High-efficiency low-noise turbine fan blade structure

By using a one-piece molded high-efficiency, low-noise turbine blade structure, the problem of increased noise and low efficiency of traditional fan turbine blades under high-speed operation is solved, achieving efficient heat dissipation and noise control, simplifying production and extending service life.

CN223648123UActive Publication Date: 2025-12-09DONGGUAN YINGFA TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202520048820.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-01-09
Publication Date
2025-12-09
Estimated Expiration
2035-01-09

AI Technical Summary

Technical Problem

Traditional fan turbine blades become noisier and less efficient under long-term high-speed operation, and unreasonable structural design leads to reduced airflow efficiency, making it difficult to achieve both efficient heat dissipation and noise control. Low production precision also increases assembly difficulty.

Method used

It adopts a one-piece molded high-efficiency, low-noise turbine fan blade structure, including a cylindrical base, umbrella section, rotating rod, evenly spaced fan blades, and magnet positioning. The aerodynamic design is optimized to improve stability and airflow efficiency, and reduce noise.

Benefits of technology

Simplify the manufacturing process, extend service life, reduce vibration and wear, improve heat dissipation efficiency, reduce noise, and enhance user experience.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a high-efficiency low-noise turbine fan blade structure which comprises a base, the base is of a cylindrical structure, and an umbrella part is integrally formed above the base. The rotating rod is formed on the inner top surface of the umbrella part, and the end part of the rotating rod is provided with an inserting end head; the fan blades are arranged on the outer surface of the umbrella part at equal intervals; and the positioning groove is formed in the inner top surface of the base, and a magnet is inserted in the positioning groove. The fan has the advantages that the integrally-formed structural design is adopted, the production process is simplified, the production efficiency is improved, meanwhile, the service life of the fan blades can be prolonged, vibration and abrasion are reduced, the maintenance cost is reduced, in addition, air flow is smoother through the optimized pneumatic design, noise is greatly reduced while the heat dissipation efficiency is improved, and the service life of the fan is prolonged. And user experience is improved.
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Description

TECHNICAL FIELD

[0001] The utility model relates to a fan blade field, concretely relates to a high efficiency low noise turbine fan blade structure. BACKGROUND

[0002] Traditional fan turbine fan blades under long time high speed operation, often because material fatigue, airflow turbulence leads to noise increase and low efficiency, air backflow etc. Problem, limit its application in high performance heat dissipation system. Although the prior art has tried to optimize by improving the shape of the fan blade, using light weight materials, etc. However, while achieving high efficiency heat dissipation, it is often difficult to balance noise control and long-term durability.

[0003] The main problem of the fan turbine fan blade on the market at present is that the overall structure design of the fan is limited, the fan blade curvature is not optimized, which reduces the efficiency of air flow delivery and cannot meet the heat dissipation demand. At the same time, the original injection molding production method has low precision, and there is risk in the subsequent installation and fixation of the fan blade, which often needs to be retested and adjusted dynamically, further increasing the assembly difficulty. UTILITY MODEL CONTENT

[0004] The utility model discloses a high efficiency low noise turbine fan blade structure, which adopts an integrated structure design, simplifies the production process, improves the production efficiency, prolongs the service life of the fan blade, reduces vibration and wear, reduces maintenance cost, and makes air flow more smooth through optimized aerodynamic design, improves heat dissipation efficiency, greatly reduces noise, improves user experience, and details are described below.

[0005] To achieve the above purpose, the utility model provides the following technical scheme:

[0006] The utility model provides a kind of high efficiency low noise turbine fan blade structure, comprising,

[0007] Base, the base is circular cylindrical structure, umbrella portion is integrally formed on the top of the base;

[0008] Rotating rod, is formed on the inner top surface of umbrella portion, and the end of the rotating rod is provided with plug-in end head;

[0009] Fan blade, equidistantly arranged on the outer surface of umbrella portion;

[0010] Positioning groove, is formed on the inner top surface of base, and the positioning groove is inserted with magnet.

[0011] As preferred, the diameter of the bottom edge of the umbrella portion is greater than the diameter of the base.

[0012] Preferably, the fan blades consist of six blades, and the blades are positioned at an angle α, which is set to a range of 15-20°.

[0013] Preferably, the thickness of the fan blade is 0.5-1 mm.

[0014] Preferably, a support frame is formed on the inner top surface of the umbrella section.

[0015] Preferably, the end face of the plug-in terminal is chamfered, and the outer wall of the rotating rod is formed with a positioning groove.

[0016] The beneficial effects are:

[0017] The one-piece molding design simplifies the manufacturing process and improves production efficiency. It also extends the lifespan of the fan blades, reduces vibration and wear, and lowers maintenance costs. In addition, the optimized aerodynamic design makes airflow smoother, improving heat dissipation efficiency while significantly reducing noise and enhancing the user experience. Attached Figure Description

[0018] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art 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.

[0019] Figure 1 This utility model is a three-dimensional structural view. Figure 1 ;

[0020] Figure 2 This is the utility model Figure 1 A magnified view of point A in the image;

[0021] Figure 3 This utility model is a three-dimensional structural view. Figure 2 ;

[0022] Figure 4 This is a top view of the present invention;

[0023] Figure 5 This is the front view of this utility model;

[0024] Figure 6 This is a bottom view of the utility model.

[0025] The annotations in the attached figures are explained as follows:

[0026] 1. Rotating rod; 2. Base; 3. Umbrella section; 4. Fan blade; 5. Positioning groove; 6. Support frame; 7. Magnet; 8. Plug-in end. Detailed Implementation

[0027] To make the objectives, technical solutions, and advantages of this utility model clearer, the technical solutions of this utility model will be described in detail below. Obviously, the described embodiments are only a part of the embodiments of this utility model, and not all of them. Based on the embodiments of this utility model, all other implementation methods obtained by those skilled in the art without creative effort are within the scope of protection of this utility model.

[0028] See Figures 1-6 As shown, this utility model provides a high-efficiency, low-noise turbine blade 4 structure. The high-efficiency, low-noise turbine blade 4 structure provided by this utility model includes a base 2, which is a cylindrical structure that facilitates rotation. An umbrella part 3 is integrally formed on the upper part of the base 2, which is a conical structure that facilitates the arrangement and installation of the blade 4.

[0029] The rotating rod 1 is formed on the inner top surface of the umbrella part 3. The end of the rotating rod 1 is provided with a plug-in end 8. The bottom of the plug-in end extends out of the bottom surface of the base 2. The plug-in end 8 can be inserted into the corresponding mounting hole for fixing, so as to cooperate with the rotation support.

[0030] Fan blades 4 are arranged at equal intervals on the outer surface of umbrella part 3. The top edge of fan blades 4 is higher than the top surface of umbrella part 3, and the edge of fan blades 4 is chamfered to avoid collision and damage during high-speed rotation of fan blades 4, thus improving safety.

[0031] The positioning groove 5 is formed on the inner top surface of the base 2. A magnet 7 is inserted into the positioning groove 5. In order to facilitate the rotation of the fan blade 4, the magnetic drive is used for conveying, which can reduce the contact between the base 2 and other parts, reduce wear, and improve the stability of the fan blade 4 during rotation.

[0032] Preferably, the diameter of the bottom edge of the umbrella part 3 is larger than the diameter of the base 2, which allows the fan blade 4 to cover a larger area than the base 2, thereby increasing the airflow circulation speed.

[0033] Preferably, there are six fan blades 4 in total, with the upper and lower ends of the fan blades 4 overlapping each other. This structural design allows the fan blades 4 to generate greater wind pressure and air volume when rotating at high speed, enabling the fan to deliver more cool air in a shorter time. The airflow generated by the fan during rotation can be distributed more evenly, reducing airflow turbulence and eddies, thereby improving heat dissipation efficiency. The fan blades 4 are set with an inclination angle α, which is set in the range of 15-20°. After testing, the inclination angle α is preferably 16°. At the same time, combined with the leading edge shape set at the top of the fan blades 4, the smooth curvature change in the middle and the optimized trailing edge design can reduce airflow separation, improve airflow efficiency, reduce turbulence noise, and improve the stability of the equipment during operation.

[0034] Preferably, the thickness of the fan blade 4 is 0.5-1mm. Using this size setting can improve the fatigue strength and thermal stability of the fan blade 4, while reducing weight and improving overall performance.

[0035] Preferably, a support frame 6 is formed on the inner top surface of the umbrella part 3. The design of the support frame 6 can enhance the overall strength of the umbrella part 3, reduce the shaking during the operation of the fan, and ensure the stability of the fan during operation.

[0036] Preferably, the end face of the plug-in terminal 8 is chamfered, and the outer wall of the rotating rod 1 is formed with a positioning groove 5. The design of the positioning groove 5 can reduce the difficulty of the fan installation process and improve the disassembly and assembly efficiency.

[0037] With the above structure, when installing the fan blade 4, the bottom plug-in end 8 is inserted into the corresponding drive device for positioning. After insertion, the drive device drives the fan blade 4 to rotate, which causes the airflow to flow along the gap between the fan blades 4. The compression function of the fan blade 4 drives the airflow to move faster, thereby achieving the airflow delivery requirement. Due to the reasonable structural design of the fan blade 4, the fan blade 4 has good stability during rotation, which can significantly reduce the noise generated during operation, while ensuring airflow efficiency and meeting the usage requirements.

[0038] The above description is merely a specific embodiment of this utility model, but the protection scope of this utility model is not limited thereto. Any variations or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in this utility model should be included within the protection scope of this utility model. Therefore, the protection scope of this utility model should be determined by the protection scope of the claims.

Claims

1. A high-efficiency, low-noise turbine blade structure, characterized in that, include: The base (2) is a cylindrical structure, and an umbrella part (3) is integrally formed on the upper part of the base (2). A rotating rod (1) is formed on the inner top surface of the umbrella part (3), and the end of the rotating rod (1) is provided with a plug-in end (8). Fan blades (4) are arranged at equal intervals on the outer surface of the umbrella part (3); A positioning groove (5) is formed on the inner top surface of the base (2), and a magnet (7) is inserted into the positioning groove (5).

2. The high-efficiency, low-noise turbine blade (4) structure according to claim 1, characterized in that: The diameter of the bottom edge of the umbrella part (3) is greater than the diameter of the base (2).

3. The high-efficiency, low-noise turbine blade (4) structure according to claim 1, characterized in that: There are a total of six fan blades (4), and the fan blades (4) are provided with an inclination angle α, which is set in the range of 15-20°.

4. The high-efficiency, low-noise turbine blade (4) structure according to claim 1, characterized in that: The thickness of the fan blade (4) is 0.5-1 mm.

5. The high-efficiency, low-noise turbine blade (4) structure according to claim 1, characterized in that: A support frame (6) is formed on the inner top surface of the umbrella part (3).

6. The high-efficiency, low-noise turbine blade (4) structure according to claim 1, characterized in that: The end face of the plug-in end (8) is chamfered, and the outer wall of the rotating rod (1) is formed with a positioning groove (5).