CN219159059U

CN219159059U - Heat radiation connection structure of turbocharger intermediate body and turbine

Info

Publication number: CN219159059U
Application number: CN202222873764.4U
Authority: CN
Inventors: 韦国
Original assignee: Wuxi Zhen Shang Machinery Co ltd
Current assignee: Wuxi Zhen Shang Machinery Co ltd
Priority date: 2022-10-31
Filing date: 2022-10-31
Publication date: 2023-06-09
Anticipated expiration: 2032-10-31

Abstract

The utility model relates to the technical field of turbocharger intermediates, and discloses a heat radiation connection structure of a turbocharger intermediate and a turbine, which comprises a heat radiation mechanism, the turbine and an air outlet device, wherein the air outlet device is movably arranged on the left side of the outer surface of the heat radiation mechanism, the turbine is movably arranged on the right side of the outer surface of the heat radiation mechanism, the heat radiation mechanism is arranged at the center position of the turbine and the air outlet device, an intercooler is arranged in a cooling box, cooling devices are fixedly arranged at two ends of the inner side of the conducting box, and an air duct is movably arranged at the center position of the inner side of the conducting box. According to the utility model, the fan blades are arranged on the surface of the heat radiation fan and movably arranged around the surface of the heat radiation fan, and the hot air in the heat radiation fan can be effectively driven to be rapidly transmitted to the cooling box, the conducting box and the purifying box through the rotation of the fan blades, so that the hot air can be effectively cooled and purified and transmitted to the outside, the heat radiation effect is good, and the comprehensive characteristics are achieved.

Description

Heat radiation connection structure of turbocharger intermediate body and turbine

Technical Field

The utility model relates to the technical field of turbocharger intermediates, in particular to a heat dissipation connection structure of a turbocharger intermediate and a turbine.

Background

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.

A turbine is an engine that generates power by fluid striking an impeller for rotation.

The existing heat dissipation connection structure of the turbocharger intermediate and the turbine is not comprehensive enough, and the effect on heat dissipation is relatively poor, so that improvement is needed.

Disclosure of Invention

The utility model aims to provide a heat dissipation connecting structure of a turbocharger intermediate and a turbine, which has the characteristics of good heat dissipation effect and comprehensiveness.

In order to achieve the above purpose, the present utility model provides the following technical solutions:

the heat radiation connecting structure of the turbocharger intermediate body and the turbine comprises a heat radiation mechanism, the turbine and an air outlet device, wherein the air outlet device is movably arranged on the left side of the outer surface of the heat radiation mechanism, the turbine is movably arranged on the right side of the outer surface of the heat radiation mechanism, and the heat radiation mechanism is arranged at the center of the turbine and the air outlet device.

The heat dissipation mechanism comprises a conducting box, the conducting box is arranged at the central position inside the heat dissipation mechanism, the two ends of the outer side of the conducting box are provided with a cooling box and a purifying box, an intercooler is arranged inside the cooling box, the two ends of the inner side of the conducting box are fixedly provided with cooling devices, and the central position of the inner side of the conducting box is movably provided with an air duct.

Preferably, the left end fixedly connected with connecting piece in the turbine outside, the air inlet has been seted up to turbine right side central point, the gas filtering mouth has been seted up at the turbine top, the gas outlet has been seted up to the left side central point of air outlet device, the air-cooling fan has been seted up to turbine left side central point.

Preferably, the right side movable mounting in the purifying box has the filter, the filter left side is provided with air cleaner.

Preferably, a through hole is formed in the center of the surface of the connecting piece, the through hole corresponds to the cooling box and the cooling fan, the cooling box is effectively communicated with the cooling fan, and the maximum effect of heat dissipation of hot gas is achieved.

Preferably, the air duct is uniformly distributed on the surface of the conducting box, the cooling device is arranged at the upper end and the lower end of the outer surface of the air duct, and hot air in the heat dissipation fan is sequentially and orderly transmitted from the air duct, so that uniform heat dissipation is achieved, leakage of the hot air to the outside is reduced, and the cooling device is always in a closed heat dissipation working state.

Preferably, the air cleaner is equipped with three altogether, and three group air cleaner outside one end is linked together with the gas outlet, can effectively carry out efficient purification with the steam of conducting box derivation, reduces the influence to external environmental factor, has the effect of environmental protection.

Preferably, the surface of the heat dissipation fan is provided with fan blades, the fan blades are movably mounted on the periphery of the surface of the heat dissipation fan, hot air in the heat dissipation fan can be effectively driven to be rapidly transmitted to the cooling box, the conducting box and the purifying box through rotation of the fan blades, the hot air is effectively cooled and purified, and the hot air is transmitted to the outside, so that the heat dissipation effect is good, and the heat dissipation fan has the comprehensive characteristics.

The utility model provides a heat radiation connection structure of a turbocharger intermediate and a turbine, which has the following beneficial effects:

(1) The heat radiation fan is characterized in that the heat radiation fan is provided with a heat radiation pipe, the heat radiation pipe is connected with the heat radiation fan, the heat radiation fan is connected with the heat radiation fan, and the heat radiation fan is connected with the heat radiation fan.

(2) According to the utility model, the fan blades are arranged on the surface of the heat radiation fan and movably arranged around the surface of the heat radiation fan, and the hot air in the heat radiation fan can be effectively driven to be rapidly transmitted into the cooling box, the conducting box and the purifying box through the rotation of the fan blades, so that the hot air can be effectively cooled and purified and transmitted to the outside, the heat radiation effect is good, and the comprehensive characteristics are achieved.

(3) The heat radiation fan is characterized in that the heat radiation fan is provided with a heat radiation pipe, the heat radiation pipe is connected with the heat radiation fan, the heat radiation fan is connected with the heat radiation fan, and the heat radiation fan is connected with the heat radiation fan.

Drawings

FIG. 1 is a schematic view of the overall structure of the front face of the present utility model;

FIG. 2 is an expanded view of the front overall structure of the present utility model;

FIG. 3 is a schematic view of the overall structure of the side face of the present utility model;

fig. 4 is a schematic view of the overall structure of the back surface of the present utility model.

In the figure: 1. a heat dissipation mechanism; 101. a conduction box; 102. a cooling box; 103. a purifying box; 104. an intercooler; 105. a cooling device; 106. an air duct; 107. a filter plate; 108. an air cleaner; 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.

Detailed Description

As shown in fig. 1-4, the present utility model provides a technical solution:

the utility model provides a turbocharger midbody and turbine's heat dissipation connection structure, including heat dissipation mechanism 1, turbine 3 and air outlet device 6, air outlet device 6 movable mounting is in heat dissipation mechanism 1 surface left side, turbine 3 movable mounting is in heat dissipation mechanism 1 surface right side, heat dissipation mechanism 1 sets up in turbine 3 and air outlet device 6 central point put, turbine 3 outside left end fixedly connected with connecting piece 2, the through-hole has been seted up at connecting piece 2 surface central point put, the through-hole corresponds with cooling tank 102 and radiator fan 8, effectively be linked together cooling tank 102 and radiator fan 8, the maximum effect is reached to the steam heat dissipation, air inlet 4 has been seted up at turbine 3 right side central point put, the filter port 5 has been seted up at turbine 3 top, air outlet 7 has been seted up at air outlet device 6 left side central point put, radiator fan 8 has been seted up at turbine 3 left side central point put, radiator fan 8 surface is provided with the flabellum, and flabellum movable mounting is around radiator fan 8 surface, through the rotation of flabellum, can effectively drive the quick transmission of steam in the radiator fan 8 to cooling tank 102, conduction case 101 and purifying box 103, carry out effective cooling purification effect to the steam, and transmission to the transmission reaches the good heat dissipation, the comprehensive characteristics of having the external world.

The heat dissipation mechanism 1 comprises a conducting box 101, the conducting box 101 is arranged at the central position inside the heat dissipation mechanism 1, the two ends of the outer side of the conducting box 101 are provided with a cooling box 102 and a purifying box 103, an intercooler 104 is arranged inside the cooling box 102, the two ends of the inner side of the conducting box 101 are fixedly provided with a cooling device 105, an air duct 106 is movably arranged at the central position inside the conducting box 101, the air duct 106 is uniformly distributed on the surface of the conducting box 101, the cooling device 105 is positioned at the upper end and the lower end of the outer surface of the air duct 106, hot air in the heat dissipation fan 8 is sequentially and orderly transmitted from the air duct 106, heat dissipation is uniform, leakage of the hot air to the outside is reduced, the heat dissipation is always in a working state of sealing and heat dissipation, the right side inside the purifying box 103 is movably provided with a filtering plate 107, the left side of the filtering plate 107 is provided with three groups, one end of the outer side of the three groups of the air filters 108 is communicated with the air outlet 7, the hot air led out from the conducting box 101 can be effectively purified, the influence on external environment factors is reduced, and the environment is protected; the air duct 106 is evenly distributed on the surface of the conducting box 101, the cooling device 105 is arranged at the upper end and the lower end of the outer surface of the air duct 106, and hot air in the heat dissipation fan 8 is sequentially and orderly transmitted from the air duct 106, so that even heat dissipation is achieved, leakage of the hot air to the outside is reduced, and the heat dissipation fan is always in a closed heat dissipation working state.

In summary, the heat dissipation device is uniformly distributed on the surface of the conducting box 101 through the air duct 106, and the cooling devices 105 are positioned at the upper end and the lower end of the outer surface of the air duct 106, so that the hot air in the heat dissipation fan 8 is sequentially and orderly transmitted from the air duct 106, uniform heat dissipation is achieved, leakage of the hot air to the outside is reduced, and the heat dissipation device is always in a closed heat dissipation working state; the fan blades are arranged on the surface of the cooling fan 8, the fan blades are movably mounted on the periphery of the surface of the cooling fan 8, hot air in the cooling fan 8 can be effectively driven to be rapidly transmitted to the cooling box 102, the conducting box 101 and the purifying box 103 through rotation of the fan blades, an effective cooling and purifying effect is carried out on the hot air, the hot air is transmitted to the outside, and the cooling effect is good, and the cooling fan has the comprehensive characteristics.

It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Finally, it should be noted that: the foregoing description is only a preferred embodiment of the present utility model, and the present utility model is not limited thereto, but it is to be understood that modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art, although the present utility model has been described in detail with reference to the foregoing embodiments. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.

Claims

1. The utility model provides a heat dissipation connection structure of turbo charger midbody and turbine, includes heat dissipation mechanism (1), turbine (3) and air outlet device (6), its characterized in that: the air outlet device (6) is movably arranged on the left side of the outer surface of the heat dissipation mechanism (1), the turbine (3) is movably arranged on the right side of the outer surface of the heat dissipation mechanism (1), and the heat dissipation mechanism (1) is arranged at the center positions of the turbine (3) and the air outlet device (6);

the heat dissipation mechanism (1) comprises a conducting box (101), the conducting box (101) is arranged at the inner central position of the heat dissipation mechanism (1), cooling boxes (102) and purifying boxes (103) are arranged at the two ends of the outer side of the conducting box (101), an intercooler (104) is arranged inside the cooling boxes (102), cooling devices (105) are fixedly arranged at the two ends of the inner side of the conducting box (101), and air guide pipes (106) are movably arranged at the central position of the inner side of the conducting box (101).

2. The heat radiation connection structure of a turbocharger intermediate and a turbine according to claim 1, characterized in that: the air inlet device is characterized in that a connecting piece (2) is fixedly connected to the left end of the outer side of the turbine (3), an air inlet (4) is formed in the center position of the right side of the turbine (3), an air filtering port (5) is formed in the top of the turbine (3), an air outlet (7) is formed in the center position of the left side of the air outlet device (6), and a heat dissipation fan (8) is formed in the center position of the left side of the turbine (3).

3. The heat radiation connection structure of a turbocharger intermediate and a turbine according to claim 1, characterized in that: the right side of the inside of the purifying box (103) is movably provided with a filter plate (107), and the left side of the filter plate (107) is provided with an air filter (108).

4. The heat radiation connection structure of the turbocharger intermediate and the turbine according to claim 2, characterized in that: a through hole is formed in the center of the surface of the connecting piece (2), and the through hole corresponds to the cooling box (102) and the cooling fan (8).

5. The heat radiation connection structure of a turbocharger intermediate and a turbine according to claim 1, characterized in that: the air ducts (106) are uniformly distributed on the surface of the conducting box (101), and the cooling device (105) is positioned at the upper end and the lower end of the outer surface of the air duct (106).

6. A turbocharger intermediate and turbine heat sink connection as set forth in claim 3, wherein: the air filters (108) are provided with three groups in total, and one end of the outer side of each air filter (108) is communicated with the air outlet (7).

7. The heat radiation connection structure of a turbocharger intermediate and a turbine according to claim 4, wherein: the surface of the heat radiation fan (8) is provided with fan blades, and the fan blades are movably arranged around the surface of the heat radiation fan (8).