CN113086197A - Be used for abluent unmanned aerial vehicle system of insulator - Google Patents
Be used for abluent unmanned aerial vehicle system of insulator Download PDFInfo
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- CN113086197A CN113086197A CN202110444337.1A CN202110444337A CN113086197A CN 113086197 A CN113086197 A CN 113086197A CN 202110444337 A CN202110444337 A CN 202110444337A CN 113086197 A CN113086197 A CN 113086197A
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- aerial vehicle
- unmanned aerial
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- 239000012212 insulator Substances 0.000 title claims abstract description 60
- 238000002347 injection Methods 0.000 claims abstract description 55
- 239000007924 injection Substances 0.000 claims abstract description 55
- 239000007921 spray Substances 0.000 claims abstract description 30
- 238000005507 spraying Methods 0.000 claims abstract description 27
- 238000004891 communication Methods 0.000 claims description 19
- 238000010248 power generation Methods 0.000 claims description 14
- 238000001802 infusion Methods 0.000 claims description 13
- 239000000463 material Substances 0.000 claims description 4
- 239000011347 resin Substances 0.000 claims description 4
- 229920005989 resin Polymers 0.000 claims description 4
- 235000012489 doughnuts Nutrition 0.000 claims 1
- 238000004140 cleaning Methods 0.000 abstract description 19
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 239000000243 solution Substances 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 239000003365 glass fiber Substances 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 230000000007 visual effect Effects 0.000 description 3
- 238000005406 washing Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 241000220317 Rosa Species 0.000 description 1
- 230000009194 climbing Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 238000011897 real-time detection Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
- B64C39/022—Tethered aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B13/00—Accessories or details of general applicability for machines or apparatus for cleaning
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B3/00—Cleaning by methods involving the use or presence of liquid or steam
- B08B3/02—Cleaning by the force of jets or sprays
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
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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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention relates to the technical field of electric power safety, and particularly provides an unmanned aerial vehicle system for insulator cleaning, wherein the unmanned aerial vehicle system comprises a single-duct unmanned aerial vehicle, an injection mechanism arranged on the single-duct unmanned aerial vehicle, a high-pressure injection pump connected with the injection mechanism, and controllers for respectively controlling the single-duct unmanned aerial vehicle and the high-pressure injection pump, wherein: the single-duct unmanned aerial vehicle comprises an unmanned aerial vehicle cover body, a first driving motor, a second driving motor, a first driving paddle arranged on the first driving motor and a second driving paddle arranged on the second driving motor, wherein the first driving motor and the second driving motor are vertically and symmetrically arranged in the unmanned aerial vehicle cover body; the controller is used for controlling the single-duct unmanned aerial vehicle to carry the spraying mechanism to a preset position and controlling the spraying flow of the high-pressure spraying pump to the spraying mechanism so that the spraying mechanism sprays and cleans the insulator. The unmanned aerial vehicle system can improve the efficiency and safety of cleaning the insulator.
Description
Technical Field
The invention relates to the technical field of electric power safety, in particular to an unmanned aerial vehicle system for insulator cleaning.
Background
The insulator that electric power iron tower built plays insulating effect between iron tower and high-voltage line, in the application scene of reality, receives factors such as environment and weather to influence, and the surface of insulator can accumulate the ash layer in certain time, and at this in-process, if do not wash the surface ash layer of insulator for a long time, because the insulating nature variation that leads to the insulator of insulator increases of insulator surface dust, the insulator will produce "pollution flashover" phenomenon, and the safe operation of electric wire netting will be seriously influenced to the pollution flashover. At present, the cleaning of the insulator mainly has two modes:
the first mode is manual tower climbing cleaning, and the mode has the disadvantages of high labor intensity, low efficiency and potential safety hazard; the other mode is high-pressure water spray cleaning by a helicopter, which has high efficiency, high cost and extremely high potential safety hazard. Therefore, the current cleaning mode for the insulator is low in applicability.
Disclosure of Invention
The invention aims to solve the problem that the insulator cleaning mode in the prior art is low in applicability, and provides an unmanned aerial vehicle system for cleaning insulators, so that the cleaning efficiency and safety of the insulator cleaning are improved.
The invention provides an unmanned aerial vehicle system for cleaning insulators, wherein the unmanned aerial vehicle system comprises a single-duct unmanned aerial vehicle, an injection mechanism arranged on the single-duct unmanned aerial vehicle, a high-pressure injection pump connected with the injection mechanism, and controllers for respectively controlling the single-duct unmanned aerial vehicle and the high-pressure injection pump, wherein:
the single-duct unmanned aerial vehicle comprises an unmanned aerial vehicle cover body, a first driving motor, a second driving motor, a first driving paddle arranged on the first driving motor, and a second driving paddle arranged on the second driving motor, wherein the first driving motor and the second driving motor are vertically and symmetrically arranged in the unmanned aerial vehicle cover body;
the controller is used for controlling the single-duct unmanned aerial vehicle to carry the spraying mechanism to a preset position and controlling the spraying flow of the high-pressure spraying pump to the spraying mechanism so that the spraying mechanism can spray and clean the insulator;
the controller is used for controlling the single-duct unmanned aerial vehicle to carry the spraying mechanism to a preset position and controlling the high-pressure spraying pump to spray the spraying flow of the spraying mechanism, so that the spraying mechanism sprays and cleans the insulator.
Optionally, the drone system further comprises a communication cable, an infusion cable, a power supply cable, and a power generation device, wherein:
the controller and the single-duct unmanned aerial vehicle are in communication connection through the communication cable;
the injection mechanism and the high-pressure injection pump are connected through the infusion cable pipeline;
the controller is connected with the power generation device and used for converting an alternating current power supply output by the power generation device into a direct current power supply and supplying power to the single-duct unmanned aerial vehicle through the power supply cable.
Optionally, the unmanned aerial vehicle system further comprises a safety mooring rope for limiting the flight distance of the single-duct unmanned aerial vehicle, one end of the safety mooring rope is installed on the single-duct unmanned aerial vehicle, and the other end of the safety mooring rope is installed on the power generation device, wherein:
the safety mooring rope, the communication cable, the infusion cable and the power supply cable are integrally arranged.
Optionally, the spray mechanism comprises a spray wand and a spray gun, wherein:
one end of the injection rod is fixed on the infusion cable, and the injection gun is rotatably arranged at the other end of the injection rod.
The controller is further used for controlling the flight height of the single-duct unmanned aerial vehicle according to the real-time wind speed.
Optionally, still be equipped with distance sensor on the single duct unmanned aerial vehicle, wherein:
the distance sensor is used for identifying the real-time distance between the single-duct unmanned aerial vehicle and the insulator and sending the real-time distance to the controller;
the controller is further used for controlling the flight range of the single-duct unmanned aerial vehicle according to the real-time distance.
Optionally, still be equipped with visual sensor on the single duct unmanned aerial vehicle, wherein:
the vision sensor is used for acquiring an image of the insulator and sending the acquired image to the controller;
the controller is used for determining the type of the insulator and the direction and the size of the insulator according to the acquired image so as to control the flying height and the moving flying path of the single-duct unmanned aerial vehicle according to the type of the insulator and the direction and the size of the insulator.
Optionally, an air speed sensor is arranged on the single-duct unmanned aerial vehicle, and the air speed sensor is used for collecting real-time air speed of a flight environment and sending the real-time air speed to the controller;
the controller is used for controlling the flight height of the single-duct unmanned aerial vehicle according to the real-time wind speed.
Optionally, the single-duct drone further comprises a safety battery backup for emergency power supply of the single-duct drone, wherein:
safe stand-by battery locates the middle part of the unmanned aerial vehicle cover body.
Optionally, the unmanned aerial vehicle's cover body with injection mechanism all adopts resin glass fiber material to make.
Optionally, the unmanned aerial vehicle cover body is set to be circular, or set to be ring shape.
The invention provides an unmanned aerial vehicle system for cleaning insulators, which is characterized in that a single-duct unmanned aerial vehicle, an injection mechanism arranged on the single-duct unmanned aerial vehicle, a high-pressure injection pump connected with the injection mechanism and controllers respectively controlling the single-duct unmanned aerial vehicle and the high-pressure injection pump are arranged, so that the single-duct unmanned aerial vehicle is controlled by the controllers to carry the injection mechanism to a preset position and to control the injection flow of the high-pressure injection pump to the injection mechanism, and the injection mechanism is controlled to perform injection cleaning on the insulators, thereby improving the efficiency and safety of the unmanned aerial vehicle system for cleaning the insulators, and in addition, the single-duct unmanned aerial vehicle is arranged in the following mode: the unmanned aerial vehicle is characterized in that the unmanned aerial vehicle comprises a first driving motor and a second driving motor, wherein the first driving motor is provided with a first driving paddle, the second driving motor is provided with a second driving paddle, the second driving motor is perpendicular to the first driving paddle, the second driving motor is symmetrical to the second driving paddle, and the unmanned aerial vehicle is arranged in a hood body.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the embodiments or the prior art descriptions will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without inventive exercise.
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle system according to an embodiment of the present invention.
Wherein, the reference numbers in the specification are as follows:
u-single duct unmanned aerial vehicle;
i-an injection mechanism;
an H-spray bar;
g-a spray gun;
c-a four-in-one cable;
m-a controller;
e-generating set, high pressure jet pump.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail below with reference to the accompanying drawings and specific embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
Furthermore, in the following description, for purposes of explanation and not limitation, specific details are set forth, such as particular systems, methods, etc., in order to provide a thorough understanding of the embodiments of the invention. It will be apparent, however, to one skilled in the art that the present invention may be practiced in other embodiments that depart from these specific details. In other instances, detailed descriptions of well-known systems, circuits, elements, and methods are omitted so as not to obscure the description of the present invention with unnecessary detail.
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 some, not all, embodiments of the present invention. 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.
In order to explain the technical means of the present invention, the following description will be given by way of specific examples.
The invention provides an unmanned aerial vehicle system for insulators, which can be applied to cleaning insulators on an electric iron tower and improve the cleaning efficiency and safety of cleaning the insulators, and the unmanned aerial vehicle system is specifically explained by the following embodiments.
Specifically, as shown in fig. 1, in one embodiment, the unmanned aerial vehicle system includes a single-ducted unmanned aerial vehicle U, an injection mechanism I fixedly provided on the single-ducted unmanned aerial vehicle U, a high-pressure injection pump E connected with the injection mechanism I, and a controller M that controls the single-ducted unmanned aerial vehicle U and the high-pressure injection pump E, respectively. The controller M is used for controlling the single-duct unmanned aerial vehicle U to carry the spraying mechanism I to a preset position and controlling the spraying flow of the high-pressure spraying pump E to the spraying mechanism I so that the spraying mechanism I sprays and cleans the insulator.
It can be understood that the single ducted unmanned aerial vehicle U is an unmanned device with a duct (unmanned aerial vehicle cover body) as a main body, and specifically, the forward and reverse driving motor and the forward and reverse driving paddle are arranged in the duct to drive the high-speed rotation of the driving paddle to fly by controlling the driving motor, and the flight attitude of the single ducted unmanned aerial vehicle U can be controlled by controlling the periodic variable pitch device of the driving paddle, wherein the single ducted unmanned aerial vehicle U has many advantages of stable flight, applicability, flexibility, strong carrying capability, insulation of a shell and the like, in the embodiment, the single ducted unmanned aerial vehicle U carries the injection mechanism I by adopting the single ducted unmanned aerial vehicle U, and the controller M is arranged to carry out flight control on the single ducted unmanned aerial vehicle U and control the injection flow of the high-pressure injection pump E to the injection mechanism I, and in the actual application scene, the single ducted unmanned aerial vehicle U can be controlled to fly in multiple angles and multiple directions, so that the spraying mechanism I can clean the insulator completely.
Specifically, single duct unmanned aerial vehicle U includes the unmanned aerial vehicle cover body (duct), first driving motor, second driving motor, locates the first drive oar on the first driving motor to and locate the second drive oar on the second driving motor, wherein: first driving motor and second driving motor install on same axial plane or same axle, can locate unmanned aerial vehicle aircraft bonnet internally with first driving motor and second driving motor perpendicular and symmetry respectively to make first driving oar and second driving oar form positive and negative double-oar. That is, coaxial central line installation (position unanimity from top to bottom) is in the unmanned aerial vehicle cover body about first driving motor and the second driving motor, and first drive oar can be understood as positive drive oar, and the second drive oar can be understood as the reverse drive oar, and unmanned aerial vehicle covers the duct formula overall arrangement that has set up coaxial and positive and negative double-oar in the body.
In the above-mentioned embodiment, through setting up single duct unmanned aerial vehicle U, locate the injection mechanism I on the single duct unmanned aerial vehicle U, the high-pressure jet pump E who is connected with injection mechanism I, and control single duct unmanned aerial vehicle U and high-pressure jet pump E's controller M respectively, so that carry on injection mechanism I to preset position through controller M control single duct unmanned aerial vehicle U, and control high-pressure jet pump E to injection mechanism I's injection flow, so that injection mechanism I sprays the washing to the insulator, thereby improve unmanned aerial vehicle system to insulator abluent efficiency and security. In addition, because unmanned aerial vehicle is single duct unmanned aerial vehicle U, unmanned aerial vehicle's power and circuit layout still can be simplified, so that reduce the influence of transmission line high voltage electromagnetic environment to this single duct unmanned aerial vehicle U's driving motor and circuit, and through the dual drive motor structure who sets up positive and negative double-oar, can also offset the deflection vector when driving motor drives driving oar horizontal rotation during can making practical application, thereby realize this single duct unmanned aerial vehicle U's flight more stable, in order to improve single duct unmanned aerial vehicle U's security.
In one embodiment, the drone system further comprises a communication cable, an infusion cable, a power supply cable and a power generation device E, wherein: the controller M is in communication connection with the single-duct unmanned aerial vehicle U through a communication cable; the injection mechanism I is connected with the high-pressure injection pump E through a transfusion cable pipeline; controller M is connected with power generation facility E, and controller M is used for, converts the alternating current power supply of power generation facility E output to DC power supply to supply power to single duct unmanned aerial vehicle U through the power supply cable.
In the above-mentioned embodiment, realize controller M and single duct unmanned aerial vehicle U's communication transmission through the mode that sets up the communication cable, can be so that the process of communication and control is more stable, and supplies power to single duct unmanned aerial vehicle U through the mode that sets up power generation facility E and power supply cable, when improving single duct unmanned aerial vehicle U's flight time, further can also improve the flexibility, suitability and the stability that unmanned aerial vehicle system used.
In one embodiment, as shown in fig. 1, the unmanned aerial vehicle system further includes a safety mooring rope for limiting the flight distance of the single ducted unmanned aerial vehicle U, specifically, one end of the safety mooring rope is installed on the single ducted unmanned aerial vehicle U, based on the power generation device E set up in the above embodiment, further, the other end of the safety mooring rope is installed on the power generation device E, wherein the safety mooring rope, the communication cable, the infusion cable and the power supply cable are set up as a whole. That is, the safety mooring rope, the communication cable, the infusion cable and the power supply cable can be integrally arranged to encapsulate the safety mooring rope, the communication cable, the infusion cable and the power supply cable into a four-in-one cable C.
In the above-mentioned embodiment, through setting up the flight distance of the single duct unmanned aerial vehicle U of safe rope restriction, so that single duct unmanned aerial vehicle U can also get back to ground safely under the out of control state, ensure that single duct unmanned aerial vehicle U can not appear the blind flight under the out of control state, thereby improve single duct unmanned aerial vehicle U's security, and through setting the rope of safe rope mooring, the communication cable, infusion cable and power supply cable to a four unification cables C, can also improve unmanned aerial vehicle system's portability and the flexibility of using.
In one embodiment, as shown in fig. 1, the spray mechanism I includes a spray bar H and a spray gun G, wherein: one end of the spray rod H is fixed on the transfusion cable, and the spray gun G is rotatably arranged at the other end of the spray rod H.
Injection mechanism I in the above-mentioned embodiment sprays pole H and spray gun G through setting up to and spray gun G rotatable other end of locating spray pole H, can make the washing liquid conveying of cable of will infusing through spray pole H to spray pole H, and spray gun G through the adjustment, with control injection angle, thereby improve the flexibility of unmanned aerial vehicle system.
In one embodiment, the single duct unmanned aerial vehicle U is further provided with a distance sensor thereon, wherein: the distance sensor can be a radar sensor, a laser sensor or an ultrasonic sensor, and the like, is not particularly limited, and can be selected according to actual scenes. The distance sensor is used for identifying the real-time distance between the single-duct unmanned aerial vehicle U and the insulator and sending the real-time distance to the controller M; the controller M is also used for controlling the flight range of the single-duct unmanned aerial vehicle U according to the real-time distance. In an application scenario, when the single-duct unmanned aerial vehicle U is controlled to fly to a predetermined height, further, the real-time distance between the single-duct unmanned aerial vehicle U and the insulator is detected in real time through the distance sensor, so as to control the distance between the injection mechanism I on the single-duct unmanned aerial vehicle U and the insulator according to the real-time distance.
In the above-mentioned embodiment, through set up distance sensor (not shown in the figure) on single duct unmanned aerial vehicle U to the real-time distance that detects through distance sensor and control the distance of injection mechanism I and insulator, can make single duct unmanned aerial vehicle U's flight more corresponding, and the accuracy of flight, in order to improve unmanned aerial vehicle system's clean efficiency.
In one embodiment, a vision sensor (not shown in the figure) is further provided on the single duct unmanned aerial vehicle U, specifically, the vision sensor may specifically be a camera or the like, wherein: the vision sensor is used for acquiring an image of the insulator and sending the acquired image to the controller M; the controller M is used for determining the type of the insulator and the direction and the size of the insulator according to the collected image so as to control the flying height and the moving flying path of the single-duct unmanned aerial vehicle U according to the type of the insulator and the direction and the size of the insulator.
In the above-mentioned embodiment, through set up visual sensor on single duct unmanned aerial vehicle U, can be so that image transmission who will gather the insulator in real time through visual sensor to controller M, in order to realize that controller M confirms the type of insulator and the direction and the size of insulator according to gathering the image, then can further make controller M according to the type of insulator and the direction and the size of insulator and the flight path of single duct unmanned aerial vehicle U of accurate control, thereby improve the accuracy of single duct unmanned aerial vehicle U flight, in order to improve unmanned aerial vehicle system's cleaning efficiency.
In one embodiment, the single-duct unmanned aerial vehicle U is further provided with an air speed sensor (not shown in the figure), and specifically, the air speed sensor is configured to collect a real-time air speed of a flight environment and send the real-time air speed to the controller M; the controller M is also used for controlling the flight height of the single-duct unmanned aerial vehicle U according to the real-time wind speed. In an application scenario, when controlling the single-duct unmanned aerial vehicle U to fly to a certain height, the current real-time wind speed is detected through the wind speed sensor, for example, the wind speed sensor will detect that the current real-time wind speed is 50M/s and send to the controller M, the controller M compares the real-time wind speed with a preset wind speed threshold value, the wind speed at the moment is relatively large, and then the controller M can control the single-duct unmanned aerial vehicle U to reduce the flying height according to the real-time wind speed, so that the single-duct unmanned aerial vehicle U is located at a safe height.
In the above-mentioned embodiment, through set up air velocity transducer on single duct unmanned aerial vehicle U, can be so that the wind speed through air velocity transducer real-time detection flight environment to according to real-time wind speed real-time regulation and control single duct unmanned aerial vehicle U's flying height, in order to improve single duct unmanned aerial vehicle U's security.
In one embodiment, the single ducted drone U further comprises a safety battery backup for emergency powering of the single ducted drone U, wherein: safe stand-by battery locates the middle part of the unmanned aerial vehicle cover body. Specifically, based on first driving motor and the second driving motor that set up in the above-mentioned embodiment, can locate this safe battery backup between first driving motor and the second driving motor to make safe battery backup locate the middle part of the unmanned aerial vehicle cover body.
In the above-mentioned embodiment, through setting up safe stand-by battery, provide safe stand-by power supply when can providing single duct unmanned aerial vehicle U flight, improve the stability of single duct unmanned aerial vehicle U flight, in addition, through locating the middle part of the unmanned aerial vehicle cover body with safe stand-by battery, can also reduce single duct unmanned aerial vehicle U's focus to the realization is on the basis of safe mooring rope, further improves the stability of single duct unmanned aerial vehicle U flight.
In one embodiment, the unmanned aerial vehicle cover body and the injection mechanism I are both made of resin glass fiber materials. In the above-mentioned embodiment, through the unmanned aerial vehicle cover body and the injection mechanism I that adopt the resin glass fiber material to make, can not cause the electric power phenomenon such as arcing to appear when can be close to the insulator on the electric power tower for single duct unmanned aerial vehicle U and injection mechanism I to improve the stability of unmanned aerial vehicle system.
In one embodiment, the unmanned aerial vehicle cover body specifically can be set to be circular, or set to be ring shape etc.. In the above-mentioned embodiment, establish to circular through the cover body with unmanned aerial vehicle, perhaps establish to ring shape, can be so that single duct unmanned aerial vehicle U when actual flight, can be so that reduce the resistance that single duct unmanned aerial vehicle U rose the back and fly, improve the stability and the security that single duct unmanned aerial vehicle U flies.
The above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; such modifications and substitutions do not substantially depart from the spirit and scope of the embodiments of the present invention, and are intended to be included within the scope of the present invention.
Claims (10)
1. The utility model provides a be used for abluent unmanned aerial vehicle system of insulator, a serial communication port, unmanned aerial vehicle system includes single duct unmanned aerial vehicle, locates last injection mechanism of single duct unmanned aerial vehicle, with the high-pressure jet pump that injection mechanism connects, and control respectively single duct unmanned aerial vehicle with the controller of high-pressure jet pump, wherein:
the single-duct unmanned aerial vehicle comprises an unmanned aerial vehicle cover body, a first driving motor, a second driving motor, a first driving paddle arranged on the first driving motor, and a second driving paddle arranged on the second driving motor, wherein the first driving motor and the second driving motor are vertically and symmetrically arranged in the unmanned aerial vehicle cover body;
the controller is used for controlling the single-duct unmanned aerial vehicle to carry the spraying mechanism to a preset position and controlling the high-pressure spraying pump to spray the spraying flow of the spraying mechanism, so that the spraying mechanism sprays and cleans the insulator.
2. The drone system of claim 1, further comprising a communication cable, an infusion cable, a power supply cable, and a power generation device, wherein:
the controller and the single-duct unmanned aerial vehicle are in communication connection through the communication cable;
the injection mechanism and the high-pressure injection pump are connected through the infusion cable pipeline;
the controller is connected with the power generation device and used for converting an alternating current power supply output by the power generation device into a direct current power supply and supplying power to the single-duct unmanned aerial vehicle through the power supply cable.
3. The drone system of claim 2, further comprising a safety tie down rope for limiting a flight distance of the single ducted drone, one end of the safety tie down rope being mounted on the single ducted drone, the other end of the safety tie down rope being mounted on the power generation device, wherein:
the safety mooring rope, the communication cable, the infusion cable and the power supply cable are integrally arranged.
4. The drone system of claim 2, wherein the spray mechanism includes a spray wand and a spray gun, wherein:
one end of the injection rod is fixed on the infusion cable, and the injection gun is rotatably arranged at the other end of the injection rod.
5. The drone system of claim 1, further including a distance sensor on the single ducted drone, wherein:
the distance sensor is used for identifying the real-time distance between the single-duct unmanned aerial vehicle and the insulator and sending the real-time distance to the controller;
the controller is further used for controlling the flight range of the single-duct unmanned aerial vehicle according to the real-time distance.
6. The drone system of claim 5, further including a vision sensor on the single ducted drone, wherein:
the vision sensor is used for acquiring an image of the insulator and sending the acquired image to the controller;
the controller is used for determining the type of the insulator and the direction and the size of the insulator according to the acquired image so as to control the flying height and the moving flying path of the single-duct unmanned aerial vehicle according to the type of the insulator and the direction and the size of the insulator.
7. The unmanned aerial vehicle system of any one of claims 1-6, wherein the single-duct unmanned aerial vehicle is provided with a wind speed sensor, and the wind speed sensor is used for acquiring real-time wind speed of a flight environment and sending the real-time wind speed to the controller;
the controller is used for controlling the flight height of the single-duct unmanned aerial vehicle according to the real-time wind speed.
8. The drone system of claim 7, wherein the single ducted drone further includes a safety backup battery for emergency powering of the single ducted drone, wherein:
safe stand-by battery locates the middle part of the unmanned aerial vehicle cover body.
9. The drone system of claim 1, wherein the unmanned aerial vehicle's hood and the spraying mechanism are both made of fiberglass-resin material.
10. The unmanned aerial vehicle system of claim 1, wherein the unmanned aerial vehicle cover body is provided in a circular shape or in a donut shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110444337.1A CN113086197A (en) | 2021-04-23 | 2021-04-23 | Be used for abluent unmanned aerial vehicle system of insulator |
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| Application Number | Priority Date | Filing Date | Title |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113697105A (en) * | 2021-09-02 | 2021-11-26 | 广东电网有限责任公司 | Unmanned aerial vehicle and earthing device |
| CN113731918A (en) * | 2021-09-16 | 2021-12-03 | 深圳供电局有限公司 | High-pressure flushing system for insulator water flushing operation |
| CN113731917A (en) * | 2021-09-16 | 2021-12-03 | 深圳供电局有限公司 | Insulator water flushing system suitable for helicopter |
| CN113967639A (en) * | 2021-11-30 | 2022-01-25 | 国网湖南省电力有限公司检修公司 | A formula unmanned aerial vehicle dry ice cleaning system moors for power equipment |
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| CN107440627A (en) * | 2017-07-19 | 2017-12-08 | 桂林电子科技大学 | A kind of captive unmanned plane high-altitude wall cleaning operation system and its method of work |
| KR20180133190A (en) * | 2017-06-05 | 2018-12-13 | 김재윤 | Unmaned aerial vehicle for washing insulator |
| CN215707129U (en) * | 2021-04-23 | 2022-02-01 | 深圳市中安维科技有限公司 | Be used for abluent unmanned aerial vehicle system of insulator |
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| CN103072690A (en) * | 2013-01-23 | 2013-05-01 | 中国航空工业空气动力研究院 | Single-ducted coaxial rotor/propeller saucer-shaped aircraft |
| KR20180133190A (en) * | 2017-06-05 | 2018-12-13 | 김재윤 | Unmaned aerial vehicle for washing insulator |
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| CN113697105A (en) * | 2021-09-02 | 2021-11-26 | 广东电网有限责任公司 | Unmanned aerial vehicle and earthing device |
| CN113731918A (en) * | 2021-09-16 | 2021-12-03 | 深圳供电局有限公司 | High-pressure flushing system for insulator water flushing operation |
| CN113731917A (en) * | 2021-09-16 | 2021-12-03 | 深圳供电局有限公司 | Insulator water flushing system suitable for helicopter |
| CN113731918B (en) * | 2021-09-16 | 2022-07-15 | 深圳供电局有限公司 | High-pressure flushing system for insulator water flushing operation |
| CN113967639A (en) * | 2021-11-30 | 2022-01-25 | 国网湖南省电力有限公司检修公司 | A formula unmanned aerial vehicle dry ice cleaning system moors for power equipment |
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