CN112721683A - Unmanned aerial vehicle charging platform is patrolled and examined to electric power - Google Patents
Unmanned aerial vehicle charging platform is patrolled and examined to electric power Download PDFInfo
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- CN112721683A CN112721683A CN202110108247.5A CN202110108247A CN112721683A CN 112721683 A CN112721683 A CN 112721683A CN 202110108247 A CN202110108247 A CN 202110108247A CN 112721683 A CN112721683 A CN 112721683A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses an electric power inspection unmanned aerial vehicle charging platform which comprises a charging platform main body, a contact type charging plate, an unmanned aerial vehicle main body, a calibration mechanism, a damping mechanism, a protective shell, a cover body, a handle, a clamping mechanism, a pulley and a telescopic pull rod. The invention can realize the quick and accurate butt joint of the charging platform main body and the contact type charging plate, effectively ensures the charging quality and speed, effectively avoids the abrasion caused by the impact of the unmanned aerial vehicle main body and the charging platform main body by arranging the damping mechanism, is beneficial to the permanent use and storage of the unmanned aerial vehicle main body and the charging platform main body, overcomes the defect that the existing contact type charging plate is inconvenient to move, and has simple operation, time and labor saving and stronger practicability.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle charging, in particular to a charging platform of an electric power inspection unmanned aerial vehicle.
Background
The unmanned aircraft is an unmanned aircraft operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, the overall investment of the power industry in China is about 1000 million yuan per year according to relevant data, wherein the hardware facilities are 73 percent, the specific gravity of power transmission equipment on the national power grid construction is higher and higher, the line patrol workload is also higher and higher along with the increasing expansion of the power grid, and the line patrol work of 100km can be completed by 20 line patrol personnel in one day. Therefore, the traditional line patrol mode cannot meet the wide requirements of modern power systems, and the unmanned aerial vehicle is required to patrol the circuit, so that the labor consumption can be effectively reduced;
at present, because the endurance time of an unmanned aerial vehicle is short, the charging of the unmanned aerial vehicle is indispensable operation, most of the existing unmanned aerial vehicles adopt contact charging, the positive electrode and the negative electrode of a power supply are respectively butted with the unmanned aerial vehicle to form a closed loop so as to charge the unmanned aerial vehicle, but the requirement on the landing point of the unmanned aerial vehicle is higher, if the landing point is slightly deviated or staggered with a butt joint, the charging efficiency is low or the unmanned aerial vehicle cannot be charged, meanwhile, because the whirling airflow around the unmanned aerial vehicle is larger, the charging platform is often subjected to larger impact force when the unmanned aerial vehicle lands, the collision and abrasion between the unmanned aerial vehicle and the charging platform are extremely easy to cause, the unmanned aerial vehicle and the charging platform are not beneficial to long-term storage, in addition, the existing charging platform is usually fixed and integrated, and usually needs to be manually transported to different use places when the, this kind of mode is wasted time and energy, is unfavorable for long-distance removal transport, consequently, based on above shortcoming, proposes an electric power and patrols and examines unmanned aerial vehicle charging platform and solve above-mentioned problem now.
Disclosure of Invention
The invention aims to provide a charging platform of an electric power inspection unmanned aerial vehicle, which at least solves the problems that the landing point of the unmanned aerial vehicle in the prior art is slightly deviated or staggered with a butt joint, the charging efficiency is low or the unmanned aerial vehicle cannot be charged, the unmanned aerial vehicle and the charging platform are easily damaged due to large impact force when the unmanned aerial vehicle lands, and the existing charging platform is inconvenient to move.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides an unmanned aerial vehicle charging platform is patrolled and examined to electric power, includes:
the top end of the charging platform main body is provided with a limiting groove from left to right;
the contact type charging plate is arranged at the center of the top end of the charging platform main body;
the unmanned aerial vehicle main body is placed at the center of the top end of the charging platform main body, and the bottom end of the unmanned aerial vehicle main body is in contact with the top end of the contact type charging plate;
the calibration mechanism is assembled in the inner cavity of the charging platform main body;
the damping mechanism is assembled at the bottom end of the charging platform main body;
the protective shell is sleeved on the outer walls of the charging platform main body and the damping mechanism;
the cover body is connected to the rear side of the top end of the protective shell through a pin shaft;
a handle mounted on the rear side of the outer wall of the cover body;
the clamping mechanism is assembled in the inner cavities of the protective shell and the cover body;
the two pulleys are respectively assembled at the front end and the rear end of the right side of the outer wall of the protective shell;
the telescopic pull rod is arranged on the left side of the outer wall of the protective shell;
the calibration mechanism includes:
the motor is arranged on the right side of the inner cavity of the charging platform main body through a screw;
one end of the screw is locked and fixed at the output end of the left surface of the motor through a coupler, and the other end of the screw is installed on the left side of the inner wall of the charging platform main body through a bearing;
the two sliding blocks are in threaded connection with the outer wall of the screw rod and are respectively embedded into the left end and the right end of an inner cavity of a limiting groove formed in the top end of the charging platform main body;
the two clamping plates are respectively arranged at the top ends of the sliding blocks in a bilateral symmetry manner;
the damper mechanism includes:
the base is embedded in the inner cavity of the protective shell;
the two connecting rods are respectively and symmetrically arranged on the front side and the rear side of the top end of the base in a front-back manner;
the number of the rectangular blocks is four, and every two rectangular blocks are in a group and are respectively sleeved on the left side and the right side of the outer wall of the connecting rod;
the first springs are four in number, every two springs are in a group and are respectively sleeved on the outer wall of the connecting rod, and two ends of each first spring are respectively fixedly installed on the rectangular block and the outer wall of the base;
the number of the supporting rods is four, and every two supporting rods are a group and are respectively and symmetrically arranged on the rectangular block and the outer wall of the charging platform main body through pin shafts;
the two ends of the telescopic rod are respectively arranged on the outer walls of the damping mechanism and the charging platform main body;
and the second spring is sleeved on the outer wall of the telescopic rod, and two ends of the second spring are respectively and fixedly installed on the outer walls of the damping mechanism and the charging platform main body.
Preferably, the threads at the left end and the right end of the outer wall of the screw rod are arranged in opposite directions.
Preferably, the front end and the rear end of the splint are obliquely arranged in an expansion trend.
Preferably, the two support rods of each group are arranged in a left-right symmetrical 'splayed' shape.
Preferably, the clamping mechanism includes:
the two clamping grooves are respectively arranged on the front side of the outer wall of the cover body in a bilateral symmetry manner;
the number of the clamping blocks is two, and the clamping blocks are embedded in the inner cavities of the clamping grooves respectively;
the two fixing blocks are fixedly arranged at the bottom ends of the clamping blocks respectively and are embedded in the inner cavity of the protective shell respectively;
the number of the third springs is two, and two ends of the third springs are fixedly arranged on the outer wall of the fixed block and the inner wall of the protective shell respectively;
and one end of the push rod extends out of the front side of the protective shell, and the other end of the push rod is embedded into the inner cavity of the protective shell and is in contact with the outer wall of the fixed block.
Preferably, the top end of the outer wall of the fixture block is inclined from outside to inside in a descending trend.
Preferably, the left side and the right side of the outer wall of the push rod are obliquely arranged from front to back in a contraction trend.
Preferably, the height of the inner cavity of the protective shell is greater than or equal to the height difference between the bottom end surface of the damping mechanism and the upper surface of the charging platform main body.
The invention has the beneficial effects that:
1. according to the invention, through the matching of the motor and the screw rod, the sliding block can drive the clamping plate to clamp and fix the unmanned aerial vehicle main body together inwards, so that the charging platform main body is accurately butted with the contact type charging plate, the charging is more accurately and rapidly carried out, and the charging quality and speed are effectively ensured;
2. according to the invention, through the matching of the support rod, the connecting rod, the rectangular block and the first spring, the first spring is in a compressed state when the unmanned aerial vehicle main body descends to the top end of the charging platform main body, elastic deformation is recovered through the first spring, and meanwhile, under the matching of the telescopic rod and the second spring, the impact force of the unmanned aerial vehicle main body and the charging platform main body can be buffered, so that the abrasion caused by the collision of the unmanned aerial vehicle main body and the charging platform main body is effectively avoided, the unmanned aerial vehicle main body and the charging platform main body can be used and stored for a long time, and the practicability is stronger;
3. according to the invention, through the matching of the fixed block and the third spring, the clamping block can be clamped into the inner cavity of the clamping groove, so that the charging platform main body and the damping mechanism which are embedded into the inner cavity of the clamping groove can be sealed, the fixed block can be driven to be separated from the inner cavity of the clamping groove through the push rod, the cover body and the protective shell can be separated and opened, and through the matching of the pulley and the telescopic pull rod, the protective shell in a closed state and the cover body can be moved, so that the protection of the contact type charging board is realized, the defect that the existing contact type charging board is inconvenient to move is overcome, and the operation is simple, time and.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a front view of the screw of the present invention;
FIG. 3 is a front view of a second spring of the present invention;
FIG. 4 is a front view of the mounting block of the present invention;
fig. 5 is a top view of the push rod of the present invention.
In the figure: 1. charging platform main part, 2, contact charging panel, 3, unmanned aerial vehicle main part, 4, aligning gear, 41, including a motor, 42, the screw rod, 43, the slider, 44, splint, 5, damper, 51, the base, 52, the connecting rod, 53, the rectangular block, 54, first spring, 55, the bracing piece, 56, the telescopic link, 57, the second spring, 6, the protective housing, 7, the lid, 8, the handle, 9, latch mechanism, 91, the draw-in groove, 92, the fixture block, 93, the fixed block, 94, the third spring, 95, the push rod, 10, the pulley, 11, flexible pull rod.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a technical solution: an electric power inspection unmanned aerial vehicle charging platform comprises a charging platform main body 1, a contact type charging plate 2, an unmanned aerial vehicle main body 3, a calibration mechanism 4, a damping mechanism 5, a protective shell 6, a cover body 7, a handle 8, a clamping mechanism 9, a pulley 10 and a telescopic pull rod 11, wherein a limiting groove is formed in the top end of the charging platform main body 1 from left to right; the contact type charging plate 2 is arranged at the center of the top end of the charging platform main body 1; the unmanned aerial vehicle main body 3 is placed at the center of the top end of the charging platform main body 1, the bottom end of the unmanned aerial vehicle main body is in contact with the top end of the contact type charging plate 2, the contact type charging plate 2 is in the prior art, and the unmanned aerial vehicle main body 3 can be charged when the contact type charging plate is in contact with a battery of the unmanned aerial vehicle main body 3; the calibration mechanism 4 is assembled in the inner cavity of the charging platform main body 1; the damping mechanism 5 is assembled at the bottom end of the charging platform main body 1; the protective shell 6 is sleeved on the outer walls of the charging platform main body 1 and the damping mechanism 5; the cover body 7 is connected to the rear side of the top end of the protective shell 6 through a pin shaft; the handle 8 is arranged at the rear side of the outer wall of the cover body 7; the clamping mechanism 9 is assembled in the inner cavities of the protective shell 6 and the cover body 7; the two pulleys 10 are respectively assembled at the front end and the rear end of the right side of the outer wall of the protective shell 6; the telescopic pull rod 11 is installed on the left side of the outer wall of the protective shell 6, and the pulley 10 is contacted with the ground by pulling and lifting the telescopic pull rod 11 upwards with the help of external force, so that the protective shell 6 and the cover body 7, in which the charging platform main body 1 and the damping mechanism 5 are embedded, can be moved;
the calibration mechanism 4 comprises a motor 41, a screw rod 42, a sliding block 43 and a clamping plate 44, the motor 41 is installed on the right side of the inner cavity of the charging platform main body 1 through screws, and the motor 41 is a forward and reverse motor which is a prior art and can rotate forward or reversely according to use requirements; one end of the screw rod 42 is locked and fixed at the output end of the left surface of the motor 41 through a coupler, the other end of the screw rod is installed on the left side of the inner wall of the charging platform main body 1 through a bearing, and the motor 41 in an open state can drive the screw rod 42 to rotate together; the number of the sliding blocks 43 is two, the sliding blocks are in threaded connection with the outer wall of the screw rod 42 and are respectively embedded into the left end and the right end of an inner cavity of a limiting groove formed in the top end of the charging platform main body 1; the number of the clamping plates 44 is two, the clamping plates are respectively arranged at the top ends of the sliding blocks 43 in a bilateral symmetry mode, the sliding blocks 43 can be driven by the rotating screw rods 42 to drive the clamping plates 44 to move inwards together, and therefore the clamping plates 44 push the support rods on the periphery of the bottom end of the unmanned aerial vehicle main body 3 to drive the unmanned aerial vehicle main body 3 to accurately move right above the contact type charging plate 2;
the damping mechanism 5 comprises a base 51, a connecting rod 52, a rectangular block 53, a first spring 54, a supporting rod 55, an expansion rod 56 and a second spring 57, wherein the base 51 is embedded in the inner cavity of the protective shell 6; the number of the connecting rods 52 is two, and the connecting rods are respectively arranged on the front side and the rear side of the top end of the base 51 in a front-back symmetrical mode; the number of the rectangular blocks 53 is four, and every two rectangular blocks are in a group and are respectively sleeved on the left side and the right side of the outer wall of the connecting rod 52; the number of the first springs 54 is four, each two springs are a group and are respectively sleeved on the outer wall of the connecting rod 52, two ends of each first spring are respectively and fixedly installed on the outer walls of the rectangular block 53 and the base 51, the first springs 54 are helical springs, and the first springs are stretched or extruded to generate elastic deformation and recover to an initial state after external force is removed; the number of the support rods 55 is four, every two support rods are a group and are respectively mounted on the outer walls of the rectangular block 53 and the charging platform main body 1 through symmetrical pin shafts, the charging platform main body 1 moving downwards enables the support rods 55 to drive the rectangular block 53 to move towards two sides along the outer wall of the connecting rod 52 and compress the first spring 54, and the impact force generated by the charging platform main body 1 when the unmanned aerial vehicle main body 3 descends can be damped and buffered by means of the elasticity of the first spring 54; the two ends of the telescopic rod 56 are respectively arranged on the outer walls of the damping mechanism 5 and the charging platform main body 1, the telescopic rod 56 is in the prior art and is connected in a manner that two sleeves with different thicknesses are sleeved with each other; second spring 57 cup joints on the outer wall of telescopic link 56, and both ends respectively fixed mounting on damper 5 and charging platform main part 1's outer wall, second spring 57 is coil spring, it produces elastic deformation after receiving tensile or extrusion, resume to initial condition after getting rid of external force, charging platform main part 1 of downstream will compress second spring 57 and telescopic link 56, the impact force that produces charging platform main part 1 when can descending unmanned aerial vehicle main part 3 with the help of second spring 57 and telescopic link 56 carries out further shock attenuation buffering.
Preferably, the left and right threads of the outer wall of the screw rod 42 are oppositely arranged, so that the two sliding blocks 43 connected with the screw rod can drive the clamping plates 44 to move inwards or outwards together along the outer wall.
As preferred scheme, still further, both ends are the slope setting that expands before and after splint 44 to can contact with unmanned aerial vehicle main part 3 on a wider range, better impel it to move gradually to the top of contact charging panel 2.
Preferably, the two support rods 55 of each set are arranged in a left-right symmetrical "eight" shape, so as to ensure that the rectangular blocks 53 can be driven to move along the outer wall of the connecting rod 52 to two sides and compress the first spring 54 under the action of the charging platform body 1.
As a preferable scheme, the clamping mechanism 9 further includes two clamping grooves 91, two clamping blocks 92, two fixing blocks 93, a third spring 94 and a push rod 95, and the two clamping grooves 91 are respectively arranged on the front side of the outer wall of the cover body 7 in a bilateral symmetry manner; the two clamping blocks 92 are respectively embedded in the inner cavity of the clamping groove 91, and the clamping blocks 92 are gradually clamped into the inner cavity of the clamping groove 91 along the inner wall of the clamping groove 91, so that the protective shell 6 and the cover body 7 can be tightly closed; the two fixing blocks 93 are respectively fixedly installed at the bottom ends of the clamping blocks 92 and respectively embedded in the inner cavity of the protective shell 6, the fixing blocks 93 moving towards the two sides drive the clamping blocks 92 to gradually separate from the inner cavity of the clamping grooves 91, and the cover body 7 can be separated from the protective shell 6 by pulling the handle 8 towards the rear side by means of external force; the number of the third springs 94 is two, and both ends of the third springs are respectively and fixedly mounted on the outer wall of the fixed block 93 and the inner wall of the protective shell 6, the third springs 94 are helical springs, and the helical springs elastically deform after being stretched or extruded, and recover to an initial state after external force is removed; push rod 95 one end extends the front side of protective housing 6, and the other end embeds the inner chamber of protective housing 6 and contacts with the fixed block 93 outer wall, promotes push rod 95 backward, and push rod 95 will support the outer wall of fixed block 93 gradually to impel it to move to both sides and compress the third spring 94 of both sides.
Preferably, the top end of the outer wall of the latch 92 is inclined downward from outside to inside, so as to ensure that the latch 92 can be gradually latched into the inner cavity of the latch groove 91 along the inner wall of the latch groove.
Preferably, the left and right sides of the outer wall of the push rod 95 are inclined from front to back in a contraction trend, so that the push rod 95 moving backwards can move backwards along the outer wall of the fixing block 93, and the push rod is driven to drive the blocking block 92 to gradually separate from the inner cavity of the blocking slot 91.
Preferably, the height of the inner cavity of the protective shell 6 is greater than or equal to the height difference between the bottom end surface of the damping mechanism 5 and the upper surface of the charging platform main body 1, so as to ensure that the damping mechanism and the charging platform main body 1 can be completely embedded into the inner cavity of the protective shell 6.
The electric elements mentioned in the scheme are all the prior art, the type of the electric elements is only one of the electric elements, and the electric elements can be used as long as the electric elements can achieve the purpose in the scheme.
All the electrical components in the present application are connected with the power supply adapted to the electrical components through the wires, and an appropriate controller should be selected according to actual conditions to meet control requirements, and specific connection and control sequences.
The method comprises the following steps: after the main body 3 of the unmanned aerial vehicle lands on the upper surface of the charging platform main body 1, the motor 41 is started, the motor 41 drives the screw rod 42 to rotate, and further the sliding block 43 drives the clamping plate 44 to move inwards together, so that the clamping plate 44 pushes the support rods around the bottom end of the main body 3 of the unmanned aerial vehicle to enable the main body 3 of the unmanned aerial vehicle to accurately move right above the contact type charging plate 2, and the full contact and charging with the contact type charging plate 2 are realized;
step two: in the process that the unmanned aerial vehicle main body 3 lands on the upper surface of the charging platform main body 1, the unmanned aerial vehicle main body 3 can impact the charging platform main body 1, the charging platform main body 1 moves downwards to compress the second springs 57 and the telescopic rods 56, meanwhile, the charging platform main body 1 enables the supporting rods 55 to drive the rectangular blocks 53 to move towards two sides along the outer wall of the connecting rod 52 and compress the first springs 54, and finally under the combined action of the elastic forces of the first springs 54 and the second springs 57, the impact force generated by the charging platform main body 1 when the unmanned aerial vehicle main body 3 lands can be damped and buffered;
step three: after charging, the handle 8 is held by hand to gradually close the cover body 7 and the protective shell 6, in the process, the fixture block 92 is gradually clamped into the inner cavity of the clamping groove 91 along the inner wall of the clamping groove, so that the protective shell 6 and the cover body 7 can be tightly closed, the telescopic pull rod 11 is pulled and lifted upwards by means of external force to enable the pulley 10 to be in contact with the ground, the protective shell 6 and the cover body 7 which are embedded with the charging platform main body 1 and the damping mechanism 5 can be moved, the push rod 95 is pushed backwards, the push rod 95 gradually butts against the outer wall of the fixing block 93 to enable the fixing block 93 to move towards two sides and compress the third springs 94 on the two sides, the fixing block 93 moving towards the two sides drives the fixture block 92 to gradually separate from the inner cavity of the clamping groove 91, and the handle 8 is pulled;
the invention can realize the quick and accurate butt joint of the charging platform main body 1 and the contact type charging plate 2, effectively ensures the charging quality and speed, effectively avoids the abrasion caused by the collision of the unmanned aerial vehicle main body 3 and the charging platform main body 1 by arranging the damping mechanism 5, is beneficial to the permanent use and storage of the unmanned aerial vehicle main body 3 and the charging platform main body 1, can protect the contact type charging plate 2, also solves the defect that the existing contact type charging plate 2 is not convenient to move, has simple operation, time and labor saving, has stronger practicability, and meets the use requirements of the existing market more.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. The utility model provides an unmanned aerial vehicle charging platform is patrolled and examined to electric power which characterized in that includes:
the top end of the charging platform main body (1) is provided with a limiting groove from left to right;
the contact type charging plate (2) is arranged at the center of the top end of the charging platform main body (1);
the unmanned aerial vehicle main body (3) is placed at the center of the top end of the charging platform main body (1), and the bottom end of the unmanned aerial vehicle main body is in contact with the top end of the contact type charging plate (2);
the calibration mechanism (4) is assembled in the inner cavity of the charging platform main body (1);
the damping mechanism (5) is assembled at the bottom end of the charging platform main body (1);
the protective shell (6) is sleeved on the outer walls of the charging platform main body (1) and the damping mechanism (5);
the cover body (7) is connected to the rear side of the top end of the protective shell (6) through a pin shaft;
a handle (8) mounted on the rear side of the outer wall of the cover body (7);
the clamping mechanism (9) is assembled in the inner cavities of the protective shell (6) and the cover body (7);
the number of the pulleys (10) is two, and the pulleys are respectively assembled at the front end and the rear end of the right side of the outer wall of the protective shell (6);
the telescopic pull rod (11) is installed on the left side of the outer wall of the protective shell (6);
the calibration mechanism (4) comprises:
the motor (41) is installed on the right side of the inner cavity of the charging platform main body (1) through a screw;
one end of the screw rod (42) is locked and fixed at the output end of the left surface of the motor (41) through a coupler, and the other end of the screw rod is installed on the left side of the inner wall of the charging platform main body (1) through a bearing;
the number of the sliding blocks (43) is two, the sliding blocks are in threaded connection with the outer wall of the screw rod (42), and the sliding blocks are respectively embedded into the left end and the right end of an inner cavity of a limiting groove formed in the top end of the charging platform main body (1);
the number of the clamping plates (44) is two, and the clamping plates are respectively arranged at the top ends of the sliding blocks (43) in a bilateral symmetry manner;
the damper mechanism (5) includes:
the base (51) is embedded in the inner cavity of the protective shell (6);
the two connecting rods (52) are respectively and symmetrically arranged at the front side and the rear side of the top end of the base (51) in a front-rear mode;
the number of the rectangular blocks (53) is four, and every two rectangular blocks are in a group and are respectively sleeved on the left side and the right side of the outer wall of the connecting rod (52);
the number of the first springs (54) is four, every two springs are in a group and are respectively sleeved on the outer wall of the connecting rod (52), and two ends of each first spring are respectively fixedly installed on the outer walls of the rectangular block (53) and the base (51);
the number of the supporting rods (55) is four, and every two supporting rods are respectively arranged on the outer walls of the rectangular block (53) and the charging platform main body (1) in a group of symmetrical pin shafts;
the two ends of the telescopic rod (56) are respectively arranged on the outer walls of the damping mechanism (5) and the charging platform main body (1);
and the second spring (57) is sleeved on the outer wall of the telescopic rod (56), and two ends of the second spring are respectively and fixedly installed on the outer walls of the damping mechanism (5) and the charging platform main body (1).
2. The power inspection unmanned aerial vehicle charging platform of claim 1, wherein: the left end and the right end of the outer wall of the screw rod (42) are provided with threads in opposite directions.
3. The power inspection unmanned aerial vehicle charging platform of claim 1, wherein: the front end and the rear end of the clamping plate (44) are obliquely arranged in an expansion trend.
4. The power inspection unmanned aerial vehicle charging platform of claim 1, wherein: the two support rods (55) in each group are arranged in a left-right symmetrical 'splayed' shape.
5. The power inspection unmanned aerial vehicle charging platform of claim 1, wherein: the clamping mechanism (9) comprises:
the number of the clamping grooves (91) is two, and the clamping grooves are respectively arranged on the front side of the outer wall of the cover body (7) in a bilateral symmetry manner;
the number of the clamping blocks (92) is two, and the two clamping blocks are respectively embedded in the inner cavity of the clamping groove (91);
the two fixing blocks (93) are fixedly arranged at the bottom ends of the clamping blocks (92) respectively and are embedded in the inner cavity of the protective shell (6) respectively;
the number of the third springs (94) is two, and two ends of each third spring are fixedly installed on the outer wall of the fixed block (93) and the inner wall of the protective shell (6) respectively;
and one end of the push rod (95) extends out of the front side of the protective shell (6), and the other end of the push rod is embedded into the inner cavity of the protective shell (6) and is in contact with the outer wall of the fixed block (93).
6. The power inspection unmanned aerial vehicle charging platform of claim 5, wherein: the top end of the outer wall of the clamping block (92) is obliquely arranged from outside to inside in a descending trend.
7. The power inspection unmanned aerial vehicle charging platform of claim 5, wherein: the left side and the right side of the outer wall of the push rod (95) are obliquely arranged from front to back in a contraction trend.
8. The power inspection unmanned aerial vehicle charging platform of claim 1, wherein: the height of the inner cavity of the protective shell (6) is larger than or equal to the height difference between the bottom end face of the damping mechanism (5) and the upper surface of the charging platform main body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110108247.5A CN112721683A (en) | 2021-01-26 | 2021-01-26 | Unmanned aerial vehicle charging platform is patrolled and examined to electric power |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110108247.5A CN112721683A (en) | 2021-01-26 | 2021-01-26 | Unmanned aerial vehicle charging platform is patrolled and examined to electric power |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112721683A true CN112721683A (en) | 2021-04-30 |
Family
ID=75594165
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110108247.5A Withdrawn CN112721683A (en) | 2021-01-26 | 2021-01-26 | Unmanned aerial vehicle charging platform is patrolled and examined to electric power |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112721683A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114655053A (en) * | 2022-04-18 | 2022-06-24 | 武汉海乐智能科技有限公司 | Unmanned aerial vehicle charging platform for electric power inspection |
| CN115339644A (en) * | 2022-09-06 | 2022-11-15 | 国网黑龙江省电力有限公司信息通信公司 | Communication electric power unmanned aerial vehicle overhauls platform |
-
2021
- 2021-01-26 CN CN202110108247.5A patent/CN112721683A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114655053A (en) * | 2022-04-18 | 2022-06-24 | 武汉海乐智能科技有限公司 | Unmanned aerial vehicle charging platform for electric power inspection |
| CN115339644A (en) * | 2022-09-06 | 2022-11-15 | 国网黑龙江省电力有限公司信息通信公司 | Communication electric power unmanned aerial vehicle overhauls platform |
| CN115339644B (en) * | 2022-09-06 | 2023-09-29 | 国网黑龙江省电力有限公司信息通信公司 | Communication electric power unmanned aerial vehicle overhauls platform |
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Application publication date: 20210430 |