Thrust disc structure

By setting spherical bearing shells and tile shells, copper tile anti-wear pads and temperature measurement holes in the thrust disk structure, the problem of easy breakage of the thrust disk is solved, achieving stronger load-bearing capacity, stable operation and extended service life of the equipment.

CN223258571UActive Publication Date: 2025-08-22YONGDENG QILIANSHAN CEMENT CO LTD
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Patent Information

Application Number
CN202422591576.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-10-25
Publication Date
2025-08-22
Estimated Expiration
2034-10-25

AI Technical Summary

Technical Problem

Due to the unreasonable setting position of the existing thrust disc, the small axial thrust force it bears, and it is easy to break under larger axial compression, resulting in unstable equipment.

Method used

The thrust disc is set at one end of the main shaft of the main and passive bracket wheels close to the bracket wheels, combined with the spherical bearing shell and the tile shell structure, anti-wear pads are provided at both ends of the copper tile, and a temperature measurement hole is set on the inner edge of the spherical bearing shell, and a heat dissipation hole is provided on the surface of the tile shell.

Benefits of technology

It enhances the load-bearing capacity of the thrust disc, avoids breakage, ensures smooth operation of the equipment, can monitor temperature more accurately and effectively dissipate heat, and extends the service life of the equipment.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a thrust disc structure which comprises a thrust disc, a tile shell and a spherical bearing bush, the thrust disc is arranged at one end of a main shaft of a driving riding wheel and a driven riding wheel close to the riding wheels, the tile shell is arranged outside the main shaft of the driving riding wheel and the driven riding wheel, and the spherical bearing bush is arranged between the inner surface of the tile shell and the main shaft of the driving riding wheel and the driven riding wheel. A copper tile is further arranged on the inner surface of the spherical tile, and anti-abrasion pads are arranged at the two ends of the copper tile. The thrust disc solves the problem that due to the fact that an existing thrust disc bears small axial thrust due to the fact that the arrangement position is unreasonable, the thrust disc is prone to breakage when subjected to large axial extrusion.
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Description

Technical Field

[0001] The utility model relates to the field of equipment for rotary kilns, in particular to a thrust plate structure. Background Art

[0002] When the cement kiln is running, the roller shaft often bears axial force. For this reason, a thrust plate needs to be set in the axial direction of the roller shaft. This can prevent the roller shaft from having excessive axial displacement and ensure the reliability and stability of the equipment. However, the existing thrust plate is set at the shaft head, so the axial thrust it bears is small, and it is prone to breakage. Therefore, the position of the existing thrust plate needs to be improved. Utility Model Content

[0003] The purpose of the utility model is to provide a thrust plate structure to solve the problem that the existing thrust plate is easily broken when subjected to large axial extrusion due to its unreasonable position and small axial thrust.

[0004] In order to solve the above-mentioned technical problems, the utility model adopts the following technical solutions: a thrust plate structure, including a thrust plate, a bearing shell and a spherical bearing shell. The thrust plate is installed on the end of the main shaft of the main and passive rollers close to the rollers. The bearing shell is arranged outside the main shaft of the main and passive rollers. The spherical bearing shell is arranged between the inner surface of the bearing shell and the main shaft of the main and passive rollers. The inner surface of the spherical bearing shell is also provided with a copper shell, and anti-wear pads are provided at both ends of the copper shell.

[0005] The thrust plate in this solution is located at the shaft shoulder, which can withstand 2 to 3 times greater axial thrust than the prior art in which the thrust plate is located at the shaft head. When the supporting wheel moves axially, the thrust plate originally located at the shaft head is easily broken, causing a kiln shutdown accident. However, the thrust plate at the shaft shoulder in this solution is not prone to breakage.

[0006] As a further preferred embodiment of the present invention, a gap is left between the inner end surface of the outer end of the thrust plate and the inner end surface of the inner end of the shoe shell, and the width of the gap is ≥10 mm.

[0007] Such a gap is more conducive to smooth rotation.

[0008] As a further preferred embodiment of the present invention, the total gap between the anti-wear pad located at the inner end of the copper shoe and both sides of the thrust plate is 6±0.5 mm.

[0009] As a further preferred embodiment of the present invention, a temperature measuring hole is drilled at the lower portion of the inner edge of the spherical bearing.

[0010] The temperature measuring hole set at this location can more accurately reflect the temperature of the inner surface of the spherical bearing.

[0011] As a further preferred embodiment of the present invention, the temperature measuring hole has a diameter of 9 mm, a tapping size of M10*1, and a depth of 35 mm.

[0012] As a further preference of the present invention, a 20*20mm packing sealing structure is provided at the main shaft mounting openings of the main and passive supporting wheels of the tile shell.

[0013] As a further preferred embodiment of the present invention, heat dissipation channels are evenly opened on the surface of the tile shell, and a circulating fan is provided outside the channel opening of one of the heat dissipation channels.

[0014] This is more conducive to heat dissipation and can better extend the service life of the equipment.

[0015] Compared with the prior art, the present invention can achieve at least one of the following beneficial effects:

[0016] 1. The thrust plate at the shaft shoulder in this solution is not prone to breakage.

[0017] 2. The accurate setting of the gap in the structure can ensure the smooth operation of the equipment.

[0018] 3. The temperature measuring hole can more accurately reflect the temperature of the inner surface of the spherical bearing.

[0019] 4. It is more conducive to heat dissipation and can better extend the service life of the equipment. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 It is a structural diagram of the present utility model. DETAILED DESCRIPTION

[0021] To make the purpose, technical solutions, and advantages of the embodiments of the present invention more clear, the technical solutions of the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings of the embodiments of the present invention. Obviously, the described embodiments are only some embodiments of the present invention, not all embodiments. Generally, the components of the embodiments of the present invention described and shown in the drawings herein can be arranged and designed in various different configurations.

[0022] Therefore, the following detailed description of the embodiments of the present invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but rather merely represents selected embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative effort are within the scope of protection of the present invention.

[0023] It should be noted that, in the absence of conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0024] It should be noted that similar reference numerals and letters denote similar items in the following drawings, and therefore, once an item is defined in one drawing, it does not require further definition or explanation in subsequent drawings.

[0025] In the description of the present invention, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," and the like, indicating orientations or positional relationships, are based on the orientations or positional relationships shown in the accompanying drawings, or are the orientations or positional relationships in which the product of the present invention is typically placed when in use, or are the orientations or positional relationships commonly understood by those skilled in the art. These terms are intended solely to facilitate the description of the present invention and to simplify the description, and are not intended to indicate or imply that the device or element referred to must have a specific orientation, be constructed, or operate in a specific orientation. Therefore, they should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and the like are used solely to distinguish descriptions and should not be construed as indicating or implying relative importance.

[0026] It should also be noted that, in the description of this utility model, unless otherwise expressly specified or limited, the terms "disposed," "installed," "connected," and "connected" should be understood in a broad sense. For example, they can refer to fixed connections, detachable connections, or integral connections; mechanical connections, electrical connections; direct connections, indirect connections through an intermediate medium, and internal connections between two components. Those skilled in the art will understand the specific meanings of the above terms in this utility model based on the specific circumstances. Specific embodiment 1:

[0028] Figure 1 A thrust plate structure is shown, including a thrust plate 1, a bearing shell 2 and a spherical bearing 3. The thrust plate 1 is installed on the main shaft 4 of the main and passive rollers close to the rollers, the bearing shell 2 is arranged outside the main shaft 4 of the main and passive rollers, and the spherical bearing 3 is arranged between the inner surface of the bearing shell 2 and the main shaft 4 of the main and passive rollers. The inner surface of the spherical bearing 3 is also provided with a copper bushing, and anti-wear pads 5 are provided at both ends of the copper bushing.

[0029] The thrust plate in this solution is located at the shaft shoulder, which can withstand 2 to 3 times greater axial thrust than the prior art in which the thrust plate is located at the shaft head. When the supporting wheel moves axially, the thrust plate originally located at the shaft head is easily broken, causing a kiln shutdown accident. However, the thrust plate at the shaft shoulder in this solution is not prone to breakage. Specific embodiment 2:

[0031] This embodiment further illustrates the thrust plate 1 based on the specific embodiment 1. A gap is left between the inner end surface of the outer end of the thrust plate 1 and the inner end surface of the inner end of the shoe shell 2. The width of the gap is ≥10 mm.

[0032] Such a gap is more conducive to smooth rotation. Specific embodiment 3:

[0034] This embodiment further illustrates the copper bushing based on the specific embodiment 1. The total gap between the anti-wear pad located at the inner end of the copper bushing and both sides of the thrust plate 1 is 6±0.5 mm. Specific embodiment 4:

[0036] This embodiment further illustrates the spherical bearing 3 based on the specific embodiment 1. A temperature measuring hole 6 is drilled at the lower portion of the inner edge of the spherical bearing 3 .

[0037] The temperature measuring hole set at this location can more accurately reflect the temperature of the inner surface of the spherical bearing. Specific embodiment 5:

[0039] This embodiment further illustrates the temperature measuring hole 6 based on the specific embodiment 4. The temperature measuring hole 6 has a diameter of 9 mm, a tapping thread M10*1, and a depth of 35 mm. Specific embodiment 6:

[0041] This embodiment further illustrates the tile shell 2 on the basis of the specific embodiment 1. A 20*20mm packing sealing structure is provided at the mounting opening of the main shaft 4 of the active and passive supporting wheels of the tile shell 2. Specific embodiment 7:

[0043] This embodiment further illustrates the tile shell 2 based on the specific embodiment 1. The surface of the tile shell 2 is evenly provided with heat dissipation channels 7, and a circulating fan is provided outside the channel opening of one of the heat dissipation channels 7.

[0044] This is more conducive to heat dissipation and can better extend the service life of the equipment.

[0045] Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art can still modify the technical solutions described in the aforementioned embodiments, or make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.

Claims

1. A thrust plate structure, characterized in that: The invention comprises a thrust plate (1), a bearing shell (2) and a spherical bearing shell (3), wherein the thrust plate (1) is mounted on one end of the main shaft (4) of the main and passive rollers close to the rollers, the bearing shell (2) is arranged outside the main shaft (4) of the main and passive rollers, and the spherical bearing shell (3) is arranged between the inner surface of the bearing shell (2) and the main shaft (4) of the main and passive rollers, and the inner surface of the spherical bearing shell (3) is further provided with a copper shell, and both ends of the copper shell are provided with anti-wear pads (5).

2. The thrust plate structure according to claim 1, characterized in that: A gap is left between the inner end surface of the outer end of the thrust plate (1) and the inner end surface of the inner end of the shell (2), and the width of the gap is ≥10 mm.

3. The thrust plate structure according to claim 1, characterized in that: The total clearance between the anti-wear pad located at the inner end of the copper washer and both sides of the thrust plate (1) is 6±0.5 mm.

4. The thrust plate structure according to claim 1, characterized in that: A temperature measuring hole (6) is drilled at the lower portion of the inner edge of the spherical bearing bush (3).

5. The thrust plate structure according to claim 4, characterized in that: The temperature measuring hole (6) has a diameter of 9 mm, a tapping size of M10*1, and a depth of 35 mm.

6. The thrust plate structure according to claim 1, characterized in that: A 20*20mm packing sealing structure is provided at the main shaft (4) mounting openings of the main and passive supporting wheels of the tile shell (2).

7. The thrust plate structure according to claim 1, characterized in that: The surface of the tile shell (2) is evenly provided with heat dissipation channels (7), and a circulating fan is provided outside the channel opening of one of the heat dissipation channels (7).