Compressor supporting ring composite structure with self-compensation function

By designing a composite structure for the compressor support ring, which includes a combined groove, an oil inlet, and an oil storage cotton core, the problems of thermal deformation and wear of the support ring are solved, achieving efficient lubrication and thermal deformation compensation, and extending its service life.

CN224245027UActive Publication Date: 2026-05-15YANGZHONG SANLI PETROCHEMICAL MASCH CO LTD
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
YANGZHONG SANLI PETROCHEMICAL MASCH CO LTD
Filing Date
2025-07-01
Publication Date
2026-05-15

AI Technical Summary

Technical Problem

Existing compressor support rings are prone to thermal deformation and wear under high-temperature friction environments, especially when lubrication is inadequate, leading to severe heat generation and wear.

Method used

A compressor support ring composite structure with self-compensation function was designed, including a combined groove, an oil inlet hole, a micro through hole and an annular inner chamber, combined with an oil storage cotton core and a hollow memory metal ring to achieve efficient lubrication and thermal deformation compensation.

Benefits of technology

It effectively reduces friction between the support ring and the cylinder body, improves service life, and provides compensation during thermal deformation to prevent increased friction.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of supporting rings, and discloses a compressor supporting ring composite structure with a self-compensation function, which solves the problem that the existing compressor supporting ring is easy to thermally deform and abrade, and comprises a supporting ring body, a plurality of combined grooves are arranged on the arc-shaped outer surface of the supporting ring body, and the combined grooves are arranged on the arc-shaped outer surface of the supporting ring body. A plurality of oil inlet holes are formed in the combined groove, a plurality of first micro through holes are formed in the top end of the arc-shaped outer surface of the supporting ring body, a plurality of second micro through holes are formed in the middle of the arc-shaped outer surface of the supporting ring body, and a plurality of third micro through holes are formed in the bottom end of the arc-shaped outer surface of the supporting ring body. An annular inner cavity is formed in the supporting ring body and communicates with the oil inlet hole, the first micro through hole, the second micro through hole and the third micro through hole. By means of the supporting ring composite structure, thermal deformation compensation can be achieved, meanwhile, the lubricating effect can be improved, friction is reduced, and the service life is prolonged.
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Description

Technical Field

[0001] This utility model belongs to the field of support ring technology, specifically a composite structure of compressor support ring with self-compensation function. Background Technology

[0002] The compressor support ring prevents the compressor piston from directly contacting and rubbing against the cylinder during operation, thus protecting the cylinder and piston from damage. However, the support ring operates under the high-temperature friction environment of the compressor for extended periods, making it highly susceptible to thermal deformation and breakage. This is especially true when the support ring is poorly lubricated, leading to excessive heat and wear. Therefore, this application proposes a composite structure for the compressor support ring with self-compensation to improve upon existing support rings. Utility Model Content

[0003] In view of the above situation and to overcome the defects of the prior art, this utility model provides a compressor support ring composite structure with self-compensation function, which effectively solves the problem of easy thermal deformation and wear of existing compressor support rings.

[0004] To achieve the above objectives, this utility model provides the following technical solution: a compressor support ring composite structure with self-compensation function, comprising a support ring body, wherein the arc-shaped outer surface of the support ring body is provided with a plurality of combined grooves, the interior of the combined grooves is provided with a plurality of oil inlet holes, the top end of the arc-shaped outer surface of the support ring body is provided with a plurality of micro through holes one, the middle position of the arc-shaped outer surface of the support ring body is provided with a plurality of micro through holes two, the bottom end of the arc-shaped outer surface of the support ring body is provided with a plurality of micro through holes three, and the interior of the support ring body is provided with an annular inner cavity, which is connected to the oil inlet holes, micro through holes one, micro through holes two and micro through holes three.

[0005] Preferably, the combined groove is composed of an oil storage vertical groove, a flow guiding inclined groove, and an oil inlet flared groove. The oil storage vertical groove, the flow guiding inclined groove, and the oil inlet flared groove are interconnected, and the oil inlet hole is located inside the oil storage vertical groove.

[0006] Preferably, the bottom end of the arc-shaped outer surface of the support ring body is provided with an annular groove that communicates with the oil storage vertical groove and the guide inclined groove.

[0007] Preferably, the diameter of the oil inlet hole is larger than the diameters of micro through-hole one, micro through-hole two, and micro through-hole three.

[0008] Preferably, an oil-storing cotton core is provided on the side of the annular inner cavity, and a hollow memory metal ring is provided at the center of the oil-storing cotton core. The hollow memory metal ring has a fully enclosed structure.

[0009] Preferably, an annular cap is snapped onto the top of the annular inner cavity, and the annular cap is welded to the support ring body.

[0010] Preferably, a plurality of positioning seats 1 matching the hollow memory metal ring are fixedly provided at the bottom of the annular inner cavity, and a plurality of positioning seats 2 matching the hollow memory metal ring are fixedly provided at the bottom of the annular cover.

[0011] Compared with the prior art, the beneficial effects of this utility model are:

[0012] (1) During operation, by setting up a combination groove, oil inlet hole, micro through hole one, micro through hole two, micro through hole three, and annular inner cavity, the oil storage function can be realized, thereby achieving efficient and comprehensive lubrication during the reciprocating motion of the support ring, reducing the friction between the support ring and the cylinder, and improving the service life of the support ring. Through the design of the combination groove, it can also have the function of expansion and contraction compensation. When the support ring undergoes thermal deformation, it can achieve the shrinkage compensation of the deformation amount, avoiding the situation of increased friction with the cylinder.

[0013] (2) By setting a combined groove consisting of an oil storage vertical groove, a guide inclined groove and an oil inlet flaring groove, the oil storage effect can be improved. By setting an annular groove, an auxiliary lubrication effect can be achieved. By setting an oil storage cotton core and a hollow memory metal ring, the lubricating oil can be squeezed out by thermal deformation, thus improving the lubrication effect. By setting an annular cap, the annular inner cavity can be sealed. Attached Figure Description

[0014] The accompanying drawings are provided to further understand the present invention and form part of the specification. They are used together with the embodiments of the present invention to explain the present invention and do not constitute a limitation thereof.

[0015] In the attached diagram:

[0016] Figure 1 This is a schematic diagram of the compressor support ring structure with self-compensation function according to this utility model;

[0017] Figure 2 This is a partial cross-sectional view of the compressor support ring composite structure with self-compensation function of this utility model;

[0018] Figure 3 This utility model Figure 1 A magnified view of a section at point A in the middle;

[0019] Figure 4 This is a partial structural diagram of the hollow memory metal ring of this utility model;

[0020] In the diagram: 1. Support ring body; 2. Combined groove; 3. Oil inlet hole; 4. Micro through hole one; 5. Micro through hole two; 6. Micro through hole three; 7. Annular inner chamber; 8. Oil storage vertical groove; 9. Guide inclined groove; 10. Oil inlet flaring groove; 11. Annular groove; 12. Oil storage cotton core; 13. Hollow memory metal ring; 14. Annular cap; 15. Positioning seat one; 16. Positioning seat two. Detailed Implementation

[0021] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative effort are within the protection scope of the present utility model.

[0022] Depend on Figures 1 to 4 The present invention discloses a compressor support ring composite structure with self-compensation function, comprising a support ring body 1, a plurality of combined grooves 2 formed on the arc-shaped outer surface of the support ring body 1, a plurality of oil inlet holes 3 formed inside the combined grooves 2, a plurality of micro through holes 4 formed at the top of the arc-shaped outer surface of the support ring body 1, a plurality of micro through holes 5 formed at the middle position of the arc-shaped outer surface of the support ring body 1, a plurality of micro through holes 6 formed at the bottom of the arc-shaped outer surface of the support ring body 1, and an annular inner cavity 7 formed inside the support ring body 1, the annular inner cavity 7 being connected to the oil inlet holes 3, micro through holes 4, micro through holes 5 and micro through holes 6;

[0023] During the up-and-down movement of the support ring body 1 following the piston, the lubricating oil inside the cylinder body will enter the interior of the combined groove 2. Some of the lubricating oil will enter the interior of the annular inner chamber 7 through the oil inlet 3, and the annular inner chamber 7 will realize the oil storage function. Then, it will be dispersed and discharged through the micro through hole 1 4, micro through hole 2 5 and micro through hole 3 6, thereby achieving continuous lubrication and improving the lubrication effect. The combined groove 2 can have the function of expansion and contraction compensation. When the support ring body 1 is deformed by heat, the combined groove 2 has the compensation space, thereby avoiding excessive friction between the support ring body 1 and the cylinder body.

[0024] The combined groove 2 is composed of an oil storage vertical groove 8, a flow guiding inclined groove 9 and an oil inlet flared groove 10. The oil storage vertical groove 8, the flow guiding inclined groove 9 and the oil inlet flared groove 10 are connected structures, and the oil inlet hole 3 is located inside the oil storage vertical groove 8.

[0025] The design of the oil storage vertical groove 8, the guide inclined groove 9 and the oil inlet flaring groove 10 can improve the oil storage effect. When the support ring body 1 moves down, the lubricating oil enters the interior of the guide inclined groove 9, and then continues to rise along the oil storage vertical groove 8 under the action of acceleration, so as to enter the interior of the oil inlet hole 3.

[0026] The bottom end of the arc-shaped outer surface of the support ring body 1 is provided with an annular groove 11 that communicates with the oil storage vertical groove 8 and the guide inclined groove 9, so that the lubricating oil inside the oil storage vertical groove 8 and the guide inclined groove 9 can enter the annular groove 11 to achieve full lubrication.

[0027] The diameter of the oil inlet hole 3 is larger than that of the micro through hole 1 4, micro through hole 2 5 and micro through hole 3 6, which can increase the oil inlet volume and achieve decentralized oil discharge.

[0028] An oil storage cotton core 12 is provided on the side inside the annular inner chamber 7. A hollow memory metal ring 13 is provided in the center of the oil storage cotton core 12. The hollow memory metal ring 13 is a fully enclosed structure. The oil storage cotton core 12 realizes the function of oil storage. After the hollow memory metal ring 13 is heated and deformed, it can squeeze the oil storage cotton core 12, so that the oil storage cotton core 12 releases lubricating oil or hydraulic oil.

[0029] An annular cover 14 is snapped onto the top of the annular inner chamber 7. The annular cover 14 is welded to the support ring body 1, which can seal the annular inner chamber 7.

[0030] The bottom of the annular inner chamber 7 is fixedly provided with several positioning seats 15 that match the hollow memory metal ring 13, and the bottom of the annular cover 14 is fixedly provided with several positioning seats 2 16 that match the hollow memory metal ring 13, which can realize the positioning of the hollow memory metal ring 13 and prevent the hollow memory metal ring 13 from shifting.

[0031] During operation, the system incorporates a combination of grooves, an oil inlet, three micro-through holes, and an annular inner chamber to achieve oil storage. This ensures efficient and comprehensive lubrication during the reciprocating motion of the support ring, reducing friction between the support ring and the cylinder and extending the support ring's service life. The combined groove design also provides expansion and contraction compensation, compensating for deformation caused by thermal deformation of the support ring and preventing increased friction with the cylinder. The combined groove, consisting of a vertical oil storage groove, a guide groove, and an flared oil inlet groove, enhances oil storage efficiency. The annular groove provides auxiliary lubrication, while the oil storage cotton core and hollow memory metal ring utilize thermal deformation to extrude lubricating oil, improving lubrication. Finally, the annular cap seals the annular inner chamber.

Claims

1. A compressor support ring composite structure with self-compensation function, comprising a support ring body (1), characterized in that: The support ring body (1) has several combined grooves (2) on its arc-shaped outer surface. Several oil inlet holes (3) are provided inside the combined grooves (2). Several micro through holes (4) are provided at the top of the arc-shaped outer surface of the support ring body (1). Several micro through holes (5) are provided at the middle position of the arc-shaped outer surface of the support ring body (1). Several micro through holes (6) are provided at the bottom of the arc-shaped outer surface of the support ring body (1). An annular inner cavity (7) is provided inside the support ring body (1). The annular inner cavity (7) is connected to the oil inlet holes (3), micro through holes (4), micro through holes (5) and micro through holes (6).

2. The compressor support ring composite structure with self-compensation function according to claim 1, characterized in that: The combined groove (2) consists of an oil storage vertical groove (8), a flow guiding groove (9), and an oil inlet flaring groove (10). The oil storage vertical groove (8), the flow guiding groove (9), and the oil inlet flaring groove (10) are interconnected, and the oil inlet hole (3) is located inside the oil storage vertical groove (8).

3. The compressor support ring composite structure with self-compensation function according to claim 1, characterized in that: The bottom end of the arc-shaped outer surface of the support ring body (1) is provided with an annular groove (11) that communicates with the oil storage vertical groove (8) and the guide inclined groove (9).

4. The compressor support ring composite structure with self-compensation function according to claim 1, characterized in that: The diameter of the oil inlet hole (3) is larger than that of the micro through hole one (4), micro through hole two (5) and micro through hole three (6).

5. A compressor support ring composite structure with self-compensating function according to claim 1, characterized in that: An oil-storing cotton core (12) is provided on the side inside the annular inner chamber (7), and a hollow memory metal ring (13) is provided at the center inside the oil-storing cotton core (12). The hollow memory metal ring (13) is a fully enclosed structure.

6. A compressor support ring composite structure with self-compensating function according to claim 5, characterized in that: The top of the annular inner chamber (7) is fitted with an annular cover (14), which is welded to the support ring body (1).

7. A compressor support ring composite structure with self-compensating function according to claim 6, characterized in that: The bottom of the annular inner cavity (7) is fixedly provided with several positioning seats (15) that match the hollow memory metal ring (13), and the bottom of the annular cover (14) is fixedly provided with several positioning seats (16) that match the hollow memory metal ring (13).