Turbocharger core
By introducing a multi-stage filtration and buffer gas pipeline design into the turbocharger core, the corrosion problem of the turbine impeller and turbine shaft is solved, and the corrosive gases are effectively filtered out, improving the stability and durability of the core.
Patent Information
- Application Number
- CN202422588943.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-24
- Publication Date
- 2025-11-04
- Estimated Expiration
- 2034-10-24
AI Technical Summary
Existing turbocharger mechanisms are inadequate in reducing corrosion of the turbine impeller and turbine shaft, and current technologies have not been able to effectively address this issue.
The system employs a gas delivery pipeline and filtration pipeline design, including a gas delivery pipe, gas delivery ring, pressure tank, gas distribution assembly, filtration assembly, and auxiliary filtration assembly. Through multi-stage filtration and buffering, it treats exhaust gas, removes corrosive gases, and reduces corrosion of the turbine impeller and turbine shaft.
It effectively filters out corrosive gases from exhaust gas, reduces the corrosion of turbine impellers and turbine shafts, and improves the stability and durability of the mechanism.
Smart Images

Figure CN223511012U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model belongs to turbocharger field, concretely relates to a turbocharger movement. BACKGROUND
[0002] The utility model discloses a utility model patent with the subject name turbocharger movement assembly, and the IPC classification number is F02B37 / 00, and its technical scheme discloses "a turbocharger movement assembly, including turbine shaft 1, impeller body 2, turbine body 3 and intermediate body 4, the intermediate body 4 is set up on the axle rod mounting hole 5, the axle rod mounting hole 5 both ends open on the intermediate body 4, the turbine shaft 1 is through the introduction axle rod mounting hole 5 in and is penetrated on the intermediate body 4, the turbine shaft 1 both ends are exported on the intermediate body 4, the turbine shaft 1 one end export end fixed mounting has the impeller body 2, the turbine shaft 1 other end export end fixed mounting has the turbine body 3".
[0003] From this, the above utility model patent has disclosed one of the technical schemes of turbocharger movement. However, the technical scheme disclosed in the above utility model patent focuses on improving the operation stability, and does not further solve the problem of reducing the corrosion degree of the turbine impeller and the turbine shaft, and needs to be further improved. UTILITY MODEL CONTENTS
[0004] The utility model provides a turbocharger movement to overcome the above defects in the prior art.
[0005] The utility model adopts the following technical scheme, a turbocharger movement, including gas pipeline and a plurality of filter pipelines, wherein:
[0006] The gas pipeline includes a gas pipe, a gas ring and a pressure tank, and the gas ring is in communication with the gas pipe.
[0007] The filter pipeline includes a gas distribution assembly, a first gas guide pipe and a second gas guide pipe. The gas distribution assembly includes a first ring pipe and a second ring pipe in communication with the first ring pipe. The second ring pipe is connected to the first gas guide pipe, and the first ring pipe is connected to the second gas guide pipe.
[0008] The filter pipeline further includes a first filter assembly and a second filter assembly. One side of the first filter assembly is connected to the first gas guide pipe or the second gas guide pipe. The other side of the first filter assembly is connected to one side of the second filter assembly. The other side of the second filter assembly is in communication with the pressure tank.
[0009] As a preferred technical scheme of the above technical scheme, the filter pipeline further includes an air inlet assembly. The air inlet assembly includes an air inlet pipe and an air inlet pipe gas storage part. One side of the air inlet pipe gas storage part is in communication with the gas distribution assembly. The other side of the air inlet pipe gas storage part is in communication with the air inlet pipe.
[0010] As a preferred technical solution of the above technical solutions, the first filter assembly includes a first volumetric container, a first filter, and a first connector. One side of the first volumetric container is fixedly connected to a first air duct or a second air duct, the other side of the first volumetric container is fixedly connected to one side of the first filter, and the other side of the first filter is fixedly connected to one side of the first connector.
[0011] As a preferred technical solution of the above technical solutions, the second filtration assembly includes a second filter, a second volumetric container, and a second connector. One side of the second filter is fixedly connected to the other side of the first connector, the other side of the second filter is fixedly connected to one side of the second volumetric container, the other side of the second volumetric container is fixedly connected to one side of the second connector, and the other side of the second connector is fixedly connected to a pressure tank.
[0012] As a preferred technical solution to the above technical solutions, the filter pipeline further includes a third filter component, which includes a first auxiliary filter, a connecting pipe, and a second auxiliary filter. One end of the connecting pipe is connected to the first auxiliary filter, and the other end of the connecting pipe is connected to the second auxiliary filter. The first auxiliary filter is connected to the second loop pipe.
[0013] The turbocharger core disclosed in this utility model has the following advantages: the exhaust gas is diverted by the gas distribution component, first passes through the primary filtration of the first filter component, and then passes through the secondary filtration of the second filter component. After filtering out some gases such as corrosive gases that may be present, the filtered gas is temporarily stored in a pressure tank for later output to the turbine impeller and turbine shaft of the turbocharger core, thereby reducing the degree of corrosion of the turbine impeller and turbine shaft. Attached Figure Description
[0014] Figure 1 This is a perspective view of this application.
[0015] Figure 2 This is a three-dimensional view from another perspective of this application.
[0016] Figure 3 This is a front view of the filter piping in this application.
[0017] Figure 4 This is a side view of the filter piping of this application.
[0018] Figure 5 This is a perspective view of the filter pipeline of this application.
[0019] Figure 6 This is a perspective view of the filter pipeline of this application.
[0020] The reference numerals in the attached drawings include: 100-Gas delivery pipeline; 110-Gas delivery pipe; 120-Gas delivery ring; 130-Pressure tank; 200-Filter pipeline; 210-Inlet assembly; 211-Inlet pipe; 212-Inlet pipe storage section; 220-Gas distribution assembly; 221-First ring pipe; 222-Second ring pipe; 230-First guide pipe; 240-Second guide pipe; 250-First filter assembly; 251-First volumetric container; 252-First filter; 253-First connector; 260-Second filter assembly; 261-Second filter; 262-Second volumetric container; 263-Second connector; 270-Third filter assembly; 271-First auxiliary filter; 272-Connecting pipe; 273-Second auxiliary filter. Detailed Implementation
[0021] This utility model discloses a turbocharger mechanism. The following description, in conjunction with a preferred embodiment (Embodiment 1), refers to the accompanying drawings. Figures 1 to 6 The specific embodiments of this utility model will be further described below.
[0022] See attached diagram. Figures 1 to 6 , Figure 1 and Figure 2 The turbocharger mechanism is shown from different perspectives. Figures 3 to 6 The filter pipes are shown from different perspectives.
[0023] Example 1.
[0024] Preferably, the turbocharger core includes an air delivery line 100 and a plurality of filter lines 200, wherein:
[0025] The gas pipeline 100 includes a gas pipeline 110, a gas ring 120 and a pressure tank 130. The gas ring 120 is connected to the gas pipeline 110 and the pressure tank 130 is connected to the gas ring 120.
[0026] The filter pipeline 200 includes a gas distribution assembly 220, a first air guide pipe 240, and a second air guide pipe 250. The gas distribution assembly 200 includes a first ring pipe 221 and a second ring pipe 222 connected to the first ring pipe 221. The second ring pipe 222 is externally connected to the first air guide pipe 230, and the first ring pipe 221 is externally connected to the second air guide pipe 240.
[0027] The filter pipeline 200 also includes (two) first filter components 250 and second filter components 260. One side of the first filter component 250 is connected to the first air guide pipe 230 or the second air guide pipe 240, and the other side of the first filter component 250 is connected to one side of the second filter component 260. The other side of the second filter component 260 is connected to the pressure tank 130. This allows the exhaust gas to be diverted by the gas distribution component 220, first passing through the primary filtration of the first filter component 250, and then through the secondary filtration of the second filter component 260. After filtering out some gases, such as corrosive gases, the filtered gas is temporarily stored in the pressure tank 130 for later output to the turbine impeller and turbine shaft of the turbocharger core, thereby reducing the corrosion of the turbine impeller and turbine shaft.
[0028] The filter pipe 200 also includes an air intake assembly 210, which includes an air intake pipe 211 and an air intake pipe storage section 212. One side of the air intake pipe storage section 212 is connected to the air distribution assembly 220, and the other side of the air intake pipe storage section 212 is connected to the air intake pipe 211. This allows the airflow to be slightly buffered in the air intake pipe storage section 212 before entering the air distribution assembly 220.
[0029] The first filter assembly 250 includes a first volumetric container 251, a first filter 252, and a first connector 253. One side of the first volumetric container 251 is fixedly connected to either the first air duct 230 or the second air duct 240, and the other side of the first volumetric container 251 is fixedly connected to one side of the first filter 252. The other side of the first filter 252 is fixedly connected to one side of the first connector 253, so that the airflow passes through the primary filter.
[0030] The second filtration assembly 260 includes a second filter 261, a second volumetric container 262, and a second connector 263. One side of the second filter 261 is fixedly connected to the other side of the first connector 253, the other side of the second filter 261 is fixedly connected to one side of the second volumetric container 262, the other side of the second volumetric container 262 is fixedly connected to one side of the second connector 263, and the other side of the second connector 263 is fixedly connected to the pressure tank 130. This allows the airflow that has undergone secondary filtration to be gradually and slowly released into the pressure tank 130.
[0031] The filter pipe 200 also includes a third filter assembly 270, which includes a first auxiliary filter 271, a connecting pipe 272, and a second auxiliary filter 273. One end of the connecting pipe 272 is connected to the first auxiliary filter 271, and the other end of the connecting pipe 272 is connected to the second auxiliary filter 273. The first auxiliary filter 271 is connected to the second ring pipe 222. This allows exhaust gas exceeding the rated capacity of the intake pipe storage section 212 to be passed into the third filter assembly 270 for auxiliary filtration, ensuring that the airflow into the first filter assembly 260 and the second filter assembly 270 remains continuous and stable.
[0032] It is worth mentioning that the specific components and other technical features of the corrosive gas involved in this utility model patent application should be regarded as prior art. The specific structure, working principle, and possible control methods and spatial arrangement of these technical features can be conventionally selected in the field and should not be regarded as the inventive point of this utility model patent. This utility model patent will not elaborate further.
[0033] For those skilled in the art, modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model.
Claims
1. A turbocharger mechanism, characterized in that, It includes a gas transmission pipeline and several filter pipelines, wherein: the gas transmission pipeline includes a gas transmission pipe, a gas transmission ring and a pressure tank, and the gas transmission ring is connected to the gas transmission pipe; The filter pipeline includes a gas distribution assembly, a first gas guide pipe, and a second gas guide pipe. The gas distribution assembly includes a first ring pipe and a second ring pipe connected to the first ring pipe. The second ring pipe is externally connected to the first gas guide pipe, and the first ring pipe is externally connected to the second gas guide pipe. The filter pipeline also includes a first filter assembly and a second filter assembly. One side of the first filter assembly is connected to either the first air guide pipe or the second air guide pipe, the other side of the first filter assembly is connected to one side of the second filter assembly, and the other side of the second filter assembly is connected to the pressure tank.
2. The turbocharger mechanism according to claim 1, characterized in that, The filter pipeline also includes an air intake assembly, which includes an air intake pipe and an air intake pipe storage section. One side of the air intake pipe storage section is connected to the air distribution assembly, and the other side of the air intake pipe storage section is connected to the air intake pipe.
3. The turbocharger mechanism according to claim 1, characterized in that, The first filtration assembly includes a first volumetric container, a first filter, and a first connector. One side of the first volumetric container is fixedly connected to a first air duct or a second air duct, the other side of the first volumetric container is fixedly connected to one side of the first filter, and the other side of the first filter is fixedly connected to one side of the first connector.
4. The turbocharger mechanism according to claim 3, characterized in that, The second filtration assembly includes a second filter, a second volumetric container, and a second connector. One side of the second filter is fixedly connected to the other side of the first connector, the other side of the second filter is fixedly connected to one side of the second volumetric container, the other side of the second volumetric container is fixedly connected to one side of the second connector, and the other side of the second connector is fixedly connected to a pressure tank.
5. The turbocharger mechanism according to claim 1, characterized in that, The filter pipeline also includes a third filter assembly, which includes a first auxiliary filter, a connecting pipe, and a second auxiliary filter. One end of the connecting pipe is connected to the first auxiliary filter, and the other end of the connecting pipe is connected to the second auxiliary filter. The first auxiliary filter is connected to the second loop pipe.
Citation Information
Patent Citations
Turbo charger core assembly
CN208153146U