CN215292669U - High heat dissipation type turbocharger intermediate - Google Patents
High heat dissipation type turbocharger intermediate Download PDFInfo
- Publication number
- CN215292669U CN215292669U CN202121941702.1U CN202121941702U CN215292669U CN 215292669 U CN215292669 U CN 215292669U CN 202121941702 U CN202121941702 U CN 202121941702U CN 215292669 U CN215292669 U CN 215292669U
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- China
- Prior art keywords
- heat dissipation
- wall
- pipe
- oil
- oil pipe
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- 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.)
- Expired - Fee Related
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- 230000017525 heat dissipation Effects 0.000 title abstract description 77
- 239000003921 oil Substances 0.000 abstract description 69
- 238000001816 cooling Methods 0.000 abstract description 28
- 239000000498 cooling water Substances 0.000 abstract description 20
- 239000000428 dust Substances 0.000 abstract description 16
- 230000000694 effects Effects 0.000 abstract description 8
- 239000010721 machine oil Substances 0.000 abstract description 7
- 230000009286 beneficial effect Effects 0.000 abstract 1
- 239000010705 motor oil Substances 0.000 description 27
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 9
- 229910052802 copper Inorganic materials 0.000 description 9
- 239000010949 copper Substances 0.000 description 9
- 229910000838 Al alloy Inorganic materials 0.000 description 5
- 239000007788 liquid Substances 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Supercharger (AREA)
Abstract
The utility model discloses a high heat dissipation type turbo charger midbody relates to turbo charger technical field, and its technical scheme is: including turbine midbody, heat dissipation chamber one is seted up to turbine midbody inner wall, heat dissipation chamber inner wall is equipped with cooling tube one, cooling tube one end fixed connection feed liquor pipe, feed liquor pipe one end fixed connection cooling water tank, the drain pipe is installed to cooling water tank one end, heat dissipation chamber two is seted up to turbine midbody top inner wall, heat dissipation chamber inner wall cup joints oil pipe one, screw thread heat conduction stick is cup jointed to oil pipe one surface, oil pipe two is installed at oil pipe one top, defeated oil pipe of two one end fixed connection of oil pipe, dust screen one is installed to two top inner walls in heat dissipation chamber, and beneficial effect is: the utility model discloses a cooling water circulation and air-cooled endless mode dispel the heat for machine oil in the turbine midbody, have the advantage that improves the radiating effect of turbine midbody.
Description
Technical Field
The utility model relates to a turbo charger technical field, concretely relates to high heat dissipation type turbo charger midbody.
Background
The turbocharger drives a turbine of the turbocharger to run at a high speed by using high-temperature exhaust gas exhausted by an engine, so as to drive a compressor impeller coaxial with the turbine to run at a high speed, compressed air generated by the compressor impeller is provided for the engine, air inlet of the engine is changed into pressure air from natural air suction, the engine can burn more fuel due to the increase of the provided air quantity, and simultaneously the combustion page is more complete and sufficient, but the turbocharger does not consume the power of the engine, so the turbocharger is also called as an exhaust gas turbocharger, the middle body part of the turbocharger commonly used in the market at present can generate a large amount of heat in the running process, the heat dissipation of the middle body part at present mainly depends on an oil cooling or water cooling mode, wherein the oil cooling not only has poor heat dissipation effect, but also has an oil leakage phenomenon, and the water cooling has good cooling effect, but requires periodic disassembly to remove scale that otherwise accumulates on the housing and can cause the intermediate to overheat and be damaged.
The prior art has the following defects: at present, most turbochargers in the market are at work, the temperature inside the turbochargers is generally high, particularly the temperature in the middle body is high in heating speed, meanwhile, all kinds of bearings inside the turbochargers need to be lubricated by engine oil, even if the engine oil is used for heat dissipation, the temperature of the engine oil is difficult to drop, the heat dissipation effect is poor, and the turbochargers are burnt out.
SUMMERY OF THE UTILITY MODEL
Therefore, the utility model provides a high heat dissipation type turbo charger midbody sets up to peg graft at a heat dissipation chamber inner wall for the screw thread form through having set up cooling tube one, the material of cooling tube one sets up to copper, two sets of heat dissipation chamber sets up respectively at turbine midbody top inner wall and bottom inner wall, two sets of oil pipe one, the quantity of every group oil pipe one sets up to four, two sets of oil pipe one all communicate with each other with heat dissipation chamber one, the material of screw thread heat conduction stick sets up to the aluminum alloy, radiator fan sets up near two dust screens, radiator fan's quantity sets up to two sets ofly, problem in the background art is solved.
In order to achieve the above object, the present invention provides the following technical solutions: the utility model provides a high heat dissipation type turbo charger midbody, includes turbine midbody body, heat dissipation chamber one is seted up to turbine midbody inner wall, heat dissipation chamber one inner wall is equipped with cooling tube one, cooling tube one end fixed connection feed liquor pipe, feed liquor pipe one end fixed connection cooling water tank, the drain pipe is installed to cooling water tank one end, heat dissipation chamber two is seted up to turbine midbody top inner wall, heat dissipation chamber inner wall cup joints oil pipe one, screw thread heat conduction stick is cup jointed to oil pipe one surface, oil pipe two is installed at oil pipe one top, defeated oil pipe of two one end fixed connection of oil pipe, dust screen one is installed to two top inner walls in heat dissipation chamber, two left end inner wall fixed connection dust screens two in heat dissipation chamber, radiator fan is installed to two inner walls in heat dissipation chamber.
Preferably, the first cooling pipe is inserted into the inner wall of the first heat dissipation cavity in a threaded manner, and the first cooling pipe is made of copper.
Preferably, the number of the second heat dissipation cavities is two, and the two heat dissipation cavities are respectively arranged on the top inner wall and the bottom inner wall of the turbine intermediate body.
Preferably, the number of the first oil pipes is two, the number of the first oil pipes in each group is four, and the first oil pipes in the two groups are respectively arranged on the inner walls of the two heat dissipation cavities in the two groups.
Preferably, the bottoms of the first oil pipes of the two groups are open, and the first oil pipes of the two groups are communicated with the first heat dissipation cavity.
Preferably, the material of the threaded heat conducting rod is aluminum alloy, the threaded heat conducting rod is uniformly wound on the outer surface of the first oil pipe, and the number of the threaded heat conducting rod is equal to that of the first oil pipe.
Preferably, the heat dissipation fans are arranged near the second dustproof net, and the number of the heat dissipation fans is two.
The utility model has the advantages that:
1. the oil pipe I is filled with the engine oil, then the engine oil circulates in the heat dissipation cavity I and the oil pipe I to dissipate heat for the bearing on the inner wall of the turbine intermediate body by starting the oil pump, the temperature of the engine oil can rise when the engine oil dissipates heat, the water pump in the cooling water tank is started at the moment, the cooling water tank sends the cooling water to the cooling pipe I which is inserted in the inner wall of the heat dissipation cavity I in a threaded manner through the liquid inlet pipe, the copper has the advantage of good heat conductivity because the material of the cooling pipe I is set to be copper, and the cooling water in the cooling pipe I cools the engine oil in the heat dissipation cavity I at the moment;
2. through starting radiator fan, the heat of the interior machine oil of oil pipe one is through the winding on oil pipe one, the heat transfer of the interior machine oil of oil pipe one is for the screw thread heat conduction stick through heat-conducting mode with oil pipe one abundant contact, the heat of machine oil is absorbed to the screw thread heat conduction stick, and give the air of heat dissipation intracavity through air transfer, and blow off the hot-air of heat dissipation intracavity through radiator fan, new cold air goes into from the other end in heat dissipation chamber, the machine oil in oil pipe one is dispelled the heat through air cycle's mode, improve the thermal diffusivity of the interior machine oil of oil pipe one, the effect of improving turbine midbody thermal diffusivity has been reached, the effect of dust screen one and dust screen two is for preventing that the dust from getting into the heat dissipation intracavity.
Drawings
Fig. 1 is a schematic structural diagram of a turbine intermediate body provided by the present invention;
FIG. 2 is a side view of a turbine intermediate body provided by the present invention;
FIG. 3 is an enlarged view of the area A in FIG. 1 according to the present invention;
fig. 4 is a cross-sectional view provided by the present invention.
In the figure: the turbine intermediate body 50, the first heat dissipation cavity 51, the first cooling pipe 52, the liquid inlet pipe 53, the liquid outlet pipe 54, the cooling water tank 55, the heat dissipation cavity 60, the first oil pipe 61, the threaded heat conduction rod 62, the second oil pipe 63, the oil pipeline 64, the first dust screen 65, the oil pump 66, the second dust screen 67 and the heat dissipation fan 68.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.
Referring to the attached drawings 1-4, the utility model provides a pair of high heat dissipation type turbo charger midbody, including turbine midbody 50, heat dissipation chamber 51 is seted up to turbine midbody 50 inner wall, heat dissipation chamber 51 inner wall is equipped with cooling tube 52, 52 one end fixed connection feed liquor pipe 53 of cooling tube, feed liquor pipe 53 one end fixed connection cooling water tank 55, drain pipe 54 is installed to cooling water tank 55 one end, heat dissipation chamber two 60 are seted up to turbine midbody 50 top inner wall, heat dissipation chamber 60 inner wall cup joints oil pipe 61, screw thread heat conduction stick 62 is cup jointed to oil pipe 61 surface, oil pipe two 63 are installed at oil pipe 61 top, defeated oil pipe 64 of two 63 one end fixed connection of oil pipe, dust screen one 65 is installed to two 60 top inner walls in heat dissipation chamber, heat dissipation chamber two 60 left end inner wall fixed connection dust screen two 67, radiator fan 68 is installed to two 60 inner walls in heat dissipation chamber.
Furthermore, the first cooling pipe 52 is arranged to be inserted into the inner wall of the first heat dissipation cavity 51 in a threaded manner, the first cooling pipe 52 is made of copper, the second heat dissipation cavity 60 is arranged in two groups which are respectively arranged on the inner wall of the top and the inner wall of the bottom of the turbine intermediate body 50, the first oil pipe 61 is arranged in two groups, the first oil pipe 61 of each group is arranged in four, the first oil pipe 61 of each group is respectively arranged on the inner walls of the second heat dissipation cavity 60 of each group, the bottom of the first oil pipe 61 of each group is open, the first oil pipe 61 of each group is communicated with the first heat dissipation cavity 51, the threaded heat conduction rod 62 is made of aluminum alloy, the threaded heat conduction rod 62 is uniformly wound on the outer surface of the first oil pipe 61, the threaded heat conduction rod 62 is equal to the first oil pipe 61, the heat dissipation fans 68 are arranged near the second dust screen 67, the heat dissipation fans 68 are arranged in two groups, when the turbine intermediate body 50 dissipates heat, the first oil pipe 61 is filled with machine oil, then, the oil pump 66 is started, so that the engine oil circulates in the first heat dissipation cavity 51 and the first oil pipe 61 to dissipate heat of the bearing on the inner wall of the turbine intermediate body 50, the temperature of the engine oil is increased when the engine oil is dissipated, the water pump in the cooling water tank 55 is started at the moment, the cooling water tank 55 pumps the cooling water into the first cooling pipe 52 which is inserted into the inner wall of the first heat dissipation cavity 51 in a threaded manner through the liquid inlet pipe 53, the first cooling pipe 52 is made of copper, the copper has the advantage of good heat conductivity, the cooling water in the first cooling pipe 52 cools the engine oil in the first heat dissipation cavity 51, the cooling fan 68 is started at the same time, the heat of the engine oil in the first oil pipe 61 is wound on the first oil pipe 61 and is fully contacted with the first oil pipe 61 to transfer the heat of the engine oil in the first oil pipe 61 to the threaded heat conducting rod 62 in a heat conduction manner, and the aluminum alloy has good heat conductivity and strong corrosion resistance, and the threaded heat conducting rod 62 absorbs the heat of the engine oil, the air is transmitted to the air in the heat dissipation cavity 60 through the air, the hot air in the heat dissipation cavity 60 is blown out through the heat dissipation fan 68, new cold air enters from the other end of the heat dissipation cavity 60, the engine oil in the oil pipe I61 is dissipated through air circulation, the heat dissipation performance of the engine oil in the oil pipe I61 is improved, the effect of improving the heat dissipation performance of the turbine intermediate body 50 is achieved, and the dust screen I65 and the dust screen II 67 are used for preventing dust from entering the heat dissipation cavity 60.
The utility model discloses a use as follows: when the turbine intermediate body 50 dissipates heat, workers in the field fill the oil pipe one 61 with engine oil, then start the oil pump 66 to circulate the engine oil in the heat dissipation cavity one 51 and the oil pipe one 61 to dissipate heat for the bearing on the inner wall of the turbine intermediate body 50, when the engine oil dissipates heat, the temperature of the engine oil itself rises, at this time, start the water pump in the cooling water tank 55, the cooling water tank 55 pumps the cooling water into the cooling pipe one 52 inserted in the inner wall of the heat dissipation cavity one 51 in a threaded manner through the liquid inlet pipe 53, because the material of the cooling pipe one 52 is copper, the copper has the advantage of good heat conductivity, at this time, the cooling water in the cooling pipe one 52 cools the engine oil in the heat dissipation cavity one 51, and simultaneously start the heat dissipation fan 68, the heat of the engine oil in the oil pipe one 61 is wound on the oil pipe one 61 and is in full contact with the oil pipe one 61 to transfer the heat of the engine oil in the oil pipe one 61 to the thread heat conduction rod 62 in a heat conduction manner, because the aluminum alloy has good heat conductivity and strong corrosion resistance, the thread heat conducting rod 62 absorbs the heat of the engine oil, the air is transmitted to the heat dissipation cavity 60 through the air, the hot air in the heat dissipation cavity 60 is blown out through the heat dissipation fan 68, new cold air enters from the other end of the heat dissipation cavity 60, the engine oil in the oil pipe 61 is dissipated through an air circulation mode, the heat dissipation performance of the engine oil in the oil pipe 61 is improved, the effect of improving the heat dissipation performance of the turbine intermediate body 50 is achieved, and the first dustproof net 65 and the second dustproof net 67 are used for preventing dust from entering the heat dissipation cavity 60.
The above description is only a preferred embodiment of the present invention, and any person skilled in the art may modify the present invention or modify it into an equivalent technical solution by using the technical solutions described above. Therefore, any simple modifications or equivalent replacements made according to the technical solution of the present invention belong to the scope of the claimed invention as far as possible.
Claims (7)
1. A high heat dissipation type turbocharger intermediate body, comprising a turbine intermediate body (50), characterized in that: the turbine intermediate body (50) inner wall is provided with a first heat dissipation cavity (51), the first heat dissipation cavity (51) inner wall is provided with a first cooling pipe (52), the first cooling pipe (52) one end fixed connection liquid inlet pipe (53), the liquid inlet pipe (53) one end fixed connection cooling water tank (55), the liquid outlet pipe (54) is installed at one end of the cooling water tank (55), the second heat dissipation cavity (60) is provided at the inner wall of the top of the turbine intermediate body (50), the first heat dissipation cavity (60) inner wall is sleeved with a first oil pipe (61), the outer surface of the first oil pipe (61) is sleeved with a threaded heat conducting rod (62), the second oil pipe (63) is installed at the top of the first oil pipe (61), the first oil pipe (64) one end fixed connection oil pipeline (63), the first dust screen (65) is installed at the inner wall of the top end of the second heat dissipation cavity (60), the second heat dissipation cavity (60) left end inner wall fixed connection dust screen (67), and a heat radiation fan (68) is arranged on the inner wall of the second heat radiation cavity (60).
2. A high heat dissipation type turbocharger intermediate body as recited in claim 1, wherein: the first cooling pipe (52) is arranged to be inserted into the inner wall of the first heat dissipation cavity (51) in a threaded mode, and the first cooling pipe (52) is made of copper.
3. A high heat dissipation type turbocharger intermediate body as recited in claim 1, wherein: the number of the second heat dissipation cavities (60) is two, and the two heat dissipation cavities are respectively arranged on the inner wall at the top and the inner wall at the bottom of the turbine intermediate body (50).
4. A high heat dissipation type turbocharger intermediate body as recited in claim 1, wherein: the number of the first oil pipes (61) is two, the number of the first oil pipes (61) in each group is four, and the first oil pipes (61) in two groups are respectively arranged on the inner walls of the second heat dissipation cavities (60) in two groups.
5. A high heat dissipation type turbocharger intermediate body as recited in claim 1, wherein: the bottoms of the first oil pipes (61) are open, and the first oil pipes (61) are communicated with the first heat dissipation cavity (51).
6. A high heat dissipation type turbocharger intermediate body as recited in claim 1, wherein: the material of screw thread heat conduction stick (62) sets up to the aluminum alloy, screw thread heat conduction stick (62) is evenly twined to oil pipe (61) surface, screw thread heat conduction stick (62) equals with the quantity of oil pipe (61).
7. A high heat dissipation type turbocharger intermediate body as recited in claim 1, wherein: the heat dissipation fans (68) are arranged near the second dustproof net (67), and the number of the heat dissipation fans (68) is two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121941702.1U CN215292669U (en) | 2021-08-18 | 2021-08-18 | High heat dissipation type turbocharger intermediate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121941702.1U CN215292669U (en) | 2021-08-18 | 2021-08-18 | High heat dissipation type turbocharger intermediate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215292669U true CN215292669U (en) | 2021-12-24 |
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ID=79527858
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121941702.1U Expired - Fee Related CN215292669U (en) | 2021-08-18 | 2021-08-18 | High heat dissipation type turbocharger intermediate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215292669U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116357448A (en) * | 2023-03-28 | 2023-06-30 | 江苏毅合捷汽车科技股份有限公司 | Engine oil heat dissipation and pressure maintaining device of turbocharger |
-
2021
- 2021-08-18 CN CN202121941702.1U patent/CN215292669U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116357448A (en) * | 2023-03-28 | 2023-06-30 | 江苏毅合捷汽车科技股份有限公司 | Engine oil heat dissipation and pressure maintaining device of turbocharger |
| CN116357448B (en) * | 2023-03-28 | 2025-05-30 | 江苏毅合捷汽车科技股份有限公司 | A turbocharger oil heat dissipation and pressure maintaining device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211224 |