Oxygen generator with filter screen convenient to assemble and disassemble
By designing the spatial relationship between the detachable connected intake valve, the fixed clamping part and the elastic clamping part on the oxygen generator, the problem of inconvenience in loading and unloading of the existing oxygen generator filter is solved, and the convenience of rapid disassembly and cleaning is achieved.
Patent Information
- Application Number
- CN202421454552.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-25
- Publication Date
- 2025-05-27
- Estimated Expiration
- 2034-06-25
AI Technical Summary
The filter on the existing oxygen generator is integrated, which is inconvenient to load and unload, making it difficult to quickly disassemble without disassembling the body.
A removable connected intake valve is designed, with a filter screen on the intake valve, and the spatial relationship between the fixed clamping part and the elastic clamping part is designed so that the filter screen can be quickly removed without disassembling the body.
It realizes the rapid disassembly of the filter screen without disassembling the oxygen generator body, which improves the convenience of loading and unloading, and through the installation of the aggregate trough, avoids impurities entering the fuselage, and is more convenient to clean.
Smart Images

Figure CN222900573U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of oxygen generators, and particularly relates to an oxygen generator facilitating the loading and unloading of a filter screen. Background Art
[0002] At present, oxygen generators are more and more widely used. During the use of an oxygen generator, air cooling and heat dissipation are required for the oxygen generator. During the heat dissipation process of the oxygen generator, air needs to be inhaled from the outside. After dust and other impurities in the air enter the oxygen generator, the heat dissipation effect inside the oxygen generator will be affected, and noise is easily generated. Therefore, a filter screen is usually arranged at the air inlet of the oxygen generator to filter impurities.
[0003] However, the filter screen on the existing oxygen generator is integrally arranged on the oxygen generator or arranged inside the oxygen generator. It is not easy to take out the filter screen from the oxygen generator without disassembling the oxygen generator, and the loading and unloading of the filter screen are inconvenient. Summary of the Utility Model
[0004] The purpose of the utility model is to provide an oxygen generator facilitating the loading and unloading of a filter screen, which can quickly disassemble the filter screen without disassembling the oxygen generator.
[0005] To solve the above technical problems, the utility model adopts the following scheme:
[0006] An oxygen generator facilitating the loading and unloading of a filter screen includes a machine body. An air inlet door is detachably connected to the machine body, and a filter screen is arranged on the air inlet door. Its function is that through the setting of the detachably connected air inlet door, the filter screen can be quickly disassembled without disassembling the machine body.
[0007] Further, the air inlet door includes an installation part for installing the filter screen. Fixed clamping parts and elastic clamping parts are respectively arranged on two opposite sides of the installation part. Its function is that through the design of the fixed clamping parts, elastic clamping parts and their spatial relationship, the fixed clamping parts can be fixed on the machine body when loading and unloading the air inlet door, and the elastic clamping parts are extruded to be separated from the machine body, so as to load and unload the air inlet door, and the loading and unloading are convenient.
[0008] Further, a clamping outer edge is arranged on the side of the installation part facing away from the machine body. The fixed clamping parts and the elastic clamping parts are both arranged on the side of the installation part facing the machine body. The elastic clamping part includes a U-shaped bending part. A barb is arranged at one end of the bending part far away from the installation part, and the barb is arranged on the side of the installation part facing the machine body. Its function is that through the setting of the clamping outer edge, the machine body can be clamped between the fixed clamping part and the clamping outer edge, and the machine body can be clamped between the barb and the clamping outer edge; through the setting of the bending part, the barb can be moved out of the machine body, so that the elastic clamping part can be completely moved out of the machine body.
[0009] Further, a push plate for pushing the bent portion to reduce the distance between the two ends of the bent portion is provided on the outer wall of the bent portion. Its function is that through the arrangement of the push plate, it is convenient to push the bent portion to be compressed.
[0010] Further, the fixed clamping portion is in the shape of a flat plate inclined to the mounting portion, and the side of the fixed clamping portion facing the clamping outer edge is rounded. Its function is that through the design of the spatial relationship between the fixed clamping portion and the clamping outer edge, the clamping outer edge can rotate at a certain angle while remaining clamped on the fuselage.
[0011] Further, the width of the barb gradually increases in the direction from the inside of the fuselage to the outside of the fuselage. Its function is that through the setting of the barb shape, it is convenient to push the barb into the fuselage when installing the intake valve.
[0012] Further, the distance between the barb and the corresponding clamping outer edge is equal to the thickness of the fuselage. Its function is that through the design of the dimensional relationship between the distance between the barb and the clamping outer edge and the thickness of the fuselage, the elastic clamping portion can be fixedly clamped on the fuselage.
[0013] Further, the fuselage includes a base and a front cover. The intake valve is arranged on the base, and an air outlet is provided on the side of the front cover away from the base. Its function is that through the design of the spatial relationship between the intake valve and the air outlet, the air used for heat dissipation moves from bottom to top in the fuselage. According to the principle that hot air rises, it is convenient to discharge the air after absorbing heat.
[0014] Further, a wind guiding plate for guiding the air entering from the intake valve into the fuselage is provided on the base, and a support plate for pressing against the top end of the wind guiding plate to close the top of the area between the wind guiding plate and the front cover is provided on the front cover. Its function is that the combined design of the wind guiding plate and the support plate enables the air entering the fuselage through the intake valve to enter the fuselage from the side wall of the wind guiding plate.
[0015] Further, an aggregate groove for covering the elastic clamping portion clamped on the base is provided below the front cover, and the aggregate groove is only open on the side facing the base. Its function is that through the arrangement of the aggregate groove, it can prevent impurities from entering the fuselage through the gap of the bent portion, and collect the impurities passing through the bent portion into the aggregate groove. When the front cover is removed, the collected impurities can be directly poured out, which is convenient for cleaning.
[0016] The beneficial effects of the present utility model are as follows:
[0017] 1. Through the arrangement of the detachable intake valve, the filter screen can be quickly disassembled without disassembling the fuselage.
[0018] 2. Through the design of the fixed clamping part, the elastic clamping part and their spatial relationship, the fixed clamping part can be fixed on the fuselage when loading and unloading the intake valve, and the elastic clamping part can be extruded to separate it from the fuselage, so as to load and unload the intake valve conveniently.
[0019] 3. Through the setting of the aggregate chute, impurities can be prevented from entering the fuselage through the gap of the bending part, and the impurities passing through the bending part can be collected in the aggregate chute. When the front cover is removed, the collected impurities can be directly poured out, which is convenient for cleaning. BRIEF DESCRIPTION OF THE DRAWINGS
[0020] Figure 1 It is a three-dimensional structural schematic diagram of Embodiment 1;
[0021] Figure 2 It is a three-dimensional structural schematic diagram of the intake valve in Embodiment 1;
[0022] Figure 3 It is a three-dimensional structural schematic diagram after the base and the front cover are connected in Embodiment 1;
[0023] Figure 4 It is a three-dimensional exploded structure diagram of the intake valve, the base and the front cover in Embodiment 1;
[0024] Figure 5 It is a three-dimensional structural schematic diagram of the base with the intake valve installed in Embodiment 1;
[0025] Figure 6 It is an enlarged structural schematic diagram at A in Embodiment 1.
[0026] Reference numerals: 1, fuselage; 101, base; 102, front cover; 2, intake valve; 3, filter screen; 4, installation part; 5, fixed clamping part; 6, elastic clamping part; 7, clamping outer edge; 8, bending part; 9, barb; 10, push plate; 11, air outlet; 12, air deflector; 13, support plate; 14, aggregate chute. DETAILED DESCRIPTION OF THE EMBODIMENTS
[0027] The following will further elaborate on the present invention in detail in conjunction with the embodiments and the drawings, but the implementation manners of the present invention are not limited thereto.
[0028] In the description of the present utility model, it should be noted that the orientation or positional relationship indicated by terms such as "center", "upper", "lower", "left", "right", "vertical", "longitudinal", "lateral", "horizontal", "inner", "outer", "front", "rear", "top", "bottom", etc. is based on the orientation or positional relationship shown in the drawings, or the orientation or positional relationship in which the product of the present utility model is customarily placed during use. It is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as a limitation to the present utility model.
[0029] In the description of the present utility model, it should also be noted that unless otherwise clearly specified and defined, the terms "set", "provided with", "installed", "connected", "coupled" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances.
[0030] Embodiment 1
[0031] An oxygen generator facilitating the loading and unloading of a filter screen, as Figure 1 shown, includes a body 1, and an air inlet door 2 is detachably connected to the body 1, and a filter screen 3 is provided on the air inlet door 2. Its function is that by providing the detachably connected air inlet door 2, the filter screen 3 can be quickly disassembled without disassembling the body 1.
[0032] Specifically, as Figure 2 shown, the air inlet door 2 includes a mounting portion 4 for mounting the filter screen 3, and a fixed clamping portion 5 and an elastic clamping portion 6 are respectively provided on opposite sides of the mounting portion 4. Its function is that through the design of the fixed clamping portion 5 and the elastic clamping portion 6 and their spatial relationship, the fixed clamping portion 5 can be fixed on the body 1 when loading and unloading the air inlet door 2, and the elastic clamping portion 6 is squeezed to separate the elastic clamping portion 6 from the body 1, so as to load and unload the air inlet door 2, and the loading and unloading are convenient.
[0033] Specifically, as Figure 2As shown, a clamping outer edge 7 is provided on the side of the installation part 4 facing away from the inside of the fuselage 1. The fixed clamping part 5 and the elastic clamping part 6 are both arranged on the side of the installation part 4 facing the inside of the fuselage 1. The elastic clamping part 6 includes a U-shaped bending part 8. A barb 9 is provided at one end of the bending part 8 away from the installation part 4, and the barb 9 is arranged on the side of the installation part 4 facing the inside of the fuselage 1. Its function is that through the setting of the clamping outer edge 7, the fuselage 1 can be clamped between the fixed clamping part 5 and the clamping outer edge 7, and the fuselage 1 can be clamped between the barb 9 and the clamping outer edge 7; through the setting of the bending part 8, the barb 9 can be moved out of the fuselage 1, so that the elastic clamping part 6 can be completely removed from the fuselage 1.
[0034] Specifically, as Figure 2 shown, a push plate 10 for pushing the bending part 8 to reduce the distance between the two ends of the bending part 8 is provided on the outer wall of the bending part 8. Its function is that through the setting of the push plate 10, it is convenient to push the bending part 8 to compress.
[0035] Specifically, as Figure 2 shown, the fixed clamping part 5 is in the shape of a flat plate inclined to the installation part 4, and the side of the fixed clamping part 5 facing the clamping outer edge 7 is rounded. Its function is that through the design of the spatial relationship between the fixed clamping part 5 and the clamping outer edge 7, the clamping outer edge 7 can rotate at a certain angle while remaining clamped on the fuselage 1.
[0036] Specifically, as Figure 2 shown, the width of the barb 9 gradually increases in the direction from the inside of the fuselage 1 to the outside of the fuselage 1. Its function is that through the setting of the shape of the barb 9, it is convenient to push the barb 9 into the fuselage 1 when installing the intake valve 2.
[0037] Specifically, as Figure 5 、 Figure 6 shown, the distance between the barb 9 and the corresponding clamping outer edge 7 is equal to the thickness of the fuselage 1. Its function is that through the design of the dimensional relationship between the distance between the barb 9 and the clamping outer edge 7 and the thickness of the fuselage 1, the elastic clamping part 6 can be fixedly clamped on the fuselage 1.
[0038] Specifically, as Figure 3 shown, the fuselage 1 includes a base 101 and a front cover 102. The intake valve 2 is arranged on the base 101, and an air outlet 11 is provided on the side of the front cover 102 away from the base 101. Its function is that through the design of the spatial relationship between the intake valve 2 and the air outlet 11, the air used for heat dissipation moves from bottom to top in the fuselage 1. According to the principle of hot air rising, it is convenient to discharge the air after absorbing heat.
[0039] Specifically, as Figure 3As shown in the figure, a wind guide plate 12 for guiding the air entering from the air inlet 2 into the fuselage 1 is provided on the base 101, and a support plate 13 for pressing against the top end of the wind guide plate 12 to close the top of the area between the wind guide plate 12 and the front cover 102 is provided on the front cover 102. Its function is that the combined design of the wind guide plate 12 and the support plate 13 enables the air entering the fuselage 1 through the air inlet 2 to enter the fuselage 1 from the side wall of the wind guide plate 12.
[0040] Specifically, as Figure 4 shown in the figure, a collecting groove 14 for covering and clamping the elastic clamping portion 6 on the base 101 is provided below the front cover 102, and the collecting groove 14 is only open on the side facing the base 101. Its function is that through the setting of the collecting groove 14, it can prevent impurities from entering the fuselage 1 from the gap of the bending portion 8, and collect the impurities passing through the bending portion 8 into the collecting groove 14. When the front cover 102 is removed, the collected impurities can be directly poured out, which is convenient for cleaning.
[0041] The working principle of this embodiment is described as follows: When installing the air inlet 2, the fuselage 1 is clamped between the clamping outer edge 7 and the fixed clamping portion 5. Rotate the air inlet 2 to push the hook into the fuselage 1. When the hook passes through the fuselage 1, the bending portion 8 is compressed and then reset, so that the fuselage 1 is clamped between the hook and the clamping outer edge 7.
[0042] When disassembling the air inlet 2, push the push plate 10 to compress the bending portion 8 until the hook moves out of the fuselage 1, and keep the bending portion 8 compressed and turn it outwards to remove the air inlet 2.
[0043] The above is only a preferred embodiment of the present invention, and it does not impose any form of limitation on the present invention. Based on the technical essence of the present invention, any simple modification, equivalent replacement and improvement made to the above embodiments within the spirit and principle of the present invention still fall within the protection scope of the technical solution of the present invention.
Claims
1. An oxygen concentrator with a filter screen that is easy to install and remove, comprising a body (1), characterized in that: The body (1) is detachably connected to an air intake valve (2), and a filter screen (3) is provided on the air intake valve (2). The air intake valve (2) comprises a mounting portion (4) for mounting the filter screen (3), and a fixed clamping portion (5) and an elastic clamping portion (6) are respectively provided on opposite sides of the mounting portion (4). The mounting portion (4) is provided with a clamping outer edge (7) on the side facing the outside of the fuselage (1); the fixed clamping portion (5) and the elastic clamping portion (6) are both provided on the side facing the inside of the fuselage (1) of the mounting portion (4); the elastic clamping portion (6) includes a U-shaped bending portion (8); a barb (9) is provided at one end of the bending portion (8) away from the mounting portion (4); and the barb (9) is provided on the side facing the inside of the fuselage (1) of the mounting portion (4).
2. The oxygen concentrator with easy-to-install and uninstall filter screen according to claim 1, characterized in that: A push plate (10) is provided on the outer wall of the bending portion (8) for pushing the bending portion (8) to reduce the distance between the two ends of the bending portion (8).
3. The oxygen concentrator with easy-to-install and uninstall filter screen according to claim 1, characterized in that: The fixed clamping portion (5) is in the shape of a flat plate which is arranged obliquely with respect to the mounting portion (4), and the fixed clamping portion (5) has a rounded corner on one side facing the clamping outer edge (7).
4. The oxygen concentrator with easy-to-install and uninstall filter screen according to claim 1, characterized in that: The width of the barb (9) gradually increases in a direction from the inside of the fuselage (1) to the outside of the fuselage (1).
5. The oxygen concentrator with easy-to-install and uninstall filter screen according to claim 1, characterized in that: The distance between the barb (9) and the clamping outer edge (7) at the corresponding position is equal to the thickness of the fuselage (1).
6. The oxygen concentrator with easy-to-install and uninstall filter screen according to claim 1, characterized in that: The body (1) comprises a base (101) and a front cover (102); an air inlet door (2) is arranged on the base (101); and an air outlet (11) is arranged on a side of the front cover (102) away from the base (101).
7. The oxygen concentrator with easy-to-install and uninstall filter screen according to claim 6, characterized in that: The base (101) is provided with an air guide plate (12) for guiding air entering from the air inlet door (2) into the fuselage (1), and the front cover (102) is provided with a support plate (13) for supporting the top of the air guide plate (12) and closing the top of the area between the air guide plate (12) and the front cover (102).
8. The oxygen concentrator with easy-to-install and uninstall filter screen according to claim 7, characterized in that: A material collecting groove (14) for covering the elastic clamping portion (6) clamped on the base (101) is provided below the front cover (102), and the material collecting groove (14) is open only on one side facing the base (101).