Automatic aviation plug plugging operation tool, system and control method

Abstract

The invention discloses an automatic aviation plug plugging and unplugging operation tool, system and control method, and belongs to the technical field of plugs, the automatic aviation plug plugging and unplugging operation tool comprises a shell, a connecting structure and a control system, one end of the connecting structure is connected with a clamping plate, the other end of the connecting structure is clamped with a positioning structure rotationally arranged on an aviation plug, and the control system is connected with the shell. The clamping plate is in sliding connection with the semicircular sliding groove in the shell, one side of the clamping plate is meshed with the driving gear, the output end of the motor is connected with the driving gear, the motor is driven by the control system to drive the driving gear to rotate, the clamping plate slides along the semicircular sliding groove, then the connecting structure drives the positioning structure to rotate, and locking or unlocking of the aviation plug is achieved. According to the automatic aviation plug operation tool, the requirement for wide-range plug operation in a narrow moving space is met, the aviation plug process is simplified, automatic plug operation is achieved, and the operation precision and stability of the tool are improved.

Description

Technical Field

[0001] The present invention relates to the technical field of plugs, and in particular to an automatic aerial plugging and unplugging operation tool, system and control method. Background Art

[0002] With the widespread adoption of power systems, electricity has become an essential part of people's lives. 10kV high-voltage switchgear is widely used in power systems to receive and distribute electrical energy. It can be used to activate or deactivate certain electrical equipment or lines based on grid operation needs. It can also quickly disconnect faulty equipment or lines from the grid when they fail, ensuring the normal operation of the remaining grid and the safety of equipment and maintenance personnel. Therefore, high-voltage switchgear is a crucial piece of electrical equipment, and its safe and reliable operation is crucial to the power system.

[0003] During power system operation and maintenance, plugging and unplugging secondary plugs and sockets on high-voltage switchgear circuit breakers in the control room are often done manually, which is cumbersome and requires limited space. Operations such as plugging and unplugging, commissioning, and routine maintenance require on-site coordination. Due to limited space, these operations are tedious and time-consuming, resulting in poor O&M efficiency. When plugging and unplugging, aligning the plug and socket in the confined space is difficult and prone to errors. The insertion process is limited by space, resulting in low plugging and unplugging efficiency and inconvenient control. Summary of the Invention

[0004] In order to solve the deficiencies in the prior art, the present invention provides an automatic aerial plugging and unplugging operation tool, system and control method.

[0005] The present invention adopts the following technical solutions.

[0006] The present invention discloses an automatic aviation plug-in and pull-out operation tool, comprising: a shell, a connecting structure and a control system. One end of the connecting structure is connected to a clamping piece, and the other end is clamped to a positioning structure rotatably arranged on the aviation plug. The clamping piece is slidably connected to a semicircular groove on the shell. One side of the clamping piece is engaged with a driving gear. The output end of a motor is connected to the driving gear. The control system drives the motor to drive the driving gear to rotate, so that the clamping piece slides along the semicircular groove, and then the connecting structure drives the positioning structure to rotate, thereby locking or unlocking the aviation plug.

[0007] Preferably, the housing comprises: a rear cover, a housing lower plate and a side plate, the rear cover is provided on one side of the housing lower plate, a semicircular slide groove is provided on the other side, and the side plate is provided on the side surface of the housing lower plate between the rear cover and the semicircular slide groove; An electric push rod is installed on one side of the rear cover, and one end of the electric push rod passes through the rear cover and is connected to the pressure plate. When the aviation plug is in the unlocked state, the clamping part moves to one side, and the pressure plate is driven forward by starting the electric push rod until it presses against the side of the aviation plug, so that the aviation plug connection is stable in the unlocked state.

[0008] Preferably, the bottom of one side of the lower plate of the shell is fixedly connected to the left support plate, and a protruding plate is provided on the other side. The protruding plate is fixedly connected to the right limiting top plate. The aviation plug is supported from the bottom by the left support plate and supported from one side by the right limiting top plate.

[0009] Preferably, the control system includes: a communication module and a relay, the communication module sends out an opening and closing signal, controls the current flow through the relay, and then operates the motor to start and close, so that the clamping part moves to a preset position and stops automatically.

[0010] The present invention also discloses a system of automatic aerial plugging and unplugging operation tools, based on the automatic aerial plugging and unplugging operation tools, including: aerial plugging and unplugging operation tools, The aviation plug includes: a fixed aviation plug, a detachable aviation plug and a positioning structure. The positioning structure is set on the detachable aviation plug. The detachable aviation plug sleeve is set on the outer surface of the fixed aviation plug. The connecting structure on the plugging and unplugging operation tool clamps the positioning structure. The positioning structure is driven to rotate by driving the connecting structure to achieve locking or unlocking of the fixed aviation plug and the detachable aviation plug.

[0011] Preferably, one side of the fixed aviation plug is fixed on a plane, a fixed protrusion is provided on the upper side of the fixed aviation plug, a fixing hole is provided at the position corresponding to the fixed protrusion of the disassembly aviation plug, and the disassembly aviation plug is sleeved on the outer surface of the fixed aviation plug by snapping the fixing hole into the fixed protrusion.

[0012] Preferably, the positioning structure includes: an upper locking plate, a lower locking plate and a connecting plate. The upper and lower surfaces of the disassembled aviation plug are hinged to the upper locking plate and the lower locking plate through hinge shafts respectively. The other ends of the upper and lower locking plates are fixed through the connecting plate. The connecting structure clamps the connecting plate, and a locking hole is set at the front end of the upper locking plate corresponding to the fixed hole position.

[0013] Preferably, when the upper and lower locking pieces are set as vertical aviation plugs, the front end of the upper locking piece does not block the fixing hole, the removed aviation plug and the fixed aviation plug are in the unlocked state, the connecting structure clamps the connecting piece, and the connecting structure drives the connecting piece to rotate circumferentially, so that the upper and lower locking pieces rotate around the hinge axis until the upper and lower locking pieces are set as parallel aviation plugs, the fixing protrusion slides into the locking hole and the front end of the upper locking piece blocks the fixing hole to lock the fixed aviation plug and the removed aviation plug.

[0014] The present invention also discloses a control method for an automatic aerial plugging and unplugging operation tool, which comprises the following steps: When the aviation plug is in the unlocked state, the positioning structure is set perpendicular to the aviation plug, and the connecting structure clamps the positioning structure; The control system drives the connection structure to slide circumferentially until the positioning structure is parallel to the aviation plug and the aviation plug is locked; The control system drives the connection structure to slide circumferentially in reverse, so that the positioning structure returns to the vertical aviation plug setting, and then performs plugging and unplugging operations to achieve the fixation and separation of the aviation plug.

[0015] The present invention also discloses an electronic device, comprising a memory, a processor, and a computer program stored in the memory and executable on the processor. The electronic device is characterized in that when the computer program is loaded into the processor, a control method for an automatic aerial plug-in and unplug-out operation tool is implemented.

[0016] The present invention also discloses a computer-readable storage medium, which stores a computer program. The computer-readable storage medium is characterized in that when the computer program is executed by a processor, the control method of the automatic aerial plug-in and plug-out operation tool is implemented.

[0017] The beneficial effect of the present invention is that, compared with the prior art, Automatic aerial plugging and unplugging operation tools that meet the needs of narrow mobile spaces and large-scale plugging and unplugging operations simplify the aerial plugging and unplugging process, realize automatic plugging and unplugging work, and improve the operating accuracy and stability of the tool.

[0018] The present invention drives the card connector to slide along the semicircular groove through the control system, so that the connecting structure drives the positioning structure to rotate, thereby realizing locking or unlocking of the aviation plug, automating locking and unlocking, simplifying the operation process, reducing the number of personnel required for on-site operation, reducing operation complexity, improving plugging and unplugging efficiency, occupying a small space, and realizing accurate and reliable automated aviation plugging and unplugging work in narrow spaces and over a large range.

[0019] The left support plate is used to support the removed aviation plug from the bottom, and the right limit top plate is used to support the removed aviation plug from one side, forming a two-way support to avoid unstable connection during installation and removal. At the same time, the electric push rod is started to drive the pressure plate to move forward until it supports the rear side of the removed aviation plug, so that the aviation plug connection is stable in the unlocked state, avoiding direct falling off in the unlocked state, thereby improving safety.

[0020] The present invention can realize automatic plugging and disassembly of the aviation plug by connecting the quick-change disk and the end of the mechanical arm, thereby further improving the degree of automation. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 It is a structural diagram of the present invention; Figure 2 This is a diagram of the aviation plug connection structure of the present invention; Figure 3 This is a structural diagram of the aerial insertion separation of the present invention; In the figure: 1-adapter bracket, 2-motor, 3-driving gear, 4-back cover, 5-housing lower plate, 6-communication module, 7-side plate, 8-electric push rod, 9-clamping part, 10-connecting structure, 101-first clamping plate, 102-second clamping plate, 103-clamping block 1, 104-clamping block 2, 105-compression spring, 106-connecting plate, 11-right limit top plate, 12-left support plate, 13-semicircular slide groove, 1 4-Aviation plug, 141-Fixed aviation plug, 1411-Fixed protrusion, 142-Removable aviation plug, 143-Hinge shaft, 144-Locking piece, 1441-Upper locking plate, 1442-Lower locking plate, 1443-Locking hole, 145-Fixed protrusion, 146-Fixed plate, 147-Connecting plate, 148-Fixed hole, 15-Relay, 16-Gear ring, 17-Protruding plate, 18-Quick change plate; 19-Pressure plate. DETAILED DESCRIPTION

[0022] To make the objectives, technical solutions, and advantages of the present invention more clear, the technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. The embodiments described in this application are only part of the embodiments of the present invention, not all of them. Based on the spirit of the present invention, other embodiments obtained by ordinary technicians in this field without making creative efforts are all within the scope of protection of the present invention.

[0023] In the description of the present invention, it should be understood that the terms "center", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "axial", "radial", "circumferential", etc., indicating the orientation or position relationship, are based on the orientation or position relationship shown in the accompanying drawings, and are 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 operate in a specific orientation, and therefore cannot be understood as limiting the present invention.

[0024] like Figure 1-Figure 3 As shown, embodiment 1 of the present invention provides an automatic aerial plugging and unplugging operation tool, the automatic aerial plugging and unplugging operation tool comprising: a housing, a connecting structure 10 and a control system; One end of the connecting structure 10 is connected to the side end of the clamping member 9, and the other end is clamped to the positioning structure rotatably arranged on the aviation plug 14. The clamping member 9 is slidably connected to the semicircular groove 13 on the shell. One side of the clamping member 9 is meshed with the driving gear 3, and the other end is fixedly connected to the connecting structure 10. The driving gear 3 is arranged on one side of the semicircular groove 13. The output end of the motor 2 passes through the shell and is fixedly connected to the driving gear 3. The motor 2 is driven by the control system to drive the driving gear 3 to rotate, so that the clamping member 9 slides along the semicircular groove 13, and then the connecting structure 10 drives the positioning structure to rotate, thereby locking or unlocking the aviation plug 14.

[0025] like Figure 1 As shown, the housing includes: a rear cover 4, a lower housing plate 5 and a side plate 7. The rear cover 4 is provided on one side of the lower housing plate 5, and a semicircular slide groove 13 is provided on the other side. The side plate 7 is provided between the semicircular slide groove 13 and the rear cover 4 on the side of the lower housing plate 5. like Figure 1 As shown, the connecting structure 10 includes: a first clamping plate 101, a second clamping plate 102, a clamping block 103, a clamping block 2 104, a compression spring 105 and a connecting plate 106, one side of the connecting plate 106 is fixedly connected to the side end of the clamping member 9, and the other side is fixedly connected to the second clamping plate 102, the middle of the second clamping plate 102 is hinged to the first clamping plate 101, a compression spring 105 is provided on one side between the first clamping plate 101 and the second clamping plate 102, a clamping block 2 104 is provided at one end of the first clamping plate 101 away from the compression spring 105, and a clamping block 103 is provided at one end of the second clamping plate 102 corresponding to the clamping block 2 104, the clamping area of ​​the clamping plate is increased by the two clamping blocks, the friction force when the clamping plate clamps the positioning structure of the aviation plug 14 is enhanced, and the stable clamping of the connecting piece 147 on the aviation plug 14 is achieved.

[0026] In a specific embodiment, the first clamping plate 101 is pressed to squeeze the compression spring 105 to separate the clamping block 103 and the clamping block 2 104, and the connecting piece 147 on the disassembled aviation plug 142 is set between the two clamping blocks. The first clamping plate 101 is released, and the clamping block 103 and the clamping block 2 104 automatically clamp and fix the connecting piece 147, and the connecting piece 147 is further clamped and fixed by the elastic force of the compression spring 105.

[0027] like Figure 2 and Figure 3 As shown, one side of the bottom of the lower plate 5 of the shell is fixedly connected to the left support plate 12, and a protruding plate 17 is provided on the other side. One end of the protruding plate 17 is fixedly connected to the right limiting top plate 11. The left support plate 12 can be used to support and remove the aviation plug 142 from the bottom. The side of the removed aviation plug 142 abuts against the right limiting top plate 11, so that the right limiting top plate 11 and the removed aviation plug 142 abut against each other to form a two-way support, thereby avoiding unstable connection during installation and removal.

[0028] like Figure 2 and Figure 3 As shown, an electric push rod 8 is installed on the back cover 4, and one end of the electric push rod 8 passes through the back cover 4 and is connected to the pressure plate 19. When one side of the clamping part 9 moves to the end of the semicircular groove 13, the disassembly aviation plug 142 and the fixed aviation plug 141 are unlocked, and the electric push rod 8 starts to drive the pressure plate 19 close to the aviation plug 14 until it supports the rear side of the disassembly aviation plug 142, preventing the disassembly aviation plug 142 from falling off directly after unlocking, thereby improving the disassembly stability.

[0029] like Figure 2 and Figure 3As shown, the control system includes: a communication module 6 and a relay 15. The communication module 6 sends an opening and closing signal to the relay 15 to control the operation of the relay 15. The relay 15 controls the direction of current flow to manipulate the forward and reverse directions of the motor 2, so that the clamping part 9 repeatedly moves in a circular motion until it reaches a preset position and stops automatically.

[0030] Preferably, the communication module 6 is implemented using existing technical means.

[0031] The adapter bracket 1 is provided in the center of the rear cover 4, and a quick-change disk 18 is provided at one end of the adapter bracket 1. The quick-change disk 18 can be connected to the end of the robotic arm, and the unlocked removal aviation plug 142 can be automatically inserted into or removed from the fixed aviation plug 141 by pushing and pulling the robotic arm. It can also be inserted and removed manually. like Figure 2 and Figure 3 As shown, embodiment 2 of the present invention discloses a system for automatic aerial plugging and unplugging operation tools, including: aerial plug 14 and plugging and unplugging operation tools; like Figure 2 and Figure 3 As shown, the aviation plug 14 includes: a fixed aviation plug 141, a disassembly aviation plug 142 and a positioning structure. A fixing plate 146 is provided on one side of the fixed aviation plug 141. The fixed aviation plug 141 is fixedly provided on a plane through the fixing plate 146 and is then installed at any position in the high-voltage switch cabinet. The disassembly aviation plug 142 is sleeved on the outer surface of the fixed aviation plug 141. A fixing protrusion 145 is provided on the upper side of the fixed aviation plug 141. A fixing hole 148 is provided at the position of the disassembly aviation plug 142 corresponding to the fixing protrusion 145. By aligning the fixing hole 148 with the fixing protrusion 145 and snapping it in, the disassembly aviation plug 142 is accurately sleeved on the fixed aviation plug 141 to achieve precise positioning and fixation. like Figure 2 and Figure 3 As shown, the positioning structure includes: an upper locking piece 1441, a lower locking piece 1442 and a connecting piece 147. The upper and lower surfaces of the disassembled aviation plug 142 are hinged to the upper locking piece 1441 and the lower locking piece 1422 at the same position through a hinge shaft 143. The upper locking piece 1441 and one end of the lower locking piece 1422 are fixedly connected through a connecting piece 147. A locking hole 1443 is set at the front end of the upper locking piece 1441 at a position corresponding to the fixing hole 148. The clamping block 103 and the clamping block 2 104 on the connecting structure 10 clamp the connecting piece 147, and then the connecting piece 147 is rotated by driving the connecting structure 10.

[0032] In a specific embodiment, when the upper and lower locking pieces of the disassembly aviation plug 142 are set perpendicular to the aviation plug 14, the end of the upper locking piece 1441 does not block the fixing hole 148. The fixing hole 148 on the disassembly aviation plug 142 is aligned with the fixing protrusion 145 on the fixed aviation plug 141 and is snapped in, so that the disassembly aviation plug 142 is sleeved on the fixed aviation plug 141 and is in an unlocked state. At this time, the connecting piece 147 is driven to rotate by the connecting structure 10, so that the upper and lower locking pieces rotate around the hinge shaft 143 until the upper and lower locking pieces are set parallel to the aviation plug 14, the fixing protrusion 145 completely slides into the locking hole 1443 and the end of the upper locking piece 1441 blocks the fixing hole 148, thereby locking the fixed aviation plug 141 and the disassembly aviation plug 142.

[0033] The working principle of the present invention is as follows: when the upper and lower locking pieces at both ends of the connecting piece 147 are set to be perpendicular to the aviation plug 14, the front end of the upper locking piece 1441 is not blocked by the fixing hole 148, and the fixing hole 148 on the disassembly aviation plug 142 is aligned with the fixing protrusion 145 on the fixed aviation plug 141 and snapped in, so that the disassembly aviation plug 142 is sleeved on the fixed aviation plug 141 and is in the unlocked state. At this time, the starting motor 2 drives the driving gear 3 to rotate and drive the clamping part 9 to slide along the semicircular groove 13, and the connecting structure 10 drives the connecting piece 147 to rotate to the right, so that the upper and lower locking pieces rotate to the right with the hinge shaft 143 as the center, until the upper and lower locking pieces are parallel to the aviation plug When the plug 14 is set, the fixing protrusion 145 slides completely into the locking hole 1443 and the front end of the upper locking piece 1441 blocks the fixing hole 148, locking the fixed aviation plug 141 and the disassembly aviation plug 142. When disassembling, the driving gear 3 is driven in reverse by the motor 2 to rotate, so that the connecting structure 10 drives the connecting piece 147 to rotate to the left, and the upper and lower locking pieces rotate to the left with the hinge shaft 143 as the center, until the upper and lower locking pieces are set in the front and rear directions, the fixing protrusion 145 slides completely out of the locking hole 1443 and there is no obstruction in front of the fixing hole 148, pull out the disassembly aviation plug 142, and separate the disassembly aviation plug 142 from the fixed aviation plug 141.

[0034] The present invention drives the clamping member 9 to slide along the semicircular groove 13, so that the connecting structure drives the positioning structure to rotate, thereby realizing automatic locking and unlocking of the aviation plug, simplifying the operation process, reducing the number of personnel required for on-site operation, reducing the complexity of operation, improving the plugging and unplugging efficiency, occupying a small space, and realizing accurate and reliable automatic aviation plugging and unplugging work in narrow spaces and over a large range.

[0035] Embodiment 3 of the present invention provides a control method for an automatic aerial plugging and unplugging operation tool, comprising the following steps: Step 1: When the aviation plug 14 is in the unlocked state, the positioning structure is arranged perpendicular to the aviation plug 14, and the connecting structure 10 clamps the positioning structure; Step 1.1: One side of the clamping member 9 is located at the end of the semicircular groove 13, and the other side of the fixed connection structure 10 presses the first clamping plate 101 to squeeze the compression spring 105, so that the clamping block 103 and the clamping block 2 104 are separated; Step 1.2: Place the connecting piece 147 on the disassembled aviation plug 142 between the two clamping blocks, loosen the first clamping plate 101, and the clamping block 103 and the clamping block 2 104 automatically clamp the connecting piece 147 under the force of the compression spring 105; Step 2: The control system drives the connecting structure 10 to slide circumferentially until the positioning structure is parallel to the aviation plug 14 and the aviation plug 14 is in a locked state; Step 2.1: The communication module 6 of the control system sends a positive start signal to the relay 15, so that the relay 15 controls the current to flow in the positive direction and thus controls the motor 2 to start; Step 2.2: The motor 2 drives the driving gear 3 to rotate, driving the clamping member 9 to slide along the semicircular groove 13, and the connecting structure 10 drives the positioning structure to slide circumferentially; Step 2.3: until the side of the connecting structure 10 provided by the clamping member 9 moves to the end of the semicircular slide groove 13, the positioning structure is arranged parallel to the aviation plug 14, and the aviation plug 14 is locked; Step 3: The control system drives the connecting structure 10 to slide circumferentially in reverse until the positioning structure is set perpendicular to the aviation plug 14. The aviation plug 14 is in an unlocked state, and the plugging and unplugging operation is performed to fix and separate the aviation plug 14.

[0036] Step 3.1: The communication module 6 sends a reverse start signal to the relay 15, causing the relay 15 to control the current to flow in the reverse direction and thereby operate the motor 2 to start in the reverse direction; Step 3.2: The motor 2 drives the driving gear 3 to rotate in the reverse direction, driving the clamping part 9 to slide along the semicircular groove 13 to return to its original position. The connecting structure 10 drives the positioning structure to slide circumferentially, so that the positioning structure returns to the vertical aviation plug 14 setting, and then the plug-in and pull-out operation is performed to achieve the fixation and separation of the aviation plug 14.

[0037] The present invention switches the rotation direction of the motor 2 through the control system, thereby causing the driving gear 3 to rotate in forward and reverse directions, driving the clamping member 9 to slide repeatedly along the semicircular groove 13, causing the connecting structure 10 to drive the positioning structure to rotate circumferentially, thereby realizing automatic locking and unlocking of the aviation plug 14, simplifying the operating process, reducing the number of personnel required for on-site operation, reducing operational complexity, improving plugging and unplugging efficiency, occupying a small space, and realizing accurate and reliable automatic aviation plugging and unplugging work in narrow spaces and over a large range.

[0038] Embodiment 4 of the present invention provides an electronic device, including a memory, a processor, and a computer program stored in the memory and executable on the processor. When the computer program is loaded into the processor, a control method for an automatic aerial plug-in and unplug-out operation tool according to embodiment 3 is implemented.

[0039] Embodiment 5 of the present invention provides a computer-readable storage medium storing a computer program. When the computer program is executed by a processor, the control method of the automatic aerial plugging and unplugging operation tool according to embodiment 3 is implemented.

[0040] The beneficial effect of the present invention is that, compared with the prior art, Automatic aerial plugging and unplugging operation tools that meet the needs of narrow mobile spaces and large-scale plugging and unplugging operations simplify the aerial plugging and unplugging process, realize automatic plugging and unplugging work, and improve the operating accuracy and stability of the tool.

[0041] The present invention drives the card connector to slide along the semicircular groove through the control system, so that the connecting structure drives the positioning structure to rotate, thereby realizing locking or unlocking of the aviation plug, automating locking and unlocking, simplifying the operation process, reducing the number of personnel required for on-site operation, reducing operation complexity, improving plugging and unplugging efficiency, occupying a small space, and realizing accurate and reliable automated aviation plugging and unplugging work in narrow spaces and over a large range.

[0042] The left support plate is used to support the removed aviation plug from the bottom, and the right limit top plate is used to support the removed aviation plug from one side, forming a two-way support to avoid unstable connection during installation and removal. At the same time, the electric push rod is started to drive the pressure plate to move forward until it supports the rear side of the removed aviation plug, so that the aviation plug connection is stable in the unlocked state, avoiding direct falling off in the unlocked state, thereby improving safety.

[0043] The present invention can realize automatic plugging and disassembly of the aviation plug by connecting the quick-change disk and the end of the mechanical arm, thereby further improving the degree of automation.

[0044] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention rather than to limit it. Although the present invention has been described in detail with reference to the above embodiments, ordinary technicians in the field should understand that the specific implementation methods of the present invention can still be modified or replaced by equivalents. Any modification or equivalent replacement that does not depart from the spirit and scope of the present invention should be covered by the scope of protection of the claims of the present invention.

Claims

1. An automatic aerial plug-in and plug-out operation tool, comprising: The housing, the connecting structure (10) and the control system are characterized by: One end of the connecting structure (10) is connected to the clamping member (9), and the other end is clamped to a positioning structure rotatably arranged on the aviation plug (14). The clamping member (9) is slidably connected to the semicircular groove (13) on the shell. One side of the clamping member (9) is meshed with the driving gear (3). The output end of the motor (2) is connected to the driving gear (3). The control system drives the motor (2) to drive the driving gear (3) to rotate, so that the clamping member (9) slides along the semicircular groove (13), and then the connecting structure (10) drives the positioning structure to rotate, thereby achieving locking or unlocking of the aviation plug (14).

2. The automatic aerial plugging and unplugging operation tool according to claim 1, characterized in that: The housing comprises: a rear cover (4), a housing lower plate (5) and a side plate (7); the rear cover (4) is provided on one side of the housing lower plate (5) and a semicircular slide groove (13) is provided on the other side; the side plate (7) is provided on the side of the housing lower plate (5) between the rear cover (4) and the semicircular slide groove (13); An electric push rod (8) is installed on one side of the rear cover (4), and one end of the electric push rod (8) passes through the rear cover (4) and is connected to the pressure plate (19). When the aviation plug (14) is in the unlocked state, the clamping member (9) moves to one side, and the pressure plate (19) is driven forward by starting the electric push rod (8) until it presses against the side of the aviation plug (142), so that the connection of the aviation plug (14) is stable in the unlocked state.

3. The automatic aerial plugging and unplugging operation tool according to claim 2, characterized in that: The bottom of one side of the shell lower plate (5) is fixedly connected to the left support plate (12), and a protruding plate (17) is provided on the other side. The protruding plate (17) is fixedly connected to the right limit top plate (11), and the aviation plug (14) is supported from the bottom by the left support plate (12) and supported from the side by the right limit top plate (11).

4. The automatic aerial plugging and unplugging operation tool according to claim 1, characterized in that: The control system comprises: a communication module (6) and a relay (15); the communication module (6) sends an opening and closing signal, controls the flow of current through the relay (15), and thereby operates the motor (2) to start and stop, so that the clamping member (9) moves to a preset position and stops automatically.

5. A system for an automatic aerial plugging and unplugging operation tool, based on the automatic aerial plugging and unplugging operation tool according to any one of claims 1 to 4, comprising: Aerial plug (14) and plug-in operation tool, characterized by: The aviation plug (14) comprises: a fixed aviation plug (141), a disassembly aviation plug (142) and a positioning structure. The positioning structure is provided on the disassembly aviation plug (142). The disassembly aviation plug (142) is sleeved on the outer surface of the fixed aviation plug (141). The connection structure (10) on the plugging and unplugging operation tool clamps the positioning structure. The fixed aviation plug (141) and the disassembly aviation plug (142) are locked or unlocked by driving the connection structure (10) to rotate the positioning structure.

6. The system of automatic aerial plugging and unplugging operation tool according to claim 5, characterized in that: One side of the fixed aviation plug (141) is fixedly arranged on a plane, a fixing protrusion (145) is provided on the upper side of the fixed aviation plug (141), a fixing hole (148) is provided at a position corresponding to the fixing protrusion (145) of the disassembly aviation plug (142), and the disassembly aviation plug (142) is sleeved on the outer surface of the fixed aviation plug (141) by snapping the fixing hole (148) into the fixing protrusion (145).

7. The system of automatic aerial plugging and unplugging operation tool according to claim 6, characterized in that: The positioning structure comprises an upper locking piece (1441), a lower locking piece (1442) and a connecting piece (147); the upper and lower surfaces of the disassembled aviation plug (142) are respectively hinged to the upper locking piece (1441) and the lower locking piece (1422) via a hinge shaft (143); the other ends of the upper and lower locking pieces are fixedly connected via the connecting piece (147); the connecting structure (10) clamps the connecting piece (147); and a locking hole (1443) is provided at the front end of the upper locking piece (1441) at a position corresponding to the fixing hole (148).

8. The system for automatic aerial plugging and unplugging operation tools according to claim 7, characterized in that: When the upper and lower locking pieces are arranged perpendicular to the aviation plug (14), the front end of the upper locking piece (1441) does not block the fixing hole (148), the disassembling aviation plug (142) and the fixing aviation plug (141) are in the unlocked state, the connecting structure (10) clamps the connecting piece (147), and the connecting structure (10) drives the connecting piece (147) to rotate circumferentially, so that the upper and lower locking pieces rotate around the hinge shaft (143) as the center, until the upper and lower locking pieces are arranged parallel to the aviation plug (14), the fixing protrusion (145) slides into the locking hole (1443) and the front end of the upper locking piece (1441) blocks the fixing hole (148) to lock the fixing aviation plug (141) and the disassembling aviation plug (142).

9. A control method for an automatic aerial plugging and unplugging operation tool, based on the automatic aerial plugging and unplugging operation tool according to any one of claims 1 to 4, characterized in that: When the aviation plug (14) is in an unlocked state, the positioning structure is arranged perpendicular to the aviation plug (14), and the connecting structure (10) clamps the positioning structure; The control system drives the connecting structure (10) to slide circumferentially until the positioning structure is arranged parallel to the aviation plug (14), and the aviation plug (14) is in a locked state; The control system drives the connecting structure (10) in reverse to slide circumferentially, so that the positioning structure returns to the vertical setting of the aviation plug (14), and then performs plugging and unplugging operations to achieve the fixation and separation of the aviation plug (14).

10. An electronic device comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, wherein: When the computer program is loaded into the processor, the control method of the automatic aerial plugging and unplugging operation tool according to claim 9 is implemented.

11. A computer-readable storage medium storing a computer program, characterized in that: When the computer program is executed by a processor, a control method for an automatic aerial plugging and unplugging operation tool according to claim 9 is implemented.

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