CROSS-REFERENCE TO RELATED APPLICATION
This application claims the priority benefit of Taiwan application serial no. 112126885, filed on Jul. 19, 2023. The entirety of the above-mentioned patent application is hereby incorporated by reference herein and made a part of this specification.
BACKGROUND
Technical Field
The invention relates to a heat-dissipation fan, and in particular, to an axial-flow heat-dissipation fan.
Description of Related Art
The axial-flow fan has a simple structure and has the characteristics of large air volume and low static pressure, so it is widely used in cooling fans or ventilation fans for personal computers and servers. In order to improve the air supply characteristics of the axial-flow fan to reduce noise and other optimization purposes, the number and structure of the blades are often adjusted, or various designs and tests are carried out on the structure of the air flow.
For example, when the axial-flow fan is used for heat dissipation, its obvious disadvantage is that the pressure of the flow field is too small. Therefore, how to improve this disadvantage is really a problem that relevant technical personnel need to solve.
SUMMARY
The present invention provides an axial-flow heat-dissipation fan, which adjusts the pressure, direction and concentration of the airflow generated by the blades by adjusting the surface roughness of the front surface and the rare surface of each of the blades.
The axial-flow heat dissipation fan of the present invention includes a frame, a hub, and a plurality of blades. The frame has an air inlet and an air outlet. The hub is rotatably arranged in the frame. The blades disposed at side of the hub respectively and rotate along with the hub. Each of the blades has a front surface facing toward the air inlet and a rear surface facing toward the air outlet. A surface roughness of the front surface is different from a surface roughness of the rear surface.
Based on the above, the axial-flow heat-dissipation fan adjusts the surface roughness of the upper blade surface (the front surface) and the lower blade surface (the rear surface) of the blades, and then reaches the effect of adjusting the pressure on the blade surface. Among them, the pressure difference or flow velocity difference between the front surface and the rear surface of the blades can be adjusted according to the premise of not changing the shape of the blades, so as to meet the demand or adjust according to the current situation of the flow field. Furthermore, the designer can also adjust the roughness of the rear surface of the blades according to the distribution of the airflow on the surface of the blades, and according to the direction and concentration of the required airflow, so as to meet the heat dissipation requirements.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a schematic diagram of the axial-flow heat-dissipation fan according to an embodiment of the present invention.
FIG. 2 is a simple side view of the axial-flow heat-dissipation fan of FIG. 1.
FIG. 3 is a partial bottom view of the axial-flow heat-dissipation fan in FIG. 1.
FIG. 4 is a schematic structural view of the rough area of FIG. 3.
FIG. 5 is a simplified schematic diagram of a fluid boundary layer.
FIG. 6 is a partial bottom view of the axial-flow heat-dissipation fan of another embodiment of the present invention.
FIG. 7 is a schematic diagram of the axial-flow heat-dissipation fan of another embodiment of the present invention.
DESCRIPTION OF THE EMBODIMENTS
FIG. 1 is a schematic diagram of an axial-flow heat-dissipation fan according to an embodiment of the present invention. FIG. 2 is a simple side view of the axial-flow heat-dissipation fan of FIG. 1. FIG. 3 is a partial bottom view of the axial-flow heat-dissipation fan in FIG. 1. Referring to FIG. 1 to FIG. 3 at the same time, in the embodiment, the axial-flow heat-dissipation fan 100 is suitable for electronic devices, such as system fans or CPU cooling fans installed in a desktop computer, and includes a frame 110, a hub 120 and a plurality of blades 130. The frame 110 has an air inlet 111 and an air outlet 112. The plurality of blades 130 are disposed at side of the hub 120 respectively, and the hub 120 is rotatably disposed in the frame 110 and located between the air inlet 111 and the air outlet 11. Then, through the connection with the motor, the hub 120 is driven to rotate along the direction RD with the axis AX as a reference, and at the same time, the blades 130 are driven to rotate along the direction RD with the hub 120 to generate airflow entering the frame 110 from the air inlet 111 and leaving the frame 110 from the air outlet 112.
In details, as shown in FIG. 2 and FIG. 3, each of the blades 130 has a front surface S1 and a rear surface S2 facing each other. The front surface S1 faces toward the air inlet 111, the rear surface S2 faces toward the air outlet 112. Furthermore, each of the blades 130 also has a leading edge E1 and a trailing edge E2, which are respectively adjacent to the front surface S1 and the rear surface S2. When the blades 130 is rotated with the hub 120, the leading edge E1 is located on a windward side and the trailing edge E2 is located on a leeward side.
FIG. 4 is a schematic structural view of the rough area of FIG. 3, which is a gold photomicrograph of the rough area 131. Referring to FIG. 3 and FIG. 4 at the same time, more importantly, the blades 130 of the embodiment also has the rough area 131 located on the rear surface S2 and occupying part of the rear surface S2, whose range extends radially with the blades 130 to extend from the hub 120 to an end edge ES of the blades 130. Herein, the end edge ES can be regarded as the farthest side edge of the rear surface S2 relative to the hub 120. In other words, as shown in FIG. 3, for the blades 130, except for the hub 120, the leading edge E1, the end edge ES and the trailing edge E2 are adjacent in sequence. In the embodiment, the rough area 131 has etched microstructures, and has a plurality of etching particles 131a. And the roughness of the rough area 131 is defined by the etching depth of the etched microstructures of 10 μm to 45 μm and the etching particles 131a of 15 to 150 per centimeter. The above-mentioned etching is for the mold forming the blades 130, and the corresponding pattern (the rough area 131) can be successfully formed on the blades 130 after forming the etching pattern on the mold.
FIG. 5 is a simplified schematic diagram of a fluid boundary layer. Referring to FIG. 5, the formation principle of vortex is briefly described below. Generally speaking, the boundary layer formed by the fluid and the surface of the object will be affected by the roughness of the surface of the object. As shown on the right side of FIG. 5, when the fluid pressure increases, the fluid at an inner edge of the boundary layer will gradually generate a reverse flow field E due to the viscous resistance on the surface of the object, thereby causing the separation of the fluid from the surface of the object. And this phenomenon of fluid separation is the main cause of vortex.
Here, boundary layer equation group:
when the boundary condition y=0, then u=v=0, and when y=∞, then u=U(x). Where u, v represent the velocity components of the fluid in the x, y direction, U(x) represents the flow velocity, μ represents the dynamic viscosity (dynamic viscosity coefficient), ρ represents the fluid density, the direction along the wall of the object is the x-axis, and the direction perpendicular to the wall is the y-axis.
Based on the separation phenomenon of the boundary layer shown in FIG. 5, the rough area 131 shown in FIG. 3 in the embodiment can provide a basis for the designer to adjust the air flow.
Referring to FIG. 2 and FIG. 3 again, in the embodiment, in order to improve the airflow pressure difference between the front surface S1 and the rear surface S2, the surface roughness of the front surface S1 in the embodiment is different from the surface roughness of the rear surface S2. And especially make the surface roughness of the rear surface S2 larger than the surface roughness of the front surface S1. Therefore, in the embodiment, the rough area 131 needs to be formed on the rear surface S2, while the front surface S1 is kept smooth to achieve the effect of increasing the air outlet pressure of the axial-flow heat-dissipation fan 100. Certainly, in another unillustrated embodiment, the rough area 131 mentioned above can also be set on the front surface S1 and the rear surface S2. However, if the premise of increasing the air outlet pressure is still desired, the surface roughness of the rear surface S2 must still be greater than that of the front surface S1.
FIG. 6 is a partial bottom view of the axial-flow heat-dissipation fan of another embodiment of the present invention. Referring to FIG. 6, different from the foregoing, the axial-flow heat-dissipation fan of the embodiment is intended to reduce noise. Therefore, a rough area 132 is formed on the rear surface S2, and the rough area 132 extends from the hub 120 along the trailing edge E2 to the end edge ES. For the blades 130, the airflow has been separated from the rear surface S2 when it reaches the trailing edge E2, but due to the difference in airflow pressure, turbulent flow will be generated on the rear surface S2, resulting in obvious aerodynamic noise. Accordingly, in the embodiment, through the arrangement of the through area 132, the degree of confusion of the turbulent flow is further increased, and the turbulent flow is further canceled out to achieve the effect of reducing noise.
FIG. 7 is a schematic diagram of the axial-flow heat-dissipation fan of another embodiment of the present invention. Referring to FIG. 7, the blades 130 of the embodiment combines the features of the embodiments of FIG. 3 and FIG. 6 described above. That is to say, in the case that the rough area 132 can effectively reduce the turbulence effect, the combination of the rough area 131 can increase the air outlet pressure effect. That is, the rough area 131, 132 is adjacent to each other on the rear surface S2 of the blades 130. Among them, the roughness of the rough area 132 must be greater than or equal to the roughness of the rough area 131 in order to control the fluid separation point or provide a better control flow field.
According to above-mentioned, the present invention also provides the design/manufacturing method about the axial-flow heat-dissipation fan according to above-mentioned embodiment. That is to say, in the design stage, the blade shape of the blades in the initial design is analyzed to check the separation state of the airflow and the blades, and then the design roughness area at a specific place of the blades is increased, so as to control (adjust) the direction and concentration of the outlet airflow. Furthermore, as shown in the aforementioned embodiments of FIG. 3, FIG. 6 or FIG. 7, the position and range of the rough area on the surface of the blades 130 are adjusted according to the specific requirements of the axial-flow heat-dissipation fan.
In summary, in the above-mentioned embodiment of the present invention, the axial-flow heat-dissipation fan adjusts the surface roughness of the upper blade surface (the front surface) and the lower blade surface (the rear surface) of the blades, and then reaches the effect of adjusting the pressure on the blade surface. Among them, the pressure difference or flow velocity difference between the front surface and the rear surface of the blades can be adjusted according to the premise of not changing the shape of the blades, so as to meet the demand or adjust according to the current situation of the flow field. Furthermore, the designer can also adjust the roughness of the rear surface of the blades according to the distribution of the airflow on the surface of the blades, and according to the direction and concentration of the required airflow, so as to meet the heat dissipation requirements.
Patent Application
20250027502
