CN214888433U - High-stability dustproof bearing assembly - Google Patents
High-stability dustproof bearing assembly Download PDFInfo
- Publication number
- CN214888433U CN214888433U CN202021919062.XU CN202021919062U CN214888433U CN 214888433 U CN214888433 U CN 214888433U CN 202021919062 U CN202021919062 U CN 202021919062U CN 214888433 U CN214888433 U CN 214888433U
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- bearing
- aircraft bonnet
- axle core
- dead eye
- bearing assembly
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Abstract
The utility model discloses a high stability bearing assembly that prevents dust, including bearing, dead eye, left aircraft bonnet, right aircraft bonnet, data plate, packing ring, axle core, the dead eye is located the bearing center, the data plate is located left aircraft bonnet top surface, the axle core is located right aircraft bonnet box and left aircraft bonnet respectively, the axle core department of left side aircraft bonnet and right aircraft bonnet is equipped with the packing ring, the bearing passes through the dead eye and installs on the axle core. Lie in right hood box and left hood respectively through the axle center on, the bearing passes through the dead eye and installs on the axle center, can protect the bearing, avoids being equipped with the corrosion that the ball form ball often received dust debris, improves the gyration precision of bearing.
Description
Technical Field
The utility model relates to a bearing assembly technical field, in particular to dustproof bearing assembly of high stability.
Background
The self-aligning ball bearing is a bearing with spherical balls between the inner ring of two ball tracks and the outer ring of which the ball tracks are spherical surfaces. The curvature center of the outer ring raceway surface is coincident with the bearing center, so that the self-aligning ball bearing has the same self-aligning function as the self-aligning ball bearing. When the shaft and the shell are bent, the automatic adjustment can be realized, and the bearing load is not increased. The self-aligning roller bearing can bear radial load and axial load in two directions. The self-aligning ball bearing has large radial load capacity and is suitable for the conditions of heavy load and impact load. The inner diameter of the inner ring is a bearing with a taper hole, and the bearing can be directly installed. Or the adapter sleeve and the dismounting cylinder are arranged on the cylindrical shaft. The self-aligning ball bearing is suitable for bearing heavy load and impact load, precision instruments, low-noise motors, automobiles, motorcycles, metallurgy, rolling mills, mines, petroleum, papermaking, cement, sugar pressing and other industries, common machinery and the like.
When the existing bearing is used in mechanical equipment, the bearing is not protected, so that the bearing provided with the spherical balls is often easily corroded by dust and sundries, the rotary friction force of the bearing is increased, and the rotary precision of the bearing is influenced.
The utility model provides a high stability bearing assembly that prevents dust solves above-mentioned technical problem.
SUMMERY OF THE UTILITY MODEL
The utility model aims to overcome current bearing when using in mechanical equipment, owing to not protect the bearing to lead to being equipped with the bearing of ball form ball and often receiving the erosion of dust debris easily, increase the bearing gyration friction dynamics, influence this technical problem of gyration precision of bearing, provide a high stability dirt bearing subassembly in order to solve above-mentioned problem.
For realizing the purpose of the utility model, the utility model adopts the technical scheme that: including bearing, dead eye, left aircraft bonnet, right aircraft bonnet, data plate, packing ring, axle core, the dead eye is located the bearing center, the data plate is located left aircraft bonnet top surface, the axle core is located right aircraft bonnet box and left aircraft bonnet respectively, the axle core department of left side aircraft bonnet and right aircraft bonnet is equipped with the packing ring, the bearing passes through the dead eye and installs on the axle core.
Furthermore, the left hood box and the right hood are made of stainless steel.
Further, the diameter of the bearing hole is 15 mm.
Compared with the prior art, the utility model has the advantages that: lie in right hood box and left hood respectively through the axle center on, the bearing passes through the dead eye and installs on the axle center, can protect the bearing, avoids being equipped with the corrosion that the ball form ball often received dust debris, improves the gyration precision of bearing.
Drawings
Fig. 1 is a schematic structural view of a high-stability dustproof bearing assembly of the present invention;
in the drawings: 1. a bearing; 2. a bearing bore; 3. a left hood; 4. a right hood; 5. a nameplate; 6. a gasket; 7. and (4) a shaft core.
Detailed Description
In view of the deficiencies in the prior art, the technical solution of the present invention can be provided through long-term research and a large amount of practice. The technical solution in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention.
Fig. 1 is a schematic structural view of a high-stability dustproof bearing assembly of the present invention; as shown in fig. 1, the embodiment of the present invention provides a high-stability dustproof bearing assembly, which is characterized in that: including bearing 1, dead eye 2, left aircraft bonnet 3, right aircraft bonnet 4, data plate 5, packing ring 6, axle core 7, dead eye 2 is located bearing 1 center, data plate 5 is located 3 top surfaces of left aircraft bonnet, axle core 7 is located right aircraft bonnet box 4 and left aircraft bonnet 3 respectively, the axle core 7 department of left aircraft bonnet 3 and right aircraft bonnet 4 is equipped with packing ring 6, bearing 1 passes through dead eye 2 to be installed on axle core 7.
Preferably, the left hood case 3 and the right hood 4 are made of stainless steel.
Preferably, the diameter of the bearing hole 2 is 15 mm.
To sum up, the utility model provides a pair of high stability bearing subassembly that prevents dust is located right hood box and left hood respectively through the axle core, the bearing passes through the dead eye and installs on the axle core, can protect the bearing, and the bearing of avoiding being equipped with ball form ball often receives the erosion of dust debris, improves the gyration precision of bearing.
The present invention provides a high-stability dustproof bearing assembly, it should be understood that the above-mentioned embodiments are only for illustration purposes, and the technical conception and characteristics of the present invention are intended to allow the people familiar with the art to understand the contents of the present invention and to limit the scope of the present invention accordingly. All equivalent changes and modifications made according to the spirit of the present invention should be covered by the protection scope of the present invention.
Claims (3)
1. A high stability dirt bearing assembly characterized by: including bearing, dead eye, left aircraft bonnet, right aircraft bonnet, data plate, packing ring, axle core, the dead eye is located the bearing center, the data plate is located left aircraft bonnet top surface, the axle core is located right aircraft bonnet box and left aircraft bonnet respectively, the axle core department of left side aircraft bonnet and right aircraft bonnet is equipped with the packing ring, the bearing passes through the dead eye and installs on the axle core.
2. A high stability dust bearing assembly as claimed in claim 1, wherein: the left hood box and the right hood are made of stainless steel.
3. A high stability dust bearing assembly as claimed in claim 1, wherein: the diameter of the bearing hole is 15 mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021919062.XU CN214888433U (en) | 2020-09-06 | 2020-09-06 | High-stability dustproof bearing assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021919062.XU CN214888433U (en) | 2020-09-06 | 2020-09-06 | High-stability dustproof bearing assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214888433U true CN214888433U (en) | 2021-11-26 |
Family
ID=78950372
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021919062.XU Active CN214888433U (en) | 2020-09-06 | 2020-09-06 | High-stability dustproof bearing assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214888433U (en) |
-
2020
- 2020-09-06 CN CN202021919062.XU patent/CN214888433U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |