Pressure-resistant anti-corrosion heat dissipation type oil tank structure

Abstract

The utility model discloses a pressure-resistant anti-corrosion heat dissipation type oil tank structure, and relates to the technical field of oil tanks. The heat dissipation device comprises a mounting base, wherein a mounting mechanism and a heat dissipation mechanism are arranged on the mounting base; the mounting mechanism comprises a clamping and fixing assembly, a limiting assembly and a buffering assembly, the clamping and fixing assembly comprises a fixing plate slidably connected to the mounting base, the sliding groove is slidably connected with a bearing block, the bearing block is hinged to a connecting strip, the bearing block is fixedly connected with a clamping block, and the clamping block is fixedly connected with a first spring. By means of the installation mechanism, elasticity of the first spring and the second spring is utilized, the second spring is arranged to conduct pressure-resistant buffering treatment on the oil tank shell, meanwhile, a worker can press the button to drive the clamping block to be clamped in the clamping groove to fixedly install the oil tank shell, and compared with the mode that an oil tank is bound on the damping device through a limiting belt, the oil tank is not prone to falling off. The limiting and fixing effects of the clamping blocks are better, corrosion and damage caused by external influences are not likely to happen, operation is easy and convenient, and durability is achieved.

Description

Technical Field

[0001] This utility model belongs to the field of fuel tank technology, and in particular relates to a pressure-resistant, corrosion-resistant and heat-dissipating fuel tank structure. Background Technology

[0002] In the prior art, a search revealed a Chinese patent entitled "A High-Stability Fuel Tank with a Heat Dissipation Structure," with publication number "CN215751902U." This patent primarily benefits from the increased contact area with air achieved through front and rear heat dissipation fins. A circulation device draws water from the reservoir into the cooling plate, where it exchanges heat with the fuel tank through water-cooling holes, achieving a water-cooling effect with higher heat dissipation efficiency. Shock-absorbing springs and limiting plates buffer vibrations to the fuel tank body, ensuring its stability and preventing excessive fuel pressure during vibration or shaking, which could affect driving performance. A magnetic base allows the support to be attached to the vehicle body, enhancing the fuel tank's stability. A fixing block enters a fixing groove, and a spring-loaded block engages with the groove under spring action, fixing the limiting band to the support and ensuring the limiting band's stabilizing effect on the fuel tank body. The structure is simple, highly stable, and provides excellent heat dissipation.

[0003] However, this device uses a limiting strap to tie the oil tank to the shock-absorbing support. Although this method can stabilize the oil tank, it is difficult to use for a long time. The limiting strap is mainly made of fiber material, which is easily worn by external influences after long-term use. In addition, the effect of using the limiting strap to tie the oil tank is relatively low and it is easy to come loose. Utility Model Content

[0004] The purpose of this utility model is to provide a pressure-resistant, corrosion-resistant, and heat-dissipating oil tank structure. By setting an installation mechanism, the elasticity of the first and second springs is utilized. While the second spring provides pressure-resistant buffering for the oil tank shell, the operator can press a button to drive the locking block into the slot to fix the oil tank shell in place. This solves the problem that the limiting belt is difficult to use for a long time and has a relatively low fixing effect.

[0005] To solve the above-mentioned technical problems, this utility model is achieved through the following technical solution:

[0006] This utility model is a pressure-resistant, corrosion-resistant and heat-dissipating oil tank structure, including a mounting base, on which a mounting mechanism and a heat dissipation mechanism are provided;

[0007] The installation mechanism includes a locking component, a limiting component, and a buffer component. The locking component includes a fixing plate slidably connected to the inner wall of the mounting base. The top surface of the fixing plate has a sliding groove. The inner wall of the sliding groove has two receiving blocks slidably connected. The top surfaces of the two receiving blocks are each hinged with two connecting strips. The top surfaces of the two receiving blocks are each fixedly connected with two locking blocks. The sides of the two locking blocks that are close to each other are each fixedly connected with a first spring.

[0008] Furthermore, the limiting component includes an oil tank shell that is slidably connected to the inner wall of the mounting base. The oil tank shell has two slots on both the front and back sides. The inner walls of several slots are slidably connected to the outer wall of the block. The ends of several first springs that are close to each other are fixedly connected to the inner wall of the groove.

[0009] Furthermore, a guide rod is fixedly connected to the inner wall of the chute, and two sliders are slidably connected to the outer wall of the guide rod. The top surfaces of the two sliders are hinged to several connecting strips, and buttons are fixedly connected to the sides of the two receiving blocks that are far apart from each other.

[0010] Furthermore, the buffer assembly includes two upper limit grooves formed on the front and back of the mounting base. The ends of the two buttons that are far apart from each other extend to the inner wall of the limit groove and are slidably connected to the limit groove. A plurality of second springs are fixedly connected to the inner bottom wall of the mounting base, and the top ends of the plurality of second springs are fixedly connected to the bottom surface of the fixing plate.

[0011] Furthermore, the heat dissipation mechanism includes an oil tank assembly, a drive assembly, and an air-cooling assembly. The oil tank assembly includes an oil storage cavity formed on the inner wall of the oil tank shell. An oil outlet pipe is fixedly connected to the top surface of the oil tank shell, and an oil inlet pipe is fixedly connected to the top surface of the oil tank shell. The bottom end of the oil outlet pipe extends to the inner bottom wall of the oil storage cavity and is fixedly connected to the oil storage cavity.

[0012] Furthermore, the drive assembly includes several heat dissipation slots all formed on the outer wall of the fuel tank housing, several air inlets are formed on the right side of the fuel tank housing, a motor is fixedly connected to the inner wall of the fuel tank housing, and a first rotating shaft is fixedly connected to the output end of the motor.

[0013] Furthermore, a second rotating shaft is rotatably connected to the inner wall of the fuel tank shell, and a connecting groove is provided on the inner wall of the fuel tank shell. The left ends of both the second rotating shaft and the first rotating shaft extend to the inner wall of the connecting groove and are rotatably connected to the connecting groove.

[0014] Furthermore, the air-cooling assembly includes two pulleys fixedly connected to the outer wall of the second rotating shaft and the first rotating shaft, with a belt sleeved between the two pulleys, and a plurality of fan blades fixedly connected to the outer wall of the second rotating shaft.

[0015] This utility model has the following beneficial effects:

[0016] By setting up an installation mechanism, the elasticity of the first and second springs is utilized. The second spring provides pressure-resistant buffering for the fuel tank shell, while the operator can press a button to move the locking blocks into the slots to fix the fuel tank shell in place. Compared with using a limit band to tie the fuel tank to the shock-absorbing device, the locking effect of multiple locking blocks is stronger, less susceptible to corrosion and damage from external influences, and is simple, convenient, and durable.

[0017] 2. By setting up a heat dissipation mechanism, the second rotating shaft driven by the motor is used to rotate several fan blades, which blow the external airflow into the oil tank shell through the air inlet. After passing through several heat dissipation slots, the airflow fully contacts the oil tank shell. Through the principle of heat exchange, the airflow carries away the heat that may exist on the surface of the oil tank shell, thus completing the air cooling heat dissipation treatment and further improving the practicality of the device.

[0018] Of course, any product implementing this utility model does not necessarily need to achieve all of the advantages described above at the same time. Attached Figure Description

[0019] To more clearly illustrate the technical solutions of the embodiments of this utility model, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0020] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0021] Figure 2 This is a schematic diagram of the rear cross-sectional structure of this utility model;

[0022] Figure 3 This is a top view sectional structural diagram of the present invention;

[0023] Figure 4 for Figure 3 Enlarged structural diagram at point A;

[0024] Figure 5 for Figure 2 A magnified structural diagram at point B in the middle.

[0025] The attached diagram lists the components represented by each number as follows:

[0026] 1. Mounting base; 2. Mounting mechanism; 3. Heat dissipation mechanism; 21. Fixing plate; 22. Slide groove; 23. Receiving block; 24. Connecting strip; 25. Locking block; 26. First spring; 27. Oil tank shell; 28. Locking groove; 29. ​​Guide rod; 210. Slider; 211. Button; 212. Limiting groove; 213. Second spring; 31. Oil storage chamber; 32. Oil outlet pipe; 33. Oil inlet pipe; 34. Heat dissipation groove; 35. Air inlet; 36. Motor; 37. First rotating shaft; 38. Second rotating shaft; 39. Connecting groove; 310. Pulley; 311. Belt; 312. Fan blade. Detailed Implementation

[0027] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of the present utility model.

[0028] Please see Figure 1-5 As shown, this utility model is a pressure-resistant, corrosion-resistant and heat-dissipating oil tank structure, including a mounting base 1, on which a mounting mechanism 2 and a heat dissipation mechanism 3 are provided;

[0029] The mounting mechanism 2 includes a locking component, a limiting component, and a buffer component. The locking component includes a fixing plate 21 slidably connected to the inner wall of the mounting base 1. The top surface of the fixing plate 21 has a groove 22. The inner wall of the groove 22 is slidably connected to two receiving blocks 23. The top surfaces of the two receiving blocks 23 are each hinged to two connecting strips 24. The top surfaces of the two receiving blocks 23 are each fixedly connected to two locking blocks 25. The sides of the two locking blocks 25 that are close to each other are each fixedly connected to a first spring 26. The limiting component includes an oil tank shell 27 slidably connected to the inner wall of the mounting base 1. The front and back of the oil tank shell 27 have two slots 28. The inner walls of several slots 28 are slidably connected to the outer walls of the locking blocks 25. Several first springs 26 are fixedly connected to the outer walls of the locking blocks 25. The ends of the springs 26 that are close to each other are fixedly connected to the inner wall of the slide groove 22. The inner wall of the slide groove 22 is fixedly connected to a guide rod 29. The outer wall of the guide rod 29 is slidably connected to two sliders 210. The top surfaces of the two sliders 210 are hinged to several connecting strips 24. The two receiving blocks 23 that are far apart from each other are fixedly connected to buttons 211. The buffer assembly includes two upper limit grooves 212 opened on the front and back of the mounting base 1. The ends of the two buttons 211 that are far apart from each other extend to the inner wall of the limit groove 212 and are slidably connected to the limit groove 212. Several second springs 213 are fixedly connected to the inner bottom wall of the mounting base 1. The top ends of the several second springs 213 are fixedly connected to the bottom surface of the fixing plate 21.

[0030] By setting up the installation mechanism 2, the elasticity of the first spring 26 and the second spring 213 is utilized. While the second spring 213 provides pressure-resistant buffering for the fuel tank shell 27, the operator can press the button 211 to drive the locking block 25 into the locking slot 28 to fix the fuel tank shell 27 in place. Compared with using a limit band to tie the fuel tank to the shock absorption device, the limiting and fixing effect of several locking blocks 25 is stronger, less susceptible to corrosion and damage from external influences, and simpler, more convenient and durable to operate.

[0031] The heat dissipation mechanism 3 includes an oil tank assembly, a drive assembly, and an air-cooling assembly. The oil tank assembly includes an oil storage cavity 31 formed on the inner wall of the oil tank housing 27. An oil outlet pipe 32 is fixedly connected to the top surface of the oil tank housing 27, and an oil inlet pipe 33 is fixedly connected to the top surface of the oil tank housing 27. The bottom end of the oil outlet pipe 32 extends to the inner bottom wall of the oil storage cavity 31 and is fixedly connected to the oil storage cavity 31. The drive assembly includes several heat dissipation slots 34 formed on the outer wall of the oil tank housing 27. Several air inlets 35 are formed on the right side of the oil tank housing 27. The inner wall of the oil tank housing 27 is fixedly connected to... The motor 36 has a first rotating shaft 37 fixedly connected to its output end. A second rotating shaft 38 is rotatably connected to the inner wall of the oil tank housing 27. A connecting groove 39 is provided on the inner wall of the oil tank housing 27. The left ends of the second rotating shaft 38 and the first rotating shaft 37 both extend to the inner wall of the connecting groove 39 and are rotatably connected to the connecting groove 39. The air-cooling assembly includes two pulleys 310 fixedly connected to the outer walls of the second rotating shaft 38 and the first rotating shaft 37. A belt 311 is sleeved between the two pulleys 310. Several fan blades 312 are fixedly connected to the outer wall of the second rotating shaft 38.

[0032] By setting up a heat dissipation mechanism 3, the second rotating shaft 38 driven by the motor 36 is used to rotate several fan blades 312, which blow external airflow into the oil tank shell 27 through the air inlet 35. After being diverted by several heat dissipation slots 34, the airflow fully contacts the oil tank shell 27. Through the principle of heat exchange, the airflow contacts the oil tank shell 27 and carries away any heat that may exist on the surface of the oil tank shell 27, thus completing the air cooling heat dissipation treatment and further improving the practicality of the device.

[0033] A specific application of this embodiment is as follows: By setting up the installation mechanism 2, the worker first fixes the installation base 1 to the tool or instrument that needs to use the oil tank through several fixing holes. Then, the worker slides the two buttons 211 inward, causing the two receiving blocks 23 to slide closer to the center within the slide groove 22, causing the locking block 25 to compress the first spring 26. At this time, the first spring 26 is in a compressed state, and the two receiving blocks 23 slide towards the center. According to the geometric distance of the rhombus, the two connecting strips 24 hinged on the receiving blocks 23 cause one end of the connecting strip 24 hinged on the slider 210 to move away from each other, causing the slider 210 to slide away from each other under the guidance and limit of the guide rod 29. Then, the oil tank shell 27 is placed in the installation base 1, and the bottom surface of the oil tank shell 27 contacts the fixing plate 21. Several locking slots 28 are aligned with the locking block 25. Then, the two buttons 211 are released. Similarly, under the elastic reset of several first springs 26, the locking block 25 is driven into the locking slot 28, and the oil tank shell 27 is moved away from the center. The bottom of the shell 27 is self-locked to the fixing plate 21. When the external environment applies downward pressure to the fuel tank shell 27, the pressure is exerted on the fixing plate 21 through the fuel tank shell 27, causing the fixing plate 21 to slide down within the mounting base 1, compressing several second springs 213. The second springs 213 provide a buffering effect against the pressure. The two buttons 211 slide within the limiting groove 212 under the action of the fixing plate 21. The buttons 211 within the limiting groove 212 also limit the elastic rise of the fixing plate 21 by the second springs 213. This achieves the effect of using the elasticity of the first spring 26 and the second spring 213 to provide pressure-resistant buffering for the fuel tank shell 27. At the same time, the operator can press the button 211 to drive the locking block 25 to lock into the locking groove 28 to fix the fuel tank shell 27 in place. Compared with using a limiting band to tie the fuel tank to the shock-absorbing device, the limiting and fixing effect of several locking blocks 25 is stronger, less susceptible to corrosion and damage from external influences, and is simple, convenient and durable to operate.

[0034] By setting up a heat dissipation mechanism 3, the drive motor 36 drives the first rotating shaft 37 to rotate, and the first rotating shaft 37 drives the lower pulley 310 to rotate. With the cooperation of the belt 311 and the two pulleys 310, the lower pulley 310 drives the upper fan blade 312 to rotate in the connecting groove 39 through the linkage of the belt 311. The upper pulley 310 then drives the second rotating shaft 38 to rotate in the oil tank outer shell 27. The second rotating shaft 38 drives several fan blades 312 to rotate, and delivers outside air into the mounting base 1 through several air inlets 35. The airflow is then blown into several heat dissipation slots 34 to fully contact the oil tank outer shell 27, so that the surface of the oil tank outer shell 27 is cooled by air through heat exchange. The heat treatment process involves extending the bottom of the oil outlet pipe 32 into the oil storage chamber 31, allowing external personnel to pump oil out of the storage chamber 31 by connecting the top of the oil outlet pipe 32 to a device such as an oil pump. The oil inlet pipe 33 facilitates the delivery of oil into the storage chamber 31 for replenishment. This process utilizes the motor 36 to drive the second rotating shaft 38, which in turn drives several fan blades 312 to rotate. External airflow is then blown into the oil tank shell 27 through the air inlet 35. After being diverted by several heat dissipation slots 34, the airflow fully contacts the oil tank shell 27. Through the principle of heat exchange, the airflow carries away any heat that may exist on the surface of the oil tank shell 27, completing the air-cooling heat dissipation process and further improving the practicality of the device.

[0035] In the description of this specification, references to terms such as "an embodiment," "example," "specific example," etc., indicate that a specific feature, structure, material, or characteristic described in connection with that embodiment or example is included in at least one embodiment or example of the present invention. In this specification, the illustrative expressions of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in one or more embodiments or examples.

[0036] The preferred embodiments of this utility model disclosed above are merely illustrative of the present utility model. These preferred embodiments do not exhaustively describe all details, nor do they limit the utility model to the specific implementations described. Clearly, many modifications and variations can be made based on the content of this specification. This specification selects and specifically describes these embodiments to better explain the principles and practical applications of this utility model, thereby enabling those skilled in the art to better understand and utilize it. This utility model is limited only by the claims and their full scope and equivalents.

Claims

1. A pressure-resistant, corrosion-resistant, and heat-dissipating oil tank structure, comprising a mounting base (1), wherein a mounting mechanism (2) and a heat dissipation mechanism (3) are provided on the mounting base (1), characterized in that: The installation mechanism (2) includes a locking component, a limiting component and a buffer component. The locking component includes a fixing plate (21) that is slidably connected to the inner wall of the mounting base (1). The top surface of the fixing plate (21) is provided with a sliding groove (22). The inner wall of the sliding groove (22) is slidably connected to two receiving blocks (23). The top surfaces of the two receiving blocks (23) are hinged with two connecting strips (24). The top surfaces of the two receiving blocks (23) are fixedly connected with two locking blocks (25). The sides of the two locking blocks (25) that are close to each other are fixedly connected with a first spring (26).

2. The pressure-resistant, corrosion-resistant, and heat-dissipating oil tank structure according to claim 1, characterized in that, The limiting component includes an oil tank shell (27) that is slidably connected to the inner wall of the mounting base (1). The oil tank shell (27) has two slots (28) on its front and back sides. The inner walls of several slots (28) are slidably connected to the outer wall of the block (25). The ends of several first springs (26) that are close to each other are fixedly connected to the inner wall of the groove (22).

3. The pressure-resistant, corrosion-resistant, and heat-dissipating oil tank structure according to claim 2, characterized in that, The inner wall of the chute (22) is fixedly connected to a guide rod (29), and the outer wall of the guide rod (29) is slidably connected to two sliders (210). The top surfaces of the two sliders (210) are hinged to several connecting strips (24), and buttons (211) are fixedly connected to the sides of the two receiving blocks (23) that are far apart from each other.

4. The pressure-resistant, corrosion-resistant, and heat-dissipating oil tank structure according to claim 3, characterized in that, The buffer assembly includes two upper limit grooves (212) on the front and back of the mounting base (1). The ends of the two buttons (211) that are far apart from each other extend to the inner wall of the limit groove (212) and are slidably connected to the limit groove (212). A number of second springs (213) are fixedly connected to the inner bottom wall of the mounting base (1). The top ends of the number of second springs (213) are fixedly connected to the bottom surface of the fixing plate (21).

5. The pressure-resistant, corrosion-resistant, and heat-dissipating oil tank structure according to claim 4, characterized in that, The heat dissipation mechanism (3) includes an oil tank assembly, a drive assembly and an air-cooling assembly. The oil tank assembly includes an oil storage cavity (31) opened on the inner wall of the oil tank shell (27). An oil outlet pipe (32) is fixedly connected to the top surface of the oil tank shell (27). An oil inlet pipe (33) is fixedly connected to the top surface of the oil tank shell (27). The bottom end of the oil outlet pipe (32) extends to the inner bottom wall of the oil storage cavity (31) and is fixedly connected to the oil storage cavity (31).

6. The pressure-resistant, corrosion-resistant, and heat-dissipating oil tank structure according to claim 5, characterized in that, The drive assembly includes several heat dissipation slots (34) that are all opened on the outer wall of the fuel tank shell (27). Several air inlets (35) are opened on the right side of the fuel tank shell (27). A motor (36) is fixedly connected to the inner wall of the fuel tank shell (27). The output end of the motor (36) is fixedly connected to a first rotating shaft (37).

7. The pressure-resistant, corrosion-resistant, and heat-dissipating oil tank structure according to claim 6, characterized in that, The inner wall of the fuel tank shell (27) is rotatably connected to a second rotating shaft (38). The inner wall of the fuel tank shell (27) is provided with a connecting groove (39). The left ends of the second rotating shaft (38) and the first rotating shaft (37) extend to the inner wall of the connecting groove (39) and are rotatably connected to the connecting groove (39).

8. The pressure-resistant, corrosion-resistant, and heat-dissipating oil tank structure according to claim 7, characterized in that, The air-cooling assembly includes two pulleys (310) fixedly connected to the outer walls of the second rotating shaft (38) and the first rotating shaft (37), with a belt (311) sleeved between the two pulleys (310), and a number of fan blades (312) fixedly connected to the outer wall of the second rotating shaft (38).

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