CN110697064A - A supporting structure for unmanned aerial vehicle - Google Patents
A supporting structure for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN110697064A CN110697064A CN201911021979.XA CN201911021979A CN110697064A CN 110697064 A CN110697064 A CN 110697064A CN 201911021979 A CN201911021979 A CN 201911021979A CN 110697064 A CN110697064 A CN 110697064A
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- China
- Prior art keywords
- cleaning
- seat
- aerial vehicle
- unmanned aerial
- sliding
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- 238000004140 cleaning Methods 0.000 claims abstract description 75
- 210000003608 fece Anatomy 0.000 abstract description 25
- 230000005540 biological transmission Effects 0.000 abstract description 5
- 238000009434 installation Methods 0.000 description 11
- 239000004020 conductor Substances 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000010871 livestock manure Substances 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B08B1/10—
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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
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- 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
Abstract
The invention relates to an unmanned aerial vehicle, in particular to a support structure for the unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body and support frames fixed on two sides of the bottom of the unmanned aerial vehicle main body, wherein the support structure comprises a sliding seat, the top of the sliding seat is slidably connected with the support frames, the bottom of the sliding seat is fixedly connected with a cleaning structure, the cleaning structure comprises a cleaning seat, a triangular prism-shaped cleaning bulge is arranged at the center position of the bottom of the cleaning seat, the head end of the cleaning bulge is of a triangular pyramid-shaped structure, sliding grooves are respectively formed in two sides of the cleaning bulge of the cleaning seat, cleaning wings are respectively slidably connected in the two sliding grooves, and fixing bolts are connected to the cleaning wings in a threaded manner. This kind of support framework can install fast on unmanned aerial vehicle's support frame, and it is convenient to install, and can carry out high efficiency to the bird droppings on the power transmission line and clear away, can adapt to multiple line footpath power transmission line simultaneously and use.
Description
Technical Field
The invention relates to an unmanned aerial vehicle, in particular to a support structure for the unmanned aerial vehicle.
Background
Overhead line on the transmission line easily has the bird droppings to pile up, generally extremely difficult clear away, generally adopts unmanned aerial vehicle to clear away now, but current obstacles removing unmanned aerial vehicle mainly has following several not enough:
firstly, the cleaning effect is not obvious and the adjustability is poor, and the existing equipment always scrapes off bird droppings on the cable when cleaning the bird droppings; secondly, the existing cleaning structure is relatively fixed and cannot be simultaneously suitable for various cables with different diameters; thirdly, the hardness of the bird droppings is higher after the bird droppings are dried on a cable, and the existing equipment is slower in cleaning; fourth, dismantle the installation convenient inadequately, the structure of removing obstacles on the unmanned aerial vehicle of removing obstacles now uses the bolt to fix mostly, just so need unscrew all fixing bolt when dismantling and take off, and it is convenient inadequately to dismantle.
Therefore, in view of the above, research and improvement are made for the existing structure and defects, and a support structure for an unmanned aerial vehicle is provided to achieve the purpose of higher practical value.
Disclosure of Invention
The invention provides a support structure for an unmanned aerial vehicle, which can be quickly installed on a support frame of the unmanned aerial vehicle, is convenient to install, can quickly and efficiently remove bird droppings on a power transmission line, and can be suitable for power transmission lines with various wire diameters.
The technical scheme of the invention is as follows:
the utility model provides a supporting structure for unmanned aerial vehicle, includes the unmanned aerial vehicle main part and fixes the support frame in unmanned aerial vehicle main part bottom both sides, and supporting structure includes the sliding seat, the top of sliding seat with support frame sliding connection, the bottom fixedly connected with clearance structure of sliding seat, clearance structure is including clearance seat, the bottom central point of clearance seat puts the clearance arch that is equipped with the triangular prism shape, just the bellied head end of clearance is triangular pyramid structure, the clearance seat is in the sliding tray has all been seted up to the bellied both sides of clearance, and two equal sliding connection has the clearance wing in the sliding tray, and threaded connection has fixing bolt on the clearance wing.
Firstly, the sliding seat is slidably mounted on a support frame of the unmanned aerial vehicle main body, and the sliding seat is convenient to dismount and mount; in the using process, the cleaning structure can be driven by the unmanned aerial vehicle main body to clean bird dung on the cable, and the triangular prism-shaped cleaning protrusions are arranged at the bottom of the cleaning seat, and the triangular pyramid-shaped structures at the head ends of the cleaning protrusions, so that when sundries of bird dung on the cable are cleaned, the bird dung can be broken and cleaned along with the flying of the unmanned aerial vehicle main body, and the bird dung can be quickly and efficiently cleaned; simultaneously sliding connection has the clearance wing in the sliding tray of clearance seat bottom to threaded connection has fixing bolt on the clearance wing, so can be according to the distance between two clearance wings of the appropriate sliding adjustment of width of cable conductor when using, and lock fixedly through fixing bolt, be used for realizing the clearance of different diameter cable conductors.
Furthermore, the two cleaning wings are symmetrically arranged on two sides of the cleaning protrusion in a splayed shape. Two clearance wings of being convenient for clear up the bird manure of cable both sides, make its clearance cleaner high-efficient.
Furthermore, the bottom end of the cleaning wing is of an inclined structure, and the inclination angle is 60 degrees, so that the cleaning wing can also play a role in crushing when cleaning the bird dung sundries on the cable, and the smooth degree of cleaning is improved.
Further, trapezoidal sliding bulges are welded on the left side and the right side of the support frame, the top of the sliding seat is of a concave structure, trapezoidal sliding grooves are formed in the left side and the right side of the inner wall of the concave structure, and the sliding seat is connected with the trapezoidal sliding bulges of the support frame in a sliding mode through the trapezoidal sliding grooves.
When the installation, through the trapezoidal sliding tray of the spill structure inner wall both sides of sliding seat and the trapezoidal slip arch of the support frame left and right sides carry out sliding connection can, convenient and fast, the installation of being convenient for is dismantled.
Furthermore, an elastic bolt is fixed on the support frame and comprises a bolt seat and a bolt shaft, the bolt seat is provided with a first clamping plate and a second clamping plate with round holes, the bolt shaft penetrates through the first clamping plate and the second clamping plate through the round holes, a limiting bulge is arranged at the round hole of the second clamping plate, the bolt shaft is located on a shaft body between the first clamping plate and the second clamping plate, a spring is sleeved on the shaft body, one end of the spring is fixed on the limiting bulge, the other end of the spring is fixed on the bolt shaft, and a bolt hole which is matched with the bolt shaft and is spliced is formed in the sliding seat.
At the in-process of sliding seat slidable mounting at the support frame of unmanned aerial vehicle main part, upwards stimulate the bolt axle, the spring is in tensile state, after the trapezoidal sliding tray of sliding seat and the trapezoidal complete sliding connection of sliding projection of support frame, puts down the bolt axle again, because the reset action of spring, the bolt axle is automatic downwards and insert the downthehole spacing fixing that carries on of bolt, makes the sliding seat install more firm on the support frame.
Furthermore, the inserting end of the bolt shaft is of an inclined structure. When the installation sliding seat, the sliding seat is direct to be advanced along the protruding slip of the trapezoidal arch of support frame both sides through the trapezoidal sliding tray of both sides, impels bolt axle department back, because the grafting end of bolt axle is slope column structure, the sliding seat continues to impel jack-up bolt axle forward, then when arriving bolt hole position, because the effect of spring, the bolt axle falls automatically to plug to the bolt downthehole, does not need the shutting that the bolt can be accomplished to the pull bolt axle, has simplified installation procedure to a certain extent.
Furthermore, the outer wall of the bolt shaft is welded with a limiting column of a rectangular structure. Can carry out spacingly to the bolt axle when using, prevent that the bolt axle from taking place the axial rotation and leading to unable shutting of realizing the sliding seat.
The invention has the beneficial effects that:
according to the invention, through the arrangement of the sliding seat, firstly, the sliding seat is in sliding connection with the support frame of the unmanned aerial vehicle main body, and is locked through the elastic bolt, and the bottom end surface of the bolt shaft is of an inclined structure, so that the bolt can be locked without drawing and pulling the bolt shaft when the sliding seat is installed, compared with the prior art, the device is more convenient and faster in installation and cleaning of the structure, and has higher practicability; meanwhile, the cleaning structure at the bottom of the sliding seat is provided with a triangular prism-shaped cleaning bulge, the head end of the cleaning bulge is of a triangular pyramid-shaped structure, and bird droppings are crushed and cleaned by utilizing the sharp edge and the end part of the cleaning bulge, so that the bird droppings can be quickly and efficiently cleaned; and, clearance wing and clearance seat are sliding connection, can suitably slide the distance between two clearance wings of adjustment according to the width of cable conductor when using to it is fixed to lock through fixing bolt, be used for realizing the clearance of different diameter cable conductors.
Drawings
Fig. 1 is a schematic structural diagram of the present invention applied to an unmanned aerial vehicle;
FIG. 2 is a schematic structural view of a stent structure;
FIG. 3 is a schematic diagram of the disassembled structure of FIG. 2;
FIG. 4 is an enlarged schematic view of FIG. 3 at A;
FIG. 5 is a schematic structural view of a cleaning structure;
in the figure: 1-an unmanned aerial vehicle main body, 2-a support frame and 201-trapezoidal sliding bulges; 3-sliding seat, 301-trapezoidal sliding groove, 4-cleaning seat, 401-sliding groove, 5-cleaning protrusion, 6-cleaning wing, 7-fixing bolt, 8-bolt seat, 801-first clamping plate, 802-second clamping plate, 803-limiting protrusion, 9-bolt shaft, 901-limiting column and 10-spring.
Detailed Description
The drawings are for illustrative purposes only and are not to be construed as limiting the patent; for the purpose of better illustrating the embodiments, certain features of the drawings may be omitted, enlarged or reduced, and do not represent the size of an actual product; it will be understood by those skilled in the art that certain well-known structures in the drawings and descriptions thereof may be omitted. The positional relationships depicted in the drawings are for illustrative purposes only and are not to be construed as limiting the present patent.
Example 1:
as shown in fig. 1-5, the invention provides a support structure for an unmanned aerial vehicle, comprising an unmanned aerial vehicle main body 1 and support frames 2 fixed on two sides of the bottom of the unmanned aerial vehicle main body 1, the support structure comprises a sliding seat 3, a trapezoidal sliding bulge 201 is welded on the left and right sides of the support frame 2, the top of the sliding seat 3 is a concave structure, a trapezoidal sliding groove 301 is arranged on each of the left and right sides of the inner wall of the concave structure, the sliding seat 3 is connected with the trapezoidal sliding bulge 201 of the support frame 2 in a sliding manner through the trapezoidal sliding groove 301, the bottom of the sliding seat 3 is fixedly connected with two cleaning structures through bolts, each cleaning structure comprises a cleaning seat 4, the cleaning seat 4 is fixed on the bottom of the sliding seat 3 through bolts, the center position of the bottom of the cleaning seat 4 is provided with a triangular prism-shaped cleaning bulge 5, the head end of the cleaning bulge 5 is of a triangular pyramid-shaped structure, the cleaning seat 4 is provided with sliding, and the cleaning wings 6 are connected in the two sliding grooves 401 in a sliding manner, and the cleaning wings 6 are connected with fixing bolts 7 in a threaded manner.
Firstly, the trapezoidal sliding grooves 301 on two sides of the inner wall of the concave structure of the sliding seat 3 are in sliding connection with the trapezoidal sliding protrusions 201 on the left side and the right side of the support frame 2, so that the sliding seat 3 is slidably mounted on the support frame 2 of the unmanned aerial vehicle main body 1, and the dismounting and mounting are convenient; in the using process, the cleaning structure can be driven by the unmanned aerial vehicle main body 1 to clean bird dung on the cable, and the bottom of the cleaning seat 4 is provided with the triangular prism-shaped cleaning protrusion 5, and the head end of the cleaning protrusion 5 is of a triangular pyramid-shaped structure, so that when debris such as bird dung on the cable is cleaned, the debris can be broken and cleaned along with the flying of the unmanned aerial vehicle main body 1, and the bird dung can be quickly and efficiently cleaned; sliding connection has clearance wing 6 in the sliding tray 401 of clearance seat 4 bottom simultaneously to threaded connection has fixing bolt 7 on the clearance wing 6, so can be according to the appropriate distance between two clearance wings 6 of sliding adjustment of the width of cable conductor when using, and lock fixedly through fixing bolt 7, be used for realizing the clearance of different diameter cable conductors.
Referring to fig. 2 and 5, in the embodiment, the two cleaning wings 6 are symmetrically arranged on two sides of the cleaning protrusion 5 in a shape like a Chinese character 'ba', so that the two cleaning wings 6 can clean bird droppings on two sides of the cable conveniently, and the cleaning is cleaner and more efficient.
Referring to fig. 5, in the embodiment, the bottom end of the cleaning wing 6 is of an inclined structure, and the inclined angle is 60 degrees, so that the cleaning wing 6 can also perform a crushing function when cleaning bird droppings on the cable, thereby improving the smoothness of cleaning.
Please refer to fig. 4, in order to further enhance the stability of the sliding seat 3 mounted on the supporting frame 2, an elastic bolt is fixed on the supporting frame 2, the elastic bolt includes a bolt seat 8 and a bolt shaft 9, the bolt seat 8 is welded at one side edge of the supporting frame 2 and is disposed above the trapezoidal sliding protrusion 201, the bolt seat 8 is provided with a first clamping plate 801 and a second clamping plate 802 having circular holes, the bolt shaft 9 passes through the first clamping plate 801 and the second clamping plate 802 via the circular holes, the circular hole of the second clamping plate 802 is provided with a limiting protrusion 803, the bolt shaft 9 is disposed on a shaft body between the first clamping plate 801 and the second clamping plate 802 and is sleeved with a spring 10, one end of the spring 10 is fixed on the limiting protrusion 803, the other end is fixed on the bolt shaft 9, and the sliding seat 3 is provided with a bolt hole engaged with.
At the in-process of 3 slidable mounting of sliding seat at support frame 2 of unmanned aerial vehicle main part 1, upwards stimulate bolt axle 9, spring 10 is in tensile state, after trapezoidal sliding tray 301 of sliding seat 3 and the complete sliding connection of trapezoidal slip protruding 201 of support frame 2, put down bolt axle 9 again, because spring 10's reset action, bolt axle 9 is automatic downwards and inserts the downthehole spacing fixed that carries on of bolt, makes sliding seat 3 install more firm on support frame 2.
Referring to fig. 4, in order to facilitate the insertion of the latch shaft 9 and improve the installation efficiency, in this embodiment, the insertion end of the latch shaft 9 is an inclined structure. When installation sliding seat 3, sliding seat 3 directly slides along the trapezoidal slip arch 201 of support frame 2 both sides through the trapezoidal sliding tray 301 of both sides and impels, impel behind bolt axle 9 department, because the grafting end of bolt axle 9 is the slope column structure, sliding seat 3 continues to impel jack-up bolt axle 9 forward, then when arriving the bolt hole position, because spring 10's effect, bolt axle 9 falls automatically and pegs graft in the bolt hole, do not need the shutting that the bolt can be accomplished to pull bolt axle 9, the installation procedure has been simplified to a certain extent.
Referring to fig. 4, in the present embodiment, a limiting post 901 with a rectangular structure is welded on an outer wall of the latch shaft 9, so that the latch shaft 9 can be limited when in use, and the latch shaft 9 is prevented from rotating axially to prevent the sliding seat 3 from being locked.
The specific use mode and function of the embodiment are as follows:
during installation, firstly, the trapezoidal sliding grooves 301 on two sides of the inner wall of the concave structure of the sliding seat 3 are in sliding connection with the trapezoidal sliding protrusions 201 on the left side and the right side of the support frame 2, so that the sliding seat 3 is slidably installed on the support frame 2 of the unmanned aerial vehicle main body 1 and locked through the elastic bolt, and at the moment, the bottom end face of the bolt shaft 9 is of an inclined structure, so that locking of the bolt can be completed without drawing the bolt shaft 9 when the sliding seat 3 is installed, and the installation steps are simplified to a certain extent;
in the using process, the unmanned aerial vehicle main body 1 can drive the cleaning structure to clean the bird dung on the cable, and the triangular prism-shaped cleaning bulge 5 is welded at the center of the bottom of the cleaning seat 4, and the head end triangular pyramid-shaped structure of the cleaning bulge 5 is adopted, so that when sundries such as the bird dung on the cable are cleaned, the bird dung is crushed and cleaned by utilizing the sharp edges and the end parts of the cleaning bulge, and the bird dung can be quickly and efficiently cleaned; meanwhile, sliding grooves 401 are formed in the bottom of the cleaning seat 4 on two sides of the cleaning protrusion 5, two cleaning wings 6 are symmetrically connected in the sliding grooves 401 in a sliding mode, and fixing bolts 7 are connected to the cleaning wings 6 in a threaded mode, so that the distance between the two cleaning wings 6 can be properly adjusted in a sliding mode according to the width of cables when the cleaning seat is used, and the cleaning seat is used for cleaning cables with different diameters; and the bottom end face of the cleaning wing 6 is of an inclined structure, and the inclination angle is 60 degrees, so that the cleaning wing 6 can also play a role in crushing when cleaning bird dung sundries on the cable, and the smooth degree of cleaning is improved.
It should be understood that the above-described embodiments of the present invention are merely examples for clearly illustrating the present invention, and are not intended to limit the embodiments of the present invention. Other variations and modifications will be apparent to persons skilled in the art in light of the above description. And are neither required nor exhaustive of all embodiments. Any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention should be included in the protection scope of the claims of the present invention.
Claims (7)
1. The utility model provides a supporting structure for unmanned aerial vehicle, includes the unmanned aerial vehicle main part and fixes the support frame in unmanned aerial vehicle main part bottom both sides, its characterized in that, supporting structure includes the sliding seat, the top of sliding seat with support frame sliding connection, the bottom fixedly connected with clearance structure of sliding seat, the clearance structure is including the clearance seat, the bottom central point of clearance seat puts the clearance arch that is equipped with the triangular prism shape, just the bellied head end of clearance is triangular pyramid structure, the clearance seat is in the sliding tray has all been seted up to the bellied both sides of clearance, just equal sliding connection has the clearance wing in the sliding tray, and threaded connection has fixing bolt on the clearance wing.
2. The support structure for unmanned aerial vehicle of claim 1, wherein two cleaning wings are symmetrically arranged in a shape like a Chinese character 'ba' on two sides of the cleaning protrusion.
3. A support structure for a drone according to claim 1 or 2, characterised in that the bottom end of the cleaning wing is of inclined configuration and the angle of inclination is 60 degrees.
4. The support structure for unmanned aerial vehicle of claim 1, wherein trapezoidal sliding protrusions are welded on both sides of the support frame, the top of the sliding seat is of a concave structure, trapezoidal sliding grooves are formed on both sides of the inner wall of the concave structure, and the sliding seat is slidably connected with the trapezoidal sliding protrusions of the support frame through the trapezoidal sliding grooves.
5. The support structure for the unmanned aerial vehicle as claimed in claim 4, wherein an elastic bolt is fixed on the support frame, the elastic bolt includes a bolt seat and a bolt shaft, the bolt seat is provided with a first clamping plate and a second clamping plate with circular holes, the bolt shaft passes through the first clamping plate and the second clamping plate through the circular holes, a limiting protrusion is arranged at the circular hole of the second clamping plate, the bolt shaft is located on a shaft body between the first clamping plate and the second clamping plate and sleeved with a spring, one end of the spring is fixed on the limiting protrusion, the other end of the spring is fixed on the bolt shaft, and a bolt hole matched and plugged with the bolt shaft is formed in the sliding seat.
6. The mounting structure of claim 5, wherein the plug end of the latch shaft is a slanted configuration.
7. The support structure for unmanned aerial vehicle of claim 5, wherein the outer wall of the bolt shaft is welded with a rectangular-structure limiting column.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911021979.XA CN110697064A (en) | 2019-10-25 | 2019-10-25 | A supporting structure for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911021979.XA CN110697064A (en) | 2019-10-25 | 2019-10-25 | A supporting structure for unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN110697064A true CN110697064A (en) | 2020-01-17 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201911021979.XA Pending CN110697064A (en) | 2019-10-25 | 2019-10-25 | A supporting structure for unmanned aerial vehicle |
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| CN (1) | CN110697064A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113636076A (en) * | 2021-08-23 | 2021-11-12 | 南京赫鸿羲科技有限公司 | Power transmission and transformation equipment detection device and detection method based on unmanned aerial vehicle |
-
2019
- 2019-10-25 CN CN201911021979.XA patent/CN110697064A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113636076A (en) * | 2021-08-23 | 2021-11-12 | 南京赫鸿羲科技有限公司 | Power transmission and transformation equipment detection device and detection method based on unmanned aerial vehicle |
| CN113636076B (en) * | 2021-08-23 | 2024-03-12 | 南京赫鸿羲科技有限公司 | Power transmission and transformation equipment detection device and detection method based on unmanned aerial vehicle |
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