Turbine structure of dust collector motor

By introducing an assembly groove and a threaded connection design for the limiting component into the turbine structure of the vacuum cleaner motor, the problem of the entire unit being scrapped after the blades are damaged is solved, enabling quick disassembly and cleaning of the blades, reducing usage costs and improving cleaning convenience.

CN223524045UActive Publication Date: 2025-11-07ANHUI ZHOUSHUI ELECTRICAL CO LTD
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Patent Information

Application Number
CN202423253886.9
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-12-28
Publication Date
2025-11-07
Estimated Expiration
2034-12-28

AI Technical Summary

Technical Problem

Existing vacuum cleaner motors are rendered unusable after the turbine blades are damaged, resulting in high operating costs and poor cleaning performance.

Method used

Design a turbine structure for a vacuum cleaner motor, which uses an assembly slot, a first limiting component, and a second limiting component. The blades are quickly installed and removed through a threaded connection, making maintenance and cleaning convenient.

Benefits of technology

It enables quick disassembly and cleaning of blades, reduces operating costs, avoids overall scrapping, and improves cleaning convenience.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a turbine structure of a dust collector motor, which comprises a turbine body arranged at the shaft end of the motor and provided with an assembly groove; the blades are slidably arranged on the inner sides of the assembling grooves; the first limiting piece is connected to the lower surface of the turbine body through a first thread part on the inner wall of the first limiting piece so as to fix one end of the blade; through the arrangement of the assembly groove, the first limiting piece and the second limiting piece, the blades can be conveniently and rapidly installed and fixed, after a single blade is damaged in the later period, disassembly and maintenance are easy, the high use cost caused by overall scrapping after the single blade is damaged is avoided, through the rapid disassembly design of the blades, disassembly, assembly and cleaning of the blades in the later period are facilitated, and the service life of the blades is prolonged. And the cleaning convenience is improved.
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Description

Technical Field

[0013]

[0001] The utility model specifically relates to a turbine structure of a vacuum cleaner motor. Background Technique

[0002] The vacuum cleaner motor is one of the core components of the vacuum cleaner, responsible for driving the turbine and generating suction force, enabling the vacuum cleaner to effectively clean dust and dirt. The turbine usually refers to a wind wheel structure on the motor, mainly used to drive the air flow.

[0003] Most of the existing vacuum cleaner motor turbines are integral, and the blades on the turbine cannot be disassembled. This results in the scrapping of the entire motor turbine after one of the blades is damaged, with a relatively high usage cost. Moreover, due to the large twist of the turbine blades, the cleaning effect on the blades with a longer axis is not good, and it is impossible to disassemble and clean and maintain the blades. For this reason, we propose a turbine structure of a vacuum cleaner motor. Content of the Utility Model

[0004] The purpose of the utility model is to provide a turbine structure of a vacuum cleaner motor to solve the problems raised in the above background technique.

[0005] To achieve the above purpose, the utility model provides the following technical solutions: A turbine structure of a vacuum cleaner motor, including:

[0006] A turbine body installed at the end of the motor shaft, and an assembly groove is provided on the turbine body;

[0007] Blades, slidably arranged inside the assembly groove;

[0008] A first limiting member, connected to the lower surface of the turbine body through a first thread portion on its inner wall to fix one end of the blade;

[0009] A second limiting member, connected to the top end of the turbine body through a second thread portion to press and fix the blade.

[0010] Preferably, the middle part of the upper surface of the turbine body protrudes upward to have a shaft cylinder, and a threaded ring block cooperating with the second limiting member is provided at the top end of the shaft cylinder.

[0011] Preferably, a guiding block is fixed at the other end of the blade, and a guiding groove cooperating with the guiding block is provided on the outer surface of the shaft cylinder.

[0012] Preferably, a threaded groove is provided on one end face of the blade, and the blade and the first limiting member are cooperated through the threaded groove. <00​​​​​

[0015] Preferably, a locking bolt is arranged inside the second limiting member and is connected to the first limiting member through threads.

[0016] Preferably, a through hole is arranged inside the first limiting member.

[0017] Compared with the prior art, the turbine structure has the advantages that:

[0018] The turbine structure has the advantages that: the turbine structure is convenient to assemble and disassemble; the turbine structure is convenient to maintain; the turbine structure is convenient to clean; the turbine structure has simple structure; and the turbine structure has high use effect. BRIEF DESCRIPTION OF DRAWINGS

[0019] Figure 1 is a structural schematic view of the turbine structure;

[0020] Figure 2 is an exploded structural schematic view of the turbine structure;

[0021] Figure 3 is a structural schematic view of the turbine structure;

[0022] Figure 4 is a structural schematic view of the turbine structure.

[0023] In the figure, 1 is a turbine body; 2 is a blade; 201 is a guide block; 202 is a threaded groove; 3 is a first limiting member; 301 is a guide plate; 302 is a through hole; 4 is a second limiting member; 5 is a locking bolt; 6 is a shaft cylinder; 7 is a threaded ring block; and 8 is an assembly groove. DETAILED DESCRIPTION

[0024] The technical solutions in the embodiments of the turbine structure will be clearly and completely described below with reference to the drawings in the embodiments of the turbine structure. Obviously, the described embodiments are only part of the embodiments of the turbine structure and not all the embodiments. Based on the embodiments of the turbine structure, all other embodiments obtained by a person of ordinary skill in the art without creative work fall within the scope of protection of the turbine structure.

[0025] Please refer to Figures 1-4 The turbine structure of the dust collector motor has the following technical scheme:

[0026] The turbine body 1 is mounted on the motor shaft end and is provided with an assembly groove 8;

[0027] The blade 2 is slidably arranged inside the assembly groove 8, facilitating quick connection of the plurality of blades 2 with the turbine body 1;

[0028] The first limiting piece 3 is connected to the lower surface of the turbine body 1 through the first threaded portion of the inner wall to fix one end of the blade 2, facilitating quick fixing of one end of the blade 2.

[0029] The second limiting piece 4 is connected to the top end of the turbine body 1 through the second threaded portion to press and fix the blade 2, facilitating quick pressing and fixing of the other end of the blade 2, so that the blade 2 is fixedly connected with the turbine body 1.

[0030] In the embodiment, preferably, the upper surface of the turbine body 1 is upwardly convex in the middle portion and has a shaft cylinder 6, and the top end of the shaft cylinder 6 is provided with a threaded ring block 7 matched with the second limiting piece 4, facilitating quick connection of the second limiting piece 4 with the turbine body 1 through the threads.

[0031] In the embodiment, preferably, the other end of the blade 2 is fixed with a guide block 201, and the outer surface of the shaft cylinder 6 is provided with a guide groove matched with the guide block 201, avoiding left and right skewing of the blade 2 and improving the assembly accuracy of the blade 2.

[0032] In the embodiment, preferably, the one end surface of the blade 2 is provided with a threaded groove 202, and the blade 2 is matched with the first limiting piece 3 through the threaded groove 202, facilitating quick locking of the one end of the blade 2 by the first limiting piece 3.

[0033] In the embodiment, preferably, the first limiting piece 3 has a "N" shape in cross section.

[0034] In the embodiment, preferably, the inner side of the first limiting piece 3 is fixed with inclined air deflectors 301, and the air deflectors 301 are circumferentially and uniformly distributed on the first limiting piece 3, facilitating flow of external natural wind, so as to improve heat dissipation of the turbine body 1 and the motor shaft.

[0035] In the embodiment, preferably, the inner side of the second limiting piece 4 is slidably provided with a locking bolt 5, and one end of the locking bolt 5 is connected with the first limiting piece 3 through threads, facilitating further close connection and fixing of the first limiting piece 3 and the second limiting piece 4 with the turbine body 1.

[0036] In the embodiment, preferably, the inner side of the first limiting piece 3 is provided with a through hole 302, facilitating air intake to improve heat dissipation.

[0037] The working principle and use process of the utility model: when using, blade 2 is inserted into the assembly groove 8 inside, at this time the guide block 201 slides into the guide groove inside, makes the first limit piece 3 and turbine body 1 cooperate through the first threaded part, at the same time the first threaded part of the first limit piece 3 cooperates with the guide block 201, can lock solid one end of blade 2, then the second limit piece 4 and threaded ring block 7 cooperate through the second threaded part, can compress the guide block 201, complete the fixing of blade 2, further can make lock bolt 5 pass through from the second limit piece 4, shaft cylinder 6 and turbine body 1 inside in turn, make lock bolt 5 and the first limit piece 3 connect through thread, can lock the second limit piece 4 and the first limit piece 3 again to turbine body 1, improve the firmness after installation.

[0038] Although the embodiments of the utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations can be made thereto without departing from the principles and spirit of the utility model, and the scope of the utility model is defined by the appended claims and their equivalents.

Claims

1. A turbine structure for a dust extractor motor, characterised in that, The utility model relates to a turbine blade fixing device for motor shaft, including: The turbine body (1) is installed to motor shaft end, and the turbine body (1) is equipped with the assembly slot (8) on it; Blade (2) is slidably arranged in the inside of assembly slot (8); First limiting piece (3) is connected to the lower surface of turbine body (1) through the first threaded portion of its inner wall to fix one end of blade (2); Second limiting piece (4) is connected to the top end of turbine body (1) through the second threaded portion to press the blade (2) solid.

2. A turbine structure for a vacuum cleaner motor according to claim 1, wherein: The upper surface of turbine body (1) is upwardly convex in the middle and has shaft cylinder (6), and the top of shaft cylinder (6) is provided with threaded ring block (7) matched with second limiting piece (4).

3. A turbine structure for a vacuum cleaner motor according to claim 2, wherein: The other end of blade (2) is fixed with guide block (201), and the outer surface of shaft cylinder (6) is provided with guide slot matched with guide block (201).

4. The turbine structure of claim 1, wherein: One end surface of blade (2) is provided with threaded groove (202), and blade (2) is matched with first limiting piece (3) through threaded groove (202).

5. The turbine structure of claim 1, wherein: The cross section of first limiting piece (3) is "N" shape.

6. The turbine structure of claim 1, wherein: The inside bottom end of first limiting piece (3) is fixed with inclined air deflector (301), and air deflector (301) is circumferentially distributed with multiple.

7. The turbine structure of claim 1, wherein: The inside of second limiting piece (4) is slidably provided with locking bolt (5), and one end of locking bolt (5) is connected with first limiting piece (3) through thread.

8. The turbine structure of claim 1, wherein: The inside of first limiting piece (3) is provided with through hole (302) penetratingly.