CN215475750U

CN215475750U - Unmanned aerial vehicle high altitude electric power detection device

Info

Publication number: CN215475750U
Application number: CN202121249661.XU
Authority: CN
Inventors: 陆文成
Original assignee: Fengxian Hanzu Shengjing Cultural Tourism Development Co ltd
Current assignee: Xiejia Power Engineering Design Co ltd
Priority date: 2021-06-05
Filing date: 2021-06-05
Publication date: 2022-01-11
Anticipated expiration: 2031-06-05

Abstract

The utility model discloses an unmanned aerial vehicle high altitude electric power detection device, which belongs to the field of unmanned aerial vehicle inspection, and comprises a machine body and a cradle head detection device which is arranged below the machine body and is used for transmitting images, wherein the cradle head detection device is rotatably arranged at the bottom of the machine body, the top of the machine body is provided with two groups of line dropping devices, the line dropping devices are arranged at the top of the machine body and are arranged at the front and back of the top of the machine body along the axial direction of the body length of the machine body, an observation camera is arranged at the top of the machine body and between the two groups of line dropping devices, the top of the machine body is provided with a notch used for limiting the line dropping devices corresponding to the line dropping devices, each line dropping device comprises a swing rod, the top of the swing rod is provided with a line hooking hook head, the bottom of the swing rod is provided with a non-faced gear A, the non-faced gear A and the swing rod are integrally formed, so that the unmanned aerial vehicle can realize the line dropping function and can be guided by cables, closely observe whether the power cable has the damage, avoid unmanned aerial vehicle to revolve thick liquid routing, reduce the accident.

Description

Unmanned aerial vehicle high altitude electric power detection device

Technical Field

The utility model relates to the field of unmanned aerial vehicle inspection, in particular to an unmanned aerial vehicle high-altitude electric power detection device.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.

Compared with piloted aircraft, unmanned aerial vehicles are often more suitable for the work with higher danger coefficient, and unmanned aerial vehicles can be divided into military use and civil use according to the application field. For military use, unmanned aerial vehicle divide into reconnaissance aircraft and target drone, civilian aspect, unmanned aerial vehicle + trade is used, be the real just needs of unmanned aerial vehicle, at present take photo by plane, agriculture, the field such as plant protection and electric power are patrolled and examined obtains very big development, great expansion the usage of unmanned aerial vehicle itself, but in current unmanned aerial vehicle is patrolled and examined in carrying out electric power, move towards when patrolling and examining to the electric wire way, part high voltage electric line is more shelters from and the position is remote easily, inconvenient regulation and control unmanned aerial vehicle's flight angle is with taking a photograph, detect and have the dead angle, easily dredge.

SUMMERY OF THE UTILITY MODEL

1. Technical problem to be solved

Aiming at the problems in the prior art, the utility model aims to provide an unmanned aerial vehicle high-altitude power detection device which can realize the function of line dropping, can lead an unmanned aerial vehicle to take a cable as the guide, observe whether a power cable is damaged or not in a short distance, avoid the unmanned aerial vehicle rotating pulp routing and reduce the accidents.

2. Technical scheme

In order to solve the above problems, the present invention adopts the following technical solutions.

The utility model provides an unmanned aerial vehicle high altitude electric power detection device, includes the fuselage and installs the cloud platform detection device who is used for transmitting the image in the fuselage below, the bottom at the fuselage is installed to cloud platform detection device rotary type, the top of fuselage is provided with the device of falling the line, the device of falling the line is provided with two sets ofly and sets up at the top of fuselage around the axial of fuselage length, and the top that is located the fuselage just is located two sets ofly be provided with the observation camera between the device of falling the line, the notch that is used for spacing device of falling the line is offered to the device of corresponding falling the line in top of fuselage.

Furthermore, the thread falling device comprises a swing rod, a thread hooking hook head is arranged at the top of the swing rod, a non-planar gear A is arranged at the bottom of the swing rod, and the non-planar gear A and the swing rod are integrally formed.

Furthermore, the hook heads of the hook wire hook heads on the two swing rods are arranged on the machine body in opposite directions.

Further, the inside of fuselage is provided with the holding chamber, the inside of holding chamber corresponds the notch and is provided with two rails, two equal slidable mounting has the pinion rack on the rail, two rotate between the rail and install the board of dialling that is used for stirring the pinion rack, the both ends of dialling the board all are provided with the scarce face gear B of integrative formation.

Furthermore, a rotating shaft is rotatably installed at the circle center of the non-planar gear A and is rotatably fixed on the inner wall of the accommodating chamber.

Further, the top of two pinion rack and relative one side lateral wall all are provided with the teeth of a cogwheel, the middle part of dialling the board still is provided with driving motor.

Furthermore, the gear teeth on the top of the toothed plate are correspondingly meshed with the gear teeth on the side of the toothed plate, and the gear teeth on the top of the toothed plate are correspondingly meshed with the gear teeth on the side of the toothed plate.

3. Advantageous effects

Compared with the prior art, the utility model has the advantages that:

(1) this scheme, dial the board through driving motor rotation, dial the board both ends meshing drive pinion rack and make the pinion rack do the opposite directions motion of leaving mutually, the corresponding syntropy adduction or the syntropy of the corresponding pendulum rod of pinion rack top meshing is opened, when unmanned aerial vehicle is close the power cable, open two pendulum rods through system remote control, make the angle between two pendulum rods open, correspond the back with power cable position adjustment, make two pendulum rod adduction, two hook line gibs hold on the power cable simultaneously, realize the function of falling the line, can make unmanned aerial vehicle use the cable as the direction, closely observe the power cable and have or not damaged, avoid unmanned aerial vehicle to revolve thick liquid routing, fly along the power cable, the accident lowers, and can detect the condition that power cable both sides and basic station are connected, avoid the dead angle to dredge.

Drawings

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic sectional view of the accommodating chamber according to the present invention;

fig. 3 is a schematic top sectional view of the accommodating chamber of the present invention.

The reference numbers in the figures illustrate:

1. a body; 2. a holder detection device; 3. a wire dropping device; 4. observing the camera; 5. a notch; 6. a swing rod; 7. a hook head for hooking the thread; 8. a face-lacking gear A; 9. an accommodating chamber; 10. a rail bar; 11. a toothed plate; 12. dialing a plate; 13. a face-lacking gear B; 14. and (4) gear teeth.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention; it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and all other embodiments obtained by those skilled in the art without any inventive work are within the scope of the present invention.

Example 1:

please refer to fig. 1, an unmanned aerial vehicle high altitude electric power detection device, include fuselage 1 and install the cloud platform detection device 2 that is used for transmitting the image below fuselage 1, the bottom at fuselage 1 is installed to cloud platform detection device 2 rotary type, the top of fuselage 1 is provided with doffing device 3, doffing device 3 is provided with two sets ofly and sets up the top at fuselage 1 around the axial of 1 body length of fuselage, it is provided with observation camera 4 just to be located between two sets of doffing device 3 to be located the top of fuselage 1, the notch 5 that is used for spacing doffing device 3 is seted up to corresponding doffing device 3 in the top of fuselage 1, the hook line situation of doffing device 3 can be observed and surveyed to observation camera 4, the operating personnel of being convenient for in time adjust.

Referring to fig. 1-3, the thread dropping device 3 includes a swing link 6, a thread hooking hook 7 is disposed on the top of the swing link 6, a face-lacking gear A8 is disposed on the bottom of the swing link 6, and the face-lacking gear A8 and the swing link 6 are integrally formed.

Referring to fig. 1, the hook heads of the thread hooking hook heads 7 on the two swing rods 6 are installed on the machine body 1 in opposite directions.

Furthermore, the inner curved surface of the wire hooking hook head 7 is transversely provided with a roller which is convenient for walking on the electric power cable, reduces resistance and abrasion damage to the electric power cable,

referring to fig. 2-3, an accommodating chamber 9 is disposed inside the machine body 1, two rails 10 are disposed inside the accommodating chamber 9 corresponding to the notches 5, toothed plates 11 are slidably mounted on the two rails 10, a shifting plate 12 for shifting the toothed plates 11 is rotatably mounted between the two rails 10, and two ends of the shifting plate 12 are provided with integrally formed face-missing gears B13.

Referring to fig. 2, a rotating shaft is rotatably mounted at the center of the circle of the non-planar gear A8, and the rotating shaft is rotatably fixed on the inner wall of the accommodating chamber 9.

Referring to fig. 2-3, the top and the opposite side wall of the two toothed plates 11 are provided with gear teeth 14, and the middle of the shifting plate 12 is further provided with a driving motor (not shown).

Please refer to fig. 2-3, the face-missing gear B13 is correspondingly engaged with the side gear teeth 14 of the toothed plate 11, the top gear teeth 14 of the toothed plate 11 is correspondingly engaged with the face-missing gear a8, the rotating shifting plate 12 drives the two swing rods 6 to retract in the same direction or open in the same direction through the transmission of the toothed plate 11, so as to realize the wire-dropping function, so that the unmanned aerial vehicle can use the cable as the guide, observe whether the power cable is damaged in a short distance, avoid the unmanned aerial vehicle to spin pulp and wire, fly along the line, reduce the accidents, and detect the condition that the two sides of the power cable are connected with the base station, and avoid the four corners to be careless.

When in use: through driving motor rotation group board 12, dial 12 both ends meshing area drive pinion rack 11 and make pinion rack 11 do the opposite directions motion, the corresponding syntropy adduction or the syntropy of the corresponding pendulum rod 6 of pinion rack 11 top meshing is opened, when unmanned aerial vehicle is close the power cable, open two pendulum rods 6 through system remote control, make the angle between two pendulum rods 6 open, correspond the back with power cable position adjustment, make two pendulum rods 6 adduction, two hook wire gib heads 7 catch on the power cable simultaneously, realize the function of falling the line, can make unmanned aerial vehicle use the cable as the direction, closely observe the power cable and have or not damaged, avoid unmanned aerial vehicle to revolve thick liquid routing, fly along the power cable, reduce the accident, and can detect the condition that power cable both sides and basic station are connected, avoid the dead angle to dredge.

The foregoing is only a preferred embodiment of the present invention; the scope of the utility model is not limited thereto. Any person skilled in the art should be able to cover the technical scope of the present invention by equivalent or modified solutions and modifications within the technical scope of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle high altitude electric power detection device, includes fuselage (1) and installs cloud platform detection device (2) that are used for transmitting the image below fuselage (1), the bottom at fuselage (1), its characterized in that are installed to cloud platform detection device (2) rotary type: the top of fuselage (1) is provided with doffing device (3), doffing device (3) are provided with two sets ofly and set up at the top of fuselage (1) around the axial of fuselage (1) length, are located the top of fuselage (1) and are located two sets of be provided with between doffing device (3) and observe camera (4), notch (5) that are used for spacing doffing device (3) are offered to the top of fuselage (1) correspondence doffing device (3).

2. The high altitude electric power detection device of unmanned aerial vehicle of claim 1, characterized in that: the thread falling device (3) comprises a swing rod (6), a thread hooking hook head (7) is arranged at the top of the swing rod (6), a non-planar gear A (8) is arranged at the bottom of the swing rod (6), and the non-planar gear A (8) and the swing rod (6) are integrally formed.

3. The high altitude electric power detection device of unmanned aerial vehicle of claim 2, characterized in that: the hook heads of the hook wire hook heads (7) on the two swing rods (6) are arranged on the machine body (1) in opposite directions.

4. The high altitude electric power detection device of unmanned aerial vehicle of claim 2, characterized in that: the inside of fuselage (1) is provided with accommodation chamber (9), the inside of accommodation chamber (9) corresponds notch (5) and is provided with two rails (10), two equal slidable mounting has pinion rack (11) on rail (10), two rotate between rail (10) and install group board (12) that are used for stirring pinion rack (11), the both ends of dialling board (12) all are provided with the scarce face gear B (13) of integrative formation.

5. The high altitude electric power detection device of unmanned aerial vehicle of claim 2, characterized in that: the circle center of the non-planar gear A (8) is rotatably provided with a rotating shaft, and the rotating shaft is rotatably fixed on the inner wall of the accommodating chamber (9).

6. The high altitude electric power detection device of unmanned aerial vehicle of claim 4, characterized in that: the top and the relative one side lateral wall of two pinion rack (11) all are provided with teeth of a cogwheel (14), the middle part of dialling board (12) still is provided with driving motor.

7. The high altitude electric power detection device of unmanned aerial vehicle of claim 4, characterized in that: the gear teeth B (13) on the side of the tooth plate (11) are correspondingly meshed with the gear teeth (14) on the side of the tooth plate (11), the gear teeth (14) on the top of the tooth plate (11) are correspondingly meshed with the gear teeth A (8) on the side of the tooth plate, and the shifting plate (12) is rotated to drive the two swing rods (6) to retract in the same direction or open in the same direction through the transmission of the tooth plate (11).