A bushing connection structure for a gas compressor bracket

By incorporating buffer pads and annular grooves into the gas compressor bracket, the bushing is protected and the rotation of the annular plate is stabilized, thus solving the problem of easy bushing damage and improving the service life of the bushing and the stability of the annular plate.

CN224432747UActive Publication Date: 2026-06-30DAYE SANHUAN ELECTRIC APPLIANCE FACTORY

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
DAYE SANHUAN ELECTRIC APPLIANCE FACTORY
Filing Date
2025-08-29
Publication Date
2026-06-30

AI Technical Summary

Technical Problem

In the prior art, the bushing of the gas compressor bracket is easily damaged at the contact point between the mounting bolts and the bushing, resulting in a reduced service life of the bushing.

Method used

The first and second buffer pads are installed inside the assembly to protect the first and second bushing bodies respectively. The design of the annular groove and the annular plate guides the rotation direction of the annular plate and reduces the risk of tilting.

Benefits of technology

This improved the service life of the bushing, stabilized the rotation process of the annular plate, and reduced bushing damage and annular plate tilting.

✦ Generated by Eureka AI based on patent content.

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  • Figure CN224432747U_ABST
    Figure CN224432747U_ABST
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Abstract

This utility model discloses a bushing connection structure for a gas compressor bracket, relating to the field of compressor bracket technology. The utility model includes an assembly with bolts internally engaged. Two first buffer pads and two second buffer pads are placed around the bolts. A first bushing body is placed on one side of the first buffer pads, and a second bushing body is placed on one side of the second buffer pads. A compressor body is located on one side of the assembly, and a bracket body is fixedly fitted to one side of the compressor body. This utility model, through the use of first and second buffer pads, protects the first bushing body through the first buffer pads and the second bushing body through the second buffer pads, reducing the risk of damage to the first and second bushing bodies during assembly and improving their service life.
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Description

Technical Field

[0001] This utility model belongs to the field of compressor brackets, specifically, it relates to a bushing connection structure for a gas compressor bracket. Background Technology

[0002] The air conditioner compressor bracket is an important component that supports the air conditioner compressor. Depending on the functional requirements, it will connect many components at the same time in the design, and the assembly of these components is extremely critical.

[0003] Patent application CN109751226A discloses a bushing connection structure for an air conditioner compressor bracket. Paragraph 0016 of the specification discloses: a compressor bracket, an assembly, assembly bolts, and a bushing; the air conditioner compressor bracket includes a first assembly through hole and a second assembly threaded hole; the assembly is installed between the first assembly through hole and the second assembly threaded hole; the bushing includes a T-shaped structure integrally formed by a large-diameter circular plate and a small-diameter cylinder.

[0004] However, in practical applications, the compressor bracket needs to be assembled on the upper side of the assembly using a bushing. Since there is no protective mechanism between the mounting bolts and the bushing, the mounting bolts can easily damage the contact point with the bushing, which will reduce the service life of the bushing.

[0005] To address these shortcomings, a bushing connection structure for a gas compressor bracket is proposed. Utility Model Content

[0006] The technical problem to be solved by this utility model is to overcome the shortcomings of the prior art and provide a bushing connection structure for a gas compressor bracket.

[0007] To solve the above-mentioned technical problems, the basic concept of the technical solution adopted by this utility model is as follows:

[0008] A bushing connection structure for a gas compressor bracket includes an assembly, wherein a bolt is internally engaged with the assembly, and two first buffer pads and two second buffer pads are placed around the bolts. A first bushing body is placed on one side of the first buffer pads, and a second bushing body is placed on one side of the second buffer pads.

[0009] The compressor body is located on one side of the assembly. A bracket body is fixedly fitted on one side of the compressor body. One end of the bracket body is sleeved around the bolt. One side of the first bushing body and the second bushing body are both attached to one side of the bracket body.

[0010] Optionally, one end of the assembly has a first through hole, the bolt is located inside the first through hole, and one end of the bolt is threaded with a first nut.

[0011] Optionally, two threaded rods are fixedly fitted on one side of the first buffer pad, and two second through holes are opened on one side of the second buffer pad, with the threaded rods located inside the second through holes.

[0012] Optionally, two annular grooves are formed on one side of the second buffer pad, and an annular plate is rotatably fitted inside the annular grooves. The cross-sections of the annular plate and the annular grooves are both T-shaped.

[0013] Optionally, a second nut is fixedly fitted on one side of the annular plate, and the second nut is threaded onto the circumference of one end of the threaded rod.

[0014] Optionally, a third through hole is provided at both ends of the bracket body, and the bolt is located inside the third through hole.

[0015] Optionally, one side of the first nut is attached to one side of one of the second buffer pads, and the first buffer pad and the second buffer pad are sleeved around the bolt.

[0016] Optionally, one end of the support body is located between the first buffer pad and the second buffer pad, and the other end of the support body is located between the first bushing body and the second bushing body.

[0017] By adopting the above technical solution, the present invention has the following beneficial effects compared with the prior art. Of course, any product implementing the present invention does not necessarily need to achieve all of the following advantages at the same time:

[0018] The first and second buffer pads are designed to protect the first bushing body through the first buffer pad and the second bushing body through the second buffer pad, thereby reducing the risk of damage to the first and second bushing bodies during assembly and improving their service life.

[0019] The annular groove is designed to allow one end of the annular plate to rotate inside the groove under the action of the operator. The groove also guides the rotation direction of the annular plate, reducing the problem of tilting during rotation and improving its performance.

[0020] The specific embodiments of this utility model will be described in further detail below with reference to the accompanying drawings. Attached Figure Description

[0021] The accompanying drawings described below are merely some embodiments. Those skilled in the art can obtain other drawings based on these drawings without any creative effort. In the drawings:

[0022] Figure 1 This is a three-dimensional structural diagram of an embodiment of the present utility model;

[0023] Figure 2 This is a bottom view of an embodiment of the present invention.

[0024] Figure 3 This is a schematic diagram of a bolt structure according to an embodiment of the present invention;

[0025] Figure 4 This is a schematic diagram of the structure of the first buffer pad and the second buffer pad according to an embodiment of the present invention.

[0026] The attached diagram lists the components represented by each number as follows:

[0027] Assembly 100, bolt 101, first nut 102, bracket body 103, compressor body 104, first buffer pad 105, threaded rod 106, first bushing body 107, second buffer pad 108, annular groove 109, annular plate 110, second nut 111, second through hole 112, second bushing body 113.

[0028] It should be noted that these accompanying drawings and textual descriptions are not intended to limit the scope of the present invention in any way, but rather to illustrate the concept of the present invention to those skilled in the art by referring to specific embodiments. Detailed Implementation

[0029] The present invention will now be described in further detail with reference to the accompanying drawings.

[0030] Please see Figure 1-4 As shown, this embodiment provides a bushing connection structure for a gas compressor bracket, including an assembly 100. The assembly 100 is internally fitted with a bolt 101. Two first buffer pads 105 and two second buffer pads 108 are placed around the bolt 101. A first bushing body 107 is placed on one side of the first buffer pad 105, and a second bushing body 113 is placed on one side of the second buffer pad 108.

[0031] The compressor body 104 is located on one side of the assembly 100. A bracket body 103 is fixedly fitted on one side of the compressor body 104. One end of the bracket body 103 is sleeved on the periphery of the bolt 101. One side of the first bushing body 107 and the second bushing body 113 are both attached to one side of the bracket body 103.

[0032] Working principle:

[0033] First, place the first buffer pad 105 on one side of the assembly 100, then place the first bushing body 107 on one side of the first buffer pad 105, then place one end of the bracket body 103 on one side of the first bushing body 107, then place the second bushing body 113 on one side of the bracket body 103, then place the second buffer pad 108 on one side of the second bushing body 113, then place the bolt 101 inside the first buffer pad 105, the first bushing body 107, the second buffer pad 108, the second bushing body 113, and the assembly 100, and fix the bracket body 103 to one end of the assembly 100 with the bolt 101, thereby completing the assembly of the compressor body 104.

[0034] The first buffer pad 105 and the second buffer pad 108 are provided to protect the first bushing body 107 through the first buffer pad 105 and the second bushing body 113 through the second buffer pad 108, thereby reducing the problem of damage to the first bushing body 107 and the second bushing body 113 during assembly and improving the service life of the first bushing body 107 and the second bushing body 113.

[0035] To make the sliding process of the annular plate 110 on the second buffer pad 108 side of this embodiment more stable, the following structure is used for improvement, such as... Figure 1-4 As shown, in this embodiment, one end of the assembly 100 has a first through hole, and a bolt 101 is located inside the first through hole. One end of the bolt 101 is threaded with a first nut 102. Two threaded rods 106 are fixedly fitted to one side of the first buffer pad 105. Two second through holes 112 are opened on one side of the second buffer pad 108, and the threaded rods 106 are located inside the second through holes 112. Two annular grooves 109 are opened on one side of the second buffer pad 108, and an annular plate 110 is rotatably fitted inside the annular grooves 109. The cross-sections of the annular plate 110 and the annular grooves 109 are both T-shaped. A second nut 111 is fixedly fitted on one side of the 0. The second nut 111 is threaded onto the periphery of one end of the threaded rod 106. Both ends of the bracket body 103 are provided with third through holes. The bolt 101 is located inside the third through hole. One side of the first nut 102 is attached to one side of one of the second buffer pads 108. The first buffer pad 105 and the second buffer pad 108 are sleeved on the periphery of the bolt 101. One end of the bracket body 103 is located between the first buffer pad 105 and the second buffer pad 108. One end of the bracket body 103 is located between the first bushing body 107 and the second bushing body 113.

[0036] In this embodiment, firstly, rotate the second nut 111. The second nut 111 drives one end of the annular plate 110 to rotate inside the annular groove 109. The second nut 111 is removed from one end of the threaded rod 106, and the positioning of one end of the threaded rod 106 is released by the second nut 111. Then, remove the bolt 101 from the inside of the first bushing body 107, the first buffer pad 105, the first bushing body 107, and the second buffer pad 108. Finally, remove the bracket body 103 from one end of the assembly 100.

[0037] The annular groove 109 is provided so that one end of the annular plate 110 can rotate inside the annular groove 109 under the action of the operator, and the annular groove 109 guides the rotation direction of the annular plate 110, reducing the problem of the annular plate 110 tilting during rotation and improving the problem of the annular plate 110 tilting during rotation.

[0038] This utility model is not limited to the above-described embodiments. Anyone should know that structural changes made under the guidance of this utility model, and any technical solutions that are the same as or similar to this utility model, fall within the protection scope of this utility model. Technical aspects, shapes, and structures not described in detail in this utility model are all publicly known technologies.

Claims

1. A bushing connection structure of a gas compressor bracket, characterized by, include: The assembly (100) has a bolt (101) internally engaged. Two first buffer pads (105) and two second buffer pads (108) are placed around the bolt (101). A first bushing body (107) is placed on one side of the first buffer pad (105), and a second bushing body (113) is placed on one side of the second buffer pad (108). The compressor body (104) is located on one side of the assembly (100). A bracket body (103) is fixedly fitted on one side of the compressor body (104). One end of the bracket body (103) is sleeved on the periphery of the bolt (101). One side of the first bushing body (107) and the second bushing body (113) are both attached to one side of the bracket body (103).

2. A gas compressor support liner connection structure according to claim 1, wherein The assembly (100) has a first through hole at one end, the bolt (101) is located inside the first through hole, and a first nut (102) is threaded onto one end of the bolt (101).

3. A gas compressor support liner connection structure according to claim 1, wherein Two threaded rods (106) are fixedly fitted on one side of the first buffer pad (105), and two second through holes (112) are opened on one side of the second buffer pad (108), with the threaded rods (106) located inside the second through holes (112).

4. A gas compressor support liner connection structure according to claim 3, wherein Two annular grooves (109) are provided on one side of the second buffer pad (108). An annular plate (110) is rotatably fitted inside the annular groove (109). The cross-sections of the annular plate (110) and the annular groove (109) are both T-shaped.

5. A gas compressor support liner connection structure according to claim 4, wherein A second nut (111) is fixedly fitted on one side of the annular plate (110), and the second nut (111) is threaded onto the circumference of one end of the threaded rod (106).

6. A gas compressor support liner connection structure according to claim 1, wherein Both ends of the bracket body (103) are provided with third through holes, and the bolt (101) is located inside the third through hole.

7. A gas compressor support liner connection structure according to claim 2, wherein One side of the first nut (102) is attached to one side of one of the second buffer pads (108), and the first buffer pad (105) and the second buffer pad (108) are sleeved on the periphery of the bolt (101).

8. The liner connection of a gas compressor support of claim 1, wherein, One end of the support body (103) is located between the first buffer pad (105) and the second buffer pad (108), and the other end of the support body (103) is located between the first bushing body (107) and the second bushing body (113).