Split type detachable wardrobe hinge

Abstract

The utility model relates to wardrobe hinge technical field, and disclose a kind of split detachable wardrobe hinge, including connecting plate, the upper end of connecting plate is fixedly arranged with door panel cover degree adjusting peg, one end of connecting plate is fixedly arranged with insertion slot, the other end of connecting plate is fixedly arranged with movable rod, one end of movable rod is fixedly arranged with spring support, the upper end of spring support is fixedly arranged with extension arm, the lower end of extension arm is fixedly arranged with aircraft pedestal one, the lower end of aircraft pedestal one is fixedly arranged with deep cup design cylinder, the upper end of aircraft pedestal one is fixedly arranged with countersunk bolt hole.The split detachable wardrobe hinge, through the improvement of wardrobe hinge, so that the splicing disassembly and protection ability of the wardrobe hinge are improved, in the actual use process of the wardrobe hinge, wardrobe hinge can be spliced according to the needs of disassembly, convenient for the protection of wardrobe hinge use, improve the use experience of split detachable wardrobe hinge.

Description

Technical Field

[0001] This utility model relates to the field of wardrobe hinge technology, specifically a split-type detachable wardrobe hinge. Background Technology

[0002] Wardrobe hinges are mechanical devices used to connect two solid objects and allow relative rotation between them. Hinges are mostly installed on cabinets. They are mainly classified by material into stainless steel hinges and iron hinges. To provide people with a better experience, hydraulic hinges have also emerged. Their feature is that they provide a buffer function when the cabinet door is closed, minimizing the noise caused by the cabinet door colliding with the cabinet body when it closes.

[0003] Existing technology publication CN209398122U discloses a wardrobe hinge. The upper part of the fixed base is fixedly connected to the outer shell, and a bottom hole is formed below the fixed base. A middle shell is disposed inside the outer shell, and the middle shell is slidably connected to the outer shell. An inner block is disposed inside the middle shell, and a fixed shaft is fixedly connected inside the middle shell, passing through the inner block. The inner block is slidably connected to the fixed shaft. The middle shell has a first cam hole, and a first rotating shaft is rotatably connected to the outer shell. The first rotating shaft is fixedly connected to a first cam, which is located in the first cam hole. The lower part of the first rotating shaft is fixedly connected to a first head. The inner block has a first through hole, and the first head is located in the first through hole. The inner block has a second cam hole, and a second rotating shaft is rotatably connected to the middle shell. The second rotating shaft is fixedly connected to a second cam, which is located in the second cam hole. The lower part of the second rotating shaft is fixedly connected to a second head. A third rotating shaft is connected to the middle shell. The system includes a movable connection, with the lower part of the third rotating shaft fixed to a lead screw, the inner layer block forming a threaded hole, the lead screw residing in and connected to the threaded hole, the lower part of the lead screw fixed to a third head, the third head passing through the inner layer block, the middle shell forming a sliding hole, the third rotating shaft residing in the sliding hole and slidably connected to the middle shell, the inner layer block rotatably connected to a fixed shaft, the hinge seat forming a connecting part, the inner layer block fixed to the connecting part, and the hinge seat forming a central shaft hole. It also includes a door frame connector, with magnet holes on both sides of the door frame connector, magnets disposed within the magnet holes, a striker hole formed in the door frame connector, a striker installed within the striker hole, and a magnet installed in the hinge seat. The magnets in the magnet holes of the door frame connector are magnetically connected to the magnets in the hinge seat, detachably connecting the hinge seat and the door frame connector. By rotating the first, second, and third rotating shafts, the hinge seat can be adjusted in three directions: left-right, front-back, and up-down, to adapt to the fit of the door frame connector.

[0004] However, the existing technology CN209398122U patent has poor splicing, disassembly and protection capabilities for a wardrobe hinge. As a result, in the actual use of the wardrobe hinge, it is impossible to splice and disassemble the wardrobe hinge as needed, making it inconvenient to protect the wardrobe hinge and affecting the user experience of the wardrobe hinge. Utility Model Content

[0005] (a) Technical problems to be solved

[0006] The purpose of this utility model is to provide a split-type detachable wardrobe hinge to solve the problem of poor splicing, disassembly, and protection capabilities of the wardrobe hinge mentioned in the background art.

[0007] (II) Technical Solution

[0008] To achieve the above objectives, this utility model provides the following technical solution: a split-type detachable wardrobe hinge, including a connecting plate, a door panel cover adjustment bolt fixedly provided at the upper end of the connecting plate, an insertion groove fixedly provided at one end of the connecting plate, a movable rod fixedly provided at the other end of the connecting plate, a spring support fixedly provided at one end of the movable rod, an extension arm fixedly provided at the upper end of the spring support, an aircraft base fixedly provided at the lower end of the extension arm, a deep cup design cylinder fixedly provided at the lower end of the aircraft base, and a countersunk bolt hole fixedly provided at the upper end of the aircraft base.

[0009] The connecting plate has an insert plate shell fixedly installed on one side, and an insert plate groove fixedly installed inside the insert plate shell. A fixing button is movably installed at the upper end of the insert plate shell. Through the improvement of the wardrobe hinge, the splicing, disassembly and protection capabilities of the wardrobe hinge are improved. In the actual use of the wardrobe hinge, the wardrobe hinge can be spliced ​​and disassembled as needed, which facilitates the use of the wardrobe hinge for protection and improves the user experience of the split-type detachable wardrobe hinge.

[0010] The lower end of the insert shell is fixedly equipped with an aircraft base two, the upper end of the aircraft base two is fixedly equipped with a mounting screw hole, and the upper end of the insert shell is movably equipped with a mounting bolt. The use of connecting plates and door panel cover adjustment bolts facilitates the installation and fixing of the split-type detachable wardrobe hinges. The use of insertion slots facilitates the insertion of the wardrobe hinges. The use of movable rods and spring supports facilitates the adjustment of the extension arm. The use of countersunk bolt holes facilitates the connection and fixing of the aircraft base one and the deep cup design cylinder.

[0011] The lower end of the connecting plate is fixedly equipped with a connecting layer, and the lower end of the connecting layer is fixedly equipped with a waterproof coating. The use of the insert plate shell and the insert plate groove facilitates the movable insertion of the connecting plate and the insert groove. Then, the use of the aircraft base and the mounting screw holes facilitates the connection and fixation of the insert plate shell. Finally, the use of the fixing button improves the disassembly and installation of the split-type detachable wardrobe hinge.

[0012] The waterproof coating has a metal fiber block fixed at the lower end, a polypropylene fiber layer fixed at the lower end of the metal fiber block, and a graphene layer fixed at the lower end of the polypropylene fiber layer. The use of the waterproof coating and graphene layer improves the protective and corrosion-resistant effect of the metal fiber block and polypropylene fiber layer. Furthermore, the use of the metal fiber block and polypropylene fiber layer enhances the strength support of the detachable wardrobe hinge.

[0013] Compared with the prior art, the beneficial effects of this utility model are:

[0014] 1. This split-type detachable wardrobe hinge improves the splicing, disassembly, and protection capabilities of the wardrobe hinge through improvements. In actual use, the wardrobe hinge can be spliced ​​and disassembled as needed, making it easier to protect the wardrobe hinge and improving the user experience of the split-type detachable wardrobe hinge.

[0015] 2. This split-type detachable wardrobe hinge facilitates the installation and fixing of the split-type detachable wardrobe hinge through the use of connecting plates and door panel cover adjustment bolts. Then, the use of insertion slots facilitates the insertion of the wardrobe hinge. Then, the use of movable rods and spring supports facilitates the adjustment of the extension arm. Finally, the use of countersunk bolt holes facilitates the connection and fixing of the aircraft base and deep cup design cylinder.

[0016] 3. This detachable wardrobe hinge features a hinge design. The use of insert plates and slots facilitates the insertion of connecting panels. The use of mounting screw holes on the base facilitates the connection and fixation of the insert plates. The use of a fixing button enhances the ease of disassembly and installation. The application of a waterproof coating and graphene layer improves the protective and corrosion-resistant properties of the metal fiber blocks and polypropylene fiber layers. Finally, the use of metal fiber blocks and polypropylene fiber layers enhances the structural strength of the detachable wardrobe hinge.

[0017] The parts of this device not covered herein are the same as or can be implemented using existing technologies. This utility model has a simple structure and is easy to operate. Attached Figure Description

[0018] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0019] Figure 2 This is a schematic diagram of the connecting plate structure of this utility model;

[0020] Figure 3 This is a schematic diagram of the insert plate shell structure of this utility model;

[0021] Figure 4 This is a schematic diagram of the metal fiber block structure of this utility model.

[0022] In the diagram: 1. Connecting plate; 2. Door panel cover adjustment bolt; 3. Insertion slot; 4. Movable rod; 5. Spring support; 6. Extension arm; 7. Aircraft base one; 8. Deep cup design cylinder; 9. Countersunk bolt hole; 10. Insertion shell; 11. Insertion slot; 12. Fixing button; 13. Aircraft base two; 14. Mounting screw hole; 15. Mounting bolt; 16. Connecting layer; 17. Waterproof coating; 18. Metal fiber block; 19. Polypropylene fiber layer; 20. Graphene layer. Detailed Implementation

[0023] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0024] Please see Figure 1 - Figure 4 This utility model provides a technical solution: a split-type detachable wardrobe hinge, including a connecting plate 1, a door panel cover adjustment bolt 2 fixedly installed at the upper end of the connecting plate 1, an insertion groove 3 fixedly installed at one end of the connecting plate 1, a movable rod 4 fixedly installed at the other end of the connecting plate 1, a spring support 5 fixedly installed at one end of the movable rod 4, an extension arm 6 fixedly installed at the upper end of the spring support 5, an aircraft base 7 fixedly installed at the lower end of the extension arm 6, a deep cup design cylinder 8 fixedly installed at the lower end of the aircraft base 7, and a countersunk bolt hole 9 fixedly installed at the upper end of the aircraft base 7.

[0025] An insertion plate shell 10 is fixedly installed on one side of the connecting plate 1. An insertion plate groove 11 is fixedly installed inside the insertion plate shell 10. A fixing button 12 is movably installed at the upper end of the insertion plate shell 10. An aircraft base 2 13 is fixedly installed at the lower end of the insertion plate shell 10. An installation screw hole 14 is fixedly installed at the upper end of the aircraft base 2 13. An installation bolt 15 is movably installed at the upper end of the insertion plate shell 10. The use of the connecting plate 1 and the door panel cover adjustment bolt 2 facilitates the installation and fixing of the split-type detachable wardrobe hinge. The use of the insertion groove 3 facilitates the insertion of the wardrobe hinge. The use of the movable rod 4 and the spring support 5 facilitates the movable adjustment of the extension arm 6. The use of the countersunk bolt hole 9 facilitates the connection and fixing of the aircraft base 1 7 and the deep cup design cylinder 8.

[0026] A connecting layer 16 is fixedly installed at the lower end of the connecting plate 1. A waterproof coating 17 is fixedly installed at the lower end of the connecting layer 16. A metal fiber block 18 is fixedly installed at the lower end of the waterproof coating 17. A polypropylene fiber layer 19 is fixedly installed at the lower end of the metal fiber block 18. A graphene layer 20 is fixedly installed at the lower end of the polypropylene fiber layer 19. The use of the insert shell 10 and the insert slot 11 facilitates the movable insertion of the connecting plate 1 and the insert slot 3. The use of the aircraft base 13 and the mounting screw hole 14 facilitates the connection and fixation of the insert shell 10. The use of the fixing button 12 improves the disassembly and installation of the split-type detachable wardrobe hinge. The use of the waterproof coating 17 and the graphene layer 20 improves the protective and corrosion-resistant effect of the metal fiber block 18 and the polypropylene fiber layer 19. The use of the metal fiber block 18 and the polypropylene fiber layer 19 improves the strength support of the split-type detachable wardrobe hinge.

[0027] Working Principle: First, the use of connecting plate 1 and door panel cover adjustment bolt 2 facilitates the installation and fixing of the split-type detachable wardrobe hinge. Then, the use of insertion slot 3 facilitates the insertion of the wardrobe hinge. Next, the use of movable rod 4 and spring support 5 facilitates the movable adjustment of extension arm 6. Then, the use of countersunk bolt hole 9 facilitates the connection and fixing of aircraft base 1 7 and deep cup design cylinder 8. Then, the use of insertion shell 10 and insertion slot 11 facilitates the movable insertion of connecting plate 1 and insertion slot 3. Then, the use of aircraft base 2 13 and mounting screw hole 14 facilitates the connection and fixing of insertion shell 10. Then, the use of fixing button 12 improves the disassembly and installation of split-type detachable wardrobe hinge. Then, the use of waterproof coating 17 and graphene layer 20 improves the protective and corrosion-resistant effect of metal fiber block 18 and polypropylene fiber layer 19. Finally, the use of metal fiber block 18 and polypropylene fiber layer 19 improves the strength support of split-type detachable wardrobe hinge.

[0028] Finally, it should be noted that the above content is only used to illustrate the technical solution of this utility model, and is not intended to limit the scope of protection of this utility model. Simple modifications or equivalent substitutions made by those skilled in the art to the technical solution of this utility model do not depart from the essence and scope of the technical solution of this utility model.

Claims

1. A detachable wardrobe hinge, comprising a connecting plate (1), characterized in that: A door panel cover adjustment bolt (2) is fixedly installed at the upper end of the connecting plate (1), an insertion slot (3) is fixedly installed at one end of the connecting plate (1), a movable rod (4) is fixedly installed at the other end of the connecting plate (1), a spring support (5) is fixedly installed at one end of the movable rod (4), an extension arm (6) is fixedly installed at the upper end of the spring support (5), an aircraft base (7) is fixedly installed at the lower end of the extension arm (6), a deep cup design cylinder (8) is fixedly installed at the lower end of the aircraft base (7), and a countersunk bolt hole (9) is fixedly installed at the upper end of the aircraft base (7).

2. A detachable wardrobe hinge according to claim 1, characterized in that: An insertion plate shell (10) is fixedly provided on one side of the connecting plate (1), an insertion plate groove (11) is fixedly provided inside the insertion plate shell (10), and a fixing button (12) is movably provided at the upper end of the insertion plate shell (10).

3. A detachable wardrobe hinge according to claim 2, characterized in that: An aircraft base (13) is fixedly installed at the lower end of the insert shell (10), and an installation screw hole (14) is fixedly installed at the upper end of the aircraft base (13). An installation bolt (15) is movably installed at the upper end of the insert shell (10).

4. A detachable wardrobe hinge according to claim 3, characterized in that: A connecting layer (16) is fixedly provided at the lower end of the connecting plate (1), and a waterproof coating (17) is fixedly provided at the lower end of the connecting layer (16).

5. A detachable wardrobe hinge according to claim 4, characterized in that: A metal fiber block (18) is fixedly installed at the lower end of the waterproof coating (17), a polypropylene fiber layer (19) is fixedly installed at the lower end of the metal fiber block (18), and a graphene layer (20) is fixedly installed at the lower end of the polypropylene fiber layer (19).

Images