CN221220625U - Heat dissipation connection structure of turbocharger and intermediate - Google Patents
Heat dissipation connection structure of turbocharger and intermediate Download PDFInfo
- Publication number
- CN221220625U CN221220625U CN202322673869.XU CN202322673869U CN221220625U CN 221220625 U CN221220625 U CN 221220625U CN 202322673869 U CN202322673869 U CN 202322673869U CN 221220625 U CN221220625 U CN 221220625U
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- Prior art keywords
- heat dissipation
- turbine
- connecting piece
- cooling
- air outlet
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- 230000017525 heat dissipation Effects 0.000 title claims abstract description 49
- 238000001914 filtration Methods 0.000 claims abstract description 16
- 238000001816 cooling Methods 0.000 claims description 38
- 238000007789 sealing Methods 0.000 claims description 26
- 230000005855 radiation Effects 0.000 claims description 13
- 239000000463 material Substances 0.000 claims description 4
- 239000000428 dust Substances 0.000 abstract description 12
- 230000006835 compression Effects 0.000 abstract description 3
- 238000007906 compression Methods 0.000 abstract description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003670 easy-to-clean Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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 application belongs to the technical field of production of heat dissipation connection structures, and discloses a heat dissipation connection structure of a turbocharger and an intermediate, which comprises a heat dissipation mechanism, wherein one side of the heat dissipation mechanism is provided with a turbine, one side of the heat dissipation mechanism, which is far away from the turbine, is provided with an air outlet device, the heat dissipation mechanism is arranged at the center positions of the turbine and the air outlet device, the left end of the outer side of the turbine is fixedly connected with a connecting piece, the center position of the right side of the turbine is provided with an air inlet, the top of the turbine is provided with a gas filtering port, the center position of the left side of the air outlet device is provided with an air outlet, the center position of the left side of the turbine is provided with a heat dissipation fan, and the heat dissipation fan and the connecting piece are convenient to detach through the cooperation of mounting holes and bolts, so that dust accumulated inside can be timely cleaned after the heat dissipation fan and the connecting piece are used, the compression efficiency of the device is improved, and the work efficiency of an engine can be reduced after the air with dust is input into a cylinder is solved.
Description
Technical Field
The application relates to the technical field of production of heat dissipation connection structures, in particular to a heat dissipation connection structure of a turbocharger and an intermediate.
Background
A turbocharger, also known as an air compressor, is a device used to compress gas. The air compressor is similar in construction to the water pump. Most air compressors are reciprocating piston, rotary vane or rotary screw, turbochargers are actually air compressors that increase the amount of intake air by compressing the air. The turbine drives a coaxial impeller by utilizing the inertial impulse of exhaust gas discharged by the engine, and the impeller presses and sends air sent by an air filter pipeline to be pressurized into a cylinder. When the rotation speed of the engine is increased, the exhaust gas discharge speed and the rotation speed of the turbine are synchronously increased, more air is compressed by the impeller to enter the cylinder, more fuel can be combusted by increasing the pressure and the density of the air, and the output power of the engine can be increased by correspondingly increasing the fuel quantity and adjusting the rotation speed of the engine.
The existing heat dissipation connecting mechanism is mainly a mechanism integrated with the turbocharger, the inside is not easy to clean after being air filtered, dust is accumulated after internal filtration after a long time, the efficiency of air compression is affected, and if the air with the dust is input into a cylinder, the working efficiency of an engine is reduced, and the internal combustion effect is weakened.
In order to solve the problems, the application provides a heat dissipation connecting structure of a turbocharger and an intermediate body.
Disclosure of utility model
The application provides a heat dissipation connection structure of a turbocharger and an intermediate, which adopts the following technical scheme:
the utility model provides a heat dissipation connection structure of turbo charger and midbody, includes the cooling mechanism, cooling mechanism one side is equipped with the turbine, cooling mechanism is kept away from the turbine one side and is equipped with the gas outlet ware, cooling mechanism sets up in turbine and gas outlet ware central point put, turbine outside left end fixedly connected with connecting piece, the air inlet has been seted up to turbine right side central point put, the gas filtering mouth has been seted up at the turbine top, the gas outlet has been seted up to gas outlet ware left side central point put, cooling fan has been seted up to turbine left side central point put, the connecting piece is close to cooling fan one side four corners all runs through and is equipped with the mounting hole, the connecting piece is close to cooling fan's one side and has been seted up annular seal groove, cooling fan is close to one side of connecting piece and is equipped with annular sealing ring, the bottom is equipped with annular sealed pad in the seal groove;
The heat dissipation mechanism comprises a conveying box, the conveying box is arranged at the central position inside the heat dissipation mechanism, and heat dissipation cooling boxes and filtering purifying boxes are arranged at two ends of the outer side of the conveying box.
Further, a through hole is formed in the center of the surface of the connecting piece, and the through hole corresponds to the heat dissipation cooling box and the heat dissipation fan.
Further, the number of the mounting holes is four, and the connecting piece is connected with the cooling fan through the mounting holes and the bolts.
Further, the sealing groove is located in the surrounding of the mounting hole, the sealing groove and the sealing ring are mutually corresponding and are mutually clamped, and the sealing gasket is made of rubber materials.
Further, a check valve is arranged in the air outlet.
In summary, the application has the following beneficial technical effects:
Through the cooperation of mounting hole and bolt, the dismantlement to equipment has been convenient for carried out, can dismantle between radiator fan and the connecting piece that make, the clearance that can be timely after the dismantlement is used for a long time piles up inside dust, increase the compression efficiency of its equipment, can cause engine work efficiency to reduce after having solved the air input cylinder that has the dust, inside combustion effect weakens, and cooperation seal groove and seal ring's sealed pad, install after the clearance is accomplished, increase the leakproofness of its equipment, avoided the leakage of inside steam.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present application;
FIG. 2 is a schematic view of a connector according to the present application;
FIG. 3 is a schematic diagram of a heat dissipating fan according to the present application;
FIG. 4 is a schematic view of the check valve structure of the present application;
fig. 5 is a schematic view of a seal groove structure according to the present application.
The reference numerals in the figures illustrate:
1. A heat dissipation mechanism; 101. a delivery box; 102. a heat-radiating cooling box; 103. a filtration purifying box; 2. a connecting piece; 3. a turbine; 4. an air inlet; 5. a gas filtering port; 6. an air outlet device; 7. an air outlet; 8. a heat radiation fan; 9. sealing grooves; 10. a mounting hole; 11. a seal ring; 12. a check valve; 13. and a sealing gasket.
Detailed Description
The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present application; it is apparent that the described embodiments are only some embodiments of the present application, not all embodiments, and that all other embodiments obtained by persons of ordinary skill in the art without making creative efforts based on the embodiments in the present application are within the protection scope of the present application.
Examples:
The embodiment of the application discloses a heat radiation connecting structure of a turbocharger and an intermediate, referring to fig. 1-5, which comprises a heat radiation mechanism 1, wherein one side of the heat radiation mechanism 1 is provided with a turbine 3, one side of the heat radiation mechanism 1 far away from the turbine 3 is provided with an air outlet 6, the heat radiation mechanism 1 is arranged at the center positions of the turbine 3 and the air outlet 6, the left end of the outer side of the turbine 3 is fixedly connected with a connecting piece 2, the center position of the right side of the turbine 3 is provided with an air inlet 4, the top of the turbine 3 is provided with a gas filtering port 5, the center position of the left side of the air outlet 6 is provided with a gas outlet 7, the center position of the left side of the turbine 3 is provided with a heat radiation fan 8, four corners of one side of the connecting piece 2 close to the heat radiation fan 8 are respectively provided with a mounting hole 10 in a penetrating manner, an annular sealing groove 9 is formed in one side, close to the cooling fan 8, of the connecting piece 2, an annular sealing ring 11 is arranged on one side, close to the connecting piece 2, of the cooling fan 8, an annular sealing gasket 13 is arranged at the inner bottom of the sealing groove 9, air outside the equipment is sucked through an air filtering port 5 on the turbine 3, the cooling fan 8 can be effectively driven to rapidly transmit hot air in the turbine 3 into the cooling mechanism 1 for cooling through rotation of fan blades, then the hot air is continuously discharged and input into an engine cylinder, the turbine 3 and the connecting piece 2 can be detached through a mounting hole 10, and the sealing performance of two sections of the sealing gasket is improved by matching with the sealing ring 11 and the sealing groove 9;
The heat dissipation mechanism 1 includes delivery box 101, and delivery box 101 sets up in the inside central point of heat dissipation mechanism 1 put, and delivery box 101 outside both ends are provided with heat dissipation cooling tank 102 and filtration purifying box 103, in orderly input heat dissipation mechanism 1 in proper order with the steam in the radiator fan 8, carries out effectual heat dissipation through heat dissipation cooling tank 102, sends into filtration purifying box 103 through delivery box 101 later and filters the interior dust of air, reaches the heat dissipation and evenly, reduces the steam seepage to the external world.
The center of the surface of the connecting piece 2 is provided with a through hole, and the through hole corresponds to the heat dissipation cooling box 102 and the heat dissipation fan 8, so that hot air can conveniently enter the heat dissipation cooling box 102 for heat dissipation.
The quantity of the mounting holes 10 is four, the connecting piece 2 is mutually connected with the cooling fan 8 through the mounting holes 10 matched with bolts, the connecting piece 2 and the cooling fan 8 are conveniently mounted through the bolts matched with the mounting holes 10, the cooling mechanism 1 is convenient to detach, and dust accumulated in the cooling mechanism after long use is convenient to clean.
The seal groove 9 is located the mounting hole 10 and encircles in, and seal groove 9 corresponds each other and joint each other with sealing ring 11, and sealing gasket 13 material is rubber material, increases the leakproofness between its connecting piece 2 and the radiator fan 8, is being convenient for carry out the inside condition of cleaning equipment, also avoids inside steam to leak.
A check valve 12 is arranged in the air outlet 7 to avoid the backflow of air in the connected engine cylinder.
The implementation principle of the embodiment is as follows: external air is sucked through the air filtering port 5 on the turbine 3, hot air in the turbine 3 is conveyed into the heat dissipation mechanism 1 through the heat dissipation fan 8 to be subjected to heat dissipation treatment, the hot air is firstly conveyed into the heat dissipation cooling box 102 to be subjected to heat dissipation treatment, then the hot air is conveyed into the filtering and purifying box 103 through the conveying box 101 to be subjected to dust filtering treatment on dust in the air, and then the dust is conveyed into a connected engine cylinder through the air outlet 7 outside the air outlet 6, the whole heat dissipation fan 8 and the connecting piece 2 can be detached by matching with bolts on the mounting hole 10 of the dust filtering and purifying box, the heat dissipation mechanism is timely cleaned, and the sealing performance of equipment is improved when the equipment is mounted by matching with the sealing groove 9 and the sealing ring 11 in a mutually clamped mode.
The above embodiments are not intended to limit the scope of the present application, so: all equivalent changes in structure, shape and principle of the application should be covered in the scope of protection of the application.
Claims (6)
1. The utility model provides a heat dissipation connection structure of turbo charger and midbody, includes heat dissipation mechanism (1), its characterized in that: the utility model discloses a heat dissipation mechanism, including turbine (1), cooling mechanism (2), air inlet (4) have been seted up to cooling mechanism (1), cooling mechanism (1) is kept away from one side of turbine (3) and is equipped with air outlet ware (6), cooling mechanism (1) sets up in turbine (3) and air outlet ware (6) central point put, turbine (3) outside left end fixedly connected with connecting piece (2), air inlet (4) have been seted up on turbine (3) right side central point put, gas filtering mouth (5) have been seted up at turbine (3) top, air outlet (7) have been seted up to air outlet ware (6) left side central point put, cooling fan (8) have been seted up to turbine (3) left side central point put, one side four corners that connecting piece (2) are close to cooling fan (8) all run through and are equipped with mounting hole (10), one side that cooling fan (2) are close to cooling fan (8) has seted up annular seal groove (9), one side that cooling fan (8) are close to connecting piece (2) is equipped with annular sealing ring (11), bottom is equipped with annular sealing pad (13) in seal groove (9).
2. The heat radiation connection structure of a turbocharger and an intermediate body according to claim 1, wherein: the heat dissipation mechanism (1) comprises a conveying box (101), the conveying box (101) is arranged at the central position inside the heat dissipation mechanism (1), and heat dissipation cooling boxes (102) and filtering purifying boxes (103) are arranged at two ends of the outer side of the conveying box (101).
3. The heat radiation connection structure of a turbocharger and an intermediate body according to claim 1, wherein: a through hole is formed in the center of the surface of the connecting piece (2), and the through hole corresponds to the heat dissipation cooling box (102) and the heat dissipation fan (8).
4. The heat radiation connection structure of a turbocharger and an intermediate body according to claim 1, wherein: the number of the mounting holes (10) is four, and the connecting piece (2) is connected with the cooling fan (8) through the mounting holes (10) matched with bolts.
5. The heat radiation connection structure of a turbocharger and an intermediate body according to claim 1, wherein: the sealing groove (9) is arranged in the surrounding of the mounting hole (10), the sealing groove (9) and the sealing ring (11) are mutually corresponding and are mutually clamped, and the sealing gasket (13) is made of rubber materials.
6. The heat radiation connection structure of a turbocharger and an intermediate body according to claim 1, wherein: a check valve (12) is arranged in the air outlet (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322673869.XU CN221220625U (en) | 2023-10-07 | 2023-10-07 | Heat dissipation connection structure of turbocharger and intermediate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322673869.XU CN221220625U (en) | 2023-10-07 | 2023-10-07 | Heat dissipation connection structure of turbocharger and intermediate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221220625U true CN221220625U (en) | 2024-06-25 |
Family
ID=91579915
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322673869.XU Active CN221220625U (en) | 2023-10-07 | 2023-10-07 | Heat dissipation connection structure of turbocharger and intermediate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221220625U (en) |
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2023
- 2023-10-07 CN CN202322673869.XU patent/CN221220625U/en active Active
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| GR01 | Patent grant |