CN112124585A - Electric power inspection device based on unmanned aerial vehicle - Google Patents
Electric power inspection device based on unmanned aerial vehicle Download PDFInfo
- Publication number
- CN112124585A CN112124585A CN202011004262.7A CN202011004262A CN112124585A CN 112124585 A CN112124585 A CN 112124585A CN 202011004262 A CN202011004262 A CN 202011004262A CN 112124585 A CN112124585 A CN 112124585A
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- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- fixedly connected
- vehicle body
- inspection device
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 238000007689 inspection Methods 0.000 title claims abstract description 17
- 230000007246 mechanism Effects 0.000 claims abstract description 8
- 230000005540 biological transmission Effects 0.000 claims description 2
- 230000003139 buffering effect Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 description 4
- 230000000149 penetrating effect Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
- H02G1/02—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Electric Cable Installation (AREA)
Abstract
The invention discloses an unmanned aerial vehicle-based power inspection device which comprises an unmanned aerial vehicle body, wherein two mounting plates are fixedly connected to the side wall of the unmanned aerial vehicle body, the lower end of one mounting plate is fixedly connected with a fixed block, one rotating rod is electrically connected with the unmanned aerial vehicle body, the lower ends of the two rotating rods are both fixedly connected with a gear lack, the lower end of the unmanned aerial vehicle body is fixedly connected with four supporting columns, and the lower ends of the four supporting columns are both provided with a buffer mechanism. The unmanned aerial vehicle camera shooting device is reasonable in structure, when the unmanned aerial vehicle shoots, the rack plate moves left and right, the connecting rod is driven to swing left and right through the empty groove, the connecting rod drives the camera to swing left and right, comprehensive shooting of the camera is achieved, when the unmanned aerial vehicle lands, the four universal wheels collide with the ground, the four limiting rods respectively compress the first springs to buffer the unmanned aerial vehicle up and down, and under the action of the second springs, the unmanned aerial vehicle is buffered left and right.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an electric power inspection device based on an unmanned aerial vehicle.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. At present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
In the process of power inspection, an unmanned aerial vehicle is required to be used, a camera in the unmanned aerial vehicle is generally fixed at the bottom of the unmanned aerial vehicle, and is not adjustable and small in camera shooting range; in addition, if too fast when unmanned aerial vehicle descends, can cause the damage of organism, and current unmanned aerial vehicle is relatively poor at the convenient effect of shock attenuation.
Disclosure of Invention
The invention 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 invention adopts the following technical scheme:
an electric power inspection device based on an unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein two mounting plates are fixedly connected to the side wall of the unmanned aerial vehicle body, one of the mounting plates is fixedly connected with a fixed block at the lower end thereof, a telescopic rod is fixedly connected to the fixed block, a rack plate is fixedly connected to the telescopic rod, a slot is arranged on the rack plate in a penetrating manner, the lower end of the unmanned aerial vehicle body is rotatably connected with a connecting rod, a camera is fixedly connected to the lower end of the connecting rod, the connecting rod penetrates through the slot and is in sliding connection with the inner wall thereof, the lower end of the unmanned aerial vehicle body is rotatably connected with two rotating rods, one rotating rod is electrically connected with the unmanned aerial vehicle body, the lower ends of the two rotating rods are fixedly connected with two missing gears, the two missing gears are mutually meshed with the rack plate, and four buffer mechanisms are installed at the lower ends of the support columns.
Preferably, the transmission mechanism comprises a driving wheel and a driven wheel which are fixedly connected with the two rotating rods and coaxial with the two gear lacking wheels, and a conveying belt is rotatably connected between the driving wheel and the driven wheel.
Preferably, buffer gear includes the limiting plate with support column lower extreme fixed connection, the lower extreme of limiting plate rotates and is connected with two baffles of cavity piece and fixedly connected with, the first spring of inner wall fixedly connected with of cavity piece, the lower extreme fixedly connected with of first spring runs through cavity piece and rather than inner wall sliding connection's gag lever post, two equal fixedly connected with second spring between baffle and the cavity piece.
Preferably, the telescopic rod and the supporting column are arranged in a staggered mode.
Preferably, the dead slot is matched with the connecting rod, and the inner wall of the dead slot is abutted to the connecting rod.
Preferably, four the equal fixedly connected with universal wheel of lower extreme of gag lever post, four the universal wheel all passes through screw and gag lever post fixed connection.
Compared with the prior art, the invention has the beneficial effects that:
1. when unmanned aerial vehicle made a video recording, the dwang drove the action wheel and rotated from the driving wheel together when rotating, and the action wheel drives two and lacks the gear and rotate together with from the synchronous rotation of driving wheel, realizes moving about the rack board, drives the connecting rod horizontal hunting through the dead slot when moving about the rack board, and the connecting rod drives the camera horizontal hunting, realizes that the camera is comprehensively made a video recording.
2. When unmanned aerial vehicle descends, when four universal wheels bump with ground, four gag lever posts compress first spring respectively, cushion unmanned aerial vehicle from top to bottom, under the effect of second spring, cushion unmanned aerial vehicle about going on.
To sum up, when unmanned aerial vehicle made a video recording, when the rack board removed about, drive the connecting rod horizontal hunting through the dead slot, the connecting rod drives the camera horizontal hunting, realizes that the camera makes a video recording comprehensively, and when unmanned aerial vehicle descended, four universal wheels bumped with ground, four gag lever posts compressed first spring respectively, cushions about going on unmanned aerial vehicle, under the effect of second spring, cushions about going on unmanned aerial vehicle.
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 top view of a rack plate in the unmanned aerial vehicle-based power inspection device provided by the invention;
fig. 3 is an enlarged view of a structure a in fig. 1.
In the figure: 1 camera, 2 unmanned aerial vehicle body, 3 mounting panels, 4 telescopic links, 5 scarce gears, 6 action wheels, 7 follow driving wheel, 8 conveyer belts, 9 connecting rods, 10 dead slots, 11 rack plates, 12 support columns, 13 limiting plates, 14 universal wheels, the hollow block in 15, 16 baffles, 17 gag lever post, 18 first spring, 19 second springs.
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. 1-3, an electric power inspection device based on an unmanned aerial vehicle comprises an unmanned aerial vehicle body 2, two mounting plates 3 are fixedly connected to the side wall of the unmanned aerial vehicle body 2, a fixing block is fixedly connected to the lower end of one of the mounting plates 3, a telescopic rod 4 is fixedly connected to the fixing block, a rack plate 11 is fixedly connected to the telescopic rod 4, the telescopic rod 4 and a support post 12 are arranged in a staggered manner, a slot 10 is arranged on the rack plate 11 in a penetrating manner, a connecting rod 9 is rotatably connected to the lower end of the unmanned aerial vehicle body 2, a camera 1 is fixedly connected to the lower end of the connecting rod 9, the connecting rod 9 penetrates through the slot 10 and is slidably connected to the inner wall of the slot, the slot 10 is matched with the connecting rod 9, the inner wall of the slot 10 abuts against the connecting rod 9, two, the rotating rod is rotated by a button.
The equal fixedly connected with of lower extreme of two dwangs lacks gear 5, two lack gear 5 all with rack plate 11 intermeshing, be equipped with drive mechanism between two dwangs, drive mechanism include with two dwang fixed connection and with two lack gear 5 coaxial action wheels 6 and follow driving wheel 7, action wheel 6 with follow the rotation between driving wheel 7 and be connected with conveyer belt 8, four support columns 12 of lower extreme fixedly connected with of unmanned aerial vehicle body 2, four support column 12 slopes to set up.
Buffer gear is all installed to the lower extreme of four support columns 12, buffer gear includes limiting plate 13 with 12 lower extreme fixed connection of support column, the lower extreme of limiting plate 13 rotates and is connected with two baffles 16 of cavity piece 15 and fixedly connected with, the first spring 18 of the inner wall fixedly connected with of cavity piece 15, the lower extreme fixedly connected with of first spring 18 run through cavity piece 15 and rather than inner wall sliding connection's gag lever post 17, equal fixedly connected with second spring 19 between two baffles 16 and the cavity piece 15, the equal fixedly connected with universal wheel 14 of the lower extreme of four gag lever posts 17, four universal wheels 14 all pass through screw and gag lever post 17 fixed connection, four universal wheels 14 carry out the guided movement to unmanned aerial vehicle.
In the invention, when the unmanned aerial vehicle takes a picture, one of the rotating rods is rotated through the remote control switch, the rotating rod drives the driving wheel 6 and the driven wheel 7 to rotate together when rotating, the driving wheel 6 and the driven wheel 7 drive the two gear-lacking wheels 5 to rotate together when synchronously rotating, one of the gear-lacking pieces 5 is engaged with the rack plate 11 at the position with teeth and drives the gear-lacking pieces to move towards the telescopic rod 4, the other gear-lacking piece 5 is not contacted with the rack plate 11, when one of the gear segments 5 rotates at a toothless place without contacting with the rack plate 11, and the other gear segment 5 contacts with the rack plate 11, the rack plate 11 is driven to move in a direction away from the telescopic rod 4, so that the left and right movement of the rack plate 11 is realized, when the rack plate 11 moves left and right, the connecting rod 9 is driven to swing left and right through the empty groove 10, and the connecting rod 9 drives the camera 1 to swing left and right, so that the camera 1 can take a picture comprehensively.
When unmanned aerial vehicle descends, when four universal wheels 14 bump against ground, four gag lever posts 17 compress first spring 18 respectively, cushion unmanned aerial vehicle from top to bottom, under the effect of second spring 19, cushion unmanned aerial vehicle about going on.
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 (6)
1. The utility model provides an electric power inspection device based on unmanned aerial vehicle, includes unmanned aerial vehicle body (2), its characterized in that, unmanned aerial vehicle body (2) lateral wall fixedly connected with two mounting panels (3), one of them the lower extreme fixedly connected with fixed block of mounting panel (3), fixedly connected with telescopic link (4) on the fixed block, fixedly connected with rack plate (11) on telescopic link (4), it is equipped with dead slot (10) to run through on rack plate (11), the lower extreme of unmanned aerial vehicle body (2) rotates and is connected with connecting rod (9), the lower extreme fixedly connected with camera (1) of connecting rod (9), connecting rod (9) run through dead slot (10) and with its inner wall sliding connection, the lower extreme of unmanned aerial vehicle body (2) rotates and is connected with two dwang, one of them dwang and unmanned aerial vehicle body (2) electric connection, two equal fixedly connected with of lower extreme of dwang lacks gear (5), two it all with rack plate (11) intermeshing, two to lack gear (5) be equipped with drive mechanism between the dwang, four support columns (12), four of the lower extreme fixedly connected with of unmanned aerial vehicle body (2) buffer gear is all installed to the lower extreme of support column (12).
2. The unmanned aerial vehicle-based power inspection device according to claim 1, wherein the transmission mechanism comprises a driving wheel (6) and a driven wheel (7) which are fixedly connected with the two rotating rods and coaxial with the two missing gears (5), and a conveying belt (8) is rotatably connected between the driving wheel (6) and the driven wheel (7).
3. The electric power inspection device based on the unmanned aerial vehicle of claim 1, wherein the buffering mechanism comprises a limiting plate (13) fixedly connected with the lower end of the supporting column (12), the lower end of the limiting plate (13) is rotatably connected with a hollow block (15) and two fixedly connected baffle plates (16), the inner wall of the hollow block (15) is fixedly connected with a first spring (18), the lower end of the first spring (18) is fixedly connected with a limiting rod (17) which penetrates through the hollow block (15) and is in sliding connection with the inner wall of the hollow block, and two second springs (19) are fixedly connected between the baffle plates (16) and the hollow block (15).
4. The unmanned aerial vehicle-based power inspection device according to claim 1, wherein the telescopic rod (4) and the support column (12) are arranged in a staggered manner.
5. The unmanned aerial vehicle-based power inspection device according to claim 1, wherein the empty slot (10) is matched with the connecting rod (9), and the inner wall of the empty slot (10) is abutted against the connecting rod (9).
6. The unmanned aerial vehicle-based power inspection device according to claim 1, wherein the lower ends of the four limiting rods (17) are fixedly connected with universal wheels (14), and the four universal wheels (14) are fixedly connected with the limiting rods (17) through screws.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011004262.7A CN112124585A (en) | 2020-09-22 | 2020-09-22 | Electric power inspection device based on unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011004262.7A CN112124585A (en) | 2020-09-22 | 2020-09-22 | Electric power inspection device based on unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112124585A true CN112124585A (en) | 2020-12-25 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011004262.7A Pending CN112124585A (en) | 2020-09-22 | 2020-09-22 | Electric power inspection device based on unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112124585A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112849405A (en) * | 2021-02-02 | 2021-05-28 | 高源� | Electric power unmanned aerial vehicle patrols and examines path planning device |
-
2020
- 2020-09-22 CN CN202011004262.7A patent/CN112124585A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112849405A (en) * | 2021-02-02 | 2021-05-28 | 高源� | Electric power unmanned aerial vehicle patrols and examines path planning device |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20201225 |