Grounding electromagnetic lock based on aviation plug integration technology

Abstract

The invention relates to the technical field of electromagnetic locks, in particular to a grounding electromagnetic lock based on an aviation plug integration technology, which comprises an electromagnetic lock body, the electromagnetic lock body comprises a bottom plate, a shell and disassembly and assembly mechanisms, the disassembly and assembly mechanisms are arranged at four corners of the bottom plate and the shell, a mounting plate is arranged at the bottom of the bottom plate, and the mounting plate is arranged on the bottom of the shell. A mounting plate is arranged on the bottom plate, a through groove is formed in the surface of the mounting plate, a grounding rod is arranged on the electromagnetic lock body, the grounding rod is inserted into the through groove, a connecting mechanism is arranged at the bottom of the mounting plate, the connecting mechanism is used for mounting the grounding rods with different diameters, and the bottom plate and the shell are connected through the dismounting and mounting mechanism. By conveniently disassembling and assembling the electromagnetic lock body, the maintenance time is shortened, fault maintenance is facilitated, and the electromagnetic lock is suitable for grounding rods of different diameter specifications.

Description

Technical Field

[0001] The invention relates to the technical field of electromagnetic locks, and in particular to a grounded electromagnetic lock based on aviation plug integration technology. Background Art

[0002] The grounding electromagnetic lock is a grounding locking device widely used in substations. When working, the operator inserts the ground wire head into the grounding electromagnetic lock to ground the maintenance equipment or lines, thereby ensuring the personal safety of the operator.

[0003] The existing electromagnetic locks are cumbersome to repair and replace, and cannot be replaced by the operation and maintenance staff themselves. The required repair and replacement time is long, and during the repair, the screws are removed with a screwdriver and then the shell is opened, and the screws are fixed after the repair is completed. Due to the large number of screws and the need to use a screwdriver, the entire disassembly and assembly process is cumbersome and time-consuming. The existing electromagnetic locks are not modularized during repair, so the repair time is long, and there are many types of grounding rods, and the existing electromagnetic locks cannot be installed with grounding rods of different specifications.

[0004] According to the above shortcomings, a grounding electromagnetic lock is designed to achieve rapid maintenance and replacement of the electromagnetic lock and shorten the replacement time. Summary of the invention

[0005] The purpose of the present invention is to solve the problem that the existing electromagnetic lock body in the prior art is cumbersome to repair and replace, cannot be replaced by the operation and maintenance staff themselves, and requires a long repair and replacement time, and proposes a grounded electromagnetic lock based on aviation plug integration technology.

[0006] In order to achieve the above-mentioned purpose, the present invention adopts the following technical scheme: a grounding electromagnetic lock based on aviation plug integration technology, including an electromagnetic lock body, the electromagnetic lock body including a base plate, a shell and a disassembly and assembly mechanism, the disassembly and assembly mechanism is arranged at the four corners of the base plate and the shell, a mounting plate is arranged at the bottom of the base plate, a through groove is arranged on the surface of the mounting plate, a grounding rod is arranged on the electromagnetic lock body, and the grounding rod is inserted in the through groove, a connecting mechanism is arranged at the bottom of the mounting plate, the connecting mechanism is used to install grounding rods of different diameters, and the base plate and the shell are connected through the disassembly and assembly mechanism.

[0007] Preferably, an interface is provided at the bottom of the electromagnetic lock body, and an aviation plug is inserted into the interface.

[0008] Preferably, the connecting mechanism includes a micro cylinder fixed to the bottom of the mounting plate, the bottom of the mounting plate is rotatably connected to two rods via a rotating shaft, a connecting plate is fixed to the output end of the micro cylinder, both ends of the connecting plate are rotatably connected to the two rods, a first arc-shaped clamping plate is fixed to one end of the two rods, and the through groove is located on the inner side of the two first arc-shaped clamping plates.

[0009] Preferably, the disassembly and assembly mechanism includes a first connecting part and a second connecting part, the first connecting part is mounted on the shell, the second connecting part is fixed to the mounting plate, and the shell and the base plate are connected through the first connecting part and the second connecting part.

[0010] Preferably, the first connecting part includes a cylinder fixed to the bottom of the shell, a circular groove is arranged on the outside of the cylinder, and the other end of the cylinder is connected to a conical head through a vertical axis, and the diameter of the vertical axis is smaller than the diameter of the cylinder and the conical head, so that a slot is formed in the peripheral area of ​​the vertical axis.

[0011] Preferably, the second connecting part comprises a hollow column arranged on the bottom plate, the bottom of the hollow column extends out of the bottom plate, a first electromagnet is fixed to the bottom of the hollow column, an iron sliding sleeve is slidably connected to the outside of the hollow column, the sliding sleeve comprises an extrusion layer and a hollow groove, a convex ring is fixed to the bottom of the hollow column, a first spring is arranged on the outside of the hollow column, the first spring is located between the sliding sleeve and the convex ring, and a conical groove is arranged at the bottom of the hollow column; Limiting grooves are evenly distributed on the outside of the hollow column, and spherical clamping blocks are arranged inside the limiting grooves, and the clamping blocks are used to cooperate with the circular grooves.

[0012] Preferably, the limiting groove is wider on a side close to the extrusion layer and narrower on a side away from the extrusion layer, and the narrowest part of the limiting groove is larger than the diameter of the block.

[0013] Preferably, an iron plug is provided inside the hollow column, the plug is deformable and connected to each other to form a whole, and a second electromagnet is provided at the bottom of the hollow column; when the second electromagnet is energized, the plug moves toward a side close to the second electromagnet, and when the second electromagnet is de-energized, the plug resets and enters the slot.

[0014] Preferably, when the first electromagnet and the second electromagnet are powered on at the same time, the first connecting part can be inserted into the second connecting part, and when the first electromagnet and the second electromagnet are powered off, the first connecting part is connected to the second connecting part.

[0015] Preferably, the electromagnetic lock body is provided with a shell structure module, a logic locking module, a manual unlocking module, and a power supply module.

[0016] The beneficial effects of the present invention are: 1. The first connecting part and the second connecting part cooperate with each other to connect the shell and the bottom plate to facilitate disassembly and maintenance. Specifically, when the electromagnetic lock body needs to be disassembled and repaired, the first electromagnet and the second electromagnet are energized again, and the card block is removed from the slot. Then, the bottom plate and the shell can be separated, which is conducive to the disassembly and installation of the electromagnetic lock body by disconnecting and energizing the first electromagnet and the second electromagnet. The whole process takes a short time.

[0017] 2. The output end of the micro cylinder extends out to move with the connecting plate, and then the two rods rotate in the opposite direction to move with the two arc-shaped clamps in the opposite direction. The arc-shaped clamps are helpful for clamping grounding rods of different diameters to adapt to grounding rods of different diameters. In addition, the electromagnetic lock body is provided with a voice prompt function, which can provide voice prompts for the status of the switch node, facilitating fault maintenance. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a structural schematic diagram of a grounding electromagnetic lock based on aviation plug integration technology in an embodiment of the present invention; Figure 2 This is a schematic diagram of the structure in which the bottom plate and the shell of the electromagnetic lock body are separated in an embodiment of the present invention; Figure 3 This is a schematic diagram of the bottom structure of the electromagnetic lock body in an embodiment of the present invention; Figure 4 It is a schematic diagram of the partial disassembly structure of the electromagnetic lock body in an embodiment of the present invention; Figure 5 for Figure 2 A partial enlarged view of the middle part; Figure 6 It is a structural schematic diagram of the disassembly and assembly mechanism in an embodiment of the present invention; Figure 7 It is a schematic diagram of the partial structure of the mounting plate in an embodiment of the present invention; Figure 8 This is a schematic diagram of the structure of the inner side of the through slot in an embodiment of the present invention; Fig. 9 It is a structural schematic diagram of a connecting mechanism in an embodiment of the present invention; Fig.10 for Figure 3 A partial enlarged view of point B in the middle.

[0019] In the figure: 1 is the electromagnetic lock body; 2 is the bottom plate; 3 is the shell; 4 is the mounting plate; 5 is the through groove; 6 is the ground rod; 7 is the connecting mechanism; 71 is the micro cylinder; 72 is the rotating shaft; 73 is the rod; 74 is the connecting plate; 75 is the first arc clamping plate; 76 is the waterproof cover; 8 is the interface; 9 is the disassembly and assembly mechanism; 901 is the cylinder; 902 is the circular groove; 903 is the vertical axis; 904 is the conical head; 905 is the slot; 906 is the hollow column; 907 is the first electromagnet; 908 is the sliding sleeve; 909 is the extrusion layer; 910 is the hollow groove; 911 is the convex ring; 912 is the first spring; 913 is the conical groove; 914 is the limit groove; 915 is the block; 916 is the plug block; 917 is the second electromagnet; 11 is the aviation plug; 12 is the second spring; 13 is the second arc clamping plate; 14 is the micro switch. DETAILED DESCRIPTION

[0020] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0021] In the description of the present invention, it should be noted that the orientation or positional relationship indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inside", "outside", etc. is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention 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 cannot be understood as limiting the present invention. In addition, the terms "first", "second", and "third" are only used for descriptive purposes and cannot be understood as indicating or implying relative importance. In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", and "set" 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, or it can be the internal connection of two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific circumstances. The following is an explanation of its embodiments based on the overall structure of the present invention.

[0022] like Figures 1 to 3As shown, in an embodiment of the present invention, a grounding electromagnetic lock based on aviation plug integration technology includes an electromagnetic lock body 1, the electromagnetic lock body 1 includes a bottom plate 2, a shell 3 and a disassembly mechanism 9, the disassembly mechanism 9 is arranged at the four corners of the bottom plate 2 and the shell 3, the bottom of the bottom plate 2 is provided with a mounting plate 4, the surface of the mounting plate 4 is provided with a through groove 5, the electromagnetic lock body 1 is provided with a grounding rod 6, and the grounding rod 6 is inserted in the through groove 5, the bottom of the mounting plate 4 is provided with a connecting mechanism 7, the connecting mechanism 7 is used to install grounding rods 6 of different diameters, and the grounding rods 6 of different diameters are connected to the grounding rods 6 of different diameters. Figure 5 As shown, the bottom plate 2 and the housing 3 are connected by a disassembly mechanism 9. The bottom plate 2 and the housing 3 are quickly disassembled and assembled by the disassembly mechanism 9 without using screws, thereby shortening the time for repairing and replacing the electromagnetic lock body 1.

[0023] like Fig.10 As shown, an interface 8 is provided at the bottom of the electromagnetic lock body 1, and an aviation plug 11 is inserted into the interface 8. The wires connected to the electromagnetic lock body 1 are first connected to the aviation plug 11, and then the aviation plug 11 is inserted into the interface 8. The aviation plug 11 is used to arrange and combine the messy wires to achieve orderly access, which is convenient for subsequent maintenance and replacement.

[0024] Furthermore, if Figure 4 , Figure 7 and Fig. 9 As shown, the connection mechanism 7 includes a micro cylinder 71 fixed to the bottom of the mounting plate 4, and the bottom of the mounting plate 4 is rotatably connected to two rods 73 through a rotating shaft 72. A connecting plate 74 is fixed to the output end of the micro cylinder 71, and both ends of the connecting plate 74 are rotatably connected to the two rods 73. A first arc-shaped clamping plate 75 is fixed to one end of the two rods 73, and the through groove 5 is located on the inner side of the two first arc-shaped clamping plates 75. It should be noted that the grounding rod 6 is installed in the electromagnetic lock body 1, and the output end of the micro cylinder 71 extends to move with the connecting plate 74, and then the two rods 73 rotate in the opposite direction to move with the two first arc-shaped clamping plates 75 in the opposite direction. The first arc-shaped clamping plate 75 is conducive to clamping grounding rods 6 of different diameters, so as to adapt to grounding rods 6 of different diameters, and the electromagnetic lock body 1 is provided with a voice prompt function, which can voice prompt the status of the switch node to facilitate fault maintenance. A waterproof cover 76 is provided on the outside of the micro cylinder 71 to protect the micro cylinder 71.

[0025] The disassembly and assembly mechanism 9 includes a first connection part and a second connection part, the first connection part is mounted on the shell 3, the second connection part is fixed on the mounting plate 2, and the shell 3 and the bottom plate 2 are connected via the first connection part and the second connection part.

[0026] The housing 3 is connected to the base plate 2 by connecting the first connecting portion and the second connecting portion.

[0027] Specifically, refer to Figure 5 and Figure 6The first connecting part includes a cylinder 901 fixed to the bottom of the shell 3, a circular groove 902 is arranged on the outside of the cylinder 901, and the other end of the cylinder 901 is connected to a conical head 904 through a vertical shaft 903. The diameter of the vertical shaft 903 is smaller than the diameters of the cylinder 901 and the conical head 904, so that a slot 905 is formed in the peripheral area of ​​the vertical shaft 903.

[0028] The second connection part includes a hollow column 906 disposed on the bottom plate 2, the bottom of the hollow column 906 extends out of the bottom plate 2, a first electromagnet 907 is fixed to the bottom of the hollow column 906, an iron sleeve 908 is slidably connected to the outside of the hollow column 906, the sleeve 908 includes an extrusion layer 909 and a hollow groove 910, a convex ring 911 is fixed to the bottom of the hollow column 906, a first spring 912 is disposed outside the hollow column 906, the first spring 912 is located between the sleeve 908 and the convex ring 911, and a conical groove 913 is disposed at the bottom of the hollow column 906; Limiting grooves 914 are evenly distributed on the outside of the hollow column 906 , and spherical clamping blocks 915 are arranged inside the limiting grooves 914 . The clamping blocks 915 are used to cooperate with the circular grooves 902 .

[0029] The limiting groove 914 is wide at one side close to the extrusion layer 909 and narrow at one side away from the extrusion layer 909 , and the narrowest part of the limiting groove 914 is larger than the diameter of the block 915 , so as to prevent the block 915 from falling out of the limiting groove 914 .

[0030] An iron plug 916 is disposed inside the hollow column 906. The plug 916 is deformable and connected to each other to form a whole. A second electromagnet 917 is disposed at the bottom of the hollow column 906. When the second electromagnet 917 is powered on, the plug 916 moves toward the side close to the second electromagnet 917. When the second electromagnet 917 is powered off, the plug 916 is reset and enters the slot 905. When the first electromagnet 907 and the second electromagnet 917 are powered on at the same time, the first connecting portion can be inserted into the second connecting portion. When the first electromagnet 907 and the second electromagnet 917 are powered off, the first connecting portion is connected to the second connecting portion.

[0031] Optionally, the housing 3 of the electromagnetic lock body 1 is separately provided with a button for controlling the first electromagnet 907 and the second electromagnet 917 , and the button is separate from the indication button and the operation button.

[0032] It should be noted that the first electromagnet 907 and the second electromagnet 917 are energized by the button of the electromagnetic lock body 1. When the first electromagnet 907 is energized, the iron sleeve 908 is attracted by a strong magnetic force, and then the sleeve 908 descends outside the hollow column 906 and compresses the first spring 912. When the sleeve 908 descends, the extrusion layer 909 on the inner side thereof leaves the position of the block 915, and the hollow groove 910 moves to the position of the block 915, and then the extrusion layer 909 presses against the block 915. The pressure disappears, and the block 915 can move between the limit groove 914 and the hollow groove 910. The limit groove 914 is wider on the side close to the extrusion layer 909 and narrower on the side away from the extrusion layer 909. The narrowest part of the limit groove 914 is larger than the diameter of the block 915, so as to prevent the block 915 from falling out of the limit groove 914. After the second electromagnet 917 is energized, the plug 916 is attracted, and then the plug 916 is deformed and close to the inner wall of the hollow column 906, and then the cylindrical 901 at the bottom of the shell 3 is Insert the conical head 904 into the interior of the hollow column 906, and then the conical head 904 moves into the interior of the conical groove 913, and the circular groove 902 is just located at the position of the block 915, and then the first electromagnet 907 and the second electromagnet 917 are powered off, and the adsorption force of the first electromagnet 907 on the sliding sleeve 908 disappears after the power is turned off, and then the first spring 912 is reset to drive the sliding sleeve 908 to rise, and then the squeezing layer 909 rises and re-presses the block 915, forcing the block 915 to enter the interior of the slot 905, and the second electromagnet After the iron 917 is powered off, the plug block 916 recovers its deformation, and then multiple plug blocks 916 enter the interior of the circular groove 902, which is conducive to firmly fixing the cylinder 901 inside the hollow column 906 through the coordinated use of the clamping block 915 and the plug block 916, and then fixing the shell 3 on the top of the bottom plate 2. When the electromagnetic lock body 1 needs to be disassembled and repaired, the first electromagnet 907 and the second electromagnet 917 are energized again, and the plug block 916 leaves the slot 905, and then the bottom plate 2 can be separated from the shell 1.

[0033] like Figure 8 As shown, further, a second spring 12 is fixed on the inner side of the through slot 5, a second arc-shaped clamping plate 13 is fixed on one end of the second spring 12, and a micro switch 14 is arranged on the inner side of the second arc-shaped clamping plate 13. The second spring 12 is arranged so that the second arc-shaped clamping plate 13 can adapt to grounding rods 6 of different diameters. Due to the rebound force of the second spring 12, grounding rods 6 of different sizes and diameters can be fitted with the second arc-shaped clamping plate 13, so that grounding rods 6 of different diameters can be in contact with the micro switch 14, and then the installed grounding rod 6 is clamped and fixed with the micro cylinder 71.

[0034] The electromagnetic lock body 1 is provided with four modules inside, including a shell structure module, a logic locking module, a manual unlocking module, and a power supply module. The modular design makes the modules replaceable and easy to assemble, saving the maintenance time of the electromagnetic lock body 1. The shell structure adopts a double-compartment design, which can realize the isolation of the lock body side and the power supply side, protect the internal components, and reduce the humidity in the cabin. The logic locking, mechanical unlocking, status indicator light and operation buttons are in one compartment, and the aviation plug terminal and the step-down module are in another compartment. A waterproof strip and an inner guide groove are added to the gap between the lock body compartment and the power supply compartment of the electromagnetic lock body 1, and a waterproof gasket is added to the grounding wire hole. This design prevents water drops and condensation from forming between the lock body compartment and the power supply compartment. The logic interlocking module adopts relay type, which has low manufacturing cost, long service life, reliable contact output and fast response. All logic interlocking is realized through relays, and more contacts are introduced through a small number of mechanical switches. The manual unlocking module includes a step-down module, a protection module, and an operation module. The step-down module converts 220V AC into 12V DC to reduce the risk of electric shock to personnel and increase the module replacement speed to less than 60s. The step-down module is plug-in type, and the power supply incoming line connection line, status indicator light, and operation button connection line are connected to the circuit board through a connector, which shortens the replacement time. The plug-in output ripple is less than <100mV, the module load short-circuit response time is short, it has excellent waterproof performance and long service life. The plug-in type is specifically encapsulated, and the overall potting glue treatment meets the requirements of the selection basis. The protection module can protect the wiring inside the lock body and prevent the mechanical device from wearing out the wiring insulation. The protection module is isolated by a metal baffle. A metal isolation baffle is installed above the coil transmission sheet. The indicator light connection line, button connection line, and coil connection line are tied with cable ties to fully isolate the connection line from the transmission sheet. After the metal isolation baffle is installed, the transmission sheet scratch rate is 0 and the service life is long. The operation module is convenient for replacing frequently damaged parts and reducing maintenance costs. The operation module adopts split installation and has a long service life. The power supply module can be hot-swapped in less than 10 seconds, quickly introduced into and out of the device, and reduces the incidence of short-circuit failures during wiring. It uses a screw-locking aviation plug with high reliability and short production time.

[0035] Working principle: through the disassembly structure 9, the first electromagnet 907 and the second electromagnet 917 are energized through the button of the electromagnetic lock body 1. When the first electromagnet 907 is energized, the iron sleeve 908 is attracted by the strong magnetic force, and then the sleeve 908 descends outside the hollow column 906 and compresses the first spring 912. When the sleeve 908 descends, the extrusion layer 909 on the inner side leaves the position of the block 915, and the hollow groove 910 moves to the position of the block 915. Then the pressure of the extrusion layer 909 on the block 915 disappears, and the block 915 can be in the limit groove 914 and The limiting groove 914 is wider on one side close to the extrusion layer 909 and narrower on the other side away from the extrusion layer 909. The narrowest part of the limiting groove 914 is larger than the diameter of the block 915 to prevent the block 915 from falling out of the limiting groove 914. After the second electromagnet 917 is energized, the plug block 916 is adsorbed, and then the plug block 916 is deformed and close to the inner wall of the hollow column 906. Then, the cylinder 901 at the bottom of the shell 3 is inserted into the interior of the hollow column 906. Then, the conical head 904 moves into the interior of the conical groove 913, and the circular groove 902 is just located at the position of the block 915. Then, the first electromagnet 917 is energized. The magnet 907 and the second electromagnet 917 are powered off. After the first electromagnet 907 is powered off, the adsorption force on the sliding sleeve 908 disappears, and then the first spring 912 is reset to drive the sliding sleeve 908 to rise, and then the extrusion layer 909 rises and re-presses the block 915, forcing the block 915 to enter the inside of the slot 905. After the second electromagnet 917 is powered off, the plug block 916 recovers its deformation, and then multiple plug blocks 916 enter the inside of the circular groove 902, which is conducive to firmly fixing the cylinder 901 inside the hollow column 906 through the cooperation of the block 915 and the plug block 916, and then fixing the shell 3 on the bottom plate 2. When the electromagnetic lock body 1 needs to be disassembled and repaired, the first electromagnet 907 and the second electromagnet 917 are energized again, and the plug block 916 is removed from the slot 905, and then the bottom plate 2 can be separated from the shell 1, which is conducive to the disassembly and installation of the electromagnetic lock body 1 by powering off and on the first electromagnet 907 and the second electromagnet 917. The whole process takes a short time, which is conducive to solving the problem that the screws are removed by a screwdriver and then the shell is opened during the existing maintenance, and the screws are fixed after the maintenance is completed. Due to the large number of screws and the need to use a screwdriver, the whole disassembly and assembly process is cumbersome and time-consuming. Through the connection mechanism 7, the grounding rod 6 is installed in the electromagnetic lock body 1, the output end of the micro cylinder 71 extends out and moves with the connecting plate 74, and then the two rods 73 rotate in the opposite direction and move with the two first arc clamping plates 75 in the opposite direction. The first arc clamping plates 75 are conducive to clamping grounding rods of different diameters, so as to adapt to grounding rods of different diameters. In addition, the electromagnetic lock body 1 is provided with a voice prompt function, which can voice prompt the status of the switch node, which is convenient for fault maintenance. The electromagnetic lock body 1 is provided with four modules inside, including a shell structure module, a logic locking module, a manual unlocking module, and a power supply module. The modular design makes the modules replaceable and easy to assemble, saving the maintenance time of the electromagnetic lock body 1. The shell structure adopts a double-compartment design, which can realize the isolation of the lock body side and the power supply side, protect the internal components, and reduce the humidity in the cabin. The logic locking, mechanical unlocking, status indicator light and operation buttons are in one compartment, and the aviation plug terminal and the step-down module are in another compartment. A waterproof strip is added to the gap between the lock body compartment and the power supply compartment of the electromagnetic lock body 1. The diversion groove and the grounding wire hole are equipped with waterproof gaskets. This design makes the lock body compartment and the power supply compartment free of water drops and condensation. The logic interlocking module adopts relay type, which has low manufacturing cost, long service life, reliable contact output and fast response. All logic interlocks are realized through relays, and more contacts are introduced through a small number of mechanical switches. The manual unlocking module includes a step-down module, a protection module and an operation module. The step-down module converts 220V AC into 12V DC to reduce the risk of electric shock to personnel and increase the module replacement speed to less than 60s. The step-down module adopts plug-in type to connect the power supply line The wires, status indicator lights and operation button connection wires are connected to the circuit board through connectors, and the required replacement time is short. The plug-in output ripple is less than <100mV, the module load short-circuit response time is short, it has excellent waterproof performance and long service life. The plug-in type is specifically encapsulated, and the overall potting glue treatment meets the requirements of the selection basis. The protection module can protect the wiring in the lock body and prevent the mechanical device from wearing the wiring insulation during movement. The protection module is isolated by a metal baffle, and a metal isolation baffle is installed above the coil transmission sheet. The indicator light connection wire, button connection wire, and coil connection wire are tied with cable ties Tie it up to fully isolate the connecting wire from the transmission sheet. After adding the metal isolation baffle, the transmission sheet scratch rate is 0 and it has a long service life. The operation module is convenient for replacing frequently damaged parts and reducing maintenance costs. The operation module adopts a split installation with a long service life. The power supply module can achieve hot plug-in as fast as less than 10 seconds, and can quickly introduce and disconnect equipment, reducing the occurrence rate of short-circuit failures during wiring. It adopts screw-locking aviation plug, which has high reliability and short production time. The modular design realizes the purpose of replaceability and easy assembly, greatly saving maintenance time, and the replacement is cumbersome, which can be completed by the operation and maintenance themselves.

[0036] The above are only preferred specific implementation modes of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes according to the technical solutions and inventive concepts of the present invention within the technical scope disclosed by the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A grounding electromagnetic lock based on aviation plug integration technology, comprising an electromagnetic lock body, characterized in that: The electromagnetic lock body includes a base plate, a shell and a disassembly and assembly mechanism, the disassembly and assembly mechanism is arranged at the four corners of the base plate and the shell, a mounting plate is arranged at the bottom of the base plate, a through groove is arranged on the surface of the mounting plate, a grounding rod is arranged on the electromagnetic lock body, and the grounding rod is inserted into the through groove, a connecting mechanism is arranged at the bottom of the mounting plate, the connecting mechanism is used to install grounding rods of different diameters, and the base plate and the shell are connected through the disassembly and assembly mechanism.

2. According to claim 1, a grounding electromagnetic lock based on aviation plug integration technology is characterized in that: An interface is provided at the bottom of the electromagnetic lock body, and an aviation plug is inserted into the interface.

3. The grounding electromagnetic lock based on aviation plug integration technology according to claim 1 is characterized in that: The connecting mechanism includes a micro cylinder fixed to the bottom of the mounting plate, the bottom of the mounting plate is rotatably connected to two rods via a rotating shaft, a connecting plate is fixed to the output end of the micro cylinder, both ends of the connecting plate are rotatably connected to the two rods, a first arc-shaped clamping plate is fixed to one end of the two rods, and the through groove is located on the inner side of the two first arc-shaped clamping plates.

4. The grounding electromagnetic lock based on aviation plug integration technology according to claim 1 is characterized in that: The disassembly and assembly mechanism includes a first connecting part and a second connecting part, the first connecting part is mounted on the shell, the second connecting part is fixed on the mounting plate, and the shell and the bottom plate are connected through the first connecting part and the second connecting part.

5. The grounding electromagnetic lock based on aviation plug integration technology according to claim 4 is characterized in that: The first connecting part includes a cylinder fixed to the bottom of the shell, a circular groove is arranged on the outside of the cylinder, and the other end of the cylinder is connected to a conical head through a vertical axis. The diameter of the vertical axis is smaller than the diameter of the cylinder and the conical head, so that a slot is formed in the peripheral area of ​​the vertical axis.

6. A grounding electromagnetic lock based on aviation plug integration technology according to claim 5, characterized in that: The second connecting part comprises a hollow column arranged on the bottom plate, the bottom of the hollow column extends out of the bottom plate, a first electromagnet is fixed to the bottom of the hollow column, an iron sleeve is slidably connected to the outside of the hollow column, the sleeve comprises an extrusion layer and a hollow groove, a convex ring is fixed to the bottom of the hollow column, a first spring is arranged outside the hollow column, the first spring is located between the sleeve and the convex ring, and a conical groove is arranged at the bottom of the hollow column; Limiting grooves are evenly distributed on the outside of the hollow column, and spherical clamping blocks are arranged inside the limiting grooves, and the clamping blocks are used to cooperate with the circular grooves.

7. The grounding electromagnetic lock based on aviation plug integration technology according to claim 6 is characterized in that: The limiting groove is wider at a side close to the extrusion layer and narrower at a side away from the extrusion layer, and the narrowest part of the limiting groove is larger than the diameter of the clamping block.

8. The grounding electromagnetic lock based on aviation plug integration technology according to claim 7 is characterized in that: An iron plug is arranged inside the hollow column, the plug is deformable and connected to each other to form a whole, and a second electromagnet is arranged at the bottom of the hollow column; when the second electromagnet is energized, the plug moves toward the side close to the second electromagnet, and when the second electromagnet is de-energized, the plug is reset and enters the slot.

9. The grounding electromagnetic lock based on aviation plug integration technology according to claim 8 is characterized in that: When the first electromagnet and the second electromagnet are powered on at the same time, the first connecting part can be inserted into the second connecting part, and when the first electromagnet and the second electromagnet are powered off, the first connecting part is connected to the second connecting part.

10. A grounding electromagnetic lock based on aviation plug integration technology according to any one of claims 1 to 9, characterized in that: The electromagnetic lock body is internally provided with a shell structure module, a logic locking module, a manual unlocking module and a power supply module.

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