Rapid heat dissipation type turbocharger assembly

Abstract

A rapid heat dissipation type turbocharger assembly comprises a turbocharger and a fan set. The side edge of the turbocharger integrally extends to form a heat dissipation butt joint end, a plurality of sets of shaft holes are evenly distributed in the heat dissipation butt joint end, the shaft holes are in butt joint with positioning shafts in a positioning mode, the positioning shafts are evenly distributed on the rear end face of a connecting piece, and the rear end face of the connecting piece is connected with a heat dissipation fan sleeve through an installation end. According to the rapid heat dissipation type turbocharger assembly, the assembly can be matched with a turbocharger to complete the synchronous heat dissipation procedure in the using process. The technical problem that an engine is damaged due to overheating in the using process of the turbocharger is solved. Meanwhile, a grouping installation structure is adopted in the structure, in the using process, centralized heating treatment is completed through the middleware, in the centralized heating process, the cooling fan sleeve completes the cooling procedure, and the structure can replace an extending end of the turbocharger and centralized heating of the cooling fan sleeve.

Description

Technical Field

[0001] The utility model belongs to the technical field of turbocharger auxiliary equipment, and in particular relates to a fast heat dissipation type turbocharger component. Background Art

[0002] A turbocharger is actually an air compressor that increases the intake volume by compressing air. It uses the inertial force of the exhaust gas discharged by the engine to drive the turbine in the turbine chamber, and the turbine drives the coaxial impeller, which presses the air sent from the air filter pipe to enter the cylinder with pressure. When the engine speed increases, the exhaust gas discharge speed and the turbine speed also increase synchronously, and the impeller compresses more air into the cylinder. The increase in air pressure and density can burn more fuel. By increasing the amount of fuel and adjusting the engine speed accordingly, the engine output power can be increased.

[0003] The necessity of turbocharger heat dissipation is mainly reflected in the following aspects: Prevent overheating damage: The turbocharger increases the intake volume by compressing air, thereby increasing the power of the engine. However, this process generates a lot of heat. Especially after a long period of high-speed driving, the temperature of the turbocharger will be very high. Without an effective heat dissipation system, excessive temperature will cause damage to the turbocharger itself and its internal structure, such as bearing lubrication failure, seal aging, etc. Protect the engine: The heat of the turbocharger comes not only from the process of compressing air, but also from the exhaust gas emissions of the engine. When the high-temperature exhaust gas passes through the turbocharger, its temperature will be further increased. If the heat cannot be dissipated in time, it will affect the normal operation of the engine and even cause the engine to overheat, thereby causing a series of faults, such as lubricant failure, engine performance degradation, etc. Improve performance and fuel efficiency: The heat dissipation system can ensure that the engine and turbocharger operate within a suitable temperature range. At the appropriate temperature, the engine can perform at its best, with higher combustion efficiency and lower fuel consumption. Therefore, an effective heat dissipation system is essential to improving the performance and fuel efficiency of the car.

[0004] Therefore, the present application adopts a fast heat dissipation turbocharger assembly, which can cooperate with the turbocharger to complete the synchronous heat dissipation process during use. It solves the technical problem of overheating damage to the engine during the use of the turbocharger. At the same time, the structure adopts a group installation structure. During use, the centralized heat treatment is completed through the middleware. During the centralized heating process, the heat dissipation fan sleeve completes the heat dissipation process. This structure can replace the extended end of the turbocharger and the heat dissipation fan sleeve for centralized heating, solving the technical problem of unified replacement of the heat dissipation structure due to damage during long-term use. Summary of the invention

[0005] In order to achieve the above object, the technical solution of the utility model is as follows:

[0006] A fast heat dissipation turbocharger assembly comprises a turbocharger and a fan group; a heat dissipation docking end head is integrally extended from the side of the turbocharger, the heat dissipation docking end head itself is evenly distributed with a plurality of axial holes, the axial holes are positioned and docked with positioning shafts, the positioning shafts are evenly distributed on the rear end face of a connecting piece, and the rear end face of the connecting piece is connected to a heat dissipation fan sleeve through a mounting end head.

[0007] Furthermore, a mounting ring is installed at the center of the heat dissipation docking end groove through a fixing bolt, and a guide sleeve is recessed and extended inwardly along the ring body of the mounting ring, and an anti-deformation balance frame is sleeved inside the guide sleeve.

[0008] Furthermore, the anti-deformation balance frame is in an irregular plate shape, the outer end of the anti-deformation balance frame is in supporting contact with the inner wall annular structure of the heat dissipation docking end, and the outer contact end of the anti-deformation balance frame is in a bent shape.

[0009] Furthermore, the outer ring of the mounting end retains a thread, and the mounting end is screwed to the screw hole of the rear end surface of the cooling fan sleeve through the outer ring thread.

[0010] Furthermore, a baffle is integrally extended along the outer ring of the positioning shaft on the rear end surface of the connector, and the baffle is an annular structure, and the baffle is sleeved on the outer ring of the heat dissipation docking end.

[0011] Furthermore, an energy-gathering grid is installed at the central through hole of the connecting piece.

[0012] The beneficial effects of the utility model are:

[0013] Compared with the prior art, the present application adopts a fast heat dissipation turbocharger assembly, which can cooperate with the turbocharger to complete the synchronous heat dissipation process during use. It solves the technical problem of overheating damage to the engine during the use of the turbocharger. At the same time, the structure adopts a group installation structure. During use, the centralized heat treatment is completed through the middleware. During the centralized heating process, the heat dissipation fan sleeve completes the heat dissipation process. The structure can replace the extended end of the turbocharger and the heat dissipation fan sleeve for centralized heating, solving the technical problem of unified replacement of the heat dissipation structure due to damage during long-term use. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 The utility model is a structural schematic diagram of a fast heat dissipation type turbocharger assembly.

[0015] Figure 2 The utility model is a top view of a fast heat dissipation type turbocharger assembly.

[0016] Figure 3The utility model is a front view of a heat dissipation docking end of a fast heat dissipation turbocharger assembly.

[0017] Figure 4 The utility model is a rear view of a fast heat dissipation type turbocharger assembly connecting piece.

[0018] List of Figure Symbols:

[0019] 1 is a turbocharger, 2 is a heat dissipation docking terminal, 3 is a heat dissipation fan sleeve, 4 is a drive port, 5 is a fan assembly, 6 is a mounting terminal, 7 is a connecting piece, 8 is an axis hole, 9 is a baffle, 10 is an anti-deformation balance frame, 11 is a guide sleeve, 12 is a fixing bolt, 13 is a mounting ring, 14 is a positioning shaft, and 15 is an energy-gathering grid. DETAILED DESCRIPTION

[0020] The present invention will be further described below in conjunction with the accompanying drawings and specific implementations. It should be understood that the following specific implementations are only used to illustrate the present invention and are not used to limit the scope of the present invention.

[0021] like Figure 1 , Figure 2 , Figure 3 and Figure 4 As shown, a fast heat dissipation turbocharger assembly includes a turbocharger and a fan group; a heat dissipation docking terminal 2 is integrally extended from the side of the turbocharger 1, and the heat dissipation docking terminal 2 itself is evenly distributed with a plurality of groups of shaft holes 8, and the shaft holes 8 are positioned and docked with the positioning shaft 14, and the positioning shaft 14 is evenly distributed on the rear end face of the connector 7, and the rear end face of the connector 7 is connected to the heat dissipation fan sleeve 3 through the mounting terminal 6. Among them, the heat dissipation fan sleeve 3 and the connector 7 are heat-dissipatingly docked with the turbocharger 1 through the heat dissipation docking terminal 2. In this process, the heat emitted by the turbocharger is uniformly collected by the heat dissipation fan sleeve 3 and the heat exchange is completed. In order to further fix the structure between the three, a multi-point positioning process of the shaft hole 8 and the positioning shaft 14 is adopted to avoid the installation stability of the equipment being affected by various vibration factors.

[0022] like Figure 1 , Figure 2 , Figure 3 and Figure 4 As shown, a mounting ring 13 is installed at the center of the groove of the heat dissipation docking terminal 2 through a fixing bolt 12, and a guide sleeve 11 is recessed and extended inwardly along the ring body of the mounting ring 13, and an anti-deformation balance frame 10 is installed inside the guide sleeve 11. Among them, the mounting ring 13, as a central mounting structure, can further fix the anti-deformation balance frame 10, and the anti-deformation balance frame 10 has the effect of resisting overheating deformation, and can also disperse the force of vibration to achieve a balancing effect.

[0023] like Figure 1 , Figure 2 , Figure 3 and Figure 4 As shown, the anti-deformation balance frame 10 is in an irregular plate shape, the outer end of the anti-deformation balance frame 10 is in contact with the inner wall ring structure of the heat dissipation docking end 2, and the outer contact end of the anti-deformation balance frame 10 is in a bent shape. Among them, the irregular structure of the anti-deformation balance frame 10 provides a certain anti-deformation bending length to avoid unnecessary force obstruction during the deformation process.

[0024] like Figure 1 , Figure 2 , Figure 3 and Figure 4 As shown, the outer ring of the mounting end 6 retains a thread, and the mounting end 6 is screwed with the screw hole of the rear end face of the cooling fan sleeve 3 through the outer ring thread. Among them, the mounting end 6 and the cooling fan sleeve 3 are screwed, which is more convenient and tighter than horizontal docking.

[0025] like Figure 1 , Figure 2 , Figure 3 and Figure 4 As shown, the rear end face of the connector 7 is integrally extended with a baffle 9 along the outer ring of the positioning shaft 14, and the baffle 9 is an annular structure, and the baffle 9 is sleeved on the outer ring of the heat dissipation docking terminal 2. Among them, the baffle 9 can ensure a certain airtightness, and at the same time, it can prevent external impurities or factors from affecting the installation structure of the positioning shaft 14.

[0026] like Figure 1 , Figure 2 , Figure 3 and Figure 4 As shown, a focusing grid 15 is installed at the central through hole of the connecting member 7. The focusing grid 15 has a certain heat absorption function and shares the pressure of the overheating load.

[0027] It should be noted that the above content only illustrates the technical idea of ​​the utility model and cannot be used to limit the protection scope of the utility model. For ordinary technicians in this technical field, several improvements and modifications can be made without departing from the principle of the utility model. These improvements and modifications all fall within the protection scope of the claims of the utility model.

Claims

1. A fast heat dissipation turbocharger assembly, comprising a turbocharger and a fan assembly; wherein: A heat dissipation docking terminal (2) is integrally extended from the side of the turbocharger (1), and the heat dissipation docking terminal (2) itself is evenly distributed with a plurality of groups of shaft holes (8), and the shaft holes (8) are positioned and docked with positioning shafts (14), and the positioning shafts (14) are evenly distributed on the rear end surface of the connecting member (7), and the rear end surface of the connecting member (7) is connected to the heat dissipation fan sleeve (3) through the mounting terminal (6).

2. A rapid heat dissipation turbocharger assembly according to claim 1, characterized in that: A mounting ring (13) is mounted at the center of the groove of the heat dissipation docking terminal (2) via a fixing bolt (12); a guide sleeve (11) is recessed and extends inwardly along the ring body of the mounting ring (13); and an anti-deformation balance frame (10) is sleeved inside the guide sleeve (11).

3. A rapid heat dissipation turbocharger assembly according to claim 2, characterized in that: The anti-deformation balance frame (10) is in an irregular plate shape, the outer end of the anti-deformation balance frame (10) is in support contact with the inner wall annular structure of the heat dissipation docking end (2), and the outer contact end of the anti-deformation balance frame (10) is in a bent shape.

4. A rapid heat dissipation turbocharger assembly according to claim 1, characterized in that: The outer ring of the mounting end head (6) retains a thread, and the mounting end head (6) is screwed to the screw hole on the rear end face of the cooling fan sleeve (3) via the outer ring thread.

5. The rapid heat dissipation turbocharger assembly according to claim 1, characterized in that: A baffle (9) is integrally extended from the rear end face of the connecting member (7) along the outer ring of the positioning shaft (14); the baffle (9) is an annular structure, and the baffle (9) is sleeved on the outer ring of the heat dissipation docking end (2).

6. A rapid heat dissipation turbocharger assembly according to claim 1, characterized in that: An energy-gathering grid (15) is installed at the central through hole of the connecting piece (7).

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