Compression-resistant flying wing type radiator radiating assembly

Abstract

The utility model discloses a compression-resistant flying wing type radiator radiating assembly, which comprises a high-pressure-resistant washing mechanism, the high-pressure-resistant washing mechanism comprises a substrate, one side of the substrate is fixedly connected with a fin, the surface of the fin is provided with a corrugated groove, the surface of the substrate is provided with a microgroove, the microgroove is arranged on the surface of one side of the substrate, and the surface of the other side of the substrate is provided with a water inlet. The corrugated grooves are formed in the surfaces of the two sides of the fin, and the microgrooves are formed in one side of the fin. According to the utility model, through the arrangement of the high-pressure-resistant washing mechanism, when the fins are formed and the tool nose retreats, a microgroove with a stress relieving effect is formed on the basal plane of the substrate, and a release effect is formed after a shoveling (stacking process); in addition, due to the fact that the corrugated grooves are formed in the surfaces of the fins, the fins are provided with tiny corrugations, the positive effects on the strength of the fins and resonance elimination are achieved, and when the heat dissipation assembly is subjected to high-pressure washing, the structural integrity and the service life can be guaranteed.

Description

Technical Field

[0001] The utility model relates to the technical field of flying wing fin heat dissipation components, and specifically relates to a compressive flying wing type radiator heat dissipation component. Background Art

[0002] The flying wing fin heat dissipation component is a specially designed radiator, usually used in electronic devices or other applications that require effective heat dissipation; the characteristic of this heat dissipation component is that its fin design is similar to the airfoil of an airplane, and the shape of this fin helps to increase air fluidity and heat exchange efficiency; the flying wing fin heat dissipation component can effectively conduct heat from a heat source (such as a processor) to the fin, and dissipate the heat to the surrounding environment through the fin.

[0003] When some electronic devices are operating, they will generate heat. In order to quickly export this heat, fin heat dissipation components are generally used, and some use flying wing fin heat dissipation components. After the flying wing fin heat dissipation component is used for a long time, its surface will be covered with dust, affecting the heat dissipation performance. Most of them use high-pressure flushing treatment. However, most of the current flying wing fin heat dissipation components are relatively fragile, and using the high-pressure flushing method may damage them, while other cleaning methods are relatively troublesome and have poor practicability. At the same time, when the fins of its heat dissipation component are in long-term use, due to the thin fin thickness, if the pressure is relatively high during use, they cannot effectively resist pressure, reducing the actual use effect and service life; therefore, in order to solve the above problems, a compressive flying wing type radiator heat dissipation component is hereby proposed. Summary of the Utility Model

[0004] The utility model mainly solves the technical problems existing in the above-mentioned prior art, and provides a compressive flying wing type radiator heat dissipation component.

[0005] To achieve the above purpose, the utility model provides the following technical solution: A compressive flying wing type radiator heat dissipation component, including an anti-high-pressure flushing mechanism. The anti-high-pressure flushing mechanism includes a substrate, one side of the substrate is fixedly connected with fins, the surface of the fins is provided with corrugated grooves, the surface of the substrate is provided with micro-grooves, the micro-grooves are opened on one side surface of the substrate, and each fin surface has corrugated grooves. The corrugated grooves can increase the strength of the fins.

[0006] Preferably, the corrugated grooves are opened on both side surfaces of the fins, and the micro-grooves are opened on one side of the fins. This fin is formed by shaving, so when the tip of the knife is pushed back, micro-grooves will be formed.

[0007] Preferably, a plurality of fins are provided, linearly distributed on one side of the substrate, and each fin is provided with a micro-groove on one side, so a plurality of micro-grooves are also provided.

[0008] Preferably, the thickness of the fin is 0.4 mm, the width of the fin is 40 mm, and the height of the fin is 18 mm. The fin is formed by shaving, so the middle part of the fin is slightly curved.

[0009] Preferably, wire grooves are formed on the surface of the fin. The wire grooves are formed on the left and right surfaces of the fin. Through the arrangement of the grooving, the root of the fin is slightly larger than the top of the fin microscopically.

[0010] Preferably, hollow grooves are formed inside the substrate. A plurality of hollow grooves are formed. Through the arrangement of the hollow grooves, the weight of the substrate will be slightly reduced, which is convenient for carrying and processing.

[0011] Compared with the prior art, the beneficial effects of the present utility model are as follows:

[0012] 1. Through the arrangement of the high-pressure flushing resistance mechanism of the present utility model, when the fin is formed, the retraction of the tip of the tool will form a micro-groove with a stress relief effect on the base surface of the substrate. After scraping (accumulation process), a release effect will be formed; this will play a certain role in eliminating the resonance of the natural frequency. In addition, through the arrangement of the corrugated grooves on the surface of the fin, the fin has minute corrugations, which also plays a positive role in the strength of the fin and the elimination of resonance, so that the heat dissipation component can ensure the structural integrity and service life during high-pressure flushing.

[0013] 2. Through the arrangement of the wire grooves of the present utility model, the root of the fin is slightly larger than the top of the fin microscopically, and the whole fin and the substrate are integrally cut and formed without secondary processing and connection. In this way, the fin and the substrate can be more firmly connected, providing stronger support for the fin, increasing the structural stability and anti-bending ability of the whole fin, and the fin will not be damaged during high-pressure flushing. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] The drawings are used to provide a further understanding of the present utility model, and constitute a part of the specification. They are used together with the embodiments of the present utility model to explain the present utility model, and do not constitute a limitation to the present utility model. In the drawings:

[0015] Figure 1 is the structural schematic diagram of the first front view as a whole of the present utility model;

[0016] Figure 2 is the structural schematic diagram of the second front view as a whole of the present utility model;

[0017] Figure 3 is the structural schematic diagram of the side view as a whole of the present utility model.

[0018] In the figure: 1. Substrate; 2. Fin; 3. Corrugated groove; 4. Micro-groove; 5. Wire groove; 6. Hollow groove. Detailed implementation mode

[0019] The following will clearly and completely describe the technical solutions in the embodiments of the present utility model with reference to the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0020] Please refer to Figures 1-3 , a compressive wing - type radiator heat dissipation component, including an anti - high - pressure flushing mechanism. The anti - high - pressure flushing mechanism includes a substrate 1. One side of the substrate 1 is fixedly connected with fins 2. Corrugated grooves 3 are formed on the surface of the fins 2. Micro - grooves 4 are formed on the surface of the substrate 1. The micro - grooves 4 are formed on one side surface of the substrate 1. The corrugated grooves 3 are formed on both side surfaces of the fins 2. The micro - grooves 4 are formed on one side of the fins 2. There are several fins 2, which are linearly distributed on one side of the substrate 1. The thickness of the fins 2 is 0.4 mm, the width of the fins 2 is 40 mm, and the height of the fins 2 is 18 mm. When the fins 2 are formed, the retraction of the tool tip will form a micro - groove 4 with a stress - relieving effect on the base surface of the substrate 1. After planing (accumulation process), a release effect is formed; this will play a certain role in eliminating the resonance of the natural frequency. In addition, through the setting of the corrugated grooves 3 on the surface of the fins 2, the fins 2 have minute corrugations, which also play a positive role in the strength of the fins 2 and eliminating resonance, so that when the heat dissipation component is subjected to high - pressure flushing, the integrity of the structure and the service life can be ensured.

[0021] Preferably, in this embodiment, the fins 2 are integrally cut and formed, and have better compressive resistance during use.

[0022] In one aspect of this embodiment, through the setting of the wire grooves 5, the root of the fins 2 is slightly larger than the top of the fins 2 microscopically, so that the fins 2 can be more firmly connected to the substrate 1, providing stronger support for the fins 2, increasing the structural stability and anti - bending ability of the entire fins 2, and preventing damage to the fins 2 during high - pressure flushing.

[0023] In one aspect of this embodiment, through the setting of the hollow grooves 6, the substrate 1 adopts a hollow design, which can significantly reduce the overall weight, and using less material can reduce the production cost. And in some cases, the hollow structure can allow air circulation, thus helping to dissipate heat better.

[0024] Working principle of the present utility model: When the flywing fin heat dissipation component capable of high-pressure flushing is in use, the heat dissipation component is vertically fixed on the machine that needs heat dissipation for heat dissipation treatment. Since when the fin 2 is formed, the tip of the tool retracts, a micro-groove 4 with a stress-relieving effect will be formed on the base surface of the substrate 1. After scraping (accumulation process), a releasing effect will be formed; this will play a certain role in eliminating the resonance of the natural frequency. In addition, through the arrangement of the corrugated grooves 3 on the surface of the fin 2, the fin 2 has minute corrugations, which also plays a positive role in the strength of the fin 2 and eliminating resonance. And through the arrangement of the wire grooves 5, the root of the fin 2 is slightly larger than the top of the fin 2 microscopically, so that the fin 2 can be more firmly connected to the substrate 1, providing stronger support for the fin 2 and increasing the structural stability and bending resistance of the entire fin 2. After the heat dissipation component has been used for a long time, its surface will be covered with dust and needs to be cleaned regularly. The heat dissipation component can be cleaned by using high-pressure flushing, and the high-pressure flushing will not cause damage to the fin 2.

[0025] Finally, it should be noted that the above are only the preferred embodiments of the present utility model and are not used to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present utility model shall be included within the protection scope of the present utility model.

Claims

1. A compression-resistant flying wing type radiator heat dissipation component, including a high-pressure flushing resistance mechanism, characterized in that: The anti-high-pressure flushing mechanism includes a substrate (1), one side of the substrate (1) is fixedly connected with fins (2), the surface of the fins (2) is provided with corrugated grooves (3), the surface of the substrate (1) is provided with micro-grooves (4), and the micro-grooves (4) are opened on one side surface of the substrate (1).

2. The heat dissipation component of a compressive wing-type radiator according to claim 1, wherein: The corrugated grooves (3) are opened on both side surfaces of the fins (2), and the micro-grooves (4) are opened on one side of the fins (2).

3. The heat dissipation component of a compressive flying wing type radiator according to claim 1, characterized in that: A plurality of the fins (2) are provided and are linearly distributed on one side of the substrate (1).

4. The heat dissipation assembly of the compression-resistant flying wing type radiator according to claim 1, wherein: The thickness of the fins (2) is 0.4 mm, the width of the fins (2) is 40 mm, and the height of the fins (2) is 18 mm.

5. The heat dissipation component of the compression-resistant flying wing type radiator according to claim 1, wherein: The surface of the fins (2) is provided with wire grooves (5), and the wire grooves (5) are opened on the left and right side surfaces of the fins (2).

6. The heat dissipation component of a compression-resistant flying wing type radiator according to claim 1, characterized in that: A hollow groove (6) is opened inside the substrate (1), and a plurality of the hollow grooves (6) are provided.

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