claim 1, wherein: the milling mode of the dense tooth comb-shaped runner (11) and the arc-shaped runner (32) is as follows:
the milling step of the dense-tooth comb-shaped runner (11) comprises the following steps: firstly, milling a plurality of grooves with the width of 0.4mm along the periphery of a splitter blade (3) by using a milling cutter, ensuring that the left side of each groove body has a margin of 0.2mm, and then side milling the margin of the left side by using the milling cutter to form grooves with the width of 0.6mm and a certain radian;
the milling step of the arc-shaped runner (32) comprises the following steps: the tool bit of the ball end mill is aligned with the top of the air inlet edge (31) of the splitter blade (3), cutting is started along the streamline direction of the blade, in the feeding process, the tool bit moves from one side to the other side along the edge radian of the air inlet edge, and then the tool retracting is repeated until the whole edge of the air inlet edge is completely machined.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310682231.4A CN116591988A (en) | 2023-06-09 | 2023-06-09 | Compressor impeller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310682231.4A CN116591988A (en) | 2023-06-09 | 2023-06-09 | Compressor impeller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN116591988A true CN116591988A (en) | 2023-08-15 |
Family
ID=87599194
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310682231.4A Pending CN116591988A (en) | 2023-06-09 | 2023-06-09 | Compressor impeller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN116591988A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118517433A (en) * | 2024-07-19 | 2024-08-20 | 潍坊富源增压器有限公司 | Impeller and processing technology thereof |
-
2023
- 2023-06-09 CN CN202310682231.4A patent/CN116591988A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118517433A (en) * | 2024-07-19 | 2024-08-20 | 潍坊富源增压器有限公司 | Impeller and processing technology thereof |
| CN118517433B (en) * | 2024-07-19 | 2024-10-11 | 潍坊富源增压器有限公司 | Impeller processing method |
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