Rotating shaft component of turbocharger
By introducing a connection assembly into the turbocharger and using threaded connections instead of welding, the problem of being unable to quickly install or disassemble damaged shaft components is solved, a convenient installation and disassembly process is achieved, and work efficiency is improved.
Patent Information
- Application Number
- CN202422100634.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-28
- Publication Date
- 2025-09-09
- Estimated Expiration
- 2034-08-28
AI Technical Summary
The rotating shaft components of existing turbochargers are connected by welding, which makes it difficult to quickly install or disassemble them when damaged, causing inconvenience to workers.
A connection assembly is used, including a fixing seat, a sealing ring, a connecting seat, a limit plate, a tight plate, a mounting cylinder, a connecting rod and bolts, etc., and the shaft component and the turbine are quickly installed and disassembled through threaded connection.
The quick installation and disassembly of the shaft components and the turbine is realized, which improves the working efficiency and facilitates the subsequent replacement and maintenance.
Smart Images

Figure CN223318107U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of turbocharger rotating shafts, in particular to a rotating shaft component of a turbocharger. Background Art
[0002] A turbocharger is actually an air compressor that increases the intake volume by compressing air. It uses the inertial force of the exhaust gas discharged by the engine to drive the turbine in the turbine chamber. The turbine in turn drives the coaxial impeller, which pressurizes the air sent from the air filter pipe and pressurizes it into the cylinder. When the engine speed increases, the exhaust gas discharge speed and the turbine speed also increase synchronously, and the impeller compresses more air into the cylinder. The increase in air pressure and density can burn more fuel. By increasing the fuel amount and adjusting the engine speed accordingly, the engine's output power can be increased.
[0003] Currently, most shaft components on the market are connected to turbochargers by welding. However, after long-term use, the shaft components of the turbocharger are easily damaged, and workers are unable to quickly install or disassemble the shaft components to the turbocharger, causing inconvenience to the workers.
[0004] To this end, we propose a rotating shaft component of a turbocharger. Utility Model Content
[0005] The purpose of the present utility model is to provide a turbocharger shaft component to solve the problem raised in the above background technology that most of the shaft components on the market are connected to the turbocharger by welding, and when the shaft component is damaged, the shaft component cannot be quickly installed or disassembled from the turbocharger.
[0006] To achieve the above objectives, the present invention provides the following technical solution: a rotating shaft component of a turbocharger comprises a turbine and a rotating shaft component body, wherein a connecting assembly capable of being detached from each other is provided between the turbine and the rotating shaft component body.
[0007] The connection assembly includes a fixing seat installed on one side of the turbine, an inner wall of the fixing seat is provided with a first thread, and one end of the fixing seat is provided with a groove.
[0008] Among them, a sealing ring is placed inside the groove, a tight groove is opened on one side of the sealing ring, a connecting seat is movably connected inside the fixing seat, and a positioning thread groove is opened on the outside of the connecting seat.
[0009] The outer wall of the connecting seat is provided with a second thread, and a limiting plate is installed at one end of the connecting seat, and the diameter of the limiting plate is larger than the diameter of the connecting seat.
[0010] Wherein, a tight plate is installed on one side of the limiting plate, and the tight plate is located in the tight groove.
[0011] A mounting tube is fixedly mounted on one side of the fixing seat, and a connecting rod is movably connected inside the mounting tube.
[0012] One end of the connecting rod is fixedly installed with a bolt, and the other end of the connecting rod passes through and extends to the top of the installation tube and is fixedly installed with an anti-slip handle.
[0013] The utility model has at least the following beneficial effects:
[0014] When the utility model is in use, the shaft component body and the turbine are connected by setting a connecting component, replacing the structure that may require welding to connect the shaft component body and the turbine. The setting of the connecting component facilitates the rapid installation and disassembly between the turbine and the shaft component body, brings convenience to the staff and improves the overall work efficiency. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Figure 1 This is a schematic diagram of the overall structure of the utility model;
[0016] Figure 2 This is a semi-exploded diagram of the structure of the utility model;
[0017] Figure 3 This is a schematic diagram of the connection components of the utility model;
[0018] Figure 4 This is a semi-exploded diagram of the connection assembly of the utility model from the first perspective;
[0019] Figure 5 This is a semi-exploded diagram of the connecting assembly of the present invention from a second perspective;
[0020] Figure 6 This is an internal diagram of the connection component of the utility model.
[0021] In the figure: 1. turbine; 2. connecting assembly; 3. rotating shaft component body; 21. fixing seat; 22. first thread; 23. groove; 24. sealing ring; 25. tight groove; 26. connecting seat; 27. second thread; 28. limit plate; 29. tight plate; 210. mounting tube; 211. connecting rod; 212. bolt; 213. anti-slip handle; 214. positioning thread groove. DETAILED DESCRIPTION
[0022] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.
[0023] Example 1
[0024] See also Figures 1 to 6 The utility model provides a technical solution: the rotating shaft component of the turbocharger includes: a turbine 1 and a rotating shaft component body 3, and a connecting component 2 that can be disassembled and assembled with each other is commonly provided between the turbine 1 and the rotating shaft component body 3; through the setting of the connecting component 2, the turbine 1 and the rotating shaft component body 3 can be quickly installed or disassembled, which is convenient for subsequent replacement or maintenance of the rotating shaft component body 3.
[0025] The connecting assembly 2 includes a fixing seat 21 mounted on one side of the turbine 1, the inner wall of the fixing seat 21 is provided with a first thread 22, one end of the fixing seat 21 is provided with a groove 23, a sealing ring 24 is placed inside the groove 23, and a tight groove 25 is provided on one side of the sealing ring 24. The interior of the fixing seat 21 is movably connected to the connecting seat 26, and a positioning thread groove 214 is provided on the outside of the connecting seat 26. A second thread 27 is provided on the outer wall of the connecting seat 26, and a limiting plate 28 is installed at one end of the connecting seat 26. The diameter of the limiting plate 28 is larger than the diameter of the connecting seat 26, and one side of the limiting plate 28 is installed. There is a tight plate 29, which is located in the tight groove 25. A mounting tube 210 is fixedly installed on one side of the fixing seat 21. A connecting rod 211 is movably connected inside the mounting tube 210. A bolt 212 is fixedly installed on one end of the connecting rod 211. The other end of the connecting rod 211 passes through and extends to the top of the mounting tube 210 and is fixedly installed with an anti-slip handle 213; the bolt 212 is threadedly connected to the inside of the positioning thread groove 214, and the first thread 22 and the second thread 27 are adapted to each other. The connecting seat 26 can be connected to the inside of the fixing seat 21 through the first thread 22 and the second thread 27.
[0026] One end of the shaft body 3 is fixedly connected to the limit plate 28. When the shaft body 3 needs to be disassembled, the user first holds the anti-slip handle 213 and rotates it. At this time, the anti-slip handle 213 drives the bolt 212 to rotate through the connecting rod 211 until the bolt 212 is disengaged from the positioning thread groove 214. The user then holds the shaft body 3 and rotates it. The shaft body 3 drives the connecting seat 26 to rotate through the limit plate 28, and the second thread 27 is disengaged from the position of the first thread 22 until the connecting seat 26 is disengaged from the fixing seat 21. When the screw thread 212 is inserted into the fixing member 21, the fixing member 21 can be disassembled. When the screw thread 212 is inserted into the fixing member 21, the fixing member 21 can be disassembled. When the screw thread 212 is inserted into the fixing member 21, the fixing member 21 can be disassembled. When the screw thread 212 is inserted into the fixing member 21, the fixing member 21 can be disassembled. When the screw thread 212 is inserted into the fixing member 21, the fixing member 21 can be disassembled.
[0027] Example 2
[0028] like Figures 3 to 6 In the second embodiment, other structures remain unchanged. The difference from the first embodiment is that when the connecting seat 26 is connected to the fixing seat 21, the tight plate 29 installed on one side of the limiting plate 28 is located in the tight groove 25 opened by the sealing ring 24. This structure can strengthen the tight connection between the connecting seat 26 and the fixing seat 21.
[0029] Although the 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 variations may be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. The rotating shaft of the turbocharger, including: The turbine (1) and the rotating shaft component body (3) are characterized in that a connecting assembly (2) capable of being detached from each other is provided between the turbine (1) and the rotating shaft component body (3); The connecting assembly (2) comprises a fixing seat (21) mounted on one side of the turbine (1), the inner wall of the fixing seat (21) is provided with a first thread (22), and one end of the fixing seat (21) is provided with a groove (23); A mounting cylinder (210) is fixedly mounted on one side of the fixing seat (21), and a connecting rod (211) is movably connected inside the mounting cylinder (210); One end of the connecting rod (211) is fixedly mounted with a bolt (212), and the other end of the connecting rod (211) passes through and extends to the top of the mounting tube (210) and is fixedly mounted with an anti-slip handle (213).
2. The rotating shaft component of the turbocharger according to claim 1, characterized in that: A sealing ring (24) is placed inside the groove (23), a tight groove (25) is provided on one side of the sealing ring (24), a connecting seat (26) is movably connected inside the fixing seat (21), and a positioning thread groove (214) is provided on the outside of the connecting seat (26).
3. The rotating shaft component of the turbocharger according to claim 2, characterized in that: The outer wall of the connecting seat (26) is provided with a second thread (27), and a limiting plate (28) is installed at one end of the connecting seat (26), and the diameter of the limiting plate (28) is larger than the diameter of the connecting seat (26).
4. The rotating shaft component of the turbocharger according to claim 3, characterized in that: A tight plate (29) is installed on one side of the limiting plate (28), and the tight plate (29) is located in the tight groove (25).