Wear-resistant turbocharger

Abstract

The utility model discloses an anti-abrasion turbocharger, and particularly relates to the technical field of turbochargers, the anti-abrasion turbocharger comprises a supporting barrel, a limiting connecting assembly is arranged on the supporting barrel, the limiting connecting assembly comprises a first flow guide chamber arranged at one end of the supporting barrel, and a second flow guide chamber is arranged at the other end of the supporting barrel. The limiting connecting assembly is arranged, and the positioning clamping sleeve is arranged on the outer side of the reinforcing transverse shaft in a sleeving mode, so that the reinforcing transverse shaft drives the positioning clamping sleeve to rotate when rotating, the positioning clamping sleeve rubs with the center lubricating sleeve when rotating, and the positioning clamping sleeve is clamped in the middle of the center lubricating sleeve through the conical section of the end of the positioning clamping sleeve; the positioning jacket is prevented from shaking when being shaken, abrasion is reduced, and stability of the positioning jacket is ensured.

Description

Technical Field

[0001] The utility model relates to the technical field of turbochargers, and more specifically, to a wear-resistant turbocharger. Background Art

[0002] The engine is the power source of the car. The engine outputs power by burning fuel in the cylinder. Since the amount of fuel input is limited by the amount of air inhaled into the cylinder, the power output of the engine is limited under the premise of a certain cylinder capacity. Turbocharging can compress more air into the cylinder to increase fuel, thereby improving the engine's ability to burn and work without changing the cylinder capacity. The turbocharger is mainly composed of a turbine chamber and a boost chamber. The turbine chamber is equipped with a turbine, and the boost chamber is equipped with an impeller. The turbine and the impeller are connected by a rotating shaft. The air inlet of the turbine chamber is used to receive the exhaust gas generated by the engine, thereby driving the turbine to rotate, and through the rotating shaft, driving the impeller in the boost chamber to rotate, and compressing more air into the cylinder for combustion.

[0003] Among them, the patent with patent application number CN202120254672.0 discloses a wear-resistant turbocharger, which includes an intermediate chamber, a shaft sleeve is fixed in the intermediate chamber, a coaxial rotating shaft is passed through the shaft sleeve, a liquid storage tank and a guide groove for storing lubricating oil are provided in the intermediate chamber, the guide groove is communicated with the liquid storage tank, and the end of the guide groove away from the liquid storage tank leads to the connection between the shaft sleeve and the rotating shaft, and the guide groove is used to introduce the lubricating oil into the connection between the shaft sleeve and the rotating shaft; a slide groove is opened in the intermediate chamber, the slide groove passes through the guide groove, and the slide groove is slidably connected to a connecting rod, the connecting rod can slide along the length direction of the slide groove, and the connecting rod is connected to the rotating shaft through a bevel gear, and the bevel gear is used to convert the rotational motion of the rotating shaft into the reciprocating motion of the connecting rod;

[0004] When the structure is in use, if the amount of lubricating oil in the liquid storage tank is small, the lubricating oil can flow along the inclined surface to the guide groove, thereby improving the utilization rate of the lubricating oil and thus improving its anti-wear performance. However, the structure is not easy to limit the various structures when in use, and the device will vibrate during long-term operation, causing the structure to loosen, resulting in reduced anti-wear performance. Utility Model Content

[0005] In order to overcome the above-mentioned defects of the prior art, the utility model provides a wear-resistant turbocharger, aiming to solve the problems raised in the above-mentioned background technology.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: A wear-resistant turbocharger comprises a support cylinder, on which a limit position connection assembly is arranged;

[0007] The position-limiting connection assembly comprises a first flow-guiding chamber arranged at one end of the support cylinder, a second flow-guiding chamber is arranged at the other end of the support cylinder, and the support cylinder, the first flow-guiding chamber and the second flow-guiding chamber are connected;

[0008] A central lubricating sleeve is provided in the middle of the supporting cylinder, and a reinforcing transverse shaft is rotatably connected to the middle of the central lubricating sleeve;

[0009] A restraining collar is sleeved on the outer side of the support cylinder, a first locking ring is arranged at one end of the second flow guide chamber facing the support cylinder, a second locking ring is arranged at one end of the support cylinder facing the second flow guide chamber, the first locking ring is located on one side of the second locking ring, the first locking ring and the second locking ring are both located in the middle of the restraining collar, a spacer ring is arranged in the middle of the restraining collar, and the spacer ring is arranged between the second locking ring and the first locking ring;

[0010] It can be seen that in the above technical solution, the positioning sleeve rubs against the central lubricating sleeve when rotating, and the conical section at the end of the positioning sleeve allows the positioning sleeve to be clamped in the middle of the central lubricating sleeve, while preventing the positioning sleeve from shaking when it is shaken, reducing wear and ensuring its stability. The first locking ring and the second locking ring are limited by the constraint ring, and the spacer ring can separate the first locking ring and the second locking ring, preventing the second turbine from rotating and shaking the second guide chamber due to resistance and transmitting it to the first guide chamber, ensuring the stability of each structure during operation and improving the wear resistance of the structure.

[0011] Optionally, in a possible implementation, a first turbine is provided at one end of the reinforced transverse shaft, and a second turbine is provided at the other end of the reinforced transverse shaft, the first turbine is provided in the middle of the first flow guide chamber, the second turbine is provided in the middle of the second flow guide chamber, a positioning sleeve is provided in the middle of the central lubricating sleeve, the positioning sleeve is sleeved on the outside of the reinforced transverse shaft, the vertical cross-sections of both ends of the positioning sleeve are set to be conical, and the positioning sleeve is rotatably connected to the central lubricating sleeve, the first turbine and the second turbine are both detachably connected to the reinforced transverse shaft by bolts, and the outer sides of the first turbine and the second turbine extend to the inner walls of the first flow guide chamber and the second flow guide chamber respectively and are rotatably connected to the first flow guide chamber and the second flow guide chamber;

[0012] Technical effects and advantages of the utility model:

[0013] By setting the limit connection assembly, compared with the prior art, the overall design is simple and the structure is reasonable. Through the corresponding coordinated use of various structures, the positioning sleeve is set on the outside of the reinforced horizontal shaft, so that when the reinforced horizontal shaft rotates, the positioning sleeve is driven to rotate. When the positioning sleeve rotates, it rubs against the central lubricating sleeve. Through the conical section at the end of the positioning sleeve, the positioning sleeve can be clamped in the middle of the central lubricating sleeve, while avoiding the shaking of the positioning sleeve when it is shaken, reducing wear and ensuring its stability.

[0014] The first locking ring and the second locking ring are limited by the constraint ring, and the spacer ring can separate the first locking ring and the second locking ring, which not only ensures the stability of the installation of the second guide chamber, but also prevents the second turbine from rotating and causing resistance and shaking in the second guide chamber, which is transmitted to the first guide chamber, thereby ensuring the stability of each structure during operation and improving the wear resistance of the structure. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] In order to more clearly illustrate the technical solution of the present invention, the following is a brief introduction to the drawings required for use in some embodiments of the present invention. Obviously, the drawings described below are only drawings of some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained based on these drawings. In addition, the drawings described below can be regarded as schematic diagrams, and are not intended to limit the actual size of the product involved in the embodiments of the present invention, the actual process of the method, the actual timing of the signal, etc.

[0016] Figure 1 It is the front view of the overall structure of the utility model.

[0017] Figure 2 It is a sectional view of the overall structure of the utility model.

[0018] Figure 3 For this utility model Figure 2 Side view of.

[0019] Figure 4 It is a cross-sectional view of the support cylinder, the central lubrication sleeve, the positioning jacket and the second guide chamber of the utility model.

[0020] Figure 5 For this utility model Figure 4 Exploded diagram.

[0021] The accompanying drawings are marked as follows: 1. Support cylinder; 2. First guide chamber; 3. Second guide chamber; 4. Central lubrication sleeve; 5. Reinforced horizontal axis; 6. First turbine; 7. Second turbine; 8. Positioning sleeve; 9. Constraint ring; 10. First locking ring; 11. Second locking ring; 12. Spacer ring. DETAILED DESCRIPTION

[0022] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0023] As attached Figure 1-5 The wear-resistant turbocharger shown in the figure, through the limit connection assembly arranged on the support cylinder 1, through the friction between the positioning sleeve 8 and the central lubricating sleeve 4 when the positioning sleeve 8 rotates, through the conical section at the end of the positioning sleeve 8, so that the positioning sleeve 8 can be clamped in the middle of the central lubricating sleeve 4, while avoiding the shaking of the positioning sleeve 8 when it is shaken, reducing wear and ensuring its stability, limiting the first locking ring 10 and the second locking ring 11 through the constraint ring 9, and the spacer ring 12 can separate the first locking ring 10 and the second locking ring 11, avoiding the second turbine 7 rotating and the second guide chamber 3 being subjected to resistance and shaking and transmitting to the first guide chamber 2, ensuring the stability of each structure during operation, improving the wear resistance of the structure, and the specific structural arrangement of the assembly is as follows;

[0024] The limit connection assembly includes a first flow guiding chamber 2 arranged at one end of the support cylinder 1, and a second flow guiding chamber 3 is arranged at the other end of the support cylinder 1, and the support cylinder 1, the first flow guiding chamber 2 and the second flow guiding chamber 3 are connected;

[0025] A central lubricating sleeve 4 is provided in the middle of the supporting cylinder 1, and a reinforcing transverse shaft 5 is rotatably connected to the middle of the central lubricating sleeve 4;

[0026] A restraining collar 9 is sleeved on the outer side of the support cylinder 1, a first locking ring 10 is provided at one end of the second flow guide chamber 3 facing the support cylinder 1, a second locking ring 11 is provided at one end of the support cylinder 1 facing the second flow guide chamber 3, the first locking ring 10 is located on one side of the second locking ring 11, the first locking ring 10 and the second locking ring 11 are both located in the middle of the restraining collar 9, a spacer ring 12 is provided in the middle of the restraining collar 9, and the spacer ring 12 is provided between the second locking ring 11 and the first locking ring 10;

[0027] A first turbine 6 is provided at one end of the reinforced transverse axis 5, and a second turbine 7 is provided at the other end of the reinforced transverse axis 5. The first turbine 6 is provided in the middle of the first guide chamber 2, and the second turbine 7 is provided in the middle of the second guide chamber 3. A positioning sleeve 8 is provided in the middle of the central lubricating sleeve 4, and the positioning sleeve 8 is sleeved on the outside of the reinforced transverse axis 5. The vertical cross-sectional shapes of both ends of the positioning sleeve 8 are set to be conical, and the positioning sleeve 8 is rotatably connected to the central lubricating sleeve 4. The first turbine 6 and the second turbine 7 are both detachably connected to the reinforced transverse axis 5 by bolts, and the outer sides of the first turbine 6 and the second turbine 7 extend to the inner walls of the first guide chamber 2 and the second guide chamber 3 respectively and are rotatably connected to the first guide chamber 2 and the second guide chamber 3.

[0028] According to the above structure, when in use, the positioning sleeve 8 is limited by the central lubricating sleeve 4, and the positioning sleeve 8 is sleeved on the outer side of the reinforced horizontal axis 5, so that when the reinforced horizontal axis 5 rotates, the positioning sleeve 8 is driven to rotate, and the positioning sleeve 8 rubs against the central lubricating sleeve 4 when rotating. The conical section at the end of the positioning sleeve 8 allows the positioning sleeve 8 to be clamped in the middle of the central lubricating sleeve 4, while avoiding shaking of the positioning sleeve 8 when it is shaken, reducing wear and ensuring its stability.

[0029] At the same time, the first locking ring 10 and the second locking ring 11 are limited by the constraint ring 9, and the spacer ring 12 can separate the first locking ring 10 and the second locking ring 11, which ensures the stability of the installation of the second guide chamber 3 and prevents the second turbine 7 from rotating the second guide chamber 3 and causing the second guide chamber 3 to encounter resistance and generate shaking, which is then transmitted to the first guide chamber 2, thereby ensuring the stability of each structure during operation and improving the wear resistance of the structure.

[0030] Different from the prior art, the present application discloses a wear-resistant turbocharger. When the positioning sleeve 8 rotates, it rubs against the central lubricating sleeve 4. The conical section at the end of the positioning sleeve 8 allows the positioning sleeve 8 to be clamped in the middle of the central lubricating sleeve 4, while preventing the positioning sleeve 8 from shaking when it is shaken, thereby reducing wear and ensuring its stability. The first locking ring 10 and the second locking ring 11 are limited by the constraint ring 9, and the spacer ring 12 can separate the first locking ring 10 and the second locking ring 11, thereby preventing the second turbine 7 from rotating and shaking in the second guide chamber 3 due to resistance and transmitting it to the first guide chamber 2, thereby ensuring the stability of each structure during operation and improving the wear resistance of the structure.

[0031] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A wear-resistant turbocharger, comprising a support cylinder (1), characterized in that: The support cylinder (1) is provided with a limited position connection assembly; The limit connection assembly comprises a first flow guiding chamber (2) arranged at one end of the support cylinder (1), and a second flow guiding chamber (3) is arranged at the other end of the support cylinder (1); the support cylinder (1), the first flow guiding chamber (2) and the second flow guiding chamber (3) are connected; A central lubricating sleeve (4) is provided in the middle of the support cylinder (1), and a reinforcing transverse shaft (5) is rotatably connected to the middle of the central lubricating sleeve (4); A restraining collar (9) is sleeved on the outer side of the support cylinder (1).

2. The wear-resistant turbocharger according to claim 1, characterized in that: A first locking ring (10) is provided at one end of the second flow guide chamber (3) facing the support cylinder (1), and a second locking ring (11) is provided at one end of the support cylinder (1) facing the second flow guide chamber (3).

3. The wear-resistant turbocharger according to claim 2, characterized in that: The first locking ring (10) is located on one side of the second locking ring (11), and the first locking ring (10) and the second locking ring (11) are both located in the middle of the restraining collar (9).

4. The wear-resistant turbocharger according to claim 3, characterized in that: A spacer ring (12) is provided in the middle of the restraining collar (9), and the spacer ring (12) is provided between the second locking ring (11) and the first locking ring (10).

5. The wear-resistant turbocharger according to claim 1, characterized in that: A first turbine (6) is disposed at one end of the reinforcing transverse shaft (5), and a second turbine (7) is disposed at the other end of the reinforcing transverse shaft (5); the first turbine (6) is disposed in the middle of the first flow guide chamber (2), and the second turbine (7) is disposed in the middle of the second flow guide chamber (3).

6. The wear-resistant turbocharger according to claim 1, characterized in that: A positioning sleeve (8) is provided in the middle of the central lubricating sleeve (4), the positioning sleeve (8) is sleeved on the outside of the reinforcing transverse axis (5), the vertical cross-sections of both ends of the positioning sleeve (8) are configured to be conical, and the positioning sleeve (8) is rotatably connected to the central lubricating sleeve (4).

7. The wear-resistant turbocharger according to claim 5, characterized in that: The first turbine (6) and the second turbine (7) are both detachably connected to the reinforced transverse shaft (5) via bolts; the outer sides of the first turbine (6) and the second turbine (7) extend to the inner walls of the first flow guide chamber (2) and the second flow guide chamber (3) respectively and are rotatably connected to the first flow guide chamber (2) and the second flow guide chamber (3).

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