Miniature inner rotor turbofan
By adopting a combined structure of booster sleeve, inner rotor, turbine blade, shaft core, MQ magnet and silicon steel sheet in the micro inner rotor turbo fan, the existing micro inner rotor turbo fan in terms of rotation stability, noise and failure rate is solved, achieving more efficient heat dissipation and longer service life.
Patent Information
- Application Number
- CN202323321120.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2023-12-07
- Publication Date
- 2025-03-14
- Estimated Expiration
- 2033-12-07
AI Technical Summary
The existing micro-internal rotor turbo fans have problems with low orbiting head, high noise and high failure rate, and have high machining accuracy requirements, making it difficult to efficiently dissipate heat in small spaces.
A miniature inner rotor turbofan is designed, which adopts a combined structure of a booster sleeve, an inner rotor, a turbine blade, a shaft core, an MQ magnet and a silicon steel sheet. The turbine blades are movably connected to the insulator through the shaft core. The inner rotor is made of neodymium iron boron, and the magnet and a silicon steel sheet are distributed in an annular array to improve rotational stability and heat dissipation efficiency.
Through this design, the rotational stability and heat dissipation efficiency of the miniature internal rotor turbofan are significantly improved, noise is reduced, and failure rate is also controlled, extending service life.
Smart Images
Figure CN222615612U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of chassis accessories, in particular to a micro inner rotor turbo fan. Background Art
[0002] Turbofan, also known as centrifugal fan, is commonly used in the field of personal computer cooling. Small centrifugal fans are usually called turbofans. The gas flow direction of turbofans is perpendicular to the rotating shaft, while the gas flow direction of common axial fans is parallel to the rotating shaft. Compared with traditional cooling fans, centrifugal fans can output larger air volume in a smaller space, thereby improving the cooling effect. They are still often used in high-performance graphics cards, especially public version graphics card radiators.
[0003] Currently, most of the micro inner rotor turbo fans are driven by a single rotor, which has a low orbital head. In addition, the processing accuracy of the centrifugal fan blades is higher than that of ordinary fans. When the impeller is dusty or runs at high speed, the noise is also louder. Utility Model Content
[0004] The utility model aims to provide a miniature inner rotor turbofan to solve the problems raised in the background technology in view of the deficiencies of the prior art.
[0005] To achieve the above-mentioned objectives, the present invention provides the following technical solutions: a miniature inner rotor turbofan, comprising a turbofan, a booster sleeve is provided on one side of the turbofan, an upper cover is provided inside the booster sleeve, an inner rotor is provided inside the turbofan, turbine blades are provided inside the inner rotor, an axis core is provided inside the turbine blades, MQ magnets are provided on the outside of the turbine blades, silicon steel sheets are provided on the outside of the MQ magnets, an upper insulator is provided on one side of the turbine blades, and a lower insulator is provided on the other side of the turbine blades.
[0006] As a preferred technical solution of the utility model, the silicon steel sheets are arranged in a plurality of groups, and the silicon steel sheets are distributed in a ring array.
[0007] As a preferred technical solution of the present utility model, the turbine fan blades are three turbine blades, and the turbine blades are arranged in a ring shape with equal angles.
[0008] As a preferred technical solution of the utility model, the turbine blades are movably connected to the lower insulator through the shaft core.
[0009] As a preferred technical solution of the present utility model, the material of the inner rotor is neodymium iron boron material.
[0010] As a preferred technical solution of the utility model, the MQ magnets are provided in a plurality and are distributed in a ring array.
[0011] The beneficial effects of the utility model are:
[0012] The micro inner rotor turbofan is provided with several groups by setting the number of silicon steel sheets, which are distributed in a ring array, so as to better provide power and improve the stability of the inner rotor rotation; the turbine blades are three turbine blades, which are arranged in a ring with equal angles, can effectively drive the flow of internal liquid, and cooperate with the externally arranged booster sleeve to pressurize the internal liquid flow; the turbine blades are movably connected with the lower insulator and the lower insulator through the shaft core, and the turbine blades can play a driving role through the inner rotor, so as to reduce the failure rate; the material of the inner rotor is neodymium iron boron material, which is a permanent magnet, so as to ensure that the inner rotor can achieve the driving effect, so that the micro inner rotor turbofan is more efficient and has a longer service life; the number of MQ magnets is provided, which are distributed in a ring array, so as to better provide power and improve the stability of the inner rotor rotation with the silicon steel sheets. BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Figure 1 This is a three-dimensional schematic diagram of a miniature inner rotor turbo fan of the utility model;
[0014] Figure 2 This is a three-dimensional schematic diagram of a miniature inner rotor turbo fan of the utility model;
[0015] Figure 3 It is a side view schematic diagram of the miniature inner rotor turbofan of the present utility model;
[0016] Figure 4 For this utility model Figure 3 Schematic diagram of the cross-sectional view at AA.
[0017] In the figure: 1. Mounting plate; 2. Mounting hole; 3. Outer rotor; 4. Outer rotor blades; 5. Inner rotor connecting shaft; 6. Holes; 7. Limiting holes; 8. Upper insulator; 9. Lower insulator; 10. Inner rotor. DETAILED DESCRIPTION
[0018] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0019] See also Figure 1-4In the present embodiment: a micro inner rotor turbofan comprises a turbofan 1, a booster sleeve 2 is arranged on one side of the turbofan 1, such arrangement can pressurize the internal liquid, an upper cover 3 is arranged inside the booster sleeve 2, such arrangement is convenient for the installation and removal of the booster sleeve 2, an inner rotor 10 is arranged inside the turbofan 1, a turbine blade 4 is arranged inside the inner rotor 10, an axis core 5 is arranged inside the turbine blade 4, an MQ magnet 6 is arranged on the outside of the turbine blade 4, a silicon steel sheet 7 is arranged on the outside of the MQ magnet 6, an upper insulator 8 is arranged on one side of the turbine blade 4, and a lower insulator 9 is arranged on the other side of the turbine blade 4.
[0020] In this embodiment, the number of silicon steel sheets 7 is arranged in several groups, and the silicon steel sheets 7 are distributed in a ring array, so that the arrangement can better provide power and improve the stability of the rotation of the inner rotor 10; the turbine blades 4 are three turbine blades, and the turbine blades are arranged in a ring with equal angles. Such an arrangement can effectively drive the flow of the internal liquid, and cooperate with the externally arranged booster sleeve 2 to pressurize the internal liquid flow; the turbine blades 4 are movably connected with the lower insulator 9 and the lower insulator 9 through the shaft core 5, so that the turbine blades 4 can play a driving role through the inner rotor 10, reducing the occurrence rate of failures; the material of the inner rotor 10 is neodymium iron boron material, so that neodymium iron boron is arranged as a permanent magnet, ensuring that the inner rotor 10 can achieve the driving effect, making the micro inner rotor turbofan more efficient and extending the service life; the number of MQ magnets 6 is arranged in several groups, and the MQ magnets 6 are distributed in a ring array, so that the arrangement cooperates with the silicon steel sheets 7 to better provide power and improve the stability of the rotation of the inner rotor 10.
[0021] Working Principle: When using, please refer to Figure 1-4 When in use, several groups are arranged by the number of silicon steel sheets 7, and the silicon steel sheets 7 are distributed in a ring array, so that the arrangement can better provide power and improve the stability of the rotation of the inner rotor 10; the turbine blades 4 are three turbine blades, and the turbine blades are arranged at equal angles in a ring. Such an arrangement can effectively drive the flow of the internal liquid, and cooperate with the externally arranged booster sleeve 2 to pressurize the internal liquid flow; the turbine blades 4 are movably connected with the lower insulator 9 and the lower insulator 9 through the shaft core 5, so that the turbine blades 4 can play a driving role through the inner rotor 10, reducing the occurrence rate of failures; the material of the inner rotor 10 is neodymium iron boron material, so that neodymium iron boron is set as a permanent magnet to ensure that the inner rotor 10 can achieve the driving effect, making the micro inner rotor turbofan more efficient and extending the service life; the number of MQ magnets 6 is arranged, and the MQ magnets 6 are distributed in a ring array, so that the arrangement cooperates with the silicon steel sheets 7 to better provide power and improve the stability of the rotation of the inner rotor 10.
[0022] The above are only preferred specific implementation methods of the utility model, but the protection scope of the utility model is not limited to this. Any technician familiar with the technical field within the technical scope disclosed by the utility model, who makes equivalent replacements or changes based on the technical scheme and utility model concept of the utility model, should be covered by the protection scope of the utility model.
Claims
1. A miniature inner rotor turbofan, comprising a turbofan (1), characterized in that: A booster sleeve (2) is provided on one side of the turbofan (1), an upper cover (3) is provided inside the booster sleeve (2), an inner rotor (10) is provided inside the turbofan (1), a turbine blade (4) is provided inside the inner rotor (10), an axis core (5) is provided inside the turbine blade (4), an MQ magnet (6) is provided on the outside of the turbine blade (4), a silicon steel sheet (7) is provided on the outside of the MQ magnet (6), an upper insulator (8) is provided on one side of the turbine blade (4), and a lower insulator (9) is provided on the other side of the turbine blade (4).
2. A micro inner rotor turbofan according to claim 1, characterized in that: The silicon steel sheets (7) are arranged in a plurality of groups, and the silicon steel sheets (7) are distributed in a ring array.
3. The micro inner rotor turbo fan according to claim 1, characterized in that: The turbine blades (4) are three turbine blades, and the turbine blades are arranged in a ring shape at equal angles.
4. The micro inner rotor turbo fan according to claim 1, characterized in that: The turbine blade (4) is movably connected to the lower insulator (9) through the shaft core (5).
5. The micro inner rotor turbo fan according to claim 1, characterized in that: The inner rotor (10) is made of neodymium iron boron material.
6. The micro inner rotor turbo fan according to claim 1, characterized in that: A plurality of the MQ magnets (6) are provided, and the MQ magnets (6) are distributed in a ring array.