Wear-resistant turbocharger

Abstract

The utility model relates to the technical field of turbochargers, in particular to an anti-abrasion turbocharger which comprises a main body, an internal impeller assembly is arranged in the main body, and a turbine assembly is arranged on the side face of the internal impeller assembly. By means of the oil inlet pipe and the oil return pipe, the operation speed of the turbocharger is very high, too much dust contained in unclean air and premature abrasion of the turbocharger are avoided, in addition, a large number of impurities contained in the air can be prevented from entering an impeller of the turbine rotating at a high speed, dust particles are prevented from impacting the impeller of the turbine, and the service life of the turbine is prolonged. A thrust ring specification is used for aiming at the use standard and requirement of a connecting piece, and the thrust ring is mainly used for fixing and connecting steel pipe components, bearing loads in the horizontal and vertical directions, ensuring the overall stability of the structure and improving the service life of the turbine impeller. The connecting structure is generally applied to frame structures, supporting systems and other occasions needing reliable connection.

Description

Technical Field

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

[0002] A turbocharger is a device that can increase the pressure of a gas or liquid medium, also known as a turbocharger or turbine unit. The working principle of a turbocharger is to use high-speed rotating turbine blades to accelerate low-speed, low-pressure gas or liquid medium and increase its pressure. The use of a turbocharger can increase the power density of the engine, improve the efficiency of the engine, and reduce exhaust emissions.

[0003] The Chinese authorized announcement number is CN219754657U, which is a wear-resistant turbocharger. The device uses materials optimization, surface treatment, coating and other technologies to make the turbine and impeller have higher hardness and wear resistance. The wear-resistant turbocharger can better maintain the gap between the impeller and the turbine, improve the supercharging efficiency, and the device has a longer service life, providing stable supercharging performance for the device for a longer time, reducing the frequency of replacement and reducing the cost of use. However, this patent still has certain shortcomings when used. If the oil is not changed for a long time or the air filter fails, too much dust will enter the supercharger, the floating bearing will be seriously worn, resulting in excessive bearing clearance and unstable oil film. When driving at high speed, the supercharger will soon become unbalanced, the vibration of the rotor shaft system will intensify, and the seals at both ends will be damaged, causing lubricating oil leakage. Therefore, we propose an anti-wear turbocharger to improve the above problems. Utility Model Content

[0004] In order to solve the problem that if the oil is not changed for a long time or the air filter fails, too much dust will enter the supercharger, the floating bearing will be seriously worn, resulting in excessive bearing clearance and unstable oil film. When driving at high speed, the supercharger will quickly become unbalanced, the rotor shaft system will vibrate more, the seals at both ends will be damaged, and lubricating oil will leak, the purpose of the utility model is to provide a wear-resistant turbocharger to solve the problems raised in the above background technology.

[0005] In order to achieve the above purpose, the utility model provides the following technical solutions:

[0006] An anti-wear turbocharger comprises a main body, an internal impeller assembly is arranged inside the main body, and a turbine assembly is arranged on the side of the internal impeller assembly;

[0007] The internal impeller assembly comprises a mounting plate, a compressor impeller is arranged inside the mounting plate, a first fixed pipe is arranged inside the compressor impeller, a bearing rod is fixedly connected to the side of the mounting plate, an oil inlet pipe is fixedly connected to the top of the bearing rod, an oil return pipe is fixedly connected to the bottom of the bearing rod, a thrust ring is fixedly connected to the side of the bearing rod, a turbine impeller is arranged on the side of the thrust ring, and a second fixed pipe is arranged inside the turbine impeller;

[0008] The turbine assembly comprises a turbine housing, the bottom of the turbine housing is fixedly connected with an exhaust gas outlet pipe, the side of the turbine housing is fixedly connected with an outlet pipe, and the side of the outlet pipe is fixedly connected with a fixing sleeve.

[0009] As a preferred solution of the utility model, an intermediate body is provided on the side of the installation plate, and two intermediate bodies are provided.

[0010] As a preferred solution of the utility model, a sealing ring is arranged on the top of the thrust ring, and two sealing rings are arranged.

[0011] As a preferred solution of the utility model, a mounting hole is provided inside the exhaust gas outlet pipe, and four mounting holes are provided.

[0012] As a preferred solution of the utility model, the main body includes a compressor casing, an air inlet pipe is fixedly connected to the side of the compressor casing, and a reinforcing steel ring is fixedly connected to the side of the compressor casing.

[0013] As a preferred solution of the utility model, an exhaust pipe is fixedly connected to the interior of the reinforced steel ring, and an inner ring is fixedly connected to the interior of the exhaust pipe.

[0014] As a preferred solution of the utility model, a fixing plate is fixedly connected to the side of the compressor casing, and a fitting is fixedly connected to the side of the fixing plate.

[0015] As a preferred solution of the utility model, a soft ring is fixedly connected inside the fitting, and a wear-resistant ring is fixedly connected inside the soft ring.

[0016] Compared with the prior art, the beneficial effects of the utility model are:

[0017] 1. In the utility model, the turbocharger is operated at a very high speed by utilizing the oil inlet pipe and the oil return pipe, thereby preventing the premature wear of the turbocharger caused by excessive dust in unclean air. In addition, it can also prevent a large amount of impurities in the air from entering the high-speed running turbine impeller, causing dust particles to hit the turbine impeller, thereby causing the turbine impeller to operate unsteadily and the bearing rod and the sealing ring to wear.

[0018] 2. In the utility model, the thrust ring specification is used for the use standards and requirements of this connector. The thrust ring is mainly used to fix and connect steel pipe components, bear horizontal and vertical loads, and ensure the overall stability of the structure. It is usually used in frame structures, support systems and other occasions that require reliable connection. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0020] Figure 2 This is a schematic diagram of the compressor casing structure of the utility model;

[0021] Figure 3 This is a schematic diagram of the structure of the internal impeller assembly of the utility model;

[0022] Figure 4 This is a schematic diagram of the structure of the turbine assembly of the utility model.

[0023] In the figure: 1. main body; 101. compressor casing; 102. air inlet pipe; 103. reinforcement steel ring; 104. exhaust pipe; 105. inner ring; 106. fixed plate; 107. fitting; 108. soft ring; 109. wear-resistant ring; 2. internal impeller assembly; 201. mounting plate; 202. compressor impeller; 203. first fixed pipe; 204. intermediate body; 205. bearing rod; 206. oil inlet pipe; 207. oil return pipe; 208. sealing ring; 209. thrust ring; 210. turbine impeller; 211. second fixed pipe; 3. turbine assembly; 301. turbine casing; 302. exhaust outlet pipe; 303. mounting hole; 304. outlet pipe; 305. fixing sleeve. DETAILED DESCRIPTION

[0024] The technical solutions in the embodiments of the utility model will be clearly and completely described below in conjunction with the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all of the embodiments. Based on the embodiments of the utility model, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the utility model.

[0025] For examples, see Figure 1-Figure 4 , the utility model provides a technical solution:

[0026] A wear-resistant turbocharger comprises a main body 1, an internal impeller assembly 2 is arranged inside the main body 1, and a turbine assembly 3 is arranged on the side of the internal impeller assembly 2.

[0027] In this embodiment, Figure 2 , Figure 3 and Figure 4 As shown, the internal impeller assembly 2 includes a mounting plate 201, a compressor impeller 202 is arranged inside the mounting plate 201, a first fixed pipe 203 is arranged inside the compressor impeller 202, a bearing rod 205 is fixedly connected to the side of the mounting plate 201, an oil inlet pipe 206 is fixedly connected to the top of the bearing rod 205, an oil return pipe 207 is fixedly connected to the bottom of the bearing rod 205, a thrust ring 209 is fixedly connected to the side of the bearing rod 205, a turbine impeller 210 is arranged on the side of the thrust ring 209, and a second fixed pipe 211 is arranged inside the turbine impeller 210. The turbine assembly 3 includes a turbine casing 301 An exhaust gas outlet pipe 302 is fixedly connected to the bottom of the turbine housing 301, an outlet pipe 304 is fixedly connected to the side of the turbine housing 301, and a fixed sleeve 305 is fixedly connected to the side of the outlet pipe 304. The oil inlet pipe 206 and the oil return pipe 207 are used to make the turbocharger run very fast, avoiding excessive dust in the unclean air and premature wear of the turbocharger. In addition, it can also prevent a large amount of impurities in the air from entering the high-speed running turbine impeller 210, causing dust particles to hit the turbine impeller 210, thereby causing the turbine impeller 210 to run unsteadily and the bearing rod 205 and the sealing ring 208 to wear.

[0028] Among them, an intermediate body 204 is arranged on the side of the mounting plate 201, and two intermediate bodies 204 are arranged. A sealing ring 208 is arranged on the top of the thrust ring 209, and two sealing rings 208 are arranged. A mounting hole 303 is opened inside the exhaust gas outlet pipe 302, and four mounting holes 303 are opened. The specification of using the thrust ring 209 is for the use standards and requirements of this connector. The function of the thrust ring 209 is mainly used to fix and connect steel pipe components, bear horizontal and vertical loads, and ensure the overall stability of the structure. It is usually used in frame structures, support systems and other occasions that require reliable connection.

[0029] In this embodiment, Figure 1 As shown, the main body 1 includes a compressor casing 101, an air inlet pipe 102 is fixedly connected to the side of the compressor casing 101, a reinforcing steel ring 103 is fixedly connected to the side of the compressor casing 101, an exhaust pipe 104 is fixedly connected inside the reinforcing steel ring 103, an inner ring 105 is fixedly connected inside the exhaust pipe 104, a fixing plate 106 is fixedly connected to the side of the compressor casing 101, a fitting 107 is fixedly connected to the side of the fixing plate 106, a soft ring 108 is fixedly connected inside the fitting 107, a wear-resistant ring 109 is fixedly connected inside the soft ring 108, and both the soft ring 108 and the wear-resistant ring 109 can increase the wear resistance of the turbocharger.

[0030] Working process of the utility model: When the wear-resistant turbocharger designed by the present invention is working, the turbocharger utilizes the inertial impulse of the exhaust gas discharged by the engine to push the turbine impeller 210 of the turbine housing 301, and the turbine impeller 210 drives the coaxial compressor impeller 202, and the compressor impeller 202 presses the air sent by the air filter pipe to make it pressurized and enter the cylinder. When the engine speed increases, the exhaust gas discharge speed and the speed of the turbine impeller 210 also increase synchronously, and the compressor impeller 202 compresses more air to enter the cylinder. The increased pressure and density of the air can burn more fuel, and the output power of the engine can be increased by correspondingly increasing the amount of fuel and adjusting the engine speed.

[0031] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A wear-resistant turbocharger, comprising a main body (1), characterized in that: An internal impeller assembly (2) is arranged inside the main body (1), and a turbine assembly (3) is arranged on the side of the internal impeller assembly (2); The internal impeller assembly (2) comprises a mounting plate (201), a compressor impeller (202) is arranged inside the mounting plate (201), a first fixed tube (203) is arranged inside the compressor impeller (202), a bearing rod (205) is fixedly connected to the side of the mounting plate (201), an oil inlet pipe (206) is fixedly connected to the top of the bearing rod (205), an oil return pipe (207) is fixedly connected to the bottom of the bearing rod (205), a thrust ring (209) is fixedly connected to the side of the bearing rod (205), a turbine impeller (210) is arranged on the side of the thrust ring (209), and a second fixed tube (211) is arranged inside the turbine impeller (210); The turbine assembly (3) comprises a turbine housing (301), the bottom of the turbine housing (301) is fixedly connected to an exhaust gas outlet pipe (302), the side of the turbine housing (301) is fixedly connected to an outlet pipe (304), and the side of the outlet pipe (304) is fixedly connected to a fixing sleeve (305).

2. The wear-resistant turbocharger according to claim 1, characterized in that: An intermediate body (204) is provided on the side of the installation plate (201), and two intermediate bodies (204) are provided.

3. The wear-resistant turbocharger according to claim 1, characterized in that: A sealing ring (208) is arranged on the top of the thrust ring (209), and two sealing rings (208) are arranged.

4. The wear-resistant turbocharger according to claim 1, characterized in that: The exhaust gas outlet pipe (302) is provided with a mounting hole (303) inside, and four mounting holes (303) are provided.

5. The wear-resistant turbocharger according to claim 1, characterized in that: The main body (1) comprises a compressor casing (101), an air inlet pipe (102) is fixedly connected to the side of the compressor casing (101), and a reinforcing steel ring (103) is fixedly connected to the side of the compressor casing (101).

6. The wear-resistant turbocharger according to claim 5, characterized in that: An exhaust pipe (104) is fixedly connected to the interior of the reinforcement steel ring (103), and an inner ring (105) is fixedly connected to the interior of the exhaust pipe (104).

7. The wear-resistant turbocharger according to claim 5, characterized in that: A fixing plate (106) is fixedly connected to the side of the compressor casing (101), and a fitting (107) is fixedly connected to the side of the fixing plate (106).

8. The wear-resistant turbocharger according to claim 7, characterized in that: The fitting part (107) is fixedly connected to a soft ring (108) inside, and the soft ring (108) is fixedly connected to a wear-resistant ring (109) inside.

Images