CN114687804A - Turbine shaft of turbocharger - Google Patents
Turbine shaft of turbocharger Download PDFInfo
- Publication number
- CN114687804A CN114687804A CN202011575991.8A CN202011575991A CN114687804A CN 114687804 A CN114687804 A CN 114687804A CN 202011575991 A CN202011575991 A CN 202011575991A CN 114687804 A CN114687804 A CN 114687804A
- Authority
- CN
- China
- Prior art keywords
- section
- turbine shaft
- reinforcing
- reinforcing section
- limiting
- 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
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 32
- 238000007789 sealing Methods 0.000 claims abstract description 6
- 238000000034 method Methods 0.000 abstract description 4
- 238000005266 casting Methods 0.000 abstract description 2
- 230000002787 reinforcement Effects 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/025—Fixing blade carrying members on shafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
The invention provides a turbine shaft of a turbocharger, which comprises a turbine shaft body, wherein the turbine shaft body comprises an impeller mounting section, a limiting section, a first reinforcing section, a threaded section, a second reinforcing section and an output section which are sequentially arranged from top to bottom; the middle end part sleeve of the second reinforcing section is sequentially provided with a sealing ring and a limiting ring from top to bottom; the turbine shaft body is formed by integrally casting the impeller mounting section, the limiting section, the first reinforcing section, the threaded section, the second reinforcing section and the output section, so that the welded part of the turbine shaft body is prevented from being broken in the use process, the structure is simple, the operation is convenient, the product percent of pass is improved, the replacement of people is convenient, and the use requirements of people are met.
Description
Technical Field
The invention mainly relates to the field of turbochargers, in particular to a turbine shaft of a turbocharger.
Background
Turbocharging is a technique of driving an air compressor using exhaust gas generated by the operation of an internal combustion engine. Both of these functions, like the super charger, increase the air flow into the engine or boiler, thereby increasing the efficiency of the machine. Turbochargers are commonly used in automotive engines to boost the horsepower output of an internal combustion engine by utilizing the heat and flow of the exhaust gases. Because the supercharger is arranged on the exhaust side of the engine, the working temperature of the supercharger is very high, the rotating speed of the rotor of the supercharger is very high during working, which can reach hundreds of thousands of revolutions per minute, and the high rotating speed and temperature make common mechanical roller pins or ball bearings incapable of working for the rotor.
The turbine shaft is the heart portion of the turbocharger. Plays a crucial role in the whole work. In the turbocharging, a turbine shaft not only bears the power transmission, but also compresses fresh air and inputs the compressed air into an engine,
therefore, the turbine shaft is under high pressure and has severe working conditions, and a turbine shaft with high reliability needs to be designed.
Disclosure of Invention
Aiming at the defects in the prior art, the invention provides a turbine shaft of a turbocharger, which comprises a turbine shaft body 1, wherein the turbine shaft body 1 comprises an impeller mounting section 2, a limiting section 3, a first reinforcing section 4, a thread section 5, a second reinforcing section 6 and an output section 7 which are sequentially arranged from top to bottom;
and the middle end part sleeve of the second reinforcing section 6 is sequentially provided with a sealing ring 8 and a limiting ring 9 from top to bottom.
Preferably, the sealing ring 8 and the limiting ring 9 are arranged in a fitting mode.
Preferably, the stop collar 9 is welded to the second reinforcing section 6.
Preferably, the impeller mounting section 2 is provided with a clamping groove 10 along the side wall.
Preferably, the impeller mounting section 2, the limiting section 3, the first reinforcing section 4, the thread section 5, the second reinforcing section 6 and the output section 7 are integrally cast.
Preferably, the second reinforcing segment 6 has a length greater than the length of the first reinforcing segment 4.
The invention has the beneficial effects that: the turbine shaft body is formed by integrally casting the impeller mounting section, the limiting section, the first reinforcing section, the threaded section, the second reinforcing section and the output section, so that the welded part of the turbine shaft body is prevented from being broken in the use process,
the invention has simple structure and convenient operation, improves the product percent of pass, is convenient for people to replace and meets the use requirements of people.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
in the figure, the position of the first and second end faces,
1. a turbine shaft body; 2. an impeller mounting section; 3. a limiting section; 4. a first reinforcement section; 5. a threaded segment; 6. a second reinforcing section; 7. an output section; 8. a seal ring; 9. a limiting ring; 10. a clamping groove.
Detailed Description
In order to make the technical solutions of the present invention better understood and make the above features, objects, and advantages of the present invention more comprehensible, the present invention is further described below with reference to the following examples. The examples are intended to illustrate the invention only and are not intended to limit the scope of the invention.
As shown in fig. 1, the present invention includes: the turbine shaft comprises a turbine shaft body 1, wherein the turbine shaft body 1 comprises an impeller mounting section 2, a limiting section 3, a first reinforcing section 4, a thread section 5, a second reinforcing section 6 and an output section 7 which are sequentially arranged from top to bottom;
and the middle end part sleeve of the second reinforcing section 6 is sequentially provided with a sealing ring 8 and a limiting ring 9 from top to bottom.
In this embodiment, the seal ring 8 and the limit ring 9 are preferably attached to each other.
In this embodiment, the stop collar 9 is preferably welded to the second reinforcing section 6.
In this embodiment, it is preferable that the impeller mounting section 2 is provided with a clamping groove 10 along a side wall.
In this embodiment, the impeller mounting section 2, the limiting section 3, the first reinforcing section 4, the threaded section 5, the second reinforcing section 6 and the output section 7 are preferably integrally cast.
In the present embodiment, it is preferred that the second reinforcement segment 6 has a length greater than the length of the first reinforcement segment 4.
In use, the impeller mounting section, the limiting section, the first reinforcing section, the thread section, the second reinforcing section and the output section are integrally cast, so that the fracture of the welding part of the turbine shaft body is prevented in the use process,
the invention has simple structure and convenient operation, improves the product percent of pass, is convenient for people to replace and meets the use requirements of people.
The above-described embodiments are merely illustrative of the principles and utilities of the present patent application and are not intended to limit the present patent application. Modifications and variations can be made to the above-described embodiments by those skilled in the art without departing from the spirit and scope of this patent application. Accordingly, it is intended that all equivalent modifications or changes which can be made by those skilled in the art without departing from the spirit and technical concepts disclosed in the present application shall be covered by the claims of this patent application.
Claims (6)
1. The turbine shaft of the turbocharger is characterized by comprising a turbine shaft body (1), wherein the turbine shaft body (1) comprises an impeller mounting section (2), a limiting section (3), a first reinforcing section (4), a thread section (5), a second reinforcing section (6) and an output section (7) which are sequentially arranged from top to bottom;
and the middle end part sleeve of the second reinforcing section (6) is sequentially provided with a sealing ring (8) and a limiting ring (9) from top to bottom.
2. The turbine shaft of a turbocharger according to claim 1, characterized in that: the sealing ring (8) and the limiting ring (9) are attached to each other.
3. The turbine shaft of a turbocharger according to claim 2, characterized in that: the limiting ring (9) is welded on the second reinforcing section (6).
4. The turbine shaft of a turbocharger according to claim 1, characterized in that: the impeller mounting section (2) is provided with a clamping groove (10) along the side wall.
5. The turbine shaft of a turbocharger according to claim 1, characterized in that: the impeller comprises an impeller mounting section (2), a limiting section (3), a first reinforcing section (4), a thread section (5), a second reinforcing section (6) and an output section (7) which are integrally cast.
6. The turbine shaft of a turbocharger according to claim 5, characterized in that: the length of the second reinforcing section (6) is larger than that of the first reinforcing section (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011575991.8A CN114687804A (en) | 2020-12-28 | 2020-12-28 | Turbine shaft of turbocharger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011575991.8A CN114687804A (en) | 2020-12-28 | 2020-12-28 | Turbine shaft of turbocharger |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114687804A true CN114687804A (en) | 2022-07-01 |
Family
ID=82129712
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011575991.8A Pending CN114687804A (en) | 2020-12-28 | 2020-12-28 | Turbine shaft of turbocharger |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114687804A (en) |
-
2020
- 2020-12-28 CN CN202011575991.8A patent/CN114687804A/en active Pending
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20220701 |