Gas compressor rotor seat easy to disassemble, assemble and maintain
By introducing buffer components, self-lubricating components, and fixing components into the gas compressor rotor housing, the problems of easy damage, poor lubrication, and complex installation of traditional rotor housings are solved, achieving higher stability, performance, and convenient maintenance.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-11
- Publication Date
- 2026-04-10
AI Technical Summary
Traditional gas compressor rotor housings lack a buffer mechanism, which makes parts easily damaged, results in poor lubrication, is complex to install, affects stability and reliability, and is inconvenient to maintain.
The design incorporates a buffer assembly, a self-lubricating assembly, and a fixing assembly, including a compression ring, a camshaft rotor disc, an oil inlet for the self-lubricating assembly, a sealing cap, and mounting sleeves and limit blocks for the fixing assembly, achieving buffering, lubrication, and stable installation.
It improves the stability and performance of gas compressors, reduces vibration and wear, simplifies the installation and disassembly process, and enhances maintenance convenience.
Smart Images

Figure CN224107417U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to a compressor technical field especially relates to an easy dismounting and maintenance's gas compressor rotor seat. BACKGROUND
[0002] The gas compressor rotor seat is an important component for supporting and fixing the rotor, and ensures the stable and efficient rotation of the rotor in the compressor. It completes the compression work of the gas together with the rotor through cooperation.
[0003] However, the traditional gas compressor rotor seat lacks effective buffering mechanism, so that the internal parts of the compressor are easily damaged by impact during the compression process. At the same time, the lubrication effect is poor, which aggravates the wear and tear inside the compressor. In addition, the installation process of the traditional gas compressor rotor seat is relatively complex, which leads to low stability and reliability. It is not only inconvenient for subsequent maintenance operation, but also affects the overall performance and use convenience of the gas compressor. UTILITY MODEL CONTENTS
[0004] The utility model discloses a gas compressor rotor seat easy to dismount and maintain, to solve the problem in the prior art.
[0005] In order to achieve the above purpose, the utility model provides the following technical scheme: it includes rotor seat main part, the rotor seat main part top is provided with the shell, a plurality of fixed components are arranged between the rotor seat main part and the shell, the buffer assembly is arranged in the rotor seat main part, a pair of self-lubricating components are symmetrically arranged in the rotor seat main part.
[0006] As preferred in the utility model, the buffer assembly includes a compression ring arranged in the rotor seat main body, a camshaft rotor disc is arranged in the compression ring, a rotor shaft is arranged on the camshaft rotor disc, a compression rod is arranged on one side of the compression ring, an open slot is formed on one side of the rotor seat main body, the compression rod is slidably arranged in the open slot, an air inlet is formed on one side of the rotor seat main body, and an air outlet is formed on the side of the rotor seat main body away from the air inlet.
[0007] As preferred in the utility model, the compression rod is provided with a mounting block one on the side away from the compression ring, a piston rod is arranged on the side of the mounting block one away from the compression rod, a piston one is arranged on the side of the piston rod away from the mounting block one, a mounting block two corresponding to the mounting block one is arranged on the inner wall of the rotor seat main body on one side of the open slot, an oil storage cylinder is arranged on one side of the mounting block two, the piston one is located in the oil storage cylinder, and a spring one is arranged between the mounting block one and the mounting block two.
[0008] As the utility model is preferred, the self-lubricating assembly includes the oil inlet arranged on the rotor seat body, the sealing cover is spirally sleeved outside the oil inlet, the restraint groove is formed in the one side of the rotor seat body, the restraint groove is connected with the oil inlet through the oil groove, the mounting block three is arranged on the inner wall of the rotor seat body on the one side of the restraint groove, the guide column guide sleeve is arranged on the one side of the mounting block three, the movable guide column is slidably arranged in the guide column guide sleeve, the extrusion block is arranged on the side of the movable guide column away from the guide column guide sleeve, the flexible spring is arranged between the extrusion block and the mounting block three, and the sealing ring corresponding to the extrusive block is arranged on the one side of the restraint groove.
[0009] As the utility model is preferred, the fixing assembly includes the mounting plate one arranged on the one side of the rotor seat body, the mounting sleeve is arranged on the mounting plate one, the disc is slidably arranged in the mounting sleeve, the return spring is arranged between the inner top surface of the mounting sleeve and the disc, the plug rod is arranged in the disc, the plug rod penetrates the mounting sleeve, the knob is arranged on the end of the plug rod away from the disc, and the pair of limit blocks is symmetrically arranged on the bottom of the knob.
[0010] As the utility model is preferred, the fixing plate corresponding to the mounting sleeve is arranged on the one side of the shell, the long hole is formed in the fixing plate, and the limit slot corresponding to the limit block is formed in the fixing plate on the two sides of the long hole.
[0011] Compared with the prior art, the above technical scheme of the utility model has the following beneficial technical effects:
[0012] The utility model discloses a buffer assembly is set up, and the cooperation of compression ring and camshaft rotor disc realizes the effective compression of gas, improves the gas pressure, and spring one effectively buffers the impact force that compression rod received, protects the internal parts of compressor from being damaged, and the movement of piston rod and piston one in the oil storage cylinder generates the damping effect, reduces the spring rebound speed, reduces the vibration, improves the stability of gas compressor operation, makes the output of high-pressure gas more stable, improves the performance and efficiency of gas compressor.
[0013] The utility model discloses a self-lubricating assembly is set up, realizes the effective lubrication of compressor inside, and the sealing cover prevents the leakage of lubricating oil, guarantees the lubrication effect, and the cooperation of extrusion block and flexible spring makes lubricating oil be extruded and lubricated when compressor works, and also can prevent lubricating oil from leaking in non-working state, in addition, the use of movable guide column and guide column guide sleeve ensures the stability of extrusion block in retracting restraint groove, improves the reliability and durability of lubrication.
[0014] The utility model discloses a fixing assembly is set up, realized the stability and convenient installation between rotor seat main part and shell, and the stability of disc along the inner wall movement is ensured by the installation sleeve, and the reliability of installation is improved, and the cooperation of spacing block and spacing groove makes the knob can be firmly clamped in spacing groove after rotating 90 degrees, realizes the stable fixed effect, makes the installation and dismounting process become simple and fast, improves the maintainability and use convenience of gas compressor rotor seat. BRIEF DESCRIPTION OF DRAWINGS
[0015] Figure 1 It is the whole structure schematic diagram of the utility model;
[0016] Figure 2 It is the buffer assembly structure schematic diagram of the utility model;
[0017] Figure 3 It is the piston one and oil storage cylinder structure schematic diagram in the buffer assembly of the utility model;
[0018] Figure 4 It is the self -lubricating assembly structure schematic diagram of the utility model;
[0019] Figure 5 It is the fixing assembly structure schematic diagram of the utility model.
[0020] Sign significance: rotor seat main part 1, shell 2, buffer assembly 3, compression ring 31, camshaft rotor disc 32, rotor shaft 33, compression rod 34, open slot 35, air inlet 36, air outlet 37, installation block one 38, piston rod 39, piston one 310, installation block two 311, oil storage cylinder 312, spring one 313, self -lubricating assembly 4, oil inlet 41, sealing cover 42, restraint groove 43, installation block three 44, guide column guide sleeve 45, mobile guide column 46, extrusion block 47, flexible spring 48, sealing ring 49, fixing assembly 5, mounting plate one 51, installation sleeve 52, disc 53, plug rod 54, knob 55, spacing block 56, fixed plate 57, long hole 58, spacing groove 59, return spring 510. DETAILED DESCRIPTION
[0021] In order to make the purpose, technical scheme and advantage of the utility model more clear and explicit, below combining specific implementation and referring to the attached drawing, the utility model is further detailed explanation.Should understand, these descriptions are only exemplary, and not to limit the scope of the utility model.Moreover, in the following explanation, the description of known structure and technology is omitted to avoid unnecessary confusion of the concept of the utility model.
[0022] As Figures 1-5The utility model provides a gas compressor rotor seat easy to disassemble and maintain, it includes rotor seat main body 1, is provided with shell 2 at rotor seat main body 1 top, is provided with a plurality of fixed components 5 between rotor seat main body 1 and shell 2, is provided with buffer assembly 3 in rotor seat main body 1, is provided with a pair of self -lubricating assembly 4 in the symmetry of rotor seat main body 1.
[0023] Buffer assembly 3 includes the compression ring 31 being set in rotor seat main body 1, and the compression ring 31 is matched with camshaft rotor disc 32, and the gas that enters is compressed, and the gas pressure is improved, and the camshaft rotor disc 32 is set in the compression ring 31, and the camshaft rotor disc 32 rotates in rotor seat main body 1, and the gas is compressed through the compression ring 31, and the camshaft rotor disc 32 is provided with rotor shaft 33, and rotor shaft 33 supports camshaft rotor disc 32, so that it can rotate stably, and the compression ring 31 side is provided with compression rod 34, and rotor seat main body 1 side is provided with opening slot 35, and compression rod 34 is slidably arranged in opening slot 35, when camshaft rotor disc 32 rotates, compression ring 31 is subjected to pressure, and compression rod 34 slides in opening slot 35 along with, and reciprocating motion is carried out, and the rotor seat main body 1 side is provided with gas inlet 36, and the rotor seat main body 1 side away from gas inlet 36 is provided with gas outlet 37, and the gas passes through gas inlet 36 and enters the compressor inside, and camshaft rotor disc 32 rotates in rotor seat main body 1, and the gas that enters is compressed through the compression ring 31, and along with the rotation of camshaft rotor disc 32, the compression ring 31 gradually reduces the gas volume, and improves the gas pressure, and high-pressure gas is exported from gas outlet 37.
[0024] The compression rod 34 is provided with a mounting block one 38 on the side away from the compression ring 31, which provides a mounting base for a piston rod 39. The piston rod 39 is provided on the side away from the mounting block one 38, which provides a mounting base for a piston one 310. The piston rod 39 is provided with the piston one 310 on the side away from the mounting block one 38. The rotor seat body 1 is provided with a mounting block two 311 corresponding to the mounting block one 38 on the inner wall of the side of the open slot 35. The mounting block two 311 provides a mounting base for an oil storage cylinder 312. The mounting block two 311 is provided with the oil storage cylinder 312 on the side. The piston one 310 is located in the oil storage cylinder 312. The oil storage cylinder 312 contains hydraulic oil and provides a moving space for the piston one 310, which produces a damping effect. The spring one 313 is provided between the mounting block one 38 and the mounting block two 311, which can buffer the impact force of the compression rod 34. When the gas compressor is working, the compression rod 34 pushes the mounting block one 38, and the spring one 313 is extruded. Through the elastic force of the spring one 313, the impact force of the compression rod 34 is buffered, and at the same time, the piston rod 39 and the piston one 310 move in the oil storage cylinder 312. The piston one 310 divides the space in the oil storage cylinder 312 into two cavities. The hydraulic oil in the oil storage cylinder 312 will flow from one cavity to another through different small holes on the piston. In the process of hydraulic oil flow, the friction between the hole wall and the hydraulic oil and the internal friction between the hydraulic oil molecules will hinder the flow of the hydraulic oil, thereby generating a damping force, reducing the rebound speed of the spring one 313, avoiding the rapid rebound of the spring one 313 to intensify the vibration, effectively buffering the vibration generated by the camshaft rotor disc 32, and improving the stability and service life of the gas compressor.
[0025] The self-lubricating assembly 4 comprises an oil inlet 41 arranged on the rotor seat body 1, which is used to add lubricating oil into the self-lubricating assembly 4, and a sealing cover 42 is arranged outside the oil inlet 41 in a spiral sleeve manner, which prevents the lubricating oil from leaking, and a restraint groove 43 is arranged on one side of the rotor seat body 1, which is connected with the oil inlet 41 through an oil groove, and the restraint groove 43 and the oil groove can guide the lubricating oil into the inside of the rotor seat body 1 to provide lubrication, and a mounting block three 44 is arranged on the inner wall of the rotor seat body 1 on one side of the restraint groove 43, which provides a mounting basis for a guide column guide sleeve 45, and the guide column guide sleeve 45 is arranged on one side of the mounting block three 44, and a moving guide column 46 is slidably arranged in the guide column guide sleeve 45, and the combination of the guide column guide sleeve 45 and the moving guide column 46 ensures the stability of the extrusion block 47 when it is retracted in the restraint groove 43, prevents deviation from causing the return to fail to cooperate with the sealing ring 49, and the moving guide column 46 is provided with the extrusion block 47 away from one side of the guide column guide sleeve 45, and the flexible spring 48 is arranged between the extrusion block 47 and the mounting block three 44, which allows the extrusion block 47 to move, and the front part of the extrusion block 47 is smaller than the rear part, which can generate a gap between the sealing ring 49 and the restraint groove 43 to provide an outlet channel for the lubricating oil, and the flexible spring 48 can also provide the extrusion block 47 with reset ability, and prevent shock and noise, prolong the service life, and the restraint groove 43 is provided with a sealing ring 49 corresponding to the extrusion block 47, and the sealing ring 49 can cooperate with the extrusion block 47 in the state of not being extruded to prevent the lubricating oil from leaking.
[0026] The fixing assembly 5 comprises a mounting plate one 51 arranged on one side of the rotor seat body 1, which provides a mounting basis for a mounting sleeve 52, and the mounting plate one 51 is provided with the mounting sleeve 52, which ensures the stability of the disc 53 when moving along the inner wall, and the disc 53 is slidably arranged in the mounting sleeve 52, which provides a mounting basis for a return spring 510 and a plug rod 54, and the return spring 510 is arranged between the top surface of the mounting sleeve 52 and the disc 53, which provides the disc 53 with reset ability, and the plug rod 54 is arranged in the middle of the disc 53, which penetrates the mounting sleeve 52, and the plug rod 54 provides a mounting basis for a knob 55, and the plug rod 54 is provided with the knob 55 away from one end of the disc 53, and a pair of limiting blocks 56 are symmetrically arranged on the bottom of the knob 55.
[0027] The shell 2 is provided with a fixed plate 57 corresponding to the mounting sleeve 52 on one side, a long hole 58 is opened on the fixed plate 57, the long hole 58 allows the insertion rod 54 and the knob 55 to pass, the fixed plate 57 on both sides of the long hole 58 is provided with a limiting slot 59 corresponding to the limiting block 56, the staff can pull up the knob 55 by hand, the knob 55 drives the insertion rod 54 and the disc 53 to rise, the disc 53 extrudes the return spring 510, then the knob 55 is rotated 90 degrees with the insertion rod 54 as the center, the limiting block 56 at the bottom of the knob 55 is aligned with the limiting slot 59 and clamped in, when the external force disappears, the return spring 510 releases the elastic potential energy, provides the downward force for the knob 55 and the limiting block 56, so that the limiting block 56 is firmly clamped in the limiting slot 59, realizes the stable and convenient installation between the rotor seat body 1 and the shell 2, and ensures the stability when the gas compressor works.
[0028] In use, first, the staff aligns the shell 2 with the rotor seat body and installs, the long hole 58 on the several fixed plates 57 on the outer side of the shell 2 passes through the knob 55 and the insertion rod 54, the fixed plate 57 is placed on the top surface of the mounting sleeve 52, then the knob 55 is pulled up by hand, the knob 55 drives the insertion rod 54 and the disc 53 to rise, the disc 53 extrudes the return spring 510, then the knob 55 is rotated 90 degrees with the insertion rod 54 as the center, the limiting block 56 at the bottom of the knob 55 is aligned with the limiting slot 59 and clamped in, when the external force disappears, the return spring 510 releases the elastic potential energy, provides the downward force for the knob 55 and the limiting block 56, so that the limiting block 56 is firmly clamped in the limiting slot 59, realizes the stable and convenient installation between the rotor seat body 1 and the shell 2, and ensures the stability when the gas compressor works.
[0029] When the gas compressor is started, the gas enters the compressor through the gas inlet 36, the camshaft rotor disc 32 rotates in the rotor seat body 1, and the entering gas is compressed by the compression ring 31. With the rotation of the camshaft rotor disc 32, the compression ring 31 gradually reduces the volume of the gas and increases the pressure of the gas, and the high-pressure gas is output from the gas outlet 37. When the camshaft rotor disc 32 rotates, the compression ring 31 is subjected to pressure, and the compression rod 34 slides in the open slot 35 and reciprocates, pushing the mounting block one 38 and compressing the spring one 313. The spring one 313 buffers the impact force on the compression rod 34 through the elastic force of the spring one 313, and the piston rod 39 and the piston one 310 move in the oil storage cylinder 312. The piston one 310 divides the space in the oil storage cylinder 312 into two chambers, and the hydraulic oil in the oil storage cylinder 312 repeatedly flows from one chamber to the other chamber through different small holes on the piston. In the process of hydraulic oil flow, the friction between the hole wall and the hydraulic oil and the internal friction between the hydraulic oil molecules hinder the flow of the hydraulic oil, thereby generating a damping force, reducing the speed of the spring one 313 rebounding, avoiding the rapid spring of the spring one 313 aggravating vibration, effectively buffering the vibration generated by the camshaft rotor disc 32, and improving the stability and service life of the gas compressor.
[0030] During the use of the gas compressor, the rotor seat body 1 can be periodically removed, the sealing cover 42 can be unscrewed and removed, and lubricating oil can be added to the oil inlet 41. The lubricating oil enters the two side restraint grooves 43 through the oil inlet 41 and the oil groove. When the extrusion block 47 is not extruded, the extrusion block 47 cooperates with the sealing ring 49 on the restraint groove 43 to prevent leakage of the lubricating oil. When the gas compressor is working, the compression ring 31 extrudes the extrusion block 47, and the flexible spring 48 is compressed. Because the front part of the extrusion block 47 is smaller than the rear part, a gap is formed between the extrusion block 47, the sealing ring 49 and the restraint groove 43. The lubricating oil in the oil groove and the restraint groove 43 is extruded by the pressure when the extrusion block 47 retracts, and flows out through the gap to lubricate the inside of the rotor seat body 1. The combination of the moving guide pillar 46 and the guide pillar guide sleeve 45 can ensure the stability of the extrusion block 47 when it retracts into the restraint groove 43, prevent the extrusion block 47 from deviating and causing the lubricating oil to leak when it returns to its original position, and solve the problem of damage to the rotor seat body 1 and the compression ring 31 caused by long-term use. The rotating compression ring 31 can be lubricated by extruding the extrusion block 47 inside the rotor seat body 1, reducing maintenance costs.
[0031] It should be understood that the above specific embodiments of the present application are only used for illustrative or explanatory purposes of the principles of the present application, and do not constitute a limitation on the present application. Therefore, any modification, equivalent replacement, improvement, etc. made without departing from the spirit and scope of the present application shall be included in the protection scope of the present application. In addition, the appended claims of the present application are intended to cover all changes and modifications falling within the scope and boundaries of the appended claims, or the equivalent forms of such scope and boundaries.
Claims
1. A gas compressor rotor frame that is easily disassembled for maintenance, comprising: The rotor seat body (1) is characterized in that: the rotor seat body (1) is provided with a shell (2) on the top, a plurality of fixing assemblies (5) are arranged between the rotor seat body (1) and the shell (2), a buffer assembly (3) is arranged in the rotor seat body (1), and a pair of self-lubricating assemblies (4) are symmetrically arranged in the rotor seat body (1); The buffer assembly (3) comprises a compression ring (31) arranged in the rotor seat body (1), a camshaft rotor disc (32) is arranged in the compression ring (31), and a rotor shaft (33) is arranged on the camshaft rotor disc (32); The self-lubricating assembly (4) comprises an oil inlet (41) arranged on the rotor seat body (1), a sealing cover (42) is spirally sleeved outside the oil inlet (41), a restraint groove (43) is formed in one side of the rotor seat body (1), and the restraint groove (43) is connected with the oil inlet (41) through an oil groove. The fixing assembly (5) comprises a mounting plate one (51) arranged on one side of the rotor seat body (1), a mounting sleeve (52) is arranged on the mounting plate one (51), a disc (53) is slidably arranged in the mounting sleeve (52), and a return spring (510) is arranged between the top surface of the mounting sleeve (52) and the disc (53).
2. A gas compressor rotor package for easy removal and maintenance according to claim 1, characterized in that: One side of the compression ring (31) is provided with a compression rod (34), an open groove (35) is formed in one side of the rotor seat body (1), the compression rod (34) is slidably arranged in the open groove (35), an air inlet (36) is formed in one side of the rotor seat body (1), and an air outlet (37) is formed in the side of the rotor seat body (1) away from the air inlet (36).
3. A gas compressor rotor package for easy removal and maintenance according to claim 2, characterized in that: The compression rod (34) is provided with a mounting block one (38) away from the compression ring (31), the mounting block one (38) is provided with a piston rod (39) away from the compression rod (34), the piston rod (39) is provided with a piston one (310) away from the mounting block one (38), a mounting block two (311) corresponding to the mounting block one (38) is arranged on the inner wall of the rotor seat body (1) on one side of the open groove (35), the mounting block two (311) is provided with an oil storage cylinder (312) on one side, the piston one (310) is located in the oil storage cylinder (312), and a spring one (313) is arranged between the mounting block one (38) and the mounting block two (311).
4. A gas compressor rotor package for easy removal and maintenance according to claim 3, characterized in that: The inner wall of the rotor seat body (1) on one side of the restraint groove (43) is provided with a mounting block three (44), the mounting block three (44) is provided with a guide column guide sleeve (45) on one side, the guide column guide sleeve (45) is slidably provided with a moving guide column (46), the moving guide column (46) is provided with an extrusion block (47) away from the guide column guide sleeve (45), the extrusion block (47) and the mounting block three (44) are provided with a flexible spring (48) therebetween, and the restraint groove (43) is provided with a sealing ring (49) corresponding to the extrusion block (47).
5. A gas compressor rotor package for easy removal and maintenance according to claim 4, characterized in that: The middle part of the disc (53) is provided with an inserting rod (54), the inserting rod (54) penetrates the mounting sleeve (52), and the end, away from the disc (53), of the inserting rod (54) is provided with a knob (55), and the bottom of the knob (55) is symmetrically provided with a pair of limiting blocks (56).
6. A gas compressor rotor package that is easily disassembled for maintenance according to claim 5, wherein: One side of the shell (2) is provided with a fixed plate (57) corresponding to the mounting sleeve (52), a long hole (58) is formed in the fixed plate (57), and limiting grooves (59) corresponding to the limiting blocks (56) are formed in the fixed plate (57) on the two sides of the long hole (58).