Compact motor

By adjusting the size of the rotor and stator inside the motor and shortening the width of the housing, the problem of increasing the full length of the motor installation is solved, and a compact design is achieved for easy installation and rapid assembly.

CN222515202UActive Publication Date: 2025-02-21DALIAN GIZHAO MOTOR TECH CO LTD
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Patent Information

Application Number
CN202420976949.4
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-05-08
Publication Date
2025-02-21
Estimated Expiration
2034-05-08

AI Technical Summary

Technical Problem

During the efficient process, existing motors lead to an increase in the installation length, resulting in a larger overall size, which makes it difficult to install or inconvenient to install in limited installation space.

Method used

By changing the size of the rotor body and the stator body inside the motor, the overall length of the fuselage is shortened, and by shortening the width of the cover, the overall length of the fuselage is further shortened, achieving a compact design.

Benefits of technology

It realizes the compact design of the motor, which is easy to install and quickly assemble, and solves the installation problems caused by limited installation space.

✦ Generated by Eureka AI based on patent content.

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  • Figure CN222515202U_ABST
    Figure CN222515202U_ABST
Patent Text Reader

Abstract

The utility model discloses a compact motor, and belongs to the technical field of motors. The utility model discloses a compact motor. The stator body is fixedly connected in the machine body; the rotor body is rotationally connected in the stator body; the driving shaft is fixedly connected to the rotor body; the outer diameter of the stator ranges from 145 mm to 380 mm. The number of the stator grooves is 24-72. The outer diameter of the rotor ranges from 75 mm to 260 mm. The number of the rotor grooves is 28 to 60; according to the utility model, the overall length of the motor body can be effectively shortened by changing the sizes of the rotor body and the stator body in the motor, and meanwhile, the overall length of the motor body is further shortened by shortening the width of the housing, so that the compact design of the motor is realized, and the motor is more convenient for workers to quickly assemble through compact size installation.
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Description

Technical Field

[0001] The utility model relates to the technical field of electric motors, in particular to a compact electric motor. Background Art

[0002] As the efficiency of electric motors continues to improve, the total length of the motor installation will inevitably increase, causing the overall size of the motor to continue to grow. During installation, workers may encounter problems such as difficulty or inconvenience in installation due to limited installation space. Utility Model Content

[0003] The purpose of the utility model is to solve the problems raised in the above background technology and to provide a compact motor.

[0004] In order to achieve the above purpose, the utility model adopts the following technical solutions:

[0005] A compact electric motor comprising:

[0006] body;

[0007] The stator body is fixedly connected to the fuselage;

[0008] A rotor body, rotatably connected to the stator body;

[0009] The driving shaft is fixedly connected to the rotor body.

[0010] Preferably, the outer diameter of the stator is 145-380 mm.

[0011] Furthermore, the number of the stator slots is 24-72.

[0012] Furthermore, the outer diameter of the rotor is 75-260 mm.

[0013] Furthermore, the number of the rotor slots is 28-60.

[0014] Preferably, the inner diameter of the rotor is 22-85 mm.

[0015] Preferably, a fan is rotatably connected to the fuselage, and the fan is fixedly connected to the driving shaft.

[0016] Furthermore, a cover is fixedly connected to the fuselage, and the fan is placed in the cover.

[0017] Furthermore, the cover shell has a size of 80-100 mm.

[0018] Compared with the prior art, the utility model provides a compact motor with the following beneficial effects:

[0019] The parts not involved in the device are the same as the existing technology or can be implemented by the existing technology. The utility model can effectively shorten the overall length of the motor body by changing the size of the rotor body and the stator body inside the motor. At the same time, by shortening the width of the cover, the overall length of the motor body is further shortened, realizing a compact design of the motor. Through compact size installation, it is more convenient for the staff to quickly assemble the motor. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 A schematic diagram of the structure of a compact motor proposed by the utility model Figure 1 ;

[0021] Figure 2 A schematic diagram of the structure of a compact motor proposed by the utility model Figure 2 ;

[0022] Figure 3 An exploded diagram of a compact electric motor proposed by the utility model;

[0023] Figure 4 A cross-sectional view of a compact motor proposed by the utility model;

[0024] Figure 5 This is a schematic diagram of the connection between the stator body and the rotor body in a compact motor proposed by the utility model;

[0025] Figure 6 The utility model is a schematic structural diagram of a stator body and a rotor body in a compact motor.

[0026] In the figure: 1, fuselage; 101, cover; 1011, fan; 2, drive shaft; 3, rotor body; 4, stator body. DETAILED DESCRIPTION

[0027] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.

[0028] Embodiment 1:

[0029] Reference Figure 1-Figure 6 , a compact electric motor comprising:

[0030] Body 1;

[0031] The stator body 4 is fixedly connected to the fuselage 1;

[0032] The rotor body 3 is rotatably connected to the stator body 4;

[0033] The driving shaft 2 is fixedly connected to the rotor body 3 .

[0034] The stator outer diameter is 145-380mm.

[0035] The number of stator slots is 24-72.

[0036] Reference Figure 4-Figure 6 By expanding the stator slot area, the working hours can be effectively shortened and production can be facilitated.

[0037] The outer diameter of the rotor is 75-260mm.

[0038] Reference Figure 4-Figure 6 By effectively increasing the outer diameter of the rotor body 3, the length of the fuselage 1 is shortened while ensuring power.

[0039] The number of rotor slots is 28-60.

[0040] Reference Figure 4-Figure 6 By effectively reducing the number of slots in the rotor body 3 and increasing the slot area of ​​the rotor body 3, the loss of the rotor body 3 and the drift load loss are reduced.

[0041] The inner diameter of the rotor is 22-85mm.

[0042] A fan 1011 is rotatably connected to the body 1 , and the fan 1011 is fixedly connected to the driving shaft 2 .

[0043] A cover 101 is fixedly connected to the body 1 , and a fan 1011 is disposed in the cover 101 .

[0044] Reference Figure 2-Figure 3 The cover 101 is provided with cooling windows, and the temperature rise of the fuselage 1 can be effectively reduced by setting multiple groups of cooling windows.

[0045] Reference Figure 2-Figure 3 An inspection window is provided at the center of the cover 101, and the size of the inspection window is 10 mm. By reducing the size of the inspection window, the safety hazard of the motor fan cover inspection window being too large and posing a risk of contact to a person is solved.

[0046] The size of the housing 101 is 90 mm.

[0047] By shortening the width of the cover 101, the overall size of the fuselage 1 is further reduced.

[0048] The utility model can effectively shorten the overall length of the body (1) by changing the size of the rotor body (3) and the stator body (4) inside the motor, and at the same time, by shortening the width of the cover shell (101), the overall length of the body (1) is further shortened, thereby realizing a compact design of the motor.

[0049] The above is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent substitutions or changes within the technical scope disclosed by the present invention according to the technical solution and inventive concept of the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A compact electric motor, characterized in that: include: Body (1); A stator body (4) is fixedly connected to the fuselage (1); A rotor body (3) rotatably connected to a stator body (4); A drive shaft (2) is fixedly connected to the rotor body (3); The stator body (4) has an outer diameter of 145-380 mm; The number of stator slots on the stator body (4) is 24-72; The outer diameter of the rotor body (3) is 75-260 mm.

2. A compact electric motor according to claim 1, characterized in that: The number of rotor slots on the rotor body (3) is 28-60.

3. A compact electric motor according to claim 1, characterized in that: The inner diameter of the rotor body (3) is 22-85 mm.

4. A compact electric motor according to claim 1, characterized in that: A fan (1011) is rotatably connected to the body (1), and the fan (1011) and the drive shaft (2) are fixedly connected.

5. A compact electric motor according to claim 4, characterized in that: A casing (101) is fixedly connected to the body (1), and the fan (1011) is disposed in the casing (101).

6. A compact electric motor according to claim 5, characterized in that: The size of the housing (101) is 80-100 mm.