CN112768972A - Unmanned aerial vehicle electric power earth connection hangs dismouting and puts - Google Patents
Unmanned aerial vehicle electric power earth connection hangs dismouting and puts Download PDFInfo
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- CN112768972A CN112768972A CN202110166015.5A CN202110166015A CN112768972A CN 112768972 A CN112768972 A CN 112768972A CN 202110166015 A CN202110166015 A CN 202110166015A CN 112768972 A CN112768972 A CN 112768972A
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- aerial vehicle
- unmanned aerial
- connecting rod
- wire
- main body
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R11/00—Individual connecting elements providing two or more spaced connecting locations for conductive members which are, or may be, thereby interconnected, e.g. end pieces for wires or cables supported by the wire or cable and having means for facilitating electrical connection to some other wire, terminal, or conductive member, blocks of binding posts
- H01R11/11—End pieces or tapping pieces for wires, supported by the wire and for facilitating electrical connection to some other wire, terminal or conductive member
- H01R11/12—End pieces terminating in an eye, hook, or fork
- H01R11/14—End pieces terminating in an eye, hook, or fork the hook being adapted for hanging on overhead or other suspended lines, e.g. hot line clamp
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R4/00—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
- H01R4/28—Clamped connections, spring connections
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R4/00—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
- H01R4/28—Clamped connections, spring connections
- H01R4/48—Clamped connections, spring connections utilising a spring, clip, or other resilient member
- H01R4/4854—Clamped connections, spring connections utilising a spring, clip, or other resilient member using a wire spring
- H01R4/4863—Coil spring
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R4/00—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
- H01R4/58—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation characterised by the form or material of the contacting members
- H01R4/64—Connections between or with conductive parts having primarily a non-electric function, e.g. frame, casing, rail
- H01R4/646—Connections between or with conductive parts having primarily a non-electric function, e.g. frame, casing, rail for cables or flexible cylindrical bodies
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R4/00—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
- H01R4/58—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation characterised by the form or material of the contacting members
- H01R4/66—Connections with the terrestrial mass, e.g. earth plate, earth pin
Abstract
The invention discloses an unmanned aerial vehicle electric grounding wire hanging and dismounting device which comprises a main body, wherein the top end of the main body is connected with a lifting ring in a sliding mode, the top end of the main body is rotatably connected with two cable clamping blocks I, a first rigid wire is arranged between the bottom ends of the cable clamping blocks I and the lifting ring, the bottom end of the main body is provided with a mounting box, the inside of the mounting box is provided with two clamping blocks, one side of each clamping block is provided with a second rigid wire, a grounding wire connector is arranged between the two clamping blocks, and the top end of the grounding wire connector is provided with an insulating wire. According to the invention, the flying ring is pulled up by the unmanned aerial vehicle, so that the first rigid wire can be pulled, the two cable clamping blocks I can be rotated and opened, a lead can conveniently enter the space between the two cable clamping blocks I to be fixedly clamped, the clamping blocks can be moved by pulling the second rigid wire, and the ground wire connector is released.
Description
Technical Field
The invention relates to the technical field of electric power grounding wires, in particular to a hanging and dismounting device for an electric power grounding wire of an unmanned aerial vehicle.
Background
The ground wire ensures the safety of personnel and maintenance operation basically, the ground wire hooking is usually completed by manual operation of an insulating rod or an insulating rope, the overhead line ground wire hooking is usually completed by climbing a tower, the transformer substation ground wire hooking is completed by auxiliary operating personnel of a crane, and the high-altitude falling and induction electric shock risks exist.
Through retrieval, the patent with the Chinese patent publication number of CN209497097U discloses a ground wire hanging and dismounting device for primary equipment of a transformer substation, and mainly relates to the field of ground wire hanging and dismounting devices. The base is included, be fixed with the insulator spindle on the base, the insulator spindle is a plurality of, can dismantle the connection between the insulator spindle, the insulator spindle top is equipped with the connecting rod of falling L shape, the horizontal pole tip of connecting rod is equipped with the pulley, pulley top one side articulates there is the apron, sliding connection has insulating rope on the pulley, the one end fixedly connected with ground connection head of insulating rope, ground connection head is connected with the earth connection, ground connection head is U-shaped and inside U-shaped chamber that is equipped with, be equipped with the fixation clamp in the U-shaped chamber.
The ground hanging and dismounting device for the grounding wire of the primary equipment of the transformer substation in the patent has the following defects: the hanging and dismantling height is limited, and the high-altitude operation is inconvenient.
Disclosure of Invention
The invention aims to solve the defects in the prior art, and provides a hanging and dismounting device for an electric grounding wire of an unmanned aerial vehicle.
In order to achieve the purpose, the invention adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle electric power earth connection hangs dismouting device, comprises a main body, the top sliding connection of main part has rings, the top of main part is rotated and is connected with two cable conductor clamp splice I, the bottom of cable conductor clamp splice I with be equipped with first rigidity line between the bottom of rings, the bottom of main part is equipped with the mounting box, and the inside of mounting box is equipped with two clamp splices, and one side of clamp splice is equipped with the second rigidity line, is equipped with the ground wire between two clamp splices and connects, and the top that the ground wire connects is equipped with the insulated wire.
Further, one side of cable conductor clamp splice I is equipped with cable conductor clamp splice II, the inside welding of main part has spring sleeve I, and the inside of spring sleeve I is equipped with first spring, and the welding of one side of first spring has spring sleeve II.
Further, the outside of main part is rotated and is connected with the baffle, and the opening has been seted up to one side of baffle, the bottom welding of rings has round pin axle I, and the outside cover of round pin axle I is equipped with a removal section of thick bamboo, the bottom of round pin axle I is equipped with the stopper, one side of a removal section of thick bamboo is rotated and is connected with first connecting rod, and the one end of first connecting rod is equipped with round pin axle II, and the one end of round pin axle II is rotated and is connected with the second connecting rod, first spout and second spout have been seted up to one side of main part, the one end of round pin axle II extends.
Further, a second spring is arranged between the first connecting rod and the main body.
Furthermore, the bottom of the main body and one side of the mounting box are both provided with large pulleys.
Furthermore, two one side of clamp splice all is equipped with the third spring, one side inner wall fixedly connected with fixed axle of mounting box, the one end of fixed axle rotates and is connected with the sheave, one side of clamp splice rotates and is connected with the third connecting rod, the one end of third connecting rod with one side of clamp splice all welds the fixed block, two fixed blocks are in respectively among two recesses of sheave.
Furthermore, the outer wall of the top end of the ground wire joint is arc-shaped, and a guide plate is welded at the bottom end of the mounting box and is conical.
Furthermore, two third chutes are formed in the top end of the main body, and the bottom end of the hanging ring is located inside the third chutes.
Furthermore, the top of mounting box is equipped with the limiting plate, and circular through-hole has been seted up at the middle part of limiting plate, the insulated wire runs through circular through-hole.
Furthermore, one side of main part is equipped with the guide bar, and the guide bar is the slope form, and the top and the bottom of mounting box are equipped with shrouding and guide sleeve respectively, and the top of main part is equipped with the hanging ring lid.
The invention has the beneficial effects that:
1. by arranging the lifting ring, the cable clamping blocks I, the clamping blocks and the rigid wire, the unmanned aerial vehicle pulls up the lifting ring so as to pull the first rigid wire, so that the two cable clamping blocks I rotate to open, a lead can conveniently enter between the two cable clamping blocks I, the clamping blocks can move by pulling the second rigid wire, so that the ground wire connector is released, and when the ground wire is grounded, the ground wire connector is pulled upwards through the insulating wire, so that the ground wire connector can enter between the two clamping blocks, the ground wire connector is clamped, and the device can be remotely operated and is more convenient;
2. by arranging the first spring and the cable clamping block II, when the cable clamping block I rotates, the spring sleeve II can be pushed to compress the first spring, and after the unmanned aerial vehicle is removed, the first spring can push the cable clamping block I to enable the cable clamping block II to clamp a lead;
3. by arranging the first connecting rod, the second connecting rod and the baffle, when the unmanned aerial vehicle pulls the lifting ring, the first connecting rod can be pulled, the second connecting rod is enabled to translate, so that the second connecting rod is in contact with the inner wall of one side of the first sliding groove, the second connecting rod is enabled to horizontally rotate, the second connecting rod enters the inside of the main body, when the wire is hung, the wire can enter the opening of the baffle, the two baffles rotate and clamp the wire in a clamping manner, then the unmanned aerial vehicle is removed, the lifting ring returns to the original position, so that the second connecting rod returns to the original position and extends out of the first sliding groove, the baffle is clamped, the baffle is prevented from rotating, and therefore the wire is further fixed;
4. through the arrangement of the second spring, the second spring can pull the first connecting rod, so that the first connecting rod can return to the original position conveniently, and the baffle is clamped by the second connecting rod;
5. through the arrangement of the grooved pulley and the third connecting rod, the second rigid wire pulls one of the clamping blocks, the fixing block on the clamping block can move in the groove of the grooved pulley at the moment, so that the grooved pulley is driven to rotate, the grooved pulley rotates to push the third connecting rod to move through the other fixing block, and the third connecting rod can push the other clamping block to move, so that the two clamping blocks are opened, and the ground wire joint can conveniently enter between the two clamping blocks;
6. the conical guide plate and the ground wire joint with the arc-shaped outer wall at the top end are arranged, so that the ground wire joint can conveniently enter between the two clamping blocks;
7. through setting up the guide bar that is the slope and changes, when the unmanned aerial vehicle carried the device of being convenient for of guide bar, the wire got into between two cable conductor clamp splice I, reduced the degree of difficulty of device carry.
Drawings
Fig. 1 is a schematic front structural view of a mounting and dismounting device for an electric ground wire of an unmanned aerial vehicle according to embodiment 1;
fig. 2 is a schematic cross-sectional structural view of an electric ground wire hanging and detaching device of an unmanned aerial vehicle according to embodiment 1;
fig. 3 is a sectional view of a front view structure of a mounting box of the device for mounting and dismounting an electric ground wire of an unmanned aerial vehicle, which is provided in embodiment 1;
fig. 4 is a front view of a first connecting rod and a second connecting rod structure of the device for hanging and dismounting the electric grounding wire of the unmanned aerial vehicle provided by the embodiment 1;
fig. 5 is a front view of a structure of the unmanned aerial vehicle electric ground wire hanging and dismounting device provided in embodiment 1 after movement of a first connecting rod and a second connecting rod;
fig. 6 is a schematic front structure view of a mounting and dismounting device for an electric ground wire of an unmanned aerial vehicle according to embodiment 2.
In the figure: the cable comprises a main body 1, a first rigid cable 2, a cable clamping block I3, a spring sleeve I4, a first spring 401, a spring sleeve II 5, a cable clamping block II 6, a first sliding chute 7, a second sliding chute 8, a lifting ring 9, a baffle plate 10, a mounting box 11, a ground wire joint 12, an insulated wire 13, a second rigid cable 14, a movable barrel 15, a first connecting rod 1501, a pin shaft I16, a second spring 17, a pin shaft II 18, a second connecting rod 19, a clamping block 20, a third spring 21, a third connecting rod 22, a grooved wheel 23, a fixed shaft 24 and a guide rod 25.
Detailed Description
The technical solution of the present patent will be described in further detail with reference to the following embodiments.
Reference will now be made in detail to embodiments of the present patent, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present patent and are not to be construed as limiting the present patent.
In the description of this patent, it is to be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings for the convenience of describing the patent and for the simplicity of description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the patent.
In the description of this patent, it is noted that unless otherwise specifically stated or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly and can include, for example, fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. The specific meaning of the above terms in this patent may be understood by those of ordinary skill in the art as appropriate.
Example 1
Referring to fig. 1-5, an unmanned aerial vehicle electric grounding wire hanging and dismounting device comprises a main body 1, a lifting ring 9 is slidably connected to the top end of the main body 1, two cable clamping blocks i 3 are rotatably connected to the top end of the main body 1, a first rigid wire 2 is arranged between the bottom ends of the cable clamping blocks i 3 and the lifting ring 9, a mounting box 11 is arranged at the bottom end of the main body 1, two clamping blocks 20 are arranged inside the mounting box 11, a second rigid wire 14 is arranged on one side of each clamping block 20, a ground wire connector 12 is arranged between the two clamping blocks 20, an insulating wire 13 is arranged at the top end of the ground wire connector 12, the lifting ring 9 is pulled up by the unmanned aerial vehicle, at the moment, due to the self gravity of the device, the lifting ring 9 and the main body 1 slide mutually, so that the first rigid wire 2 is pulled, the two cable clamping blocks i 3 are rotated and opened, a lead can conveniently, remove unmanned aerial vehicle, two cable conductor clamp splice I3 press from both sides the wire tightly, and the earth connection of being convenient for can make clamp splice 20 remove through pulling second rigid line 14 to release ground wire joint 12, during the earth connection, upwards stimulate ground wire joint 12 through insulated wire 13, can make ground wire joint 12 get into between two clamp splices 20, thereby press from both sides ground wire joint 12 tightly.
Wherein, one side of cable conductor clamp splice I3 is equipped with cable conductor clamp splice II 6, the inside welding of main part 1 has spring sleeve I4, the inside of spring sleeve I4 is equipped with first spring 401, one side welding of first spring 401 has spring sleeve II 5, when cable conductor clamp splice I3 rotates, can promote spring sleeve II 5, make first spring 401 compress, after unmanned aerial vehicle withdraws, first spring 401 can promote cable conductor clamp splice I3, press from both sides the wire tightly, cable conductor clamp splice II 6 can adapt to the wire of different specifications, it is different according to wire thickness degree, can change cable conductor clamp splice II 6, thereby be convenient for press from both sides the wire tightly.
Wherein, the outer part of the main body 1 is rotatably connected with a baffle 10, one side of the baffle 10 is provided with an opening, the bottom end of the lifting ring 9 is welded with a pin shaft I16, the outer part of the pin shaft I16 is sleeved with a movable barrel 15, the bottom end of the pin shaft I16 is provided with a limit block, one side of the movable barrel 15 is rotatably connected with a first connecting rod 1501, one end of the first connecting rod 1501 is provided with a pin shaft II 18, one end of the pin shaft II 18 is rotatably connected with a second connecting rod 19, one side of the main body 1 is provided with a first chute 7 and a second chute 8, one end of the pin shaft II 18 extends into the second chute 8, when the unmanned aerial vehicle pulls the lifting ring 9, the pin shaft I16 is driven to ascend, the limit block at the bottom of the pin shaft I16 pulls the movable barrel 16 to ascend, the movable barrel 16 pulls the first connecting rod 1501 to enable the first connecting rod 1501 to pull the second connecting, thereby contact one side inner wall of first spout 7, make second connecting rod 19 rotate, get into the inside of main part 1, during the mount wire, the wire can get into among the opening of baffle 10, two baffles 10 can press from both sides the wire tightly and block, it rotates to drive baffle 10 simultaneously, unmanned aerial vehicle withdraws afterwards, rings 9 get back to the home position, thereby make second connecting rod 19 get back to the home position, stretch out among the first spout 7, thereby block baffle 10, avoid baffle 10 to rotate, thereby make the wire by further fixed.
A second spring 17 is arranged between the first link 1501 and the body 1, and the second spring 17 pulls the first link 1501, so that the first link 15 returns to the original position, and the second link 19 blocks the baffle 10.
Wherein, the bottom of main part 1 and one side of mounting box 11 all are equipped with big pulley, and insulated wire 13 can be pulled through big pulley, the carry of ground wire joint 12 of being convenient for.
The third springs 21 are arranged on one sides of the two clamping blocks 20, a fixing shaft 24 is fixedly connected to the inner wall of one side of the mounting box 11, a grooved wheel 23 is rotatably connected to one end of the fixing shaft 24, a third connecting rod 22 is rotatably connected to one side of the clamping block 20, fixing blocks are welded to one end of the third connecting rod 22 and one side of the clamping block 20, the two fixing blocks are respectively located in two grooves of the grooved wheel 23, one of the clamping blocks 20 is pulled through the second rigid wire 14, the fixing block on the clamping block 20 can move in the groove of the grooved wheel 23 at the moment, the grooved wheel 23 is driven to rotate, the third connecting rod 22 can be pushed to move through the other fixing block by the rotation of the grooved wheel 23, and the other clamping block 20 can be pushed to move by the third connecting rod 22, so that the two clamping blocks 20 are opened.
The top outer wall of the ground wire joint 12 is arc-shaped, the bottom end of the mounting box 11 is welded with a guide plate, the guide plate is conical, and the conical guide plate and the arc-shaped top outer wall of the ground wire joint 12 facilitate the ground wire joint 12 to enter between the two clamping blocks 20.
Wherein, two third spouts have been seted up on the top of main part 1, and the bottom of rings 9 is in the inside of third spout, and the third spout is convenient for rings 9 and reciprocates.
Wherein, the top of mounting box 11 is equipped with the limiting plate, and circular through-hole has been seted up at the middle part of limiting plate, and insulated wire 13 runs through circular through-hole, and the limiting plate can carry out spacingly to ground wire joint 12 to make ground wire joint 12 can just in time be in between two clamp splice 20, the installation of ground wire joint 12 of being convenient for.
The working principle is as follows: the lifting ring 9 is pulled up by an unmanned aerial vehicle, the lifting ring 9 and the main body 1 slide mutually, the first rigid wire 2 connected with the lifting ring 9 can pull the cable clamping blocks I3, at the moment, the gravity of the device is larger than the elastic force of the first spring 401, the two cable clamping blocks I3 are rotated and opened, a lead can conveniently enter between the two cable clamping blocks I3, the unmanned aerial vehicle is removed after the lead enters between the two cable clamping blocks I3, the two cable clamping blocks I3 clamp the lead under the action of the spring 401, the ground wire is conveniently grounded, the clamping blocks 20 can be moved by pulling the second rigid wire 14, the ground wire connector 12 is released, the ground wire connector 12 can enter between the two clamping blocks 20 by pulling the ground wire connector 12 upwards through the insulating wire 13 during grounding, and the ground wire connector 12 is clamped;
when the cable clamping block I3 rotates, the spring sleeve II 5 can be pushed to compress the first spring 401, after the unmanned aerial vehicle is removed, the first spring 401 can push the cable clamping block I3 to clamp the wires, the cable clamping block II 6 can adapt to the wires with different specifications, and the cable clamping block II 6 can be replaced according to different wire thickness degrees, so that the wires can be clamped conveniently;
when the unmanned aerial vehicle pulls the flying ring 9, the pin shaft I16 can be driven to ascend, the limiting block at the bottom of the pin shaft I16 pulls the moving cylinder 16 to ascend, the moving cylinder 16 pulls the first connecting rod 1501, the first connecting rod 1501 pulls the second connecting rod 19, the pin shaft II 18 can slide in the second sliding groove 8 at the moment, the second connecting rod 19 can translate, so that the first connecting rod 7 is contacted with the inner wall of one side of the first sliding groove 7, the second connecting rod 19 rotates to enter the main body 1, when the wire is hung, the wire can enter the opening of the baffle 10, the two baffles 10 can clamp and clamp the wire, meanwhile, the baffle 10 is driven to rotate, the unmanned aerial vehicle is removed, the flying ring 9 returns to the original position, the second connecting rod 19 returns to the original position and extends out of the first sliding groove 7, so that the baffle 10 is clamped, the baffle 10 is prevented from rotating, and the wire is further;
when the cable conductor clamping block I3 clamps cable conductors of different specifications, the rotating angles of the cable conductor clamping block I3 are different, so that the requirement is that the second connecting rod 19 can extend out of the first sliding groove 7 to limit the baffle 10, and the pin shaft I16 can slide upwards within a period of time when the hanging ring 9 is pulled up, so that the second connecting rod 19 cannot be driven to move, and the second connecting rod 19 can be guaranteed to limit the baffle 10 all the time.
The second spring 17 will pull the first link 1501, so that the first link 15 returns to the original position, and the second link 19 will block the baffle 10;
the insulated wire 13 can be pulled through a large pulley, so that the ground wire joint 12 can be conveniently mounted;
one of the clamping blocks 20 is pulled through the second rigid wire 14, at this time, the fixed block on the clamping block 20 moves in the groove of the grooved pulley 23, so as to drive the grooved pulley 23 to rotate, the grooved pulley 23 rotates, and pushes the third connecting rod 22 to move through the other fixed block, and the third connecting rod 22 pushes the other clamping block 20 to move, so that the two clamping blocks 20 are opened, and the ground wire connector 12 can enter between the two clamping blocks 20;
the conical guide plate and the ground lug 12 with the curved outer wall at the top end facilitate the entry of the ground lug 12 between the two clamping blocks 20.
Example 2
Referring to fig. 6, an unmanned aerial vehicle electric power earth connection hangs dismouting and puts, this embodiment compares in embodiment 1, in order to increase the practicality of device, one side of main part 1 is equipped with guide bar 25, guide bar 25 is the slope form, the top and the bottom of mounting box 11 are equipped with shrouding and guide sleeve respectively, the top of main part 1 is equipped with the rings lid, when the unmanned aerial vehicle of guide bar 25 be convenient for carry the device, the wire gets into between two cable conductor clamp splice I3, the degree of difficulty that reduces the device carry, the shrouding is convenient for the location of ground wire joint 12, protect the inner structure simultaneously, guide sleeve is convenient for the direction of ground wire joint 12, it is spacing to be convenient for the slip box of rings 9.
The working principle is as follows: the lifting ring 9 is pulled up by an unmanned aerial vehicle, at the moment, due to the self gravity of the device, the lifting ring 9 and the main body 1 slide mutually, so that a first rigid wire 2 is pulled, two cable clamping blocks I3 are rotated to be opened, a lead can conveniently enter between the two cable clamping blocks I3, the unmanned aerial vehicle is removed after the lead enters into the two cable clamping blocks I3, the two cable clamping blocks I3 clamp the lead, so that a ground wire is conveniently grounded, the clamping blocks 20 can be moved by pulling the second rigid wire 14, so that the ground wire connector 12 is released, when the ground wire is grounded, the ground wire connector 12 is pulled upwards by the insulating wire 13, so that the ground wire connector 12 can enter between the two clamping blocks 20, and the ground wire connector 12 is clamped;
when the cable clamping block I3 rotates, the spring sleeve II 5 can be pushed to compress the first spring 401, after the unmanned aerial vehicle is removed, the first spring 401 can push the cable clamping block I3 to clamp the wires, the cable clamping block II 6 can adapt to the wires with different specifications, and the cable clamping block II 6 can be replaced according to different wire thickness degrees, so that the wires can be clamped conveniently;
when the unmanned aerial vehicle pulls the flying ring 9, the pin shaft I16 can be driven to ascend, the limiting block at the bottom of the pin shaft I16 pulls the movable cylinder 16 to ascend, the movable cylinder 16 pulls the first connecting rod 1501, the first connecting rod 1501 pulls the second connecting rod 19, the pin shaft II 18 can slide in the second sliding groove 8 at the moment, the second connecting rod 19 can translate, so that the first connecting rod 7 is contacted with the inner wall of one side of the first sliding groove 7, the second connecting rod 19 rotates to enter the main body 1, when the wire is hung, the wire can enter the opening of the baffle 10, the two baffles 10 can clamp and clamp the wire, meanwhile, the baffle 10 is driven to rotate, the unmanned aerial vehicle is driven to move away, the flying ring 9 returns to the original position, the second connecting rod 19 extends back to the original position, the first sliding groove extends out, the baffle 10 is clamped, the baffle 10 is prevented from rotating, and the wire is;
when the cable conductor clamping block I3 clamps cable conductors of different specifications, the rotating angles of the cable conductor clamping block I3 are different, so that the requirement is that the second connecting rod 19 can extend out of the first sliding groove 7 to limit the baffle 10, and the pin shaft I16 can slide upwards within a period of time when the hanging ring 9 is pulled up, so that the second connecting rod 19 cannot be driven to move, and the second connecting rod 19 can be guaranteed to limit the baffle 10 all the time.
The second spring 17 will pull the first link 1501, so that the first link 15 returns to the original position, and the second link 19 will block the baffle 10;
the insulated wire 13 can be pulled through a large pulley, so that the ground wire joint 12 can be conveniently mounted;
one of the clamping blocks 20 is pulled through the second rigid wire 14, at this time, the fixed block on the clamping block 20 moves in the groove of the grooved pulley 23, so as to drive the grooved pulley 23 to rotate, the grooved pulley 23 rotates, and pushes the third connecting rod 22 to move through the other fixed block, and the third connecting rod 22 pushes the other clamping block 20 to move, so that the two clamping blocks 20 are opened, and the ground wire connector 12 can enter between the two clamping blocks 20;
the conical guide plate and the ground wire joint 12 with the arc-shaped top outer wall facilitate the ground wire joint 12 to enter between the two clamping blocks 20;
when the unmanned aerial vehicle of guide bar 25 was convenient for carry the device, the wire got into between two cable conductor clamp splice I3, reduced the degree of difficulty of device carry, and the shrouding is convenient for ground wire connector 12's location, protects inner structure simultaneously, and the guide sleeve is convenient for ground wire connector 12's direction, and it is spacing that the rings lid is convenient for the slip box of rings.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle electric power earth connection hangs dismouting device, includes main part (1), its characterized in that, the top sliding connection of main part (1) has rings (9), the top of main part (1) is rotated and is connected with two cable conductor clamp splice I (3), the bottom of cable conductor clamp splice I (3) with be equipped with first rigidity line (2) between the bottom of rings (9), the bottom of main part (1) is equipped with mounting box (11), and the inside of mounting box (11) is equipped with two clamp splice (20), and one side of clamp splice (20) is equipped with second rigidity line (14), is equipped with ground wire joint (12) between two clamp splice (20), and the top of ground wire joint (12) is equipped with insulated wire (13).
2. The unmanned aerial vehicle electric grounding wire hanging and dismounting device is characterized in that one side of the cable clamp block I (3) is provided with a cable clamp block II (6), the inside of the main body (1) is fixedly connected with a spring sleeve I (4), the inside of the spring sleeve I (4) is provided with a first spring (401), and one side of the first spring (401) is fixedly connected with a spring sleeve II (5).
3. The unmanned aerial vehicle electric grounding wire hanging and dismounting device is characterized in that a baffle (10) is connected to the main body (1) in a rotating mode, an opening is formed in one side of the baffle (10), a pin shaft I (16) is fixedly connected to the bottom end of the hanging ring (9), a moving cylinder (15) is sleeved outside the pin shaft I (16), a limiting block is arranged at the bottom end of the pin shaft I (16), a first connecting rod (1501) is connected to one side of the moving cylinder (15) in a rotating mode, a pin shaft II (18) is arranged at one end of the first connecting rod (1501), a second connecting rod (19) is connected to one end of the pin shaft II (18) in a rotating mode, a first sliding groove (7) and a second sliding groove (8) are formed in one side of the main body (1), and one end of the pin shaft II (18) extends to the inside of the second sliding groove (.
4. The unmanned aerial vehicle electric ground wire hanging and dismounting device is characterized in that a second spring (17) is arranged between the first connecting rod (1501) and the main body (1).
5. The hanging and dismounting device for the electric grounding wire of the unmanned aerial vehicle as claimed in claim 1, wherein the bottom of the main body (1) and one side of the mounting box (11) are provided with large pulleys.
6. The unmanned aerial vehicle electric grounding wire hanging and dismounting device is characterized in that a third spring (21) is arranged on one side of each of two clamping blocks (20), a fixed shaft (24) is fixedly connected to the inner wall of one side of the mounting box (11), a grooved wheel (23) is rotatably connected to one end of the fixed shaft (24), a third connecting rod (22) is rotatably connected to one side of each clamping block (20), fixed blocks are fixedly connected to one end of each third connecting rod (22) and one side of each clamping block (20), and the two fixed blocks are respectively positioned in two grooves of the grooved wheel (23).
7. The hanging and dismounting device for the electric grounding wire of the unmanned aerial vehicle as claimed in claim 1, wherein the top outer wall of the grounding wire connector (12) is arc-shaped, and a guide plate is fixedly connected to the bottom end of the mounting box (11) and is cone-shaped.
8. The hanging and dismounting device for the electric grounding wire of the unmanned aerial vehicle as claimed in claim 1, wherein two third sliding grooves are formed at the top end of the main body (1), and the bottom end of the hanging ring (9) is positioned inside the third sliding grooves.
9. The hanging and dismounting device for the electric grounding wire of the unmanned aerial vehicle as claimed in claim 1, wherein a limiting plate is arranged at the top end of the mounting box (11), a circular through hole is formed in the middle of the limiting plate, and the insulating wire (13) penetrates through the circular through hole.
10. The unmanned aerial vehicle electric grounding wire hanging and dismounting device is characterized in that a guide rod (25) is arranged on one side of the main body (1), the guide rod (25) is inclined, a sealing plate and a guide sleeve are respectively arranged at the top end and the bottom end of the mounting box (11), and a hanging ring cover is arranged at the top end of the main body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110166015.5A CN112768972A (en) | 2021-02-03 | 2021-02-03 | Unmanned aerial vehicle electric power earth connection hangs dismouting and puts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110166015.5A CN112768972A (en) | 2021-02-03 | 2021-02-03 | Unmanned aerial vehicle electric power earth connection hangs dismouting and puts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112768972A true CN112768972A (en) | 2021-05-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110166015.5A Pending CN112768972A (en) | 2021-02-03 | 2021-02-03 | Unmanned aerial vehicle electric power earth connection hangs dismouting and puts |
Country Status (1)
| Country | Link |
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| CN (1) | CN112768972A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113937519A (en) * | 2021-11-01 | 2022-01-14 | 国网山西省电力公司输电检修分公司 | High-altitude grounding wire detaching and hanging method based on unmanned aerial vehicle |
| CN115591144A (en) * | 2022-09-30 | 2023-01-13 | 广东冠能电力科技发展有限公司（Cn） | Go up and hang device and anti-falling device thereof |
-
2021
- 2021-02-03 CN CN202110166015.5A patent/CN112768972A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113937519A (en) * | 2021-11-01 | 2022-01-14 | 国网山西省电力公司输电检修分公司 | High-altitude grounding wire detaching and hanging method based on unmanned aerial vehicle |
| CN113937519B (en) * | 2021-11-01 | 2023-04-28 | 国网山西省电力公司输电检修分公司 | Method for disassembling and hanging ground wire at high altitude based on unmanned aerial vehicle |
| CN115591144A (en) * | 2022-09-30 | 2023-01-13 | 广东冠能电力科技发展有限公司（Cn） | Go up and hang device and anti-falling device thereof |
| CN115591144B (en) * | 2022-09-30 | 2023-09-19 | 广东电网有限责任公司佛山供电局 | Hanging device and anti-falling device thereof |
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