CN216070501U - Electric power inspection device based on unmanned aerial vehicle - Google Patents
Electric power inspection device based on unmanned aerial vehicle Download PDFInfo
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- CN216070501U CN216070501U CN202121449194.5U CN202121449194U CN216070501U CN 216070501 U CN216070501 U CN 216070501U CN 202121449194 U CN202121449194 U CN 202121449194U CN 216070501 U CN216070501 U CN 216070501U
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Abstract
The utility model discloses an electric power inspection device based on unmanned aerial vehicle, including the unmanned aerial vehicle body, unmanned aerial vehicle body lower extreme cross-section is circular, unmanned aerial vehicle body side is encircleed and is equipped with a plurality of supports, the one end that unmanned aerial vehicle body was kept away from to a plurality of supports all matches and is equipped with the power rotor, unmanned aerial vehicle body downside is horizontal side and fixedly connected with jib, jib lower extreme fixedly connected with equipment nacelle, unmanned aerial vehicle body downside matches and is equipped with a plurality of electric telescopic handle, unmanned aerial vehicle body downside is equipped with a plurality of dwang that correspond respectively with a plurality of electric telescopic handle, the flexible end of a plurality of electric telescopic handle all is equipped with control dwang pivoted control mechanism, dwang one end matches and is equipped with supporting mechanism and rotor protection mechanism. The utility model can ensure the stability of landing while satisfying the power patrol, has better protection effect and can be effectively applied to the field.
Description
Technical Field
The utility model relates to the technical field of power inspection devices, in particular to a power inspection device based on an unmanned aerial vehicle.
Background
Along with the continuous development of electric power industry, electric power industry begins to use unmanned aerial vehicle extensively to carry out electric power and patrols and examines, and unmanned aerial vehicle can accomplish safely and patrol and examine the operation high-efficiently to can realize patrolling and examining on a large scale, can realize the condition to insulating cluster string hanging point and drainage wire and insulator on the circuit of patrolling and examining, still can patrol and examine stockbridge damper and fastener and wire condition, unmanned aerial vehicle has become the best instrument that the personnel of patrolling and examining accomplished the operation.
The operational environment that current electric power patrolled and examined is mostly in the field, when using unmanned aerial vehicle to patrol and examine, often can receive the topography influence, and open-air topography condition is complicated, and ground often levels inadequately and the rubble is more, when descending, current unmanned aerial vehicle's supporting leg has can not satisfy the effect of steady descending, often can be because the focus is not steady when descending, leads to unmanned aerial vehicle slope to overturn, causes the loss of equipment.
Therefore, the power inspection device based on the unmanned aerial vehicle is provided to solve the problems.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the defects in the prior art, and provides an electric power inspection device based on an unmanned aerial vehicle.
In order to achieve the purpose, the utility model adopts the following technical scheme:
the utility model provides an electric power inspection device based on unmanned aerial vehicle, includes the unmanned aerial vehicle body, unmanned aerial vehicle body lower extreme cross-section is circularly, unmanned aerial vehicle body side is encircleed and is equipped with a plurality of supports, and is a plurality of the one end that unmanned aerial vehicle body was kept away from to the support all matches and is equipped with the power rotor, unmanned aerial vehicle body downside is horizontal side and fixedly connected with jib, jib lower extreme fixedly connected with equipment nacelle, unmanned aerial vehicle body downside matches and is equipped with a plurality of electric telescopic handle, unmanned aerial vehicle body downside is equipped with a plurality of dwang that correspond respectively with a plurality of electric telescopic handle, and is a plurality of the flexible end of electric telescopic handle all is equipped with control dwang pivoted control mechanism, the matching of dwang one end is equipped with supporting mechanism and rotor protection mechanism.
Preferably, it is a plurality of electric telescopic handle is even setting up, the horizontal fixedly connected with connecting plate of unmanned aerial vehicle body downside, it is a plurality of electric telescopic handle all with connecting plate fixed connection.
Preferably, control mechanism includes the connecting block, connecting block and electric telescopic handle telescopic end fixed connection, it is connected with horizontal dwang to rotate on the connecting block, dwang and horizontal dwang middle part side fixed connection, the equal coaxial fixedly connected with gear in horizontal dwang both ends, two stoppers of fixedly connected with on the connecting plate, two the stopper matches with two gear positions respectively, two the bar notch has all been seted up to the stopper, be equipped with in the bar notch and correspond gear engagement's annular rack.
Preferably, supporting mechanism includes the supporting leg, unmanned aerial vehicle body one end fixed connection is kept away from with the dwang to supporting leg one end, the supporting leg is the slope setting with the dwang, supporting leg lower extreme fixedly connected with supporting shoe.
Preferably, the supporting block is arc-shaped, and the lower side surface of the supporting block is made of rubber.
Preferably, rotor protection mechanism includes the arc frame, the arc frame is through bending pole and supporting leg upper end fixed connection, the arc frame matches with the power rotor.
Compared with the prior art, the utility model has the beneficial effects that:
1. according to the unmanned aerial vehicle, the rotating rods are arranged on the lower side of the unmanned aerial vehicle body, the electric telescopic rods matched with the rotating rods are arranged, the control mechanism matched with the rotating rods is arranged at the telescopic end of the electric telescopic rods, so that the rotating control of the rotating rods is realized, the control effect is good, the rotating rods can be controlled to rotate to a horizontal state and an inclined state, and the hanging rod and the hanging cabin are arranged on the lower side of the unmanned aerial vehicle body, so that the installation of inspection equipment is realized, and the requirement of electric inspection is met.
2. According to the utility model, the support mechanism and the rotor wing protection mechanism are arranged at the lower end of the rotating rod, when the rotating rod is controlled by the electric telescopic rod to rotate to an inclined state, the plurality of support mechanisms can form a support frame similar to a circle, so that a good support effect is realized, the stability is high, the stability of the unmanned aerial vehicle body during landing can be effectively ensured, and meanwhile, when the rotating rod is controlled by the electric telescopic rod to rotate to a horizontal state, the plurality of rotor wing protection mechanisms can correspond to the plurality of power rotor wings, so that a good protection effect is achieved.
Drawings
Fig. 1 is a schematic structural diagram of an electric power inspection device based on an unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic view of a bottom view structure of the power inspection device based on the unmanned aerial vehicle according to the present invention;
fig. 3 is a schematic structural diagram of a plurality of rotating rods in the unmanned aerial vehicle-based power inspection device rotating to horizontal positions;
fig. 4 is a schematic structural diagram of a control mechanism, a support mechanism and a rotor protection mechanism in the unmanned aerial vehicle-based power inspection device provided by the utility model.
In the figure: 1 unmanned aerial vehicle body, 2 supports, 3 power rotors, 4 jibs, 5 nacelle, 6 electric telescopic handle, 7 dwangs, 8 control mechanism, 9 supporting mechanism, 10 rotor protection mechanism, 11 connecting plates, 12 connecting blocks, 13 horizontal dwang, 14 gears, 15 stoppers, 16 cyclic annular rack, 17 supporting legs, 18 supporting shoes, 19 arc framves, 20 bending rod, 21 motors.
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.
Referring to fig. 1-4, an electric power inspection device based on an unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, the inside of the unmanned aerial vehicle body 1 can be used for installing the existing components such as a flight control system and a battery, and providing an installation platform for other components, which is not described herein, the cross section of the lower end of the unmanned aerial vehicle body 1 is circular, the sides of the unmanned aerial vehicle body 1 are surrounded by a plurality of brackets 2, the plurality of brackets 2 have a better supporting function, one ends of the plurality of brackets 2 away from the unmanned aerial vehicle body 1 are respectively provided with a power rotor 3 in a matching manner, the power rotors 3 are the same as the existing ones and are used as a power source of the unmanned aerial vehicle body 1, the front ends of the plurality of brackets 2 are respectively fixedly provided with a motor 21 matched with the power rotors 3, the motors 21 are the same as the existing ones and are used for driving the power rotors 3, which are not described herein, the lower side surface of the unmanned aerial vehicle body 1 is a horizontal side surface and is fixedly connected with a suspender 4, the lower end of the suspender 4 is fixedly connected with an equipment nacelle 5, the suspender 4 plays a role in supporting and connecting the nacelle 5, the nacelle 5 is used for installing the existing inspection equipment, such as a camera and the like, a plurality of electric telescopic rods 6 are arranged on the lower side of the unmanned aerial vehicle body 1 in a matching manner, the electric telescopic rods 6 are the same as the existing ones and can electrically extend and retract, a plurality of rotating rods 7 respectively corresponding to the electric telescopic rods 6 are arranged on the lower side of the unmanned aerial vehicle body 1, the extending and retracting ends of the electric telescopic rods 6 are respectively provided with a control mechanism 8 for controlling the rotating rods 7 to rotate, the control mechanism 8 has a better mask effect, one end of each rotating rod 7 is provided with a supporting mechanism 9 and a rotor wing protecting mechanism 10 in a matching manner, the supporting mechanism 9 plays a supporting role, and the rotor wing protecting mechanism 10 has a better protecting role and is used for protecting the power rotor wing 3;
the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a plurality of electric telescopic rods 6, a connecting plate 11, a plurality of corner angles, a plurality of electric telescopic rods 6 and a connecting plate 11, wherein the electric telescopic rods 6 are uniformly arranged, the lower side of the unmanned aerial vehicle body 1 is horizontally and fixedly connected with the connecting plate 11, the connecting plate 11 is provided with the corner angles, the electric telescopic rods 6 are fixedly connected with the connecting plate 11, and the connecting plate 11 has a good connecting and fixing effect;
wherein, the control mechanism 8 comprises a connecting block 12, the connecting block 12 is fixedly connected with the telescopic end of the electric telescopic rod 6, the electric telescopic rod 6 can be started to drive the connecting block 12 to horizontally move, a transverse rotating rod 13 is rotatably connected to the connecting block 12, the transverse rotating rod 13 plays a role of supporting, the connecting block 12 can drive the transverse rotating rod 13 when horizontally moving, the rotating rod 7 is fixedly connected with the middle side surface of the transverse rotating rod 13, two ends of the transverse rotating rod 13 are coaxially and fixedly connected with gears 14, two limit blocks 15 are fixedly connected to the connecting plate 11, the two limit blocks 15 are respectively matched with the two gears 14 in position, the two limit blocks 15 are respectively provided with a strip-shaped notch, an annular rack 16 meshed with the corresponding gear 14 is arranged in the strip-shaped notch, the transverse rotating rod 13 can drive the two gears 14, under the action of the annular rack 16, the two gears 14 rotate, and further drive the transverse rotating rod 13 to rotate, so that the state of the rotating rod 7 is changed, and the meshing action of the gear 14 and the annular rack 16 can ensure that the state of the rotating rod 7 is not changed;
the support mechanism 9 comprises support legs 17, the support legs 17 have a good support effect, one ends of the support legs 17 are fixedly connected with one ends of the rotating rods 7, which are far away from the unmanned aerial vehicle body 1, the support legs 17 and the rotating rods 7 are obliquely arranged, when the rotating rods 7 rotate to an oblique state, the corresponding support legs 17 are just vertical to the ground, the lower ends of the support legs 17 are fixedly connected with support blocks 18, and the support blocks 18 are used for being in contact with the ground to play a support effect;
the supporting blocks 18 are arc-shaped, the supporting blocks 18 can form a circular frame body to play a role in stable supporting, the center of gravity of the unmanned aerial vehicle body 1 is stable due to the circular frame body and is not prone to toppling, the lower side surfaces of the supporting blocks 18 are made of rubber, the rubber plays a role in buffering protection, and the unmanned aerial vehicle has a protection function;
wherein, rotor protection machanism 10 includes arc frame 19, and arc frame 19 plays the effect of connecting through bending pole 20 and supporting leg 17 upper end fixed connection, bending pole 20, and arc frame 19 matches with power rotor 3, and bending pole 20 makes dwang 7 rotate to the tilt state time, and corresponding arc frame 19 can be the horizontality, and the arc frame 19 that corresponds this moment encircles just in 3 week sides of the electric power rotor that correspond, plays better guard action.
In the utility model, the device comprises the following steps:
when the aircraft takes off, the electric telescopic rods 6 are synchronously started and contracted to drive the corresponding connecting blocks 12 to horizontally move, the corresponding connecting blocks 12 drive the corresponding transverse rotating rods 13 to move, the corresponding transverse rotating rods 13 drive the corresponding two gears 14, under the action of the two corresponding annular racks 16, the two corresponding gears 14 rotate to further drive the corresponding transverse rotating rods 13 to rotate, so that the corresponding rotating rods 7 rotate to an inclined state, at the moment, the corresponding arc-shaped frames 19 just surround the periphery sides of the corresponding electric rotary wings 3 to play a role in protection, and at the moment, electric inspection can be carried out; when descending, the extension of 6 synchronous start-ups of a plurality of electric telescopic handle, the drive corresponds connecting block 12 horizontal migration, it drives the horizontal dwang 13 action that corresponds to correspond connecting block 12, the horizontal dwang 13 that corresponds drives two gears 14 that correspond, under the effect of two cyclic annular racks 16 that correspond, two gears 14 that correspond rotate, and then drive the horizontal dwang 13 rotation that corresponds, make corresponding dwang 7 rotate to the tilt state, corresponding supporting leg 17 is just perpendicular with ground, a circular support body is constituteed to a plurality of supporting shoes 18, play the effect of outrigger.
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 equivalent alternatives or modifications according to the technical solution of the present invention and the inventive concept thereof should be covered by the scope of the present invention.
Claims (6)
1. The electric power inspection device based on the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1) and is characterized in that the cross section of the lower end of the unmanned aerial vehicle body (1) is circular, a plurality of supports (2) are arranged on the side surface of the unmanned aerial vehicle body (1) in a surrounding manner, a plurality of power rotors (3) are arranged at the ends, away from the unmanned aerial vehicle body (1), of the supports (2) in a matching manner, the lower side surface of the unmanned aerial vehicle body (1) is a horizontal side surface and is fixedly connected with a suspender (4), an equipment nacelle (5) is fixedly connected to the lower end of the suspender (4), a plurality of electric telescopic rods (6) are arranged on the lower side of the unmanned aerial vehicle body (1) in a matching manner, a plurality of rotating rods (7) respectively corresponding to the plurality of electric telescopic rods (6) are arranged on the lower side of the unmanned aerial vehicle body (1), and control mechanisms (8) for controlling the rotating rods (7) to rotate are arranged at the telescopic ends of the electric telescopic rods (6), dwang (7) one end matches and is equipped with supporting mechanism (9) and rotor protection mechanism (10).
2. The unmanned aerial vehicle-based power inspection device according to claim 1, wherein a plurality of electric telescopic rods (6) are uniformly arranged, a connecting plate (11) is horizontally and fixedly connected to the lower side of the unmanned aerial vehicle body (1), and the plurality of electric telescopic rods (6) are fixedly connected with the connecting plate (11).
3. The electric power inspection device based on unmanned aerial vehicle of claim 2, characterized in that, control mechanism (8) includes connecting block (12), connecting block (12) and electric telescopic handle (6) flexible end fixed connection, it is connected with horizontal dwang (13) to rotate on connecting block (12), dwang (7) and horizontal dwang (13) middle part side fixed connection, the equal coaxial fixedly connected with gear (14) in horizontal dwang (13) both ends, two stopper (15) of fixedly connected with on connecting plate (11), two stopper (15) match with two gear (14) position respectively, two the bar notch has all been seted up in stopper (15), be equipped with in the bar notch and correspond cyclic annular rack (16) of gear (14) meshing.
4. The unmanned aerial vehicle-based power inspection device according to any one of claims 1-3, wherein the supporting mechanism (9) comprises a supporting leg (17), one end of the supporting leg (17) is fixedly connected with one end of the rotating rod (7) far away from the unmanned aerial vehicle body (1), the supporting leg (17) is obliquely arranged with the rotating rod (7), and a supporting block (18) is fixedly connected with the lower end of the supporting leg (17).
5. The unmanned aerial vehicle-based power inspection device according to claim 4, wherein the support block (18) is arc-shaped, and the lower side of the support block (18) is made of rubber.
6. The unmanned aerial vehicle-based power inspection device according to claim 4, wherein the rotor protection mechanism (10) comprises an arc-shaped frame (19), the arc-shaped frame (19) is fixedly connected with the upper ends of the supporting legs (17) through bending rods (20), and the arc-shaped frame (19) is matched with the power rotor (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121449194.5U CN216070501U (en) | 2021-06-29 | 2021-06-29 | Electric power inspection device based on unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121449194.5U CN216070501U (en) | 2021-06-29 | 2021-06-29 | Electric power inspection device based on unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN216070501U true CN216070501U (en) | 2022-03-18 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121449194.5U Active CN216070501U (en) | 2021-06-29 | 2021-06-29 | Electric power inspection device based on unmanned aerial vehicle |
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| Country | Link |
|---|---|
| CN (1) | CN216070501U (en) |
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2021
- 2021-06-29 CN CN202121449194.5U patent/CN216070501U/en active Active
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